Patent Application
20240261563
Some applications of the present invention generally relate to medical apparatus. Specifically, some applications of the present invention relate to a ventricular assist device and methods of use thereof.
Ventricular assist devices are mechanical circulatory support devices designed to assist and unload cardiac chambers in order to maintain or augment cardiac output. They are used in patients suffering from a failing heart and in patients at risk for deterioration of cardiac function during percutaneous coronary interventions. Most commonly, a left-ventricular assist device is applied to a defective heart in order to assist left-ventricular functioning. In some cases, a right-ventricular assist device is used in order to assist right-ventricular functioning. Such ventricular assist devices are either designed to be permanently implanted or mounted on a catheter for temporary placement.
In accordance with some applications of the present invention, a drive cable, which includes a plurality of coiled wires, is coupled to a hollow shaft. Typically, an end of the hollow shaft (referred to as the “hollow-shaft end”) is shaped to define multiple shaft pores. For some applications, an end of the drive cable (referred to as the “drive-cable end”) and the hollow-shaft end of the hollow shaft are placed into opposing ends of a coupling tube, which is shaped to define multiple coupling-tube pores. While the drive-cable end and hollow-shaft end are inside the coupling tube, a molten material is flowed between the coiled wires at the drive-cable end via the coupling-tube pores, and into the hollow-shaft end via the coupling-tube pores and shaft pores, such that, upon solidifying, the material bonds the drive cable to the shaft.
Typically, the drive cable is also hollow, and it is desired that the drive cable and axial shaft be shaped to define a continuous lumen even after the bonding material solidifies. Hence, prior to the flowing of the molten bonding material, the drive cable and axial shaft are placed over a mandrel, such that the continuous lumen is maintained.
Typically, the molten material includes a molten polymer including, for example, polyether ether ketone (PEEK). The polymer is heated such that it passes through the coupling-tube pores and flows between the wires of the drive cable and into the shaft. Upon drying and solidifying, the polymeric material bonds the drive cable to the axial shaft.
In some embodiments, the molten material is flowed using a heat-shrinking process. In particular, a sleeve of the bonding material (e.g., a PEEK sleeve) is placed around the coupling tube, and an outer sleeve (made of polytetrafluoroethylene, for example) is placed around the sleeve of the material. Next, heat is applied to the sleeve of the material and to the outer sleeve. The applied heat melts the sleeve of the material, thereby forming the molten material, and shrinks the outer sleeve such that the outer sleeve forces the molten material between the coiled wires of the drive cable and into the proximal end of the axial shaft. Following the solidification of the molten material, the outer sleeve and any protruding pieces of the solidified material may be removed.
In some embodiments, the wall of the coupling tube is shaped to define multiple tabs. Prior to the flowing of the molten material, at least some of tabs are pushed into the shaft pores such that these tabs protrude into the shaft pores, thereby strengthening the coupling of the drive cable to the axial shaft. In some embodiments, to strengthen the coupling even further, at least two of the tabs pushed into the shaft pores have different respective orientations with respect to the longitudinal axis of the coupling tube. In other words, at least two of these tabs are rotatable about rotation axes having different respective orientations with respect to the longitudinal axis.
In some embodiments, prior to flowing the molten material between the coiled wires of the drive cable at the distal end of the drive cable and into the proximal end of the axial shaft, some of tabs are pushed between the coiled wires such that these tabs protrude between the coiled wires, thereby strengthening the coupling of the drive cable to the axial shaft. These tabs may have any shape that allows the tabs to fit between the coiled wires, which may be different from the shape of those of the tabs pushed into the shaft pores. For example, in some embodiments, U-shaped tabs are pushed between the coiled wires. In some embodiments, at least one of the coiled wires is cut, at the distal end of the drive cable, so as to define one or more enlarged gaps between successive windings of the coiled wires, and some of the tabs are pushed into the enlarged gaps.
In general, in the specification and in the claims of the present application, the term “proximal” and related terms, when used with reference to a device or a portion thereof, should be interpreted to mean an end of the device or the portion thereof that, when inserted into a subject's body, is typically closer to a location through which the device is inserted into the subject's body. The term “distal” and related terms, when used with reference to a device or a portion thereof, should be interpreted to mean an end of the device or the portion thereof that, when inserted into a subject's body, is typically further from the location through which the device is inserted into the subject's body.
There is therefore provided, in accordance with some embodiments of the present invention, a method, including:
In some embodiments, the method further includes, prior to inserting the drive-cable end of the drive cable into the coupling tube, merging the coiled wires together at the drive-cable end of the drive cable.
In some embodiments, the method further includes, while the molten material solidifies, compressing and heating the drive-cable end of the drive cable, the hollow-shaft end of the hollow shaft, and the coupling tube.
In some embodiments, the drive cable is hollow, and the method further includes, prior to flowing the molten material between the coiled wires and into the shaft, placing the drive cable and shaft over a mandrel.
In some embodiments,
In some embodiments, flowing the molten material includes:
In some embodiments, the coupling tube is polymeric.
In some embodiments, the coupling tube is ceramic.
In some embodiments,
In some embodiments, at least two of the at least some of the tabs have different respective orientations with respect to a longitudinal axis of the coupling tube.
In some embodiments, the at least two of the at least some of the tabs include a first tab oriented parallelly to the longitudinal axis and a second tab oriented perpendicularly to the longitudinal axis.
In some embodiments, the at least some of the tabs are shaped to define respective holes.
In some embodiments, the method further includes, prior to flowing the molten material between the coiled wires and into the hollow-shaft end, pushing others of the tabs between the coiled wires.
In some embodiments, at least one of the coiled wires is cut, at the drive-cable end of the drive cable, so as to define one or more enlarged gaps between successive windings of the coiled wires, and pushing the others of the tabs includes pushing the others of the tabs into the enlarged gaps.
In some embodiments, the others of the tabs are U-shaped.
In some embodiments,
In some embodiments, the adaptor tube is polymeric.
In some embodiments, the adaptor tube includes a metallic alloy.
In some embodiments,
In some embodiments,
In some embodiments, the method further includes inserting the drive cable through a delivery tube, which is coupled to a bearing housing that houses a radial bearing configured to radially stabilize the axial shaft while the axial shaft rotates the impeller, such that the distal end of the drive cable is disposed within the bearing housing proximally to the radial bearing.
In some embodiments, the molten material includes a molten polymer.
In some embodiments, the polymer includes polyether ether ketone (PEEK).
There is further provided, in accordance with some embodiments of the present invention, an apparatus, including:
In some embodiments, at the drive-cable end of the drive cable, the coiled wires are merged together.
In some embodiments, the drive cable and hollow shaft are shaped to define a continuous lumen.
In some embodiments,
In some embodiments, the bonding material includes a polymer.
In some embodiments, the coupling tube is polymeric.
In some embodiments, the coupling tube is ceramic.
In some embodiments,
In some embodiments, the adaptor tube is polymeric.
In some embodiments,
In some embodiments,
In some embodiments, the apparatus further includes:
There is further provided, in accordance with some embodiments of the present invention, a method, including:
In some embodiments, coupling the drive cable to the shaft further includes, subsequently to pushing the at least some of the tabs into the shaft pores, flowing a molten material between the coiled wires at the drive-cable end, and into the hollow-shaft end, via multiple pores in the coupling tube, such that, upon solidifying, the material bonds the drive cable to the shaft.
In some embodiments, the at least some of the tabs are shaped to define respective holes.
In some embodiments, the method further includes, prior to inserting the drive-cable end of the drive cable into the coupling tube, merging the coiled wires together at the drive-cable end of the drive cable.
In some embodiments,
In some embodiments, the coupling tube is polymeric.
In some embodiments, the coupling tube is ceramic.
In some embodiments, at least two of the at least some of the tabs have different respective orientations with respect to a longitudinal axis of the coupling tube.
In some embodiments, the at least two of the at least some of the tabs include a first tab oriented parallelly to the longitudinal axis and a second tab oriented perpendicularly to the longitudinal axis.
In some embodiments, coupling the drive cable to the shaft includes coupling the drive cable to the shaft by pushing others of the tabs between the coiled wires.
In some embodiments, at least one of the coiled wires is cut, at the drive-cable end of the drive cable, so as to define one or more enlarged gaps between successive windings of the coiled wires, and pushing the others of the tabs includes pushing the others of the tabs into the enlarged gaps.
In some embodiments, the others of the tabs are U-shaped.
In some embodiments,
In some embodiments, the adaptor tube is polymeric.
In some embodiments,
In some embodiments, the method further includes inserting the drive cable through a delivery tube, which is coupled to a bearing housing that houses a radial bearing configured to radially stabilize the axial shaft while the axial shaft rotates the impeller, such that the distal end of the drive cable is disposed within the bearing housing proximally to the radial bearing.
There is further provided, in accordance with some embodiments of the present invention, an apparatus, including:
In some embodiments, the apparatus further includes a bonding material, which bonds the drive cable to the shaft by virtue of being solidified between the coiled wires and in the hollow-shaft end opposite pores in the coupling tube and the shaft pores.
In some embodiments, the at least some of the tabs are shaped to define respective holes.
In some embodiments, at the drive-cable end of the drive cable, the coiled wires are merged together.
In some embodiments, the drive cable and hollow shaft are shaped to define a continuous lumen.
In some embodiments,
In some embodiments, the coupling tube is polymeric.
In some embodiments, the coupling tube is ceramic.
In some embodiments, at least two of the at least some of the tabs are rotatable about rotation axes having different respective orientations with respect to a longitudinal axis of the coupling tube.
In some embodiments, the rotation axes include a first rotation axis that is parallel to the longitudinal axis and a second rotation axis that is perpendicular to the longitudinal axis.
In some embodiments, others of the tabs protrude between the coiled wires.
In some embodiments, at least one of the coiled wires is cut, at the drive-cable end of the drive cable, so as to define one or more enlarged gaps between successive windings of the coiled wires, and the others of the tabs protrude into the enlarged gaps.
In some embodiments, the others of the tabs are U-shaped.
In some embodiments,
In some embodiments, the adaptor tube is polymeric.
In some embodiments,
In some embodiments,
In some embodiments, the apparatus further includes:
There is further provided, in accordance with some embodiments of the present invention, an apparatus, including:
In some embodiments, the bearing housing is configured to inhibit bending of the drive cable within the bearing housing.
In some embodiments, a radial separation between the bearing housing and a distal end of the drive cable, which is within the bearing housing, is less than 2 mm.
In some embodiments,
In some embodiments, the radial bearing includes a ceramic radial bearing, and the coupling tube is a ceramic coupling tube that is configured to rotate within the radial bearing during rotation of the axial shaft.
In some embodiments, at the distal end of the drive cable, the coiled wires are merged together.
In some embodiments, the drive cable and hollow shaft are shaped to define a continuous lumen.
In some embodiments, the bonding material includes a polymer.
In some embodiments, the coupling tube is polymeric.
In some embodiments,
In some embodiments, the adaptor tube is polymeric.
In some embodiments,
In some embodiments, the apparatus further includes a coupling tube having a wall shaped to define multiple tabs,
In some embodiments, the coupling tube is ceramic.
In some embodiments, the at least some of the tabs are shaped to define respective holes.
In some embodiments, at least two of the at least some of the tabs are rotatable about rotation axes having different respective orientations with respect to a longitudinal axis of the coupling tube.
In some embodiments, the rotation axes include a first rotation axis that is parallel to the longitudinal axis and a second rotation axis that is perpendicular to the longitudinal axis.
In some embodiments, others of the tabs protrude between the coiled wires.
In some embodiments, at least one of the coiled wires is cut, at the distal end of the drive cable, so as to define one or more enlarged gaps between successive windings of the coiled wires, and the others of the tabs protrude into the enlarged gaps.
In some embodiments, the others of the tabs are U-shaped.
The present invention will be more fully understood from the following detailed description of embodiments thereof, taken together with the drawings, in which:
Reference is now made to
As shown in
For some applications, the ventricular assist device is used to assist the functioning of a subject's left ventricle during a percutaneous coronary intervention. In such cases, the ventricular assist device is typically used for a period of up to six hours (e.g., up to ten hours), during a period in which there is risk of developing hemodynamic instability (e.g., during or immediately following the percutaneous coronary intervention). Alternatively or additionally, the ventricular assist device is used to assist the functioning of a subject's left ventricle for a longer period (e.g., 2-20 days, e.g., 4-14 days) upon a patient suffering from cardiogenic shock, which may include any low-cardiac-output state (e.g., acute myocardial infarction, myocarditis, cardiomyopathy, post-partum, etc.). For some applications, the ventricular assist device is used to assist the functioning of a subject's left ventricle for yet a longer period (e.g., several weeks or months), e.g., in a “bridge to recovery” treatment. For some such applications, the ventricular assist device is permanently or semi-permanently implanted, and the impeller of the ventricular assist device is powered transcutaneously, e.g., using an external antenna that is magnetically coupled to the impeller.
As shown in
For some applications (not shown), the ventricular assist device and/or delivery catheter 143 includes an ultrasound transducer at its distal end and the ventricular assist device is advanced toward the subject's ventricle under ultrasound guidance.
Reference is made to
For some applications, control console 21 (shown in
For some applications, a purging system 29 (shown in
Typically, along distal portion 102 of pump-outlet tube 24, a frame 34 is disposed within the pump-outlet tube around impeller 50. The frame is typically made of a shape-memory alloy, such as nitinol. For some applications, the shape-memory alloy of the frame is shape set such that at least a portion of the frame (and thereby distal portion 102 of tube 24) assumes a generally circular, elliptical, or polygonal cross-sectional shape in the absence of any forces being applied to distal portion 102 of tube 24. By assuming its generally circular, elliptical, or polygonal cross-sectional shape, the frame is configured to hold the distal portion of the pump-outlet tube in an open state. Typically, during operation of the ventricular assist device, the distal portion of the pump-outlet tube is configured to be placed within the subject's body, such that the distal portion of the pump-outlet tube is disposed at least partially within the left ventricle.
For some applications, along proximal portion 106 of pump-outlet tube 24, the frame is not disposed within the pump-outlet tube, and the pump-outlet tube is therefore not supported in an open state by frame 34. Pump-outlet tube 24 is typically made of a blood-impermeable collapsible material, such that the pump-outlet tube is collapsible. For example, pump-outlet tube 24 may include polyurethane, polyester, and/or silicone. Alternatively or additionally, the pump-outlet tube is made of polyethylene terephthalate (PET) and/or polyether block amide (e.g., PEBAX®). For some applications (not shown), the pump-outlet tube is reinforced with a reinforcement structure, e.g., a braided reinforcement structure, such as a braided nitinol tube. Typically, the proximal portion of the pump-outlet tube is configured to be placed such that it is at least partially disposed within the subject's ascending aorta. For some applications, the proximal portion of the pump-outlet tube traverses the subject's aortic valve, passing from the subject's left ventricle into the subject's ascending aorta, as shown in
As described hereinabove, the pump-outlet tube typically defines one or more blood-inlet openings 108 at the distal end of the pump-outlet tube, via which blood flows into the pump-outlet tube from the left ventricle, during operation of the impeller. For some applications, the proximal portion of the pump-outlet tube defines one or more blood-outlet openings 109, via which blood flows from the pump-outlet tube into the ascending aorta, during operation of the impeller. Typically, the pump-outlet tube defines a plurality of blood-outlet openings 109, for example, between two and eight blood-outlet openings (e.g., between two and four blood-outlet openings). During operation of the impeller, the pressure of the blood flow through the pump-outlet tube typically maintains the proximal portion of the tube in an open state. For some applications, in the event that, for example, the impeller malfunctions, the proximal portion of the pump-outlet tube is configured to collapse inwardly, in response to pressure outside of the proximal portion of the pump-outlet tube exceeding pressure inside the proximal portion of the pump-outlet tube. In this manner, the proximal portion of the pump-outlet tube acts as a safety valve, preventing retrograde blood flow into the left ventricle from the aorta.
Referring again to
For some applications, within at least a portion of frame 34 (e.g., along all of, or a portion of, the central cylindrical portion of the frame), an inner lining 39, shown in
Typically, pump-outlet tube 24 includes a conical proximal portion 42 and a cylindrical central portion 44. The proximal conical portion is typically proximally-facing, i.e., facing such that the narrow end of the cone is proximal with respect to the wide end of the cone. Typically, blood-outlet openings 109 are defined by pump-outlet tube 24, such that the openings extend at least partially along the proximal conical portion of tube 24. For some such applications, the blood-outlet openings are teardrop-shaped, as shown in
For some applications (not shown), the diameter of pump-outlet tube 24 changes along the length of the central portion of the pump-outlet tube, such that the central portion of the pump-outlet tube has a frustoconical shape. For example, the central portion of the pump-outlet tube may widen from its proximal end to its distal end, or may narrow from its proximal end to its distal end. For some applications, at its proximal end, the central portion of the pump-outlet tube has a diameter of between 5 and 7 mm, and at its distal end, the central portion of the pump-outlet tube has a diameter of between 8 and 12 mm.
