Adapter assembly for surgical device

Information

  • Patent Grant
  • 10617411
  • Patent Number
    10,617,411
  • Date Filed
    Thursday, November 17, 2016
    8 years ago
  • Date Issued
    Tuesday, April 14, 2020
    4 years ago
Abstract
An adapter assembly for connecting an end effector to a surgical instrument includes first, second, and third drive assemblies configured for converting rotational motion into linear motion. Each of the second and third drive assemblies includes a cam assembly for longitudinally advancing and retracting respective second and third drive members.
Description
BACKGROUND

1. Technical Field


The present disclosure relates generally to powered surgical devices. More specifically, the present disclosure relates to adapter assemblies for selectively connecting end effectors to actuation units of powered surgical devices.


2. Background of Related Art


Powered devices for use in surgical procedures typically convert rotational motion from a handle assembly to linear motion for effectuating one or more functions, e.g., clamping, stapling, cutting. To permit reuse of the handle assemblies of these powered surgical devices and so that the handle assembly may be used with a variety of end effectors, adapter assemblies have been developed for selective attachment to the handle assemblies and to