Again referring to
As shown in the enlarged portion of
It is noted that the lateral blood-inlet openings are typically defined by the distal conical portion of the pump-outlet tube. As such, even the blood-inlet openings that are described as “lateral blood-inlet openings” are typically not oriented entirely laterally with respect to the longitudinal axis of the pump-outlet tube. Rather, they are obliquely disposed with respect to the longitudinal axis of the pump-outlet tube. By contrast, in some embodiments, the blood-outlet openings are described as “laterally-facing blood-outlet openings” because in such embodiments the blood-outlet openings are disposed laterally with respect to the longitudinal axis of the pump-outlet tube, by virtue of being defined by the central cylindrical portion of the pump-outlet tube. It is noted that in other embodiments, the blood-outlet openings are disposed obliquely with respect to the longitudinal axis of the pump-outlet tube, by virtue of being defined at least partially by the proximal conical portion of the pump-outlet tube.
In general, the scope of the present disclosure includes combining a pump-outlet-tube that defines a single axially-facing blood-inlet opening 108 as shown in
Reference is now made to
Typically, the frame is a stent-like frame, in that it comprises struts that, in turn, define cells. Further typically, the frame is covered with pump-outlet tube 24, and/or covered with an inner lining 39, described hereinbelow with reference to
Referring to
Still referring to
Still referring to
Typically, when disposed in its non-radially constrained configuration, frame 34 has a total length of more than 25 mm (e.g., more than 30 mm), and/or less than 50 mm (e.g., less than 45 mm), e.g., 25-50 mm, or 30-45 mm. Typically, when disposed in its radially-constrained configuration (within delivery catheter 143), the length of the frame increases by between 2 and 5 mm. Typically, when disposed in its non-radially constrained configuration, the central cylindrical portion of frame 34 has a length of more than 10 mm (e.g., more than 12 mm), and/or less than 25 mm (e.g., less than 20 mm), e.g., 10-25 mm, or 12-20 mm. For some applications, a ratio of the length of the central cylindrical portion of the frame to the total length of the frame is more than 1:4 and/or less than 1:2, e.g., between 1:4 and 1:2.
Reference is now made to
Each of the helical elongate elements, together with the film extending from the helical elongate element to the spring, defines a respective impeller blade, with the helical elongate elements defining the outer edges of the blades, and the axial spring defining the axis of the impeller. Typically, the film of material extends along and coats the spring. For some applications, sutures 53 (e.g., polyester sutures, shown in
Typically, proximal ends of spring 54 and helical elongate elements 52 extend from a proximal bushing (i.e., sleeve bearing) 64 of the impeller, such that the proximal ends of spring 54 and helical elongate elements 52 are disposed at a similar radial distance from the longitudinal axis of the impeller, as each other. Similarly, typically, distal ends of spring 54 and helical elongate elements 52 extend from a distal bushing 58 of the impeller, such that the distal ends of spring 54 and helical elongate elements 52 are disposed at a similar radial distance from the longitudinal axis of the impeller, as each other. The helical elongate elements typically rise gradually from the proximal bushing before reaching a maximum span and then falling gradually toward the distal bushing. Typically, the helical elongate elements are symmetrical along their lengths, such that the rising portions of their lengths are symmetrical with respect to the falling portions of their lengths. Typically, the impeller defines a lumen 62 therethrough (shown in
Reference is now made to
As shown in
For some applications, when impeller 50 and frame 34 are both disposed in non-radially-constrained configurations and prior to operation of the impeller, gap G between the outer edge of the impeller and the inner lining 39, at the location at which the span of the impeller is at its maximum, is greater than 0.05 mm (e.g., greater than 0.1 mm), and/or less than 1 mm (e.g., less than 0.4 mm), e.g., 0.05-1 mm, or 0.1-0.4 mm. For some applications, when the impeller is disposed in its non-radially-constrained configurations and prior to operation of the impeller, the outer diameter of the impeller at the location at which the outer diameter of the impeller is at its maximum is more than 7 mm (e.g., more than 8 mm), and/or less than 10 mm (e.g., less than 9 mm), e.g., 7-10 mm, or 8-9 mm. For some applications, when frame 34 is disposed in its non-radially-constrained configuration, the inner diameter of frame 34 (as measured from the inside of inner lining 39 on one side of the frame to the inside of inner lining on the opposite side of the frame) is greater than 7.5 mm (e.g., greater than 8.5 mm), and/or less than 10.5 mm (e.g., less than 9.5 mm), e.g., 7.5-10.5 mm, or 8.5-9.5 mm. For some applications, when the frame is disposed in its non-radially-constrained configuration, the outer diameter of frame 34 is greater than 8 mm (e.g., greater than 9 mm), and/or less than 13 mm (e.g., less than 12 mm), e.g., 8-13 mm, or 9-12 mm.
Typically, an axial shaft 92 passes through the axis of impeller 50, via lumen 62 of the impeller. For some applications, the axial shaft is rigid, e.g., a rigid tube. For some applications, the axial shaft is made of a shape-memory material (e.g., a shape memory alloy, such as nitinol). Typically, such materials have some elasticity, such that in the event that the axial shaft becomes bent (e.g., during delivery of the pump head to the left ventricle), the axial shaft still assumes a straight shape, once deployed inside the subject's body.
Proximal bushing 64 is disposed over axial shaft 92, and distal bushing 58 is disposed over the axial shaft distally from the proximal bushing. For some applications, proximal bushing 64 of the impeller is coupled to the shaft such that the axial position of the proximal bushing with respect to the shaft is fixed, and distal bushing 58 of the impeller is slidable with respect to (i.e., is slidable along) the shaft. For example, the proximal bushing may be coupled to a coupling element 65 disposed on the axial shaft (shown in
The axial shaft itself is radially stabilized via a proximal radial bearing 116 and a distal radial bearing 118 (
Referring again to
For some applications, the elongate elements 67 maintain helical elongate element 52 (which defines the outer edge of the impeller blade) within a given distance with respect to the central axial spring. In this manner, the elongate elements are configured to prevent the outer edge of the impeller from being forced radially outward due to forces exerted upon the impeller during the rotation of the impeller. The elongate elements are thereby configured to maintain the gap between the outer edge of the blade of the impeller and the inner surface of frame 34, during rotation of the impeller. Typically, more than one (e.g., more than two) and/or fewer than eight (e.g., fewer than four) elongate elements 67 are used in the impeller, with each of the elongate elements typically being doubled (i.e., extending radially from central axial spring 54 to an outer helical elongate element 52, and then returning from the helical elongate element back to the central axial spring). For some applications, a plurality of elongate elements, each of which extends from the spring to a respective helical elongate element and back to the spring, are formed from a single piece of string or a single wire.
Reference is now made to
It is noted that the scope of the present application includes using single integrated impeller-overexpansion-prevention element 72 with an impeller having a different construction from that shown in
For some applications, the following assembly technique is used to manufacture the impeller while enhancing bonding of an elastomeric material that is used to form film 56 to the at least one helical elongate element. Typically, bonding of the elastomeric material to the at least one helical elongate element is performed in a manner that does not cause a protrusion from the effective edge of the impeller blade. Further typically, bonding of the elastomeric material to the at least one helical elongate element is performed in a manner that provides the impeller blade with a rounded outer edge, by the elastomeric material rounding edges of the helical elongate element. Proximal bushing 64, distal bushing 58, and helical elongate elements 52 are cut from a tube of shape-memory material, such as nitinol. The cutting of the tube, as well as the shape setting of the shape-memory material, is typically performed such that the helical elongate elements and the bushings are defined by a tube of shape-memory material that is cut and shape set.
For some applications, prior to being coupled to spring 54, a plasma treatment is applied to the helical elongate elements. Alternatively or additionally, prior to being coupled to spring 54, the helical elongate elements are coated with a coupling agent. Typically, a coupling agent is selected that has at least two functional groups that are configured to bond respectively with the helical elongate elements and with the elastomeric material. For example, a silane compound, such as n-(2-aminoethyl)-3-aminopropyltrimethoxysilane, may be used, with the silane compound containing a first functional group (e.g., (OH)) which is configured to bond with the helical elongate elements (which are typically made of an alloy, such a nitinol), and the silane compound containing a second functional group (e.g., (NH2)) which is configured to bond with the elastomeric material. Typically, the functional groups in the coupling agent are active only for a given time period (e.g., approximately an hour or less). Therefore, during this time period, a coat of elastomeric material is applied around the helical elongate elements. Typically, the coat of elastomeric material is the same elastomeric material or a similar elastomeric material to that used in film 56. For example, a polycarbonate-based thermoplastic polyurethane, such as Aromatic Carbothane™ (e.g., Aromatic Carbothane™ 75A) may be used in film 56, and the coating may be the same polycarbonate-based thermoplastic polyurethane, or a similar polycarbonate-based thermoplastic polyurethane, such as Pellethane® (e.g., Pellethane® 90A).
As described hereinabove, proximal bushing 64, distal bushing 58, and helical elongate elements 52 are typically cut from a tube of shape-memory material, such as nitinol. For some applications, subsequently to the coating having been applied to the helical elongate elements 52, spring 54 is coupled to the helical elongate elements. Typically, spring 54 is inserted into the cut and shape-set tube, such that the spring extends along the length of the tube from at least the proximal bushing to the distal bushing. For some applications, the spring is inserted into the cut and shape-set tube while the spring is in an axially compressed state, and the spring is configured to be held in position with respect to the tube, by exerting a radial force upon the proximal and distal bushings. Alternatively or additionally, portions of the spring are welded to the proximal and distal bushings. For some applications, the spring is cut from a tube of a shape-memory material, such as nitinol. For some such applications, the spring is configured such that, when the spring is disposed in a non-radially-constrained configuration (in which the spring is typically disposed during operation of the impeller), there are substantially no gaps between windings of the spring and adjacent windings thereto.
Typically, at this stage, overexpansion-prevention element 72 is placed between the spring and the helical elongate elements, as described hereinabove, such that an assembly is formed that includes coated helical elongate elements 52, spring 54, and overexpansion-prevention element 72.
For some applications, at this stage, the assembly of coated helical elongate elements 52, spring 54, and overexpansion-prevention element 72 is sprayed with a further layer of an elastomeric material. Typically, the elastomeric material that is sprayed is the same elastomeric material or a similar elastomeric material to that used as film 56. For example, a polycarbonate-based thermoplastic polyurethane, such as Aromatic Carbothane™ (e.g., Aromatic Carbothane™ 75A) may be used as film 56, and the sprayed material may be the same polycarbonate-based thermoplastic polyurethane, or a similar polycarbonate-based thermoplastic polyurethane, such as Pellethane® (e.g., Pellethane® 90A). For some applications, applying the spray to the helical elongate elements rounds the helical elongate elements. Typically, when the helical elongate element has a rounded cross section, the elastomeric material forms a layer having a substantially uniform thickness at the interface with the helical elongate element. For some applications, the step of applying the coat of elastomeric material to the helical elongate elements, as described above, at least partially rounds the helical elongate elements.
For some applications, subsequently to the spray having been applied, the assembly of coated helical elongate elements 52, spring 54, and overexpansion-prevention element 72 is dipped in the elastomer from which film 56 is made. For some applications, the material from which the film is made is an elastomer having an ultimate elongation of more than 300 percent, e.g., more than 400 percent. Typically, the material has a relatively low molecular weight. For some applications, the material has a melt flow index (which is an indirect measure of molecular weight) of at least 4, e.g., at least 4.3. For some applications, the material has an ultimate tensile strength of more than 6000 psi, e.g., more than 7000 psi, or more than 7500 psi. For some applications, the material is a polycarbonate-based thermoplastic polyurethane, e.g., a Carbothane™. For some applications, Aromatic Carbothane™ (e.g., Aromatic Carbothane™ 75A) is used. Typically, such materials combine one or more of the following properties: no outer diameter loss caused during the dip process, resistance to fatigue, resistance to becoming misshaped by being crimped, and low outer diameter loss during crimping. Subsequently, the material is cured such that it solidifies, e.g., by being left to dry. Typically, during this stage, the impeller is disposed on a mandrel, such that the mandrel passes through lumen 62 defined by the bushings and the spring, thereby maintaining the lumen during the drying. For some applications, while the material from which the film is made is drying, the impeller is rotated, which typically facilitates the formation of a film of material having a substantially uniform thickness within each of the impeller blades. Once the material has dried, the mandrel is typically removed from lumen 62.
In accordance with the above description of the application of film 56 to the helical elongate elements, the scope of the present disclosure includes any technique whereby, prior to the helical elongate elements being dipped into the elastomeric material from which film 56 is made, additional layers of the same elastomeric material, a different elastomeric material, and/or a mediating material are applied to the helical elongate elements, whether by spraying, dipping, or a different coating method. For some applications, additional layers of elastomeric material are configured to round the helical elongate elements, and/or to act as mediators to enhance bonding between the helical elongate elements and film 56 of material. For some applications, a mediating material (such as silane) is configured to act as a mediator to enhance bonding between the helical elongate elements and film 56 of material.
Typically, impeller 50 is inserted into the left ventricle transcatheterally, while impeller 50 is in a radially-constrained configuration. In the radially-constrained configuration, both helical elongate elements 52 and central axial spring 54 are axially elongated and radially constrained. Typically, film 56 of the material (e.g., silicone and/or polyurethane) changes shape to conform to the shape changes of the helical elongate elements and the axial support spring, both of which support the film of material. Typically, using a spring to support the inner edge of the film allows the film to change shape without the film becoming broken or collapsing, due to the spring providing a large surface area to which the inner edge of the film bonds. For some applications, using a spring to support the inner edge of the film reduces a diameter to which the impeller can be radially constrained, relative to if, for example, a rigid shaft were to be used to support the inner edge of the film, since the diameter of the spring itself can be reduced by axially elongating the spring.
As described hereinabove, for some applications, proximal bushing 64 of impeller 50 is coupled to axial shaft 92 such that the axial position of the proximal bushing with respect to the shaft is fixed, and distal bushing 58 of the impeller is slidable with respect to the shaft. For example, the proximal bushing may be coupled to coupling element 65 disposed on the axial shaft (shown in
Reference is now made to
For some applications, each of the impeller blades comprises an inner helical elongate element 52i, an outer helical elongate element 52o, and a film 56 of material extending between the inner helical elongate element and the outer helical elongate element. Each blade is proximally coupled to proximal bushing 64 and distally coupled to distal bushing 58 such that, as axial shaft 92 (
Typically, the materials used for the blades in the impeller as shown in
In some applications, proximal bushing 64, distal bushing 58, inner helical elongate elements 52i, and outer helical elongate elements 52o are cut from a tube of shape-memory material, such as nitinol. For some applications, the inner helical elongate elements, the outer helical elongate elements and the proximal and distal bushings are all formed from a single integral structure, for example, a single tube of a shape-memory alloy, such as nitinol. The structure is typically cut and shaped such as to define the aforementioned structures. Alternatively, the outer helical elongate elements and the proximal and distal bushings are formed from a first structure (which is a single integral structure) and the inner helical elongate elements are formed from one or more additional structures that are coupled to the first structure. For example, the outer helical elongate elements and the proximal and distal bushings may be formed from a first tube of a shape-memory alloy, such as nitinol, and the inner helical elongate elements may be cut and formed from a second tube of a shape-memory alloy, such as nitinol. Further alternatively, the inner helical elongate elements and the proximal and distal bushings are formed from a first structure (which is a single integral structure) and the outer helical elongate elements are formed from one or more additional structures that are coupled to the first structure. For example, the inner helical elongate elements and the proximal and distal bushings may be formed from a first tube of a shape-memory alloy, such as nitinol, and the outer helical elongate elements may be cut and formed from a second tube of a shape-memory alloy, such as nitinol.
As shown in
Typically, in such applications, as shown in
Typically, for each of the blades, the distance DO between the inner helical elongate element and the outer helical elongate element increases moving, from the proximal or distal end of the blade, toward a middle portion of the blade. For example, DO may attain its maximum value midway between proximal bushing 64 and distal bushing 58 and/or at a maximal radial span of the outer helical elongate element. For some applications, the maximum value of DO is between 1 and 3.5 mm.
Reference is now made to
As indicated in
As described hereinabove, typically, axial shaft 92 passes through the axis of impeller 50, via lumen 62 of the impeller. Typically, proximal bushing 64 of the impeller is coupled to the shaft via a coupling element 65 such that the axial position of the proximal bushing with respect to the shaft is fixed, and distal bushing 58 of the impeller is slidable with respect to the shaft. Alternatively, distal bushing 58 of the impeller is coupled to the shaft such that the axial position of the distal bushing with respect to the shaft is fixed, and proximal bushing 64 of the impeller is slidable with respect to the shaft.
The axial shaft itself is radially stabilized via a proximal radial bearing 116 and a distal radial bearing 118. Typically, proximal bearing housing 116H is disposed around, and houses, the proximal bearing, and distal bearing housing 118H is disposed around, and houses, the distal bearing. For some such applications, the radial bearings and the bearing housings are made of respective, different materials from each other. For example, the radial bearings may be made of a first material that has a relatively high hardness, such as ceramic (e.g., zirconia), and the bearing housings may be made of a second material that is moldable into a desired shape, such as a metal or an alloy (e.g., stainless steel, cobalt chromium, and/or nitinol).
For some applications, axial shaft 92 is made of a metal or an alloy, such as stainless steel. For some such applications, the axial shaft is covered with ceramic sleeves 240 (e.g., zirconia sleeves) along regions of the axial shaft that come into contact with either of the proximal and distal bearings 116, 118 during operation of the ventricular assist device. In this manner, the radial interfaces between the axial shaft and the proximal and distal bearings are ceramic-ceramic interfaces. As described in further detail herein, typically, the impeller and the axial shaft are configured to undergo axial back-and-forth motion during operation of the ventricular assist device. Therefore, for some applications, at locations along the axial shaft corresponding to each of the proximal and distal bearings, the axial shaft is covered with the ceramic sleeve along a length of more than 5 mm, e.g., more than 7 mm. In this manner, over the course of the axial back-and-forth motion of the axial shaft, the ceramic sleeves remain in contact with the radial bearings.
For some applications, along each portion of the axial shaft that is covered with a ceramic sleeve, the shaft is shaped (e.g., via milling, molding, or a different shaping process) to define one or more grooves or indents 95, as shown in the transverse cross-sectional view of
For some applications, the proximal bearing housing 116H and distal bearing housing 118H perform additional functions. Referring first to the proximal bearing housing, as described hereinabove, for some applications, proximal strut junctions 33 of frame 34 are closed around the outside of the proximal bearing housing. For some applications, the outer surface of the proximal bearing housing defines grooves that are shaped such as to receive the proximal strut junctions. For example, as shown, the proximal strut junctions have widened heads, and the outer surface of the proximal bearing housing defines grooves that are shaped to conform with the widened heads of the proximal strut junctions. Typically, securing element 117 (which typically includes a ring) holds the strut junctions in their closed configurations around the outside of proximal bearing housing 116H.
For some applications, additional portions of the ventricular assist device are coupled to the proximal bearing housing. For example, for some applications, a drive cable 130 extends from outside the subject's body to axial shaft 92, and is coupled to the axial shaft such that the axial shaft rotates with the drive cable. Typically, the drive cable rotates within a first outer tube 140, which functions as a drive-cable-bearing tube, and which extends from outside the subject's body to the proximal bearing housing. For some applications, the first outer tube is disposed within a second outer tube 142 (also referred to herein as a “delivery tube”), which also extends from outside the subject's body to the proximal bearing housing. For some applications, first outer tube 140 and/or second outer tube 142 is coupled to the proximal bearing housing (e.g., using an adhesive). For example, first outer tube 140 may be coupled to an inner surface of the proximal bearing housing, and second outer tube 142 may be coupled to an outer surface of the proximal bearing housing.
Referring now to distal bearing housing 118H, for some applications, distal coupling portion 31 of frame 34 is coupled to an outer surface of distal bearing housing 118H, e.g., via a snap-fit mechanism. For example, the outer surface of a proximal-most portion 119 of the distal bearing housing may include a snap-fit mechanism to which distal coupling portion 31 of frame 34 is coupled. For some applications, distal bearing 118 is disposed within the proximal-most portion 119 of the distal bearing housing, as shown in
As described above, axial shaft 92 is radially stabilized via proximal radial bearing 116 and distal radial bearing 118. In turn, the axial shaft, by passing through lumen 62 defined by the impeller, radially stabilizes the impeller with respect to the inner surface of frame 34 and inner lining 39, such that even a relatively small gap between the outer edge of the blade of the impeller and inner lining 39 (e.g., a gap that is as described above) is maintained, during rotation of the impeller, as described hereinabove. Typically, the impeller itself is not directly disposed within any radial bearings or thrust bearings. Rather, bearings 116 and 118 act as radial bearings with respect to the axial shaft.
In some embodiments, pump-head portion 27 (and more generally ventricular assist device 20) does not include any thrust bearing that is configured to be disposed within the subject's body and that is configured to oppose thrust generated by the rotation of the impeller. For some applications, one or more thrust bearings are disposed outside the subject's body (e.g., within motor unit 23, shown in
In alternate embodiments, axial shaft 92 is omitted, and the impeller is instead coupled to a distal portion of drive cable 130; for example, the drive cable may pass through lumen 62 (
Reference is now made to
The coupling element is coupled to proximal bushing 64 at second region 71. This coupling may be effected via a snap-fit mechanism, as noted above. For example, second region 71 may be shaped to define one or more protrusions 19, proximal bushing 64 may be shaped to define one or more indentations 18, and the proximal bushing may couple to second region 71 by virtue of protrusions 19 snapping into indentations 18. Alternatively, the proximal bushing may be shaped to define protrusions 19, second region 71 may be shaped to define indentations 18, and the proximal bushing may couple to second region 71 by virtue of the protrusions snapping into the indentations.
The coupling element is coupled to axial shaft 92 at first region 66. For example, for some applications, the first region of the coupling element is welded to the shaft. For other applications, the coupling element (or at least first region 66) is made of a shape-memory material (e.g., a shape-memory alloy, such as nitinol or cobalt chromium). For example, the coupling element may comprise a tube of the shape-memory material that is cut to define the first and second regions. For some such applications, at least the first region of the coupling element (or the entire coupling element) is shape set to have an inner diameter that is smaller (e.g., between 0.01 and 0.1 mm smaller) than the outer diameter of the axial shaft. For example, the axial shaft may have an outer diameter of 0.9 mm and the inner diameter of the first region of the coupling element may be between 0.85 and 0.89 mm (e.g., 0.87 mm). Thus, following the placement of the first region around the axial shaft, the first region becomes radially contracted around, and thus locked in place with respect to, the axial shaft. For some applications, coupling the coupling element to the axial shaft via this method, rather than via welding, is desirable, since the coupling element and/or the axial shaft can be weakened by being heated during the welding.
For some applications, the first region of the coupling element is shaped to define one or more slits 75, e.g., by virtue of comprising a tube that defines slits 75. Slits 75 facilitate a radial expansion of the first region such that the first region is placeable around the axial shaft. Following the placement around the axial shaft, the first region may radially contract around the axial shaft, as described above.
Slits 75 may incorporate various features for facilitating the expansion of first region 66. For example, in some embodiments, one or more of slits 75 are open-ended slits 75o, each of which has an open end. Open-ended slits 75o may include one or more proximally-open slits 75op, which are open at the proximal end of first region 66, and/or one or more distally-open slits 75od, which are open at the distal end of the first region. Optionally, the length L0 of each of the open-ended slits may be 5-40% of the length L1 of the coupling element. Alternatively or additionally to open-ended slits 75o, one or more of slits 75 may be closed-ended slits 75c, each of which does not have any open end. In some embodiments, as shown in
During manufacture of the blood pump, first region 66 is placed around axial shaft 92 such that, as described above, the first region becomes radially contracted around the axial shaft. Typically, in addition to first region 66, second region 71 is placed around the axial shaft.
Typically, the coupling element is coupled to the axial shaft in the above-described manner without altering the temperature of the coupling element or of portions thereof. Alternatively, for some applications, the temperature of the coupling element is altered in order to facilitate the coupling of the coupling element to the axial shaft. For example, the first region may be radially expanded (with slits 75 facilitating the radial expansion) while the temperature of the first region is below the transformation temperature of the shape-memory material, and the first region may then be placed around the axial shaft while the first region is radially expanded. In other words, prior to the radial expansion, the coupling element may be cooled to below the transformation temperature of the shape-memory material, which is typically below ambient temperature, such as to increase the flexibility of the shape-memory material. The coupling element may then be placed around the axial shaft, while it is in its expanded configuration. Subsequently, the coupling element heats up to above its transformation temperature, causing it to radially contract towards the shape to which it was shape set. As described above, at least the first region of the coupling element (or the entire coupling element) is shape set to have an inner diameter that is smaller (e.g., between 0.01 and 0.1 mm smaller) than the outer diameter of the axial shaft. Therefore, as the coupling element radially contracts it exerts inward radial pressure on the axial shaft, causing it to become locked in place with respect to the axial shaft.
Subsequent to coupling the coupling element to the axial shaft, the impeller is coupled to the axial shaft, by coupling proximal bushing 64 to the second region of the coupling element. As described above, this coupling may be performed via a snap-fit mechanism; for example, protrusions 19 may be snapped into indentations 18. Thus, as the axial shaft rotates, the blades of the impeller rotate, thereby pumping blood of the subject.
In alternate embodiments, second region 71 is coupled to distal bushing 58 (e.g., via a snap-fit mechanism, as described), such that the distal bushing is fixed in place with respect to the axial shaft, and proximal bushing 64 is slidable along the axial shaft.
Reference is now made to
For some applications, by moving in the axial back-and-forth motion, the portions of the axial shaft that are in contact with proximal bearing 116 and distal bearing 118 are constantly changing. For some such applications, in this manner, the frictional force that is exerted upon the axial shaft by the bearings is spread over a larger area of the axial shaft than if the axial shaft were not to move relative to the bearings, thereby reducing wear upon the axial shaft, ceteris paribus. Alternatively or additionally, by moving in the back-and-forth motion with respect to the bearing, the axial shaft cleans the interface between the axial shaft and the bearings from any residues, such as blood residues.
For some applications, at the proximal-most position of the impeller during its motion cycle, the proximal end of the impeller is disposed within the proximal conical section of frame 34, as shown in
Reference is again made to
Typically, during the insertion of the ventricular assist device into the subject's ventricle, delivery catheter 143 (
For some applications, distal-tip element 107 defines an overall curvature that is similar to that of a question mark or a tennis-racket, with the distal-tip element defining a straight proximal portion and a bulge on one side of the longitudinal axis of the straight proximal portion. Typically, the ventricular assist device is introduced into the subject's ventricle over a guidewire, as described hereinabove. Distal-tip portion 120 defines lumen 122, such that the distal-tip portion is held in a straightened configuration during the introduction of the ventricular assist device into the subject's ventricle (e.g., as shown in the left frame of
Referring again to
Typically, during normal operation of the impeller, the axial shaft does not come into contact with stopper 128, even when drive cable 130 (shown in
It is noted that, at the proximal end of frame 34, proximal radial bearing 116 also functions as a stopper, by preventing coupling element 65 and/or proximal bushing 64 of impeller 50 from being able to move beyond the proximal radial bearing. Typically, during normal operation of the impeller, coupling element 65 and proximal bushing 64 do not come into contact with proximal radial bearing 116. However, proximal radial bearing 116 is configured to prevent coupling element 65 and/or proximal bushing 64 of impeller 50 from migrating proximally from inside the frame, for example, when the impeller and the frame are held in radially-constrained (i.e., crimped) configurations inside delivery catheter 143. Typically, the coupling element and/or the proximal bushing is proximally-extended such as to prevent a central region of the impeller (at which the span of the impeller is at its maximum) from sliding proximally into the proximal conical portion of frame 34. For example, in the systolic phase of the impeller's motion cycle (shown in
Typically, during operation of the ventricular assist device, and throughout the axial back-and-forth motion cycle of the impeller, the impeller is disposed relatively close to the distal-tip portion. For example, the distance of the impeller to the distal-tip portion may be within the distal-most 50 percent, e.g., the distal-most 30 percent (or the distal-most 20 percent) of tube 24, throughout the axial back-and-forth motion cycle of the impeller.
Reference is now made to
Typically, the motion-cushioning spring is disposed around axial shaft 92 between the distal end of the impeller (e.g., distal bushing 58 of the impeller) and distal bearing 118. For some applications, the motion-cushioning spring is coupled to distal bearing 118 or the distal bearing housing 118H and extends proximally over axial shaft 92 from the distal bearing or the distal bearing housing 118H. Typically, in such cases, the motion-cushioning spring remains rotationally stationary as the impeller rotates, and the impeller is configured to rotate with respect to the motion-cushioning spring. Alternatively or additionally, the motion-cushioning spring is coupled to the distal end of the impeller (e.g., distal bushing 58 of the impeller) and/or extends distally over axial shaft 92 from the distal end of the impeller (e.g., distal bushing 58 of the impeller). For some such applications, the motion-cushioning spring is configured to rotate together with the impeller. Alternatively, the motion-cushioning spring extends from a radial bearing that is disposed around the distal end of the impeller (e.g., distal bushing 58 of the impeller), such that motion-cushioning spring remains rotationally stationary as the impeller rotates, and the impeller is configured to rotate with respect to the motion-cushioning spring.
For some applications, the motion-cushioning spring is coupled to an elastomeric material 69 (such as polyurethane, and/or silicone), such that at least a portion of axial shaft 92 that is between the distal end of the impeller and the distal radial bearing is covered by the elastomeric material. For some applications, coupling the elastomeric material to the spring reduces a risk of the generation of thrombi and/or hemolysis by the spring, relative to if the spring were not coupled to the elastomeric material. It is noted that the scope of the present disclosure includes providing the motion-cushioning spring in the absence of elastomeric material, as may be desirable in some cases.
Typically, purging fluid is pumped between first outer tube 140 and second outer tube 142. Typically, within the pump head, a portion of the purging fluid flows through the lumen defined by axial shaft 92 and then exits the axial shaft in the vicinity of distal bearing 118, in order to purge the interface between the axial shaft and the distal bearing. For some applications, the purging system is configured such that purging fluid flows proximally from the distal bearing along an interface between the axial shaft and the elastomeric material. In this manner, the interface between the axial shaft and the elastomeric material is purged and/or lubricated.
For some applications (not shown), a proximal motion-cushioning spring is disposed on the proximal side of the impeller. For some such applications, the proximal motion-cushioning spring is disposed around axial shaft 92 between the proximal end of the impeller (e.g., proximal bushing 64 of the impeller) and proximal bearing 116. For some applications, the proximal motion-cushioning spring is coupled to proximal bearing 116 or proximal bearing housing 116H and extends distally over axial shaft 92 from the proximal bearing or the proximal bearing housing. Typically, in such cases, the proximal motion-cushioning spring remains rotationally stationary as the impeller rotates, and the impeller is configured to rotate with respect to the motion-cushioning spring. Alternatively or additionally, the proximal motion-cushioning spring is coupled to the proximal end of the impeller (e.g., proximal bushing 64 of the impeller) and/or extends distally over axial shaft 92 from the proximal end of the impeller (e.g., proximal bushing 64 of the impeller). For some such applications, the motion-cushioning spring is configured to rotate together with the impeller. Alternatively, the proximal motion-cushioning spring extends from a radial bearing that is disposed around the proximal end of the impeller (e.g., proximal bushing 64 of the impeller), such that motion-cushioning spring remains rotationally stationary as the impeller rotates, and the impeller is configured to rotate with respect to the motion-cushioning spring.
For some applications, the pump head includes both a proximal motion-cushioning spring disposed on a proximal side of the impeller, and a distal motion-cushioning spring disposed on a distal side of the impeller, such that axial movement of the impeller in either the distal or the proximal direction is cushioned by the motion-cushioning springs.
Reference is now made to
Referring to
Typically, the motor is magnetically coupled to the drive cable. For some applications, the magnetic coupling of the motor to the drive cable is as shown in
It is noted that in the application shown in
Typically, driven magnet 82 and pin 131 are held in axially fixed positions within motor unit 23. For some applications, driven-magnet unit 310 includes snap-fit prongs 91 (shown in
Referring now to
Still referring to
Referring again to
For some applications, ventricular assist device 20 includes a magnetic sensor 84 configured to detect changes in the magnetic field caused by the variation in the axial position of the driven magnet. For example, sensor 84 may include a magnetometer (e.g., a Hall sensor) that is disposed within motor unit 23, as shown in
Reference is now made to
For some applications, a printed circuit board 104 is disposed inside a protective container 105. For some applications, magnetometer 84 is housed inside a magnetometer housing 112 that orients the magnetometer toward the interface between drive magnets 77 and driven magnet 82, such as to facilitate the detection of changes in magnetic flux density and/or magnetic phase by the magnetometer. For some applications, the magnetometer is disposed behind a metallic element 113 that is shaped to act as a passive magnetic lens, by directing the changes in magnetic flux and magnetic phase that are generated at the interface between the drive magnet and the driven magnet toward the magnetometer.
Referring now to
Referring again to
As described hereinabove, typically purging system 29 (shown in
Reference is now made to
For some applications, during operation of the ventricular assist device, computer processor 25 of control console 21 (
For some applications, it is the case that the axial back-and-forth motion of the impeller gives rise to a measurable back-and-forth motion of the inner, driven magnet 82 relative to the outer, one or more drive magnets 77 (
For some applications, the magnetometer measurements are initially calibrated, such that the change in magnetic flux per unit change in pressure against which the impeller is pumping (i.e., per unit change in the pressure difference between the left ventricle and the aorta, or per unit change in the pressure gradient) is known. It is known that, in most subjects, at systole, the left-ventricular pressure is equal to the aortic pressure. Therefore, for some applications, the subject's aortic pressure is measured, and the subject's left-ventricular pressure at a given time is then calculated by the computer processor, based upon (a) the measured aortic pressure, and (b) the difference between the magnetic flux measured by the magnetometer at that time, and the magnetic flux measured by the magnetometer during systole (when the pressure in the left ventricle is assumed to be equal to that of the aorta). For example, the subject's aortic pressure may be measured by measuring pressure in a channel 224 defined by delivery catheter 143, as described in further detail hereinbelow with reference to
For some applications, generally similar techniques to those described in the above paragraph are used, but as an alternative to or in addition to utilizing magnetometer measurements, a different parameter is measured in order to determine left ventricular blood pressure (and/or a different physiological parameter, e.g., events in the subject's cardiac cycle and/or the subject's cardiac afterload) at a given time. For example, it is typically the case that there is a relationship between the amount of power (and/or current) that is required to power the rotation of the impeller at a given rotation rate and the pressure difference that is generated by the impeller. (It is noted that some of the pressure difference that is generated by the impeller is used to overcome the pressure gradient against which the impeller is pumping, and some of the pressure difference that is generated by the impeller is used to actively pump the blood from the left ventricle to the aorta, by generating a positive pressure difference between the left ventricle and the aorta. Moreover, the relationship between the aforementioned components typically varies over the course of the cardiac cycle.) For some applications, calibration measurements are performed, such that the relationship between (a) power (and/or current) consumption by the motor that is required to rotate the impeller at a given rotation rate and (b) the pressure difference that is generated by the impeller, is known. For some applications, the subject's aortic pressure is measured, and the subject's left-ventricular pressure at a given time is then calculated by the computer processor, based upon (a) the measured aortic pressure, (b) the power (and/or current) consumption by the motor that is required to rotate the impeller at a given rotation rate at that time, and (c) the predetermined relationship between power (and/or current) consumption by the motor that is required to rotate the impeller at a given rotation rate and the pressure difference that is generated by the impeller. For some applications, the above-described technique is performed while maintaining the rotation rate of the impeller at a constant rate. Alternatively or additionally, the rotation rate of the impeller is varied, and the variation of the rotation rate of the impeller is accounted for in the above-described calculations. For some applications, alternative or additional physiological parameters are determined using the above-described technique. For example, events in the subject's cardiac cycle and/or the subject's cardiac afterload may be determined.
Typically, tube 24 has a known cross-sectional area (when the tube is in an open state due to blood flow through the tube). For some applications, the flow through tube 24 that is generated by the impeller is determined based on the determined pressure difference that is generated by the impeller, and the known cross-sectional area of the tube. For some applications, such flow calculations incorporate calibration parameters in order to account for factors such as flow resistance that are specific to the ventricular assist device (or type of ventricular assist device) upon which the calculations are performed. For some applications, the ventricular pressure-volume loop is derived, based upon the determined ventricular pressure.
For some applications, the computer processor determines one or more physiological parameters of the subject based upon data that are received via the ventricular assist device. Typically, the following parameters are detected via the ventricular assist device: arterial pressure (AP), electrical current consumption by the motor (I) and revolutions per minute (RPM) of the impeller. For some applications, the left ventricular pressure (LVP), the left ventricular end-diastolic pressure (LVEDP) and/or the pump flow rate are derived.
As described hereinabove, for some applications, the pressure difference between the left ventricle and the aorta (dP) is derived based upon electrical current consumption by the motor (I) and revolutions per minute (RPM) of the impeller. Left ventricular pressure (LVP) is derived by subtracting the pressure difference (dP) from the aortic pressure (AP). Left ventricular end-diastolic pressure (LVEDP) is then derived by analyzing the LVP curve, and pump flow rate is derived by integrating the pressure difference over time (along with empirically determined pumping performance parameters of the device).
For some applications, the dP curve is derived by determining (a) the maximum dP within a given first current time period (e.g., within the last second, within the last 0.5 seconds, or within a different time period that is typically between 0.1 seconds and 2 seconds, i.e., at a first frequency of between 0.5 Hz and 2 Hz), (b) the minimum dP within the given first current time period (e.g., within the last second, within the last 0.5 seconds, or within a different time period that is typically between 0.1 seconds and 2 seconds, i.e., at a first frequency of between 0.5 Hz and 2 Hz), and (c) the real-time value of the dP within a given second current time period (e.g., the current hundredth of second, or within a different time period that is typically between the current fiftieth of a second and the current two-hundredth of a second, i.e., at a second frequency that is typically between 50 Hz and 200 Hz). Typically, the second time period is smaller than the first time period, i.e., the second frequency is greater than the first frequency.
Typically, the value of each of (a), (b), and (c) is derived using a linear model. Further typically, within the first current time period, the real-time values of dP (which are detected at the second frequency) are corrected based upon the maximum dP and the minimum dP (which are detected at the first frequency), such as to generate a corrected dP curve. The LVP curve is then derived from the corrected dP curve. Typically, this results in more accurate values of LVP than if uncorrected real-time values of dP were to be used.
Referring again to
The torque that is transmitted to the driven magnet typically gives rise to a phase difference between the signal that is measured by magnetometer 84 (which measures magnetic flux density of the driven magnet) and the signal that is measured by second magnetometer 84A (which measures magnetic flux density of the motor and/or the driving magnet). For some applications, as the torque upon the impeller varies, this gives rise to a variation in the phase difference between the signal that is measured by magnetometer 84 and the signal that is measured by second magnetometer 84A. For some applications, the computer processor detects the variation in the aforementioned phase difference, and determines a physiological parameter of the subject, at least partially in response thereto. For example, at least partially based upon variations in the phase difference, the computer processor may determine the difference between the subject's left-ventricular pressure and the subject's aortic pressure, the subject's left ventricular pressure, an event in the subject's cardiac cycle, the subject's cardiac afterload, and/or a different physiological parameter. For some applications, the technique described in the present paragraph is used as an alternative to the above-described technique for using magnetic flux density measurements and/or power consumption measurements to determine physiological parameters. Alternatively, two or more of these techniques are used in combination with each other. For example, the subject's physiological parameters may be determined based upon a mathematical model that incorporates two or more measurements, and/or one of the techniques may be used to validate estimations of the subject's physiological parameters that are made using another one of the techniques.
Reference is now made to
The graph shown in
The graph shown in
In accordance with the above, and in accordance with some applications of the invention, a magnetic phase difference between the one or more driven magnets and the one or more drive magnets is measured, and a physiological parameter of the subject is determined, at least partially in response thereto. For example, at least partially based upon variations in the phase difference, the computer processor may determine the difference between the subject's left-ventricular pressure and the subject's aortic pressure, the subject's left-ventricular pressure, an event in the subject's cardiac cycle, the subject's cardiac afterload, and/or a different physiological parameter. For some applications, the physiological parameter is determined based upon the phase difference measurements in combination with one or more additional measurements, such as magnetic flux amplitude measurements, power consumed by the motor, and/or current consumed by the motor. Typically, such measurements are combined into a mathematical model, such as a linear regression model, and/or a space state model.
Reference is now made to
For some applications, the ventricular assist device includes two or more such ventricular blood-pressure-measurement tubes 222, e.g., as shown in
For some applications, second outer tube 142 defines a groove 215 in a portion of the outer surface of the second outer tube that is configured to be disposed within tube 24. Typically, during insertion of the ventricular assist device into the subject's body, the portion of ventricular blood-pressure-measurement tube 222 that extends from within tube 24 at least to an outer surface of tube 24, is configured to be disposed within the groove, such that the portion of the ventricular blood-pressure-measurement tube does not protrude from the outer surface of the outer tube.
For some applications (not shown), distal portions of blood-pressure-measurement tubes 222 are disposed on the outside of pump-outlet tube 24. For example, blood-pressure-measurement tubes 222 may extend from outer tube 142 to the proximal end of pump-outlet tube 24, and thereafter the blood pressure measurement tubes may be built into the outer surface of tube pump-outlet tube 24, as shown in FIG. 16D of U.S. Pat. No. 10,881,770 to Tuval, which is incorporated herein by reference, for example.
As described hereinabove, for some applications, drive cable 130 extends from a motor outside the subject's body to axial shaft 92 upon which impeller 50 is disposed. Typically, the drive cable is disposed within first outer tube 140 and second outer tube 142, as described hereinabove. For some applications, a proximal portion of blood-pressure-measurement tube 222 comprises a channel between first outer tube 140 and second outer tube 142, as shown in the cross-section of
Referring to
Typically, distal end 230 of optical fiber 228 is configured to be within the subject's left ventricle proximal to the blood pump (e.g., proximal to impeller 50). Typically, by measuring pressure of blood at distal end 230 of optical fiber 228, the pressure sensor thereby measures the subject's blood pressure outside tube 24 (i.e., left-ventricular blood pressure). For some applications, computer processor 25 (
For some applications, the ventricular assist device includes two or more such optical fibers 228, e.g., as shown in
For some applications, along the length of second outer tube 142, the optical fibers are disposed within the second outer tube. Typically, at the distal end of second outer tube, the optical fibers are coupled to proximal conical portion 36 of frame 34, such that the optical fibers extend radially to the outer surface of pump-outlet tube 24. For example, as shown in
Referring to both blood-pressure measurement tube 222 and optical fiber 228, it is noted that the distal end of the tube or the fiber is typically in direct fluid communication with the left-ventricular bloodstream of the subject at a location that is proximal to the proximal-most portion of blood-inlet opening(s) 108 (e.g., at least 1 cm, or at least 1.5 cm proximal to the proximal-most portion of blood-inlet opening(s) 108). Thus, the distal end of the tube or the fiber is typically exposed to blood that has a pressure that reflects the blood pressure of the left ventricle itself and that is not affected by any pressure variations that are generated in the vicinity of the blood-inlet openings as a result of fluid-flow dynamics generated at the blood-inlet openings.
Referring to both blood-pressure measurement tube 222 and optical fiber 228, for some applications, the tube or the fiber is coupled to the outer surface of second outer tube 142. For some applications, the tube or the fiber terminates within the aorta (e.g., on second outer tube 142 or at the proximal end of pump-outlet tube 24) in order to measure aortic pressure. For some applications, the tube or the fiber terminates at the outside of the pump-outlet tube, in the vicinity of frame 34, and is configured to measure left-ventricular pressure. For some such applications, the computer processor determines whether the frame is properly placed with reference to the aortic valve and the left ventricle based upon the blood pressure that is measured using the tube or the fiber. For some applications, the tube or the fiber terminates at the distal bearing housing 118H or at the distal-tip element 107, and is configured to measure pressure in the vicinity of the blood-inlet openings. For some applications, the tube or the fiber runs along the outside of at least a portion of the pump-outlet tube (e.g. from the proximal end of the pump-outlet tube until the vicinity of frame 34).
For some applications, the tube or the fiber is coupled to the outside of the pump-outlet tube by sandwiching the tube or the fiber between a polymeric membrane and the outer surface of the pump-outlet tube, using a bonding method, such as thermal boding, dipping, or gluing. For some applications, along the entire length of the overlap between the tube or the fiber and the pump-outlet tube, the tube or the fiber is bonded to the outside of the pump-outlet tube (e.g., using the aforementioned method(s)). Alternatively, the tube or the fiber is bonded to the outside of the pump-outlet tube (e.g., using the aforementioned method(s)) only at segmented locations along the length of the overlap between the tube or the fiber and the pump-outlet tube. For some applications, by bonding the tube or the fiber only at the segmented locations, the flexibility of the pump-outlet tube is greater than if the tube or the fiber were bonded to the pump-outlet tube along the entire length of the overlap between the tube or the fiber and the pump-outlet tube. As described above, for some applications, the tube or the fiber is coupled to the outside of the pump-outlet tube by sandwiching the tube or the fiber between a polymeric membrane and the outer surface of the pump-outlet tube. For some applications, the polymeric layer is applied at the segmented locations. For some such applications, a ring-shaped polymeric layer is applied around the full circumference of the pump-outlet tube at each of the segmented locations. Alternatively, as described below with reference to
Reference is now made to
Typically, the inner lining is disposed over the inner surface of at least a portion of central cylindrical portion 38 of frame 34. For some applications, pump-outlet tube 24 also covers central cylindrical portion 38 of frame 34 around the outside of the frame, for example, such that pump-outlet tube 24 and inner lining 39 overlap over at least 50 percent of the length of the inner lining, for example, over the entire length of the cylindrical portion of frame 34, e.g., as shown in
Typically, over the area of overlap between inner lining 39 and pump-outlet tube 24, the inner lining is shaped to form a smooth surface (e.g., in order to reduce hemolysis, as described hereinabove), and pump-outlet tube 24 is shaped to conform with the struts of frame 34 (e.g., as shown in the cross-section in
For some applications, inner lining 39 and pump-outlet tube 24 are made of different materials from each other. For example, the inner lining may be made of polyurethane, and the pump-outlet tube may be made of polyether block amide (PEBAX®). Typically, for such applications, the material from which the inner lining is made has a higher thermoforming temperature than that of the material from which the pump-outlet tube is made. Alternatively, inner lining 39 and pump-outlet tube 24 are made of the same material as each other. For example, both the inner lining and the pump-outlet tube may be made of polyurethane or polyether block amide (PEBAX®).
For some applications, the pump-outlet tube and the inner lining are bonded to each other and/or the frame in the following manner. For some applications, the inner lining is directly bonded to the inner surface of the frame before the pump-outlet tube is bonded to the outside of the frame. It is noted that, by bonding the inner lining directly to the inner surface of the frame (rather than simply bonding the inner lining to the pump-outlet tube and thereby sandwiching the frame between the inner lining to the pump-outlet tube), any air bubbles, folds, and other discontinuities in the smoothness of the surface provided by the inner lining are typically avoided. For some applications, similar techniques to those described hereinabove for enhancing bonding between the elastomeric film and the helical elongate elements of the impeller, are used to enhance bonding between the inner lining and the inner surface of the frame. For some applications, initially, the frame is treated so as to enhance bonding between the inner lining and the inner surface of the frame. For some applications, the treatment of the frame includes applying a plasma treatment to the frame (e.g., to the inner surface of the frame), dipping the frame in a coupling agent that has at least two functional groups that are configured to bond respectively with the frame and with the material form which the inner lining is made (e.g., silane solution), and/or dipping the frame in a solution that contains the material from which the inner lining is made (e.g., polyurethane solution). For some applications, the inner lining is made of an elastomeric material (e.g., polyurethane) and the coupling agent is a silane solution, such as a solution of n-(2-aminoethyl)-3-aminopropyltrimethoxysilane, with the silane containing a first functional group (e.g., (OH)) which is configured to bond with the frame (which is typically made of an alloy, such a nitinol), and the silane containing a second functional group (e.g., (NH2)) which is configured to bond with the elastomeric material.
For some applications, subsequently, a solution that contains the material from which the inner lining is made (e.g., polyurethane solution) is sprayed over the central cylindrical portion of the frame. Once the inner surface of the frame has been treated, the inner lining is bonded to the inner surface of the central cylindrical portion of the frame (e.g., to the inner surface of a central cylindrical portion of the frame). Typically, the inner lining (which is shaped as a tube), is placed over a mandrel, the frame is placed over the inner lining, and pressure is applied by a heat shrinking process. Further typically, the assembly of the inner lining and the frame is heated in an oven.
Subsequently to the inner lining having been bonded to the frame, a portion of pump-outlet tube 24 is placed around the outside of the frame. As described above, for some applications, inner lining 39 and pump-outlet tube 24 are made of different materials from each other. For example, the inner lining may be made of polyurethane, and the pump-outlet tube may be made of polyether block amide (PEBAX®). Typically, for such applications, the material from which the inner lining is made has a higher thermoforming temperature than that of the material from which the pump-outlet tube is made. For some applications, in order to mold pump-outlet tube 24 to conform with the struts of frame 34, without causing the inner lining to deform, the frame is heated to a temperature that is above the thermoforming temperature of pump-outlet tube 24 but below the thermoforming temperature of inner lining 39.
Typically, the frame is heated from inside the frame, using the mandrel. Typically, while the frame is heated to the aforementioned temperature, an outer tube (which is typically made from silicone) applies pressure to pump-outlet tube 24 that causes pump-outlet tube 24 to be pushed radially inwardly, in order to cause the pump-outlet tube to conform with the shapes of the struts of the frame, as shown in the cross-section of
Reference is now made to
Reference is now made to
For some applications (not shown), the pump-outlet tube defines two to four lateral blood-inlet openings. Typically, for such applications, each of the blood-inlet openings defines an area of more than 20 square mm (e.g., more than 30 square mm), and/or less than 60 square mm (e.g., less than 50 square mm), e.g., 20-60 square mm, or 30-50 square mm. Alternatively or additionally, the outlet tube defines a greater number of smaller blood-inlet openings 108, e.g., more than 10 blood-inlet openings, more than 50 blood-inlet openings, more than 100 blood-inlet openings, or more than 150 blood-inlet openings, e.g., 50-100 blood-inlet openings, 100-150 blood-inlet openings, or 150-200 blood-inlet openings. For some applications, the blood-inlet openings are sized such as (a) to allow blood to flow from the subject's left ventricle into the tube and (b) to block structures from the subject's left ventricle from entering into the frame. Typically, for such applications, the distal conical portion 46 of pump-outlet tube 24 is configured to reduce a risk of structures from the left ventricle (such as chordae tendineae, trabeculae carneae, and/or papillary muscles) entering into frame 34 and potentially being damaged by the impeller and/or the axial shaft, and/or causing damage to the left ventricular assist device. Therefore, for some applications, the blood-inlet openings are shaped such that, in at least one direction, the widths (or spans) of the openings are less than 1 mm, e.g., 0.1-1 mm, or 0.3-0.8 mm. By defining such a small width (or span), it is typically the case that structures from the left ventricle (such as chordae tendineae, trabeculae carneae, and/or papillary muscles) are blocked from entering into frame 34. For some such applications, each of the blood-inlet openings defines an area of more than 0.05 square mm (e.g., more than 0.1 square mm), and/or less than 3 square mm (e.g., less than 1 square mm), e.g., 0.05-3 square mm, or 0.1-1 square mm. Alternatively, each of the blood-inlet openings defines an area of more than 0.1 square mm (e.g., more than 0.3 square mm), and/or less than 5 square mm (e.g., less than 1 square mm), e.g., 0.1-5 square mm, or 0.3-1 square mm.
Typically, the portion of the pump-outlet tube that defines the blood-inlet openings has a porosity of more than 40 percent, e.g., more than 50 percent, or more than 60 percent (where porosity is defined as the percentage of the area of this portion that is porous to blood flow). Thus, on the one hand, the blood-inlet openings are relatively small (in order to prevent structures of the left ventricular from entering the frame), but on the other hand, the porosity of the portion of the pump-outlet tube that defines the blood-inlet openings is relatively high, such as to allow sufficient blood flow into the pump-outlet tube.
For some applications, each of the blood-inlet openings has a circular or a polygonal shape. For some applications, each of the blood-inlet openings has a hexagonal shape, as shown in
As described hereinabove with reference to
Typically, width W of the gaps between the hexagonal (or other type of polygonal) holes and distance D between opposing sides of each of the hexagons (or other type of polygons) within distal region 46D of distal conical portion 46 of the pump-outlet tube are as described hereinabove. For some applications, width W1 of gaps between adjacent hexagonal (or other polygonal) holes within proximal region 46P of distal conical portion 46 of pump-outlet tube 24 is more than 0.05 mm (e.g., more than 0.07 mm), and/or less than 0.2 mm (e.g., less than 0.15 mm), for example, 0.05-0.2 mm, or 0.07-0.15 mm. For some applications, distance D1 between opposing sides of each of the hexagons (or other types of polygons) within proximal region 46P of distal conical portion 46 of pump-outlet tube 24 is more than 0.1 mm (e.g., more than 0.3 mm) and/or less than 0.6 mm (e.g., less than 0.5 mm), e.g., 0.1-0.6 mm, or 0.3-0.5 mm.
The scope of the present disclosure includes having non-uniformly sized and/or shaped lateral blood-inlet openings (e.g., circular, rectangular, polygonal, and/or hexagonal lateral blood-inlet openings), disposed in any arrangement along the distal conical portion 46 of the pump-outlet tube. Similarly, the scope of the present disclosure includes a distal conical portion 46 of the pump-outlet tube that defines lateral blood-inlet openings being arranged such that the distal conical portion has a non-uniform porosity, with the porosity varying over different regions of the distal conical portion. For some applications, the shapes and/or sizes of the lateral blood-inlet openings, and/or the porosity of the distal conical portion, is varied such as to account for varying blood flow dynamics at different regions of the distal conical portion. Alternatively or additionally, the shapes and/or sizes of the lateral blood-inlet openings, and/or the porosity of the distal conical portion, is varied such as to account for changes in the shape of the distal conical portion along its length.
For some applications, along distal conical portion 46 of pump-outlet tube 24, the thickness of the polymeric material from which the pump-outlet tube is made is greater than the thickness in other regions of the pump-outlet tube (e.g., within the central cylindrical portion and/or the proximal conical portion of the pump-outlet tube). For some such applications, the tube is manufactured in this manner in order to prevent tearing of the tube within the distal conical portion 46, which defines blood-inlet openings 108, and may (in some cases) be at greater risk of tearing than other portions of the pump-outlet tube.
Reference is now made to
As described hereinabove, for some applications, coupling portion 41 is coupled to the outer surface of portion 123 of distal bearing housing 118H. For some applications, coupling portion 41 defines a hole 111 (e.g., toward the distal end of the coupling portion), as shown in
Reference is now made to
For some applications, the drive cable includes a plurality of coaxial layers of coiled wires. For example, as shown in
The drive cable is typically disposed within a first outer tube 140, which is configured to remain stationary while the drive cable undergoes rotational and/or axial back-and-forth motion. The first outer tube is configured to effectively act as a bearing tube for the drive cable, along the length of the drive cable. As such, first outer tube is also referred to herein as the drive-cable-bearing tube. The drive-cable-bearing tube is described in further detail hereinbelow with reference to
Typically, during insertion of the impeller and the frame into the left ventricle, impeller 50 and frame 34 are maintained in radially-constrained configurations by delivery catheter 143. As described hereinabove, in order for the impeller and the frame to assume non-radially-constrained configurations, the delivery catheter is retracted. For some applications, as shown in
Reference is now made to
For some applications, within at least some portions of the drive cable, the outer coiled wires of the drive cable are swaged such as to flatten the wires in the coil. For some applications, along a portion of the drive cable that is disposed within the aortic arch, the outer coiled wires of the drive cable are swaged in the above-described manner. Typically, if the outer coiled wires are rounded, then the outer coiled wires of the drive cable contact the inner surface of the drive-cable-bearing tube only at the outside of the circular cross-section of each of the wires, such that the frictional force that each wire exerts on the inner surface of the drive-cable-bearing tube is concentrated at that location. By contrast, if the wires are flattened, then the frictional force that each wire exerts on the inner surface of the drive-cable-bearing tube is evenly spread around the full circumference of the drive cable.
Reference is now made to
For some applications (not shown), the bearing tube is made of one or more layers of coiled wires (e.g., as described hereinabove with reference to the drive cable). Typically the coiled wires are covered with and/or embedded within a polymeric material such as polyether block amide (e.g., PEBAX®) or thermoplastic polyurethane (e.g., Pellethane®). For some applications, the coiled wires are flattened, for example, using swaging. For some applications, different regions of the tube are formed using different numbers of layers of wires, and or different numbers of wires within each layer, in order to provide different regions of the tube with respective flexibilities. For example, a region of the tube that is configured to be positioned within the aortic arch, or within the ascending aorta, may be configured to have a greater flexibility than a portion that is configured to be positioned within the descending aorta.
For some applications, in order to reduce frictional forces between the drive cable and the drive-cable-bearing tube, beads are disposed between the drive cable and the drive-cable-bearing tube. Typically, the beads have diameters of between 0.05 mm and 0.15 mm. Further typically, the beads are not held in fixed positions within the space between the drive cable and the drive-cable-bearing tube, but rather are able to move within this space thereby facilitating movement of the drive cable relative to the drive-cable-bearing tube.
Reference is now made to
For some applications, drive-cable-bearing tube 140 comprises one or more inwardly-facing ceramic portions and drive cable 130 comprises one or more outwardly-facing ceramic portions. Drive cable 130 is configured to pass through the drive-cable-bearing tube such that the outwardly-facing ceramic portions are aligned with the inwardly-facing ceramic portions, i.e., such that, at one or more regions, the interface between the drive cable and the inner surface of the drive-cable-bearing tube is ceramic on ceramic. Drive cable 130 is further configured to couple to an intracorporeal device such as a blood pump (as described above), at the distal end of the drive-cable-bearing tube, and to rotate within the drive-cable-bearing tube, thereby rotating the intracorporeal device, while the outwardly-facing ceramic portions are aligned with the inwardly-facing ceramic portions. In some embodiments, the inwardly-facing ceramic portions and/or the outwardly-facing ceramic portions comprise zirconia.
In some embodiments, the inwardly-facing ceramic portions of the drive-cable-bearing tube comprise respective ceramic sleeves 147, which may line the inside of the main body of the drive-cable-bearing tube, or alternatively, may be integrated with the main body of the drive-cable-bearing tube. For example, the main body of the drive-cable-bearing tube may comprise a structure such as laser-cut tube 145 (or wires or a braid or a coil) that is covered with or embedded within a polymeric material 148. Ceramic sleeves 147 may line the structure, or alternatively, replace the structure, at certain locations, e.g., as shown in
Similarly, the outwardly-facing ceramic portions of the drive cable may comprise respective ceramic sleeves 146, which may cover the main body of the drive cable or alternatively, may be integrated with the main body of the drive cable.
Typically, regions of drive cable 130 and drive-cable-bearing tube 140 along which the drive cable exerts strong frictional forces on the inner surface of the drive-cable-bearing tube are configured in this manner, in order to prevent wear and heating along such regions. For example, for embodiments in which the drive-cable-bearing tube is configured to pass through the aorta of the subject, the drive-cable-bearing tube may comprise the inwardly-facing ceramic portions at a section of the drive-cable-bearing tube that is configured to sit (i.e., to be disposed) within the aortic arch of the subject, and/or a section of the drive-cable-bearing tube that is configured to sit within the ascending aorta of the subject. Thus, the drive-cable-bearing tube may be inserted through the aorta such that the inwardly-facing ceramic portions are within the aortic arch and/or the ascending aorta of the subject.
In some embodiments, each of the inwardly-facing ceramic portions is 10-200% longer than each of the outwardly-facing ceramic portions. Thus, even if the drive cable moves axially within the drive-cable-bearing tube, the outwardly-facing ceramic portions may remain aligned with the inwardly-facing ceramic portions.
Reference is now made to
As described hereinabove, drive cable 130 passes through delivery tube 142, typically by virtue of passing through first outer tube 140, which functions as a drive-cable-bearing tube, which in turn passes through the delivery tube. Typically, both drive-cable-bearing tube 140 and the delivery tube extend from motor unit 23 until the proximal bearing housing 116H. Further typically, during delivery of pump-head portion 27 to the left ventricle, the pump-head portion, drive cable 130, drive-cable-bearing tube 140, and delivery tube 142 are disposed inside delivery catheter 143, with the delivery catheter maintaining the pump head in a radially constrained configuration. Once pump-head portion 27 has been delivered to the left ventricle, the delivery catheter is retracted (e.g., to the descending aorta, as shown in
Typically, delivery tube 142 is configured to impart respective mechanical properties to respective portions of the length of the drive cable. Further typically, a purging fluid is pumped between drive-cable-bearing tube 140 and the delivery tube, such that the purging fluid flows to the pump head and purges interfaces between axial shaft 92 and the proximal and distal radial bearings 116 and 118, for example, as described with reference to FIGS. 11A-C of US 2022/0226632 to Tuval, which is incorporated herein by reference.
As shown in the enlarged cross-section through delivery tube 142, typically, the delivery tube comprises an outer layer 167, with an optional braid 157 (e.g., a metal or alloy (e.g., a stainless steel) braid) or coil disposed within outer layer 167.
For some applications, delivery tube 142 is configured to provide different mechanical properties to respective regions along the delivery tube. For example, outer layer 167 may vary along the length of the delivery tube, e.g., by virtue of having a variable composition and/or a variable thickness. Alternatively or additionally to outer layer 167 varying along the length of the delivery tube, braid 157 may have a pick density that varies along the length of the delivery tube, or the aforementioned coil (substituting for braid 157) may have a pitch that varies along the length of the delivery tube. Due to this variation in outer layer 167 and/or braid 157 (or the aforementioned coil), the flexural rigidity (or “stiffness”) of the delivery tube at a first portion P1 of the delivery tube, which is configured to traverse the aortic valve of the subject, is less than the flexural rigidity at a second portion P2 of the delivery tube, which is configured to traverse at least a portion of the aortic arch of the subject, and the flexural rigidity at second portion P2 is less than the flexural rigidity at a third portion P3 of the delivery tube, which is configured to traverse the descending aorta of the subject. Advantageously, this variation in flexural rigidity facilitates the passage of the delivery tube through the aorta and into the left ventricle.
For example, outer layer 167 may comprise a (thermoplastic) polyurethane (e.g., Pellethane®) jacket (or “coating”) at first portion P1, a polyether block amide (e.g. PEBAX®) jacket at second portion P2, and a polyamide (e.g. Grilamid®) jacket at third portion P3.
For some applications, the ratio between the pick density of the braid within first portion P1 of the delivery tube to pick density of the braid within third portion P3 of the delivery tube is between 3:2 and 5:2. For some applications, the pick density of the braid within the first portion of the delivery tube is between 30 and 50 picks per inch and the pick density of the braid within the third portion of the delivery tube is between 15 and 25 picks per inch.
In some embodiments, the flexural rigidity of delivery tube 142 monotonically increases between first portion P1 and third portion P3. For example, between a polyurethane jacket at first portion P1 and a polyamide jacket at third portion P3, outer layer 167 may comprise a single polyether block amide jacket, or multiple polyether block amide jackets having an increasing durometer moving proximally along the tube.
For some applications, the delivery tube defines a first region R1, a second region R2, and a third region R3. First region R1 comprises first portion P1, second region R2 comprises second portion P2, and third region R3 comprises third portion P3.
Typically, first region R1 is configured to extend proximally from the proximal end of the frame (e.g., from proximal bearing housing 116H) through the aortic valve and into the ascending aorta. For some applications, first region R1 has a length of between 70 mm and 100 mm, e.g., between 75 mm and 95 mm.
Typically, second region R2 extends proximally from the proximal end of first region R1 and around at least a portion of the aortic arch. For some applications, second region R2 has a length of between 40 mm and 80 mm (e.g., between 50 mm and 70 mm). Alternatively, second region R2 has a length of between 150 mm and 210 mm (e.g., between 160 mm and 200 mm). For some applications, along second region R2, there is a gradual decrease in the flexibility (i.e., a gradual increase in the flexural rigidity) of the delivery tube. For example, along second region R2, outer layer 167 may comprise multiple polyether block amide jackets having an increasing durometer moving proximally along the tube. Alternatively, the flexural rigidity of delivery tube 142 may be uniform along second region R2.
Typically, third region R3 extends from the proximal end of second region R2 along the descending aorta, out of the patient's vasculature (e.g., via a femoral puncture FP), and to motor unit 23. For some applications, third region R3 has a length of between 1200 mm and 1500 mm (e.g., between 1250 mm and 1450 mm). In some embodiments, there is a gradual decrease in flexibility from the distal end of region R3 to third portion P3. For example, along region R3 distally to third portion P3, outer layer 167 may comprise multiple polyether block amide jackets having an increasing durometer moving proximally along the tube.
In some embodiments, the flexural rigidity at the distal end of the delivery tube, which is identified in
For example, outer layer 167 may comprise a polyurethane jacket at first portion P1 and a polyether block amide (e.g. PEBAX®) jacket at the distal end. The outer layer may further comprise a polyamide jacket at third portion P3, such that the flexural rigidity at the distal end is between that of first portion P1 and that of third portion P3.
In some such embodiments, the flexural rigidity monotonically increases between first portion P1 and the distal end of the delivery tube. (The flexural rigidity may thus increase monotonically moving both proximally and distally from first portion P1.) For example, distally to first portion P1, outer layer 167 may comprise multiple polyether block amide jackets having an increasing durometer moving distally along the tube.
In some embodiments, the flexural rigidity at a fourth portion P4 of the delivery tube, which is configured to span the point of insertion into the body of the subject (e.g., femoral puncture FP), is less than the flexural rigidity at third portion P3. Advantageously, this lesser flexural rigidity may facilitate the insertion into the body. Nonetheless, even in such embodiments, the flexural rigidity at the proximal end of the delivery tube—i.e., the flexural rigidity proximally to fourth portion P4, along the most proximal portion of third region R3, which may have a length of between 360 mm and 460 mm (e.g., between 380 mm and 440 mm)—is greater than the flexural rigidity at fourth portion P4 (and, optionally, greater than that of third portion P3), in order to facilitate advancing and retracting this portion of the delivery tube with respect to a handle 149, and/or in order to facilitate clamping of the delivery tube without causing the delivery tube to kink. For example, proximally to fourth portion P4, outer layer 167 may comprise a polyether block amide (e.g. PEBAX®) jacket with a high-performance polyamide (e.g., Grilamid®) outer coating. In some embodiments, along this most proximal portion of the delivery tube, the delivery tube comprises a coil or metal frame positioned between braid 157 and outer layer 167, e.g., between fiber 159, which is described immediately below, and outer layer 167. Advantageously, the coil or metal frame may further inhibit kinking of the delivery tube.
In some embodiments, the delivery tube further comprises at least one fiber 159 (e.g., an aromatic polyamide (i.e., aramid) fiber) that extends along the length of delivery tube 142 and increases the tensile rigidity (or “tensile strength”) of the delivery tube, relative to if the delivery tube would not comprise fiber 159. In other words, fiber 159 resists elongation, thereby inhibiting elongation of the delivery tube. Thus, braid 157 resists bending (the degree of this resistance optionally varying along the length of the delivery tube) and elongation, while fiber 159 provides additional resistance to elongation (i.e., the fiber provides additional tensile strength). For some applications, a relatively high resistance to elongation (i.e., a relatively high tensile strength) is desirable along the full length of the delivery tube, in order to prevent elongation of the delivery tube when the delivery tube is disposed inside delivery catheter 143.
Typically, fiber 159 is disposed inside outer layer 167. For example, as shown in
Typically, the tensile rigidity of the delivery tube is more uniform than the flexural rigidity of the delivery tube.
For example, (a) the ratio between the tensile strength of third portion P3 and that of first portion P1 may be lower than (b) the ratio between the flexural rigidity of third portion P3 and that of first portion P1. For example, the ratio between the tensile strength of third portion P3 and that of first portion P1 is typically between 3:2 and 5:2 (e.g. 2:1), and the ratio between the flexural rigidity of third portion P3 and that of first portion P1 is typically between 5:2 and 7:2 (e.g., 3:1). Thus, for some applications, a ratio between the former ratio and the latter ratio is between 4:3 and 5:3, e.g., 3:2.
Alternatively or additionally, the ratio between the tensile rigidity at second portion P2 and the tensile rigidity at first portion P1 may be less than the ratio between the flexural rigidity at second portion P2 and the flexural rigidity at first portion P1. Alternatively or additionally, the ratio between the tensile rigidity at third portion P3 and the tensile rigidity at second portion P2 may be less than the ratio between the flexural rigidity at third portion P3 and the flexural rigidity at second portion P2. This latter ratio—or, for embodiments in which second region R2 has a variable flexural rigidity, the ratio between the flexural rigidity of third portion P3 and the mean flexural rigidity of second region R2—is typically between 3:2 and 5:2 (e.g. 2:1).
Typically, notwithstanding the nonuniformity of outer layer 167 and/or of braid 157, the delivery tube comprises a uniform inner surface. For example, braid 157 may be coated with a uniform polymeric inner lining 155 (e.g., a thermoplastic polyurethane (e.g., Pellethane®) inner lining) along the length of delivery tube 142. Thus, advantageously, outer tube 140 (or, in some embodiments, the drive cable itself) is exposed to the uniform inner surface.
In some embodiments, outer layer 167 becomes at least partly fused with the more inner portions of the delivery tube 142 during the manufacture thereof, e.g., via a reflow soldering process.
In the context of the above discussion regarding the flexural rigidity of respective portions of delivery tube 142, it is noted that a metric for quantifying flexural rigidity is Young's modulus multiplied by the second moment of area (which is also known as area moment of inertia).
Reference is now made to
As described hereinabove, typically, the drive cable, which comprises a plurality of (e.g., three layers of) coiled wires 134, extends from the motor unit 23 (which is disposed outside the subject's body) until the axial shaft 92, which is hollow. Rotational motion that is generated by the motor within the motor unit is typically transmitted to the axial shaft (and thereby transmitted to the impeller) via the drive cable.
For some applications, the drive cable is coupled to the axial shaft via welding. In some cases, however, the interface between the drive cable and the axial shaft can be weakened as a result of the heating that the drive cable and the axial shaft undergo during welding. Therefore, for some applications, the drive cable is coupled to the axial shaft via a coupling technique other than welding. To facilitate this coupling technique, the proximal end of the axial shaft may be shaped to define multiple shaft pores 152.
More specifically, for some applications, a porous coupling tube 150 (which may be polymeric) is placed around the distal end of drive cable and the proximal end of the axial shaft. In other words, the distal end of the drive cable and the proximal end of the axial shaft are inserted into opposing ends of coupling tube 150, which is shaped to define multiple coupling-tube pores 173. Subsequently, while the ends of the drive cable and axial shaft are inside the coupling tube, a molten bonding material is flowed between coiled wires 134 at the distal end of the drive cable via coupling-tube pores 173, and into the proximal end of the axial shaft via the coupling-tube pores and shaft pores 152, such that, upon solidifying, the material bonds the drive cable to the axial shaft. Typically, while the molten bonding material solidifies, the distal end of the drive cable, the proximal end of the axial shaft, and the coupling tube are compressed and heated.
Typically, the drive cable is also hollow, and it is desired that the drive cable and axial shaft be shaped to define a continuous lumen even after the bonding material solidifies. Hence, prior to the flowing of the molten bonding material, the drive cable and axial shaft are placed over a mandrel, such that the continuous lumen is maintained. (This continuous lumen is shown, for example, in
Typically, the molten material includes a molten polymer including, for example, polyether ether ketone (PEEK). The polymer is heated such that it passes through the coupling-tube pores 173 and flows between the wires of the drive cable and into the shaft. Upon drying and solidifying, the polymeric material bonds the drive cable to the axial shaft.
In some embodiments, the molten material is flowed using a heat-shrinking process. In particular, a sleeve of the bonding material (e.g., a PEEK sleeve) is placed around the coupling tube, and an outer sleeve (made of polytetrafluoroethylene, for example) is placed around the sleeve of the material. Next, heat is applied to the sleeve of the material and to the outer sleeve. The applied heat melts the sleeve of the material, thereby forming the molten material, and shrinks the outer sleeve such that the outer sleeve forces the molten material between coiled wires 134 and into the proximal end of the axial shaft. Following the solidification of the molten material, the outer sleeve and any protruding pieces of the solidified material may be removed.
For some applications, the axial shaft (or at least the proximal end thereof) has a smaller outer diameter than the drive cable (or at least the distal end thereof). For example, the axial shaft may have a diameter of 0.9 mm and the drive cable may have a diameter of 1.1 mm, 1.2 mm, or 1.3 mm. For some such applications, prior to the insertion of the proximal end of the axial shaft into the coupling tube, a porous adaptor tube 151, which is shaped to define multiple adaptor-tube pores 129, is placed around the proximal end of the axial shaft so as to add to the outer diameter of the axial shaft, e.g., such that the outer diameter of the axial shaft with porous adaptor tube 151 disposed around it is approximately equal to the outer diameter of the distal end of the drive cable. Porous coupling tube 150 is then placed over the distal end of the drive cable and over the porous adaptor tube (which, in turn, is disposed over the proximal end of the axial shaft). The molten material is then flowed into the axial shaft via adaptor-tube pores 129.
In some embodiments, adaptor tube 151 is polymeric. In other embodiments, the adaptor tube comprises a metallic alloy.
For some applications, the distal end of the drive cable is coupled to the proximal end of the axial shaft using the following procedure. Porous adaptor tube 151 is placed over the proximal end of the axial shaft, and the porous coupling tube is then placed over the distal end of the drive cable and over the porous adaptor tube. The above-described assembly is then placed over a mandrel, which passes through the lumen defined by the axial shaft and the distal end of the drive cable. A polymeric material, such as polyether ether ketone, is heated such that it passes through the pores of the porous coupling tube, the porous adaptor tube, and into pores 152 of the axial shaft (e.g., using a heat-shrinking process). Typically, the mandrel prevents the polymeric material from entering the lumen defined by the axial shaft and the distal end of the drive cable. Upon drying and solidifying, the polymeric material bonds the drive cable to the axial shaft.
As described above, typically, delivery tube 142 is coupled to proximal bearing housing 116H (
With reference to
Reference is now made to
In some embodiments, coupling tube 150 is compliant so as to conform both to the larger outer diameter of the drive cable and to the smaller outer diameter of the axial shaft, thus typically obviating the need for adaptor tube 151.
Reference is now made to
In some embodiments, the wall of coupling tube 150 is shaped to define multiple tabs 154. Prior to the flowing of the molten material, at least some of tabs 154 are pushed into shaft pores 152 (
In some embodiments, to strengthen the coupling even further, at least two of the tabs pushed into shaft pores 152 have different respective orientations with respect to the longitudinal axis of the coupling tube. In other words, at least two of these tabs are rotatable about rotation axes having different respective orientations with respect to the longitudinal axis. For example, in the embodiment shown in
In some embodiments, the tabs pushed into shaft pores 152 are shaped to define respective holes 137, which allow the molten material to flow therethrough.
Reference is now made to
In some embodiments, prior to flowing the molten material between coiled wires 134 at the distal end of the drive cable and into the proximal end of the axial shaft, some of tabs 154 are pushed between the coiled wires such that these tabs protrude between the coiled wires, thereby strengthening the coupling of the drive cable to the axial shaft. These tabs may have any shape that allows the tabs to fit between the coiled wires, which may be different from the shape of those of the tabs pushed into the shaft pores. For example, in some embodiments, U-shaped tabs 154c are pushed between the coiled wires.
In some embodiments, at least one of the coiled wires (in any one or more of the layers of the drive cable) is cut, at the distal end of the drive cable, so as to define one or more enlarged gaps between successive windings of the coiled wires, and some of the tabs (such as U-shaped tabs 154c) are pushed into the enlarged gaps. Such cuts 135 are shown in
It is noted that the scope of the present invention includes the use of tabs 154 to strengthen the coupling of the drive cable to the axial shaft even without the subsequent flowing of a molten material through coupling-tube pores 173.
In some embodiments, as shown in
Alternatively or additionally to coupling the distal end of the drive cable to the proximal end of the axial shaft, the techniques described above may be used to couple the proximal end of the drive cable to the distal end of another hollow shaft configured to couple the drive cable to a rotating element configured to rotate the drive cable. For example, as noted hereinabove with reference to
For some applications, the drive cable continues into the pump-head portion, rather than the drive cable ending at the coupling to the axial shaft. For some such applications, a reinforcing element is added inside the drive cable within the pump-head portion, in order to add to the rigidity of the drive cable within the pump-head portion. Typically, the reinforcing element defines a lumen therethrough, which functions as a portion of the continuous lumen described hereinbelow with reference to
For some applications, the ventricular assist device does not define a lumen within the pump head, i.e., the axial shaft, which is coupled to the impeller, is solid. For some such applications, the axial shaft may have a relatively small diameter, such as a diameter less than 1 mm, e.g., less than 0.8 mm, 0.6 mm, or 0.4 mm. Thus, the axial shaft may have a smaller diameter than the drive cable (which, as noted above, is typically hollow, to facilitate the flow of purging fluid therethrough). For example, the drive cable may have an outer diameter greater than 1 mm (e.g., between 1 mm and 1.5 mm), and the axial shaft may have a diameter of less than 1 mm, e.g., less than 0.8 mm, 0.6 mm, or 0.4 mm. Advantageously, as a result of the axial shaft defining a smaller diameter, the pump-head portion can be radially constrained (i.e., crimped) to a smaller diameter.
Optionally, the drive cable may be coupled to the smaller-diameter axial shaft as described above with reference to
Reference is now made to
Referring to
For some applications, by using lumen 132 of the axial shaft and the cable in the above-described manner, it is not necessary to provide an additional guidewire guide to be used during insertion of left-ventricular assist device 20. For some applications, the axial shaft and the drive cable each have outer diameters of more than 0.6 mm (e.g., more than 0.8 mm), and/or less than 1.4 mm (e.g., less than 1 mm), e.g., 0.6-1.4 mm, such as 0.6-1.2 mm or 0.8-1 mm. For some applications, the diameter of lumen 132, defined by the shaft and the cable, is more than 0.3 mm (e.g., more than 0.4 mm), and/or less than 0.7 mm (e.g., less than 0.6 mm), e.g., 0.3-0.7 mm, or 0.4-0.6 mm. For some applications, drive cable 130 has a total length of more than 1 m (e.g., more than 1.1 m), and/or less than 1.4 m (e.g., less than 1.3 m), e.g., 1-1.4 m, or 1.1-1.3 m. Typically, the diameters of lumen 122 and lumen 133 are generally similar to that of lumen 132.
For some applications, the continuous lumen is additionally used by purging system 29 (shown in
Referring to
As described hereinabove, typically, the drive cable includes a plurality of coiled wires. For some applications, purging fluid passes into lumen 132 defined by the drive cable via gaps in the coiled wires. Once the purging fluid is disposed within lumen 132 it flows in both proximal and distal directions, as indicated by a bidirectional purging-fluid-flow arrow 162c of
As described above, once the purging fluid is disposed within lumen 132 it flows in both proximal and distal directions, as indicated by arrow 162c of
Referring again to
Reference is now made to
Some applications of the present invention are described hereinabove as being directed toward a ventricular assist device that does not include any thrust bearing disposed within the subject's body and that is configured to allow axial back-and-forth motion of impeller 50 and axial shaft 92. For some alternative applications, the ventricular assist device does include a thrust bearing that is disposed distally from axial shaft 92 so as to inhibit distal movement of the axial shaft beyond the thrust bearing. Optionally, the thrust bearing may further inhibit proximal movement of the axial shaft, such that the thrust bearing may prevent any axial movement of the axial shaft. For example, in some embodiments, thrust bearing 260 prevents axial shaft 92 from undergoing axial motion in response to variations in the pressure gradient against which the impeller is pumping (thereby, typically, preventing the impeller from undergoing axial motion in response to variations in the pressure gradient against which the impeller is pumping).
For some applications, thrust bearing 260 is disposed within frame 34 as shown. For example, the thrust bearing may be disposed within the cylindrical portion of the frame or within the distal conical portion of the frame. For some applications, at a distal end of axial shaft, the axial shaft defines a widened portion 262 that is configured to engage the thrust bearing and to prevent the axial shaft (and thereby prevent the impeller) from undergoing axial motion. (In addition, the widened portion of the axial shaft is constrained radially by bearing 260, such that the bearing also functions as a distal radial bearing.) For some applications, the thrust bearing is coupled to the frame via connecting struts 264, which extend radially inwardly from the frame to the thrust bearing. Typically, in order to manufacture frame 34, the frame is cut from a tube of a shape-memory alloy, such as nitinol. For some applications, connecting struts 264 are cut from the tube from which the frame is cut, such that the frame and the connecting struts form a single integral body, without requiring coupling to each other (e.g., via adhesive, welding, etc.). In general, for some applications, the frame and the connecting struts are cut from a single piece of a material such as to form a single integral body. For some applications, connecting struts 264 as well as thrust bearing 260 itself are cut from the tube from which the frame is cut, such that the frame, the connecting struts, and the thrust bearing form a single integral body, without requiring coupling to each other (e.g., via adhesive, welding, etc.). In general, for some applications, the frame, the connecting struts, and thrust bearing 260 itself are cut from a single piece of a material such as to form a single integral body.
Reference is now made to
Reference is now made to
For some applications, a thrust bearing 270 is disposed within distal bearing housing 118H, adjacent to the distal end of axial shaft 92. Typically, the distal end of the axial shaft is configured to be in contact with the distal thrust bearing. When the impeller pumps blood in the proximal direction, this causes the axial shaft to be biased in the distal direction. The thrust bearing prevents distal movement of the axial shaft, such that the axial shaft and the impeller typically remain in axially fixed positions within frame 34.
In some embodiments, thrust bearing 270 comprises a proximally-facing ceramic surface 271 comprising, for example, zirconia. A distally-facing ceramic cover 273, comprising zirconia for example, covers the distal end of axial shaft 92, such that ceramic cover 273 contacts ceramic surface 271 as the axial shaft rotates. Thus, advantageously, there is a low-friction interface between the axial shaft and the thrust bearing.
For some applications, the thrust bearing is made of a ceramic material (e.g., zirconia), i.e., the thrust bearing comprises a piece of ceramic comprising proximally-facing ceramic surface 271. In other embodiments, the thrust bearing is made of a different material but is coated with a ceramic material, i.e., the thrust bearing comprises the proximally-facing ceramic surface by virtue of being coated with a ceramic coating.
It is noted that thrust bearing 270 differs from thrust bearing 260 of
As described hereinabove, for some such applications, the axial shaft is covered with ceramic sleeves 240 (e.g., zirconia sleeves) along regions of the axial shaft that come into contact with either of the proximal and distal bearings 116, 118 during operation of the ventricular assist device. In this manner, the radial interfaces between the axial shaft and the proximal and distal bearings are ceramic-ceramic interfaces. For some applications, the ceramic sleeve at the distal end of the axial shaft extends around the distal end of the axial shaft, such that the axial interface between the axial shaft and thrust bearing 270 is a ceramic-ceramic interface. In other words, a ceramic cap, which comprises ceramic cover 273, fits around the distal end of the axial shaft, such that the ceramic cap covers both the distal end and side wall of the axial shaft. (Thus, in effect, ceramic cover 273 and ceramic sleeve 240 are combined into a single element.) In other embodiments, as shown in
In some embodiments, axial shaft 92 is shaped to define a shaft lumen 132d, which is the distal portion of lumen 132 (
For some applications, at least a portion of bearing lumen 272 is frustoconically-shaped, with a wider end of the bearing lumen facing distally. In other words, at its distal end 272d, the lumen defines a portion of a cone, with a wide end of the cone-portion facing the distal direction. Typically, the frustoconical portion of the lumen facilitates the advancement of the guidewire through the thrust bearing in the distal-to-proximal direction.
For some applications, thrust bearing 270 is configured such as to allow proximal (or “reverse”) flow of fluid (in particular, purging fluid) into the interface between the distal end of the axial shaft and the thrust bearing (e.g., between ceramic cover 273 and proximally-facing ceramic surface 271). For some such applications, the thrust bearing defines at least one additional bearing lumen (not shown) for proximal flow of the purging fluid, through the additional bearing lumen, into the interface. In other words, to facilitate the flow of purging fluid in the distal-to-proximal direction and through the interface between the thrust bearing and the axial shaft, the thrust bearing may define one or more additional flow channels.
Reference is now made to
Typically, when the ventricular assist device includes a thrust bearing within the pump-head portion, the impeller and the axial shaft do not undergo axial back-and-forth motion. This is because, when the impeller pumps blood in the proximal direction, this causes the axial shaft to be biased in the distal direction. The thrust bearing prevents distal movement of the axial shaft, such that the axial shaft and the impeller remain in axially fixed positions within frame 34.
For some such applications, and even for some applications in which there is no thrust bearing (such that proximal bearing housing 116H houses proximal radial bearing 116 but no thrust bearing, and the impeller and axial shaft undergo axial motion), drive cable 130 is coupled to axial shaft 92 within the proximal bearing housing. In other words, the interface between the distal end of drive cable 130 and the proximal end of axial shaft 92 (i.e., the location at which the drive cable and the axial shaft are coupled to each other) is within the proximal bearing housing 116H. Typically, the proximal bearing housing is rigid, such that the proximal bearing housing protects the location at which the drive cable and the axial shaft are coupled to each other from being exposed to forces, such as bending forces, that could weaken the coupling and thereby damage the ventricular assist device. For example, the proximal bearing housing may inhibit bending of the drive cable within the bearing housing.
Typically, in such embodiments, the radial separation between the proximal bearing housing and the distal end of the drive cable, which is within the proximal bearing housing, is less than 2 mm, e.g., less than 1 mm. Advantageously, this small radial separation may help inhibit bending of the drive cable.
For some applications, the drive cable and the axial shaft are coupled to each other using the apparatus and methods described with reference to
As described above, proximal radial bearing 116 surrounds the axial shaft and is configured to radially stabilize the axial shaft while the axial shaft rotates. A proximal sleeve 240 is disposed around the axial shaft such that proximal sleeve 240 contacts proximal radial bearing 116 as the axial shaft rotates. Similarly, distal radial bearing 118 (
For some applications, when the ventricular assist device includes a thrust bearing within the pump-head portion (and therefore the impeller and axial shaft do not undergo axial back-and-forth motion), sleeves 240 (which are placed around the axial shaft at the interfaces between the axial shaft and the proximal and distal radial bearings) are shorter than in cases in which the ventricular assist device does not include a thrust bearing within the pump-head portion (and in which the impeller and axial shaft undergo axial back-and-forth motion). This is because the portion of the axial shaft that is located at the interfaces with the proximal and distal radial bearings is relatively fixed. For some applications, the length of each of the proximal and distal radial bearings are between 2 and 4 mm (e.g., approximately 3 mm) and the length of each of the sleeves is between 2.5 and 4.5 mm (e.g., approximately 3.5 mm). For some applications, the length of each of the sleeves is between 4 and 6 mm (e.g., approximately 5 mm), in order to provide a larger margin at the ends of the radial bearings.
For some applications, the axial shaft is more flexible than the sleeves. For example, the sleeves may be made of a ceramic material (e.g., zirconia), and the axial shaft may be made of a material more flexible than ceramic, such as nitinol or another shape-memory alloy. Typically, it is desirable for the axial shaft to be sufficiently flexible as to pass through curved portions of the vasculature during delivery of the device to the left ventricle, but also sufficiently rigid to be able to provide support to the impeller during the operation of the impeller without the axial shaft undergoing vibration.
For some such applications, the lengths of the sleeves relative to the length of the shaft is configured to provide a desired overall flexibility to the axial shaft and/or to provide a desired flexibility to respective portions of the axial shaft. For example, the ratio between the length of the axial shaft and the combined length of the proximal and distal sleeves may be more than 2:1 (e.g., more than 3:1) and/or less than 6:1 (e.g., less than 5:1), for example between 2:1 and 6:1 or between 3:1 and 5:1. For some such applications, the length of the axial shaft is between 30 and 50 mm, e.g., between 35 mm and 45 mm. As described hereinabove, the length of each of the proximal and distal sleeves may be between 4 and 6 mm (e.g., approximately 5 mm), such that the combined length of the sleeves is 8-12 mm, in order to provide a larger margin at the ends of the radial bearings.
Reference is now made to
Reference is now made to
Referring now to
For some applications, distal-tip element 107 is configured to separate the blood inlet opening from a posterior wall of the subject's left ventricle when the distal-tip element is placed against the apex of the subject's left ventricle. Typically, the distal-tip element is configured to separate the blood-inlet opening from a septal wall of the subject's left ventricle as the distal-tip element contacts the apex of the subject's left ventricle.
Typically, distal-tip element 107 is inserted into the left ventricle, such that bulge 351 bulges toward the septal wall 338. When disposed in this configuration, in response to distal-tip element 107 being pushed against the apex (e.g., due to a physician advancing the device or in response to movement of the left ventricle), blood inlet openings 108 typically get pushed in the direction of free wall 334 and away from the septal wall 338 (in the direction of the arrows shown in
Referring now to
In some embodiments, the tip portion further comprises a straight portion 353 proximal to proximal curved portion 350. Straight portion 353 may be configured to receive the axial shaft while the axial shaft rotates, as described above, with reference to
In some embodiments, the angle between the distal end of the proximal curved portion and the axial shaft is between 100 and 170 degrees. Alternatively or additionally, the angle between the distal end of the proximal curved portion and the plane in which distal curved portion 349 lies is between 25 and 65 degrees, such as between 35 and 55 degrees. For some applications, the angle between the distal end of the proximal curved portion and the plane in which distal curved portion 349 lies is 60 and 120 degrees.
For example, as shown in
In some embodiments, distally to proximal curved portion 350, the distal-tip portion undergoes the above-described curvature (i.e., the curvature that is similar to that of a question mark or a tennis-racket) in a second plane. In other words, distal curved portion 349 comprises a straight segment 355 (analogous to straight portion 346 of
Typically, lumen 122 (
In some embodiments, the impeller of the blood pump is rotated (i.e., the blood pump is operated) while distal curved portion 349 pushes against apex 342. For some applications, the proximal curved portion is configured such that if the tip is pushed against apex 342, then even in the event that distal curved portion 349 curls up, the distal blood-inlet openings 108 are still pushed in the direction of free wall 334 and away from the septal wall 338, by the tip flexing about proximal curved portion 350.
Reference is now made to
In some embodiments, one or more steering wires 301 are coupled to frame 34 and are configured to extend from the frame, to outside the body of the subject, while the frame is within the body. In some embodiments, steering wires 301 pass through delivery tube 142. For example, the steering wires may be disposed between drive-cable-bearing tube 140 and the delivery tube.
In some embodiments, one of the steering wires is coupled to the proximal end of frame 34. Alternatively or additionally, one of the steering wires may be coupled to the distal end of frame 34. This coupling may be via proximal bearing housing 116H or distal bearing housing 118H, i.e., the steering wire may be coupled to the frame by virtue of being coupled to the proximal or distal bearing housing.
Typically, for such applications, handle 149 of the ventricular assist device comprises a steering control 300, and the steering wires are coupled to steering control 300 so as to be controllable via the steering control.
Advantageously, steering wires 301 may be configured for orienting the frame, e.g., prior to rotating the impeller so as to pump blood of the subject. For example, the steering wires may be configured to extend from the frame while the frame is within the left ventricle of the subject's heart, and the steering wires may be configured for orienting the frame within the left ventricle, e.g., such that the frame extends toward the apex of the left ventricle. The frame may be oriented by applying a force to a steering wire coupled to the proximal end of the frame while applying a counterforce to the delivery tube or to another steering wire coupled to the distal end of the frame.
For some such applications, a controller steers the proximal end of the frame with respect to a portion of the device disposed proximally thereto, for example, in order to direct the distal end of the frame to extend in the direction of the apex of the left ventricle. Typically, upon releasing the pump head within the left ventricle, the operator steers the proximal end of the frame in the above-described manner, in order to conform with the anatomy (e.g., the shape of the left ventricle) of the subject.
As described hereinabove with reference to
Reference is now made to
In some embodiments, an expandable element 314, such as an expandable stent, an expandable braided element, or an inflatable element 316 (e.g., a balloon 114), surrounds delivery tube 142 proximally to blood-outlet openings 109, with the length of the delivery tube between expandable element 314 and the blood-outlet openings being less than 30 mm. For example, expandable element 314 may be disposed in the vicinity of the interface between delivery tube 142 and the region at which the proximal end of pump-outlet tube 24 is coupled to the delivery tube (as shown in
In some embodiments, as shown in
Typically, expandable element 314, whether configured as shown in
In some embodiments, expandable element 314 is an inflatable element 316 that is shaped to direct the blood through blood-outlet openings 109, as indicated in
For some applications, the inflatable element (e.g., balloon) is inflated using a fluid (e.g., a purging fluid), which is pumped through the ventricular-assist device. For example, as shown in
It is noted that expandable element 314 may be combined with any of the embodiments of pump-outlet tube 24 described below with reference to
As shown in
For some applications, the pump-outlet tube is manufactured using a single continuous tube, with respective portions of the pump-outlet tube being molded to define the tubular coupling portion, the proximal conical portion, the distal conical portion, and the cylindrical central portion, as in the former method described in the above paragraph. However, before adhering the tubular coupling portion to outer tube 142 of the ventricular assist device, the tubular coupling is cut (e.g., in a tapered manner), so as to reduce the thickness of the layer of the pump-outlet tube that is coupled to outer tube 142 and/or to prevent folds forming in the tubular coupling portion of the pump-outlet tube.
Typically, (a) blood-outlet openings 109 are defined by portions of the wall of the blood outlet tube that at least partially extends into the proximal conical portion of the pump-outlet tube, e.g., as shown in
Reference is now made to
For some applications, the expandable element is configured to act as a blood flow director, by directing blood from the proximal end of the pump-outlet tube through the blood outlet openings, as indicated by blood-flow arrows 360. For some applications, the expandable element is shaped such as to direct the blood flow in this manner. For example, the expandable element may have an angled and/or a curved surface that is configured to direct the blood flow in this manner. For some applications, by directing blood flow in this manner, the overall pumping efficiency of the device is increased relative to if the device does not include an expandable element.
As described hereinabove, typically, expandable element 314 is configured to center a portion of the ventricular assist device (e.g., a portion of delivery tube 142 and, in particular, the portion of the delivery tube near pump-outlet tube 24) within the aorta, by contacting the aorta wall or, if the expandable element is within the pump-outlet tube, by pushing the wall of the pump-outlet tube against the aorta wall.
Referring to
As described hereinabove, typically, the porous expandable element is configured to center a portion of the ventricular assist device (e.g., a portion of delivery tube 142 and, in particular, the portion of the delivery tube near pump-outlet tube 24) within the aorta, by contacting the aorta wall or, if the expandable element is within the pump-outlet tube, pushing the wall of the pump-outlet tube against the aorta wall.
Referring to
Referring to
Reference is now made to
For some applications, internal membrane 368 is a continuation of pump-outlet tube 24, and the internal membrane is covered with an external membrane, which defines blood-outlet openings, and which forms the external surface of blood-flow chamber 366. For such applications, the proximal end of the blood-outlet tube is shaped so as to direct the blood flow out of the blood-outlet openings.
Typically, the combination of the proximal end of the blood-outlet tube and an additional membrane (whether an internal membrane or an external membrane) are configured to define blood-flow chamber 366, which typically functions as described above. In general, the scope of the present disclosure includes any structure that provides a blood-flow chamber disposed at a proximal end of the pump-outlet tube, the blood-flow chamber defining (a) holes 370 via which blood is pumped into the blood-flow chamber and (b) blood-outlet openings 109 configured to be disposed with within the aorta via which the blood flows out of the blood-flow chamber and into the aorta.
Reference is now made to
Reference is now made to
For some applications, inlet guard 400 is flat and/or is disposed such that it is perpendicular to the axial shaft (i.e., to the longitudinal axis of the frame). Thus, advantageously, the inlet guard may occupy relatively little space, and/or may provide an advantageous flow direction for the blood. Typically, the inlet guard is toric.
As described hereinabove (with reference to
For some applications, the inlet guard is placed within the frame at the distal end of the central cylindrical portion of the frame or in the vicinity thereof, e.g., within 1 mm of the distal end of the cylindrical portion. This placement may simplify the assembly of the blood pump.
Typically, the inlet guard is polymeric, i.e., is made of a polymeric material (such as polyurethane (e.g., Pellethane®), polyethylene terephthalate (“PET”), ultra-high-molecular-weight polyethylene (“UHMWPE”), and/or polyether block amide (e.g., Pebax®)) that is shaped to define holes 402. For some applications, the thickness of the inlet guard is more than 40 microns (e.g., more than 50 microns), and/or less than 100 microns (e.g., less than 80 microns), for example, 40-100 microns or 50-80 microns. Thus, the inlet guard may be configured to withstand pressure yet be crimpable.
Typically, for applications in which ventricular assist device 20 includes inlet guard 400 disposed inside frame 34, pump-outlet tube 24 does not extend until the distal end of distal conical portion 40 of frame 34. Moreover, pump-outlet tube 24 may have an open distal end, rather than terminating in a distal conical portion. (Thus, the inlet guard may simplify the manufacture of the blood pump.) The distal end of the pump-outlet tube may be proximal to the distal end of the distal conical portion of the frame. For example, the distal end of the pump-outlet tube may be within 1 mm of the distal end of the central cylindrical portion of frame 34, i.e., the pump-outlet tube may extend only until the end of the cylindrical portion of frame 34, or the vicinity thereof. Blood may thus flow into frame 34 via openings defined by the distal conical portion of the frame.
For some applications, holes 402 of inlet guard 400 are sized such as (a) to allow blood to flow from the subject's left ventricle into pump-outlet tube 24 and (b) to block structures from the subject's left ventricle from entering into the pump-outlet tube. Typically, for such applications, the inlet guard is configured to reduce a risk of structures from the left ventricle (such as chordae tendineae, trabeculae carneae, and/or papillary muscles) entering into pump-outlet tube 24 and potentially being damaged by the impeller and/or the axial shaft, and/or causing damage to the ventricular assist device.
For some applications, inlet guard 400 defines more than 10 holes, more than 50 holes, more than 100 holes, or more than 150 holes, e.g., 50-100 holes, 100-150 holes, or 150-200 holes. For some applications, the holes are sized such as (a) to allow blood to flow from the subject's left ventricle into the tube and (b) to block structures from the subject's left ventricle from entering into the frame. Typically, for such applications, the inlet guard is configured to reduce a risk of structures from the left ventricle (such as chordae tendineae, trabeculae carneae, and/or papillary muscles) entering into the cylindrical portion of frame 34 and potentially being damaged by the impeller and/or the axial shaft, and/or causing damage to the left ventricular assist device. Therefore, for some applications, the holes are shaped such that, for each of the holes, the span of the hole in at least one direction is less than 1 mm, e.g., 0.1-1 mm, or 0.3-0.8 mm. By defining such a small width (or span), it is typically the case that structures from the left ventricle (such as chordae tendineae, trabeculae carneae, and/or papillary muscles) are blocked from entering into the cylindrical portion of frame 34.
For some applications, each of the holes defines an area of more than 0.05 square mm (e.g., more than 0.1 or 0.3 square mm), and/or less than 5 square mm (e.g., less than 3 or 1 square mm), e.g., 0.05-5, 0.05-3, 0.1-1, 0.1-5, or 0.3-1 square mm.
Typically, the inlet guard has a porosity of at least 40 percent, e.g., more than 50 percent, or more than 60 percent (where porosity is defined as the percentage of the area of this portion that is porous to blood flow). Thus, on the one hand, the holes are relatively small (in order to prevent structures of the left ventricular from entering the frame), but on the other hand, the porosity of the portion of the pump-outlet tube that defines the holes is relatively high, such as to allow sufficient blood flow into the pump-outlet tube.
For some applications, each of the holes has a circular or a polygonal shape. For some applications, each of the holes has a hexagonal shape, as shown most clearly in
As shown in
As further shown in
For some applications, the frame is assembled with the inlet guard inside in the following manner. As described hereinabove, during assembly of the pump-head portion, the proximal end of frame 34 is typically open. For some applications, the inlet guard is placed through the open proximal end of the frame while being supported upon a rod (e.g., a mandrel). The inlet guard typically has an overall torus shape, with the edges of the shape defining inner and outer circles, as shown in
As noted above, in some embodiments, the inlet guard is coupled to the distal bearing housing, which may house a radial and/or thrust bearing. In such embodiments, typically, the distal bearing housing is partly or entirely disposed within frame 34. For example, at least 10%, 50%, or 80% of the length of the bearing housing may be disposed within the frame. Moreover, the distal bearing housing may extend into the frame even for applications in which the blood pump does not comprise inlet guard 400.
For further details in this regard, reference is now made to
Typically, it is desirable for the relatively rigid portions of the pump-head portion of the device (such as the frame, the impeller, and the bearing housings) to have a combined length that is as short as possible, in order to safely navigate the device through curved vasculature of the subject (such as the aortic arch). For some applications, by configuring the device such that distal bearing housing 118H extends at least partially into the distal conical portion of frame 34, the combined length of the relatively rigid portions of the pump-head portion of the device (such as the frame, the impeller, and the bearing housings) is shortened relative to if the device were configured such distal bearing housing 118H would not extend proximally at least partially into the distal conical portion of frame 34.
In some embodiments, the bearing housing occupies at least 10% of the length of the distal conical portion of the frame. For some applications, the distal bearing housing extends until, or even at least partially into, cylindrical portion 38 of frame 34.
As noted above, distal bearing housing 118H houses a radial and/or thrust bearing, which is adjacent to the axial shaft and is configured to stabilize the axial shaft (radially and/or axially) while the axial shaft rotates. An advantage of a thrust bearing is that the impeller does not advance into the distal conical portion of the frame (or into a portion thereof) either during operation of the device or during delivery of the device to the left ventricle (when the impeller is in a radially constrained configuration within the frame), such that it may be easier to configure distal bearing housing 118H to extend proximally into the distal conical portion of frame 34. However, the scope of the present disclosure includes a distal bearing housing that extends into frame 34 in the manner described above, but which houses only distal radial bearing 118 and does not house a thrust bearing.
Likewise, the proximal bearing housing, which houses a radial and/or thrust bearing adjacent to the axial shaft and configured to stabilize the axial shaft (radially and/or axially) while the axial shaft rotates, may be disposed partly or entirely within the proximal conical portion of the frame. For example, at least 10%, 50%, or 80% of the length of the proximal bearing housing may be disposed within the frame. Alternatively or additionally, the proximal bearing housing may occupy at least 10% of the length of the proximal conical portion of the frame; for example, the proximal bearing housing may be disposed at least partly within the cylindrical portion of the frame. The scope of the present disclosure includes a proximal bearing housing that extends into frame 34 in the manner described above, but which houses only proximal radial bearing 116 and does not house a thrust bearing.
In some embodiments, both the proximal and distal bearing extend into the frame as described above. In such embodiments, the distance between the proximal end of the proximal bearing housing and the distal end of the distal bearing housing may be less than 10% greater than the length of the frame, thus reducing the total length of the more rigid elements of the blood pump.
Reference is now made to
Reference is now made to
Reference is now made to
For some applications, once the ventricular assist device has been deployed within the left ventricle, and the delivery catheter has been retracted to its intraprocedural position (e.g., such that its distal end is disposed within the descending aorta), it is desirable to secure delivery tube 142 and delivery catheter 143 in fixed positions with respect to each other. For some applications, a fixation unit such as fixation unit 97 (shown in
For other applications, locking unit 279, which is configured to couple to the proximal end of the delivery catheter and comprises a clip 280, is used instead of a fixation unit such as that shown in
As shown in
Typically, as shown in
Reference is now made to
In some embodiments, the clip is configured to remain in its open state, following a placement of the clip in its open state, unless the clip is returned to its closed state. In other words, the fixation mechanism can be disengaged by opening the clip, and the user does not then need to actively maintain disengagement of the fixation mechanism.
In other embodiments, the clip is configured to return to its closed state, following a placement of the clip in its open state, unless the clip is held in its open state. In other words, the user needs to actively apply force to the clip in order to maintain disengagement of the fixation mechanism. Clip 286 is an example of such a clip.
Reference is now made to
Typically, delivery catheter 143 is inserted from outside the subject's body into the patient's vasculature via introducer sheath 290, which is configured to extend from outside the body of the subject into the body of the subject. For example, the introducer sheath may be used to provide access to the subject's femoral artery, and the delivery catheter may be advanced from the femoral artery to the subject's left ventricle as described hereinabove.
For some applications, locking unit 287 is configured to couple to the proximal end of introducer sheath 290, and delivery catheter 143 is configured to pass through locking unit 287 and introducer sheath 290. Locking unit 287 comprises a clip 288, which is used to fix the position of the delivery catheter with respect to the introducer sheath (typically, once the delivery catheter has been positioned in a desired intraprocedural position). Clip 288 is configured such that it has only two states (or “positions”): a closed state, in which the clip grips the delivery catheter so as to inhibit movement of the delivery catheter relative to the introducer sheath, and an open state, in which the clip does not grip the delivery catheter. This differs from a fixation unit such as that shown in
Typically, locking unit 287 comprises at least one internal seal 289 configured to surround the delivery catheter and to inhibit backflow of blood of the subject, from the introducer sheath, through the second locking unit, while the delivery catheter passes through the second locking unit.
Typically, locking unit 287 further comprises a fluid port, and is shaped to define a channel 291 in fluid communication with the fluid port and introducer sheath 290. Thus, the space between the delivery catheter and the introducer sheath may be purged with a purging fluid.
In some embodiments, clip 288 is configured to remain in its open state, following a placement of the second clip in its open state, unless the clip is returned to its closed state. In other embodiments, the clip is configured to return to its closed state, following a placement of the clip in its open state, unless the clip is held in its open state.
Reference is now made to
In some embodiments, the proximal end of pump-outlet tube 24 is folded inwardly so as to define one or more surfaces 322 configured to direct the blood through blood-outlet openings 109 by virtue of being oblique with respect to the longitudinal axis 324 of the pump-outlet tube.
In some embodiments, surfaces 322 define a projection 325, such as a frustoconical projection, having a width that decreases moving distally. Blood is directed by projection 325, at an angle, through the blood-outlet openings. In such embodiments, typically, projection 325 is distally coupled to the delivery tube.
Reference is now made to
In some embodiments, an elongation-resistant fiber, e.g., an aramid fiber 292 (which may be equivalent to fiber 159 shown in
In some embodiments, as shown in the distal-end view 294 of the delivery tube, aramid fiber 292 is disposed within the wall of the delivery tube (e.g., as in
As described above, pump-outlet tube 24 is coupled to delivery tube 142. Thus, in addition to biasing the orientation of the blood pump, which is disposed at least partly within the pump-outlet tube, aramid fiber 292 biases the orientation of the pump-outlet tube.
Typically, as shown in
For example, the delivery tube may be configured to curve (even without aramid fiber 292), and the pump-outlet tube may curve by virtue of the delivery tube curving. Alternatively or additionally, the pump-outlet tube may be configured to curve by virtue of being pre-shaped. Alternatively or additionally, the pump-outlet tube may be shaped to define multiple openings (e.g., blood-inlet openings and/or blood-outlet openings) arranged in a non-axisymmetric arrangement, and the pump-outlet tube may curve by virtue of blood flowing through the openings. For some applications, the pump-outlet tube is configured to curve by virtue of one or more features described with reference to FIGS. 19A-F of US 2022/0226632 to Tuval, which is incorporated herein by reference. Alternatively or additionally, as described below with reference to
Due to the curvature of the pump-outlet tube, the orientation-biasing properties of the aramid may be particularly helpful. For example, the aramid fiber may bias the orientation of the delivery tube such that, while the delivery tube traverses the aortic arch (and the aramid fiber biases the roll angle of the delivery tube such that the aramid fiber is disposed at the inside of the curve of the aortic arch), the pump-outlet tube curves away from the posterior wall and/or septal wall 338 of the left ventricle. Alternatively or additionally, the aramid fiber may bias the orientation of the delivery tube such that, while the delivery tube traverses the aortic arch (and the aramid fiber biases the roll angle of the delivery tube such that the aramid fiber is disposed at the inside of the curve of the aortic arch), the pump-outlet tube curves toward apex 342 and/or free wall 334 of the left ventricle.
In some embodiments, the circumferential angle between the aramid fiber and the circumferential position on the pump-outlet tube at the inside of the curve of the pump-outlet tube is close to zero, e.g., between −10 and 10 degrees. In other words, the aramid fiber is positioned at or near the inside of the curve, such that the delivery tube curves in the same direction as the pump-outlet tube. This feature may further help orient the blood pump in the desired orientation.
As described hereinabove, for some applications, distal-tip portion is configured to curve within a plane. For example, within a given plane, the distal tip portion may have a curvature such as that described hereinabove with reference to
It is noted that aramid fiber 292 may be used to bias the orientation of delivery tube 142 regardless of the type of device coupled to the distal end of the delivery tube. In fact, the aramid fiber may be used even if no device at all is coupled to the distal end of the delivery tube. Moreover, the delivery tube may extend into any chamber of the heart. Furthermore, it is noted that although some embodiments have been described with reference to an aramid fiber, the scope of the present disclosure includes using other types of elongation-resistant fibers (e.g., polymeric and/or natural fibers) and/or elongation-resistant wires to provide the functionalities described hereinabove both with reference to fiber 159 (shown in
Reference is now made to
As noted above, frame 34 is disposed at least partly within the distal portion of pump-outlet tube 24 and is configured to hold the distal portion of the pump-outlet tube open. The impeller is disposed within frame 34 and is configured to pump blood of the subject, through the pump-outlet tube, from the left ventricle into the aorta, thereby maintaining the proximal portion of the pump-outlet tube, which is proximal to the frame and traverses the aortic valve, in an open state.
In some embodiments, the left-ventricular assist device comprises one or more (e.g., 1-8) bands 298, each of which is bonded to the outer wall of the proximal portion of the pump-outlet tube, without extending around the full circumference of the pump-outlet tube. For example, each of the bands may extend around 20-80% of the full circumference of the pump-outlet tube. Thus, while the proximal portion of the pump-outlet tube remains open by virtue of the blood flowing proximally through the tube, the proximal portion of the pump-outlet tube curves at respective locations of bands 298.
Advantageously, the curvature of the proximal portion of the pump-outlet tube helps orient the distal portion of the pump-outlet tube. For example, by virtue of the proximal portion of the pump-outlet tube curving at the locations of the bands, the distal portion of the pump-outlet tube may point toward apex 342 or toward free wall 334 (
In some embodiments, bands 298 are polymeric.
In some embodiments, as described above with reference to
In some embodiments, two or more bands 298 are spaced from one other, along the length of the pump-outlet tube, by 1-5 mm. In some embodiments, two or more bands 298 are displaced circumferentially from one another, e.g., by 20-120 degrees. Advantageously, this circumferential displacement may provide a twist to the pump-outlet tube upon blood being pumped through the pump-outlet tube, thus orienting the pump-outlet tube even more precisely. For some applications, the axial spacing between adjacent bands is non-uniform along the length of the pump-outlet tube, in such a manner that it causes different regions of the pump-outlet tube to assume respective degrees of curvature upon blood being pumped through the pump-outlet tube.
Reference is now made to
In some embodiments, as shown in
To assemble the left-ventricular assist device, impeller 50 (and frame 34) are passed through the proximal end of first section 24a, such that impeller 50 (and frame 34) are disposed within first section 24a. Next, as shown in
Following the assembly of the left-ventricular assist device, the pump-outlet tube may be inserted, through the aorta of the subject, into the left ventricle of the subject's heart such that the pump-outlet tube traverses the aortic valve of the subject with blood-outlet openings 109 being disposed within the aorta. While the pump-outlet tube is positioned in this manner, the impeller may pump blood of the subject, through blood-outlet openings 109, from the left ventricle into the aorta.
In some embodiments, the blood-outlet openings occupy 20-80% of the circumference of the pump-outlet tube. Advantageously, although overlap 312 between the tabs adds to the minimum diameter to which this region of the pump-outlet tube can be radially constrained, within this region the blood-outlet openings occupy much of the circumference of the pump-outlet tube. Thus, overall this region does not increase the minimum diameter to which the pump-outlet tube can be radially constrained. More generally, typically, overlap 312 between the tabs provides the pump-outlet tube with the right balance between strength and crimpability.
As noted above, the pump-outlet tube may be configured to curve proximally to the impeller, e.g., by virtue of being pre-shaped, by virtue of blood-outlet openings 109 being arranged in a non-axisymmetric arrangement, by virtue of blood-inlet openings 108 being arranged in a non-axisymmetric arrangement, and/or by virtue of bands 298 (
Reference is now made to
Pump-outlet tube 24 may be configured in various ways so as to provide various directions of blood flow from the pump-outlet tube into the aorta.
In
In
In some embodiments, each of the blood-outlet openings spans the interface between narrower section 24c and wider section 24d. In other embodiments, each of the blood-outlet openings is positioned entirely within the wider section.
In some embodiments, as shown in
In some embodiments, wider section 24d is folded inwardly so as to define one or more surfaces 322 configured to direct the blood through blood-outlet openings 109, as described above with reference to
With regards to all aspects of ventricular assist device 20 described with reference to
The scope of the present invention includes combining any of the apparatus and methods described herein with any of the apparatus and methods described in one or more of the following applications, all of which are incorporated herein by reference:
It will be appreciated by persons skilled in the art that the present invention is not limited to what has been particularly shown and described hereinabove. Rather, the scope of the present invention includes both combinations and subcombinations of the various features described hereinabove, as well as variations and modifications thereof that are not in the prior art, which would occur to persons skilled in the art upon reading the foregoing description.
The present application is a continuation of International Application PCT/IB2023/059138 to Tuval (published as WO 24/057254), entitled “Coupling between shaft and drive cable,” filed Sep. 14, 2023, which claims priority from: U.S. Provisional Patent Application 63/406,427 to Tuval, entitled “Ventricular assist device,” filed Sep. 14, 2022;U.S. Provisional Patent Application 63/432,496 to Tuval, entitled “Ventricular assist device,” filed Dec. 14, 2022;U.S. Provisional Patent Application 63/443,519 to Tuval, entitled “Ventricular assist device,” filed Feb. 6, 2023; andU.S. Provisional Patent Application 63/470,259 to Tuval, entitled “Ventricular assist device,” filed Jun. 1, 2023. All of the above-referenced US Provisional applications are incorporated herein by reference.
| Number | Date | Country | |
|---|---|---|---|
| 63406427 | Sep 2022 | US | |
| 63432496 | Dec 2022 | US | |
| 63443519 | Feb 2023 | US | |
| 63470259 | Jun 2023 | US |
| Number | Date | Country | |
|---|---|---|---|
| Parent | PCT/IB2023/059138 | Sep 2023 | WO |
| Child | 18637655 | US |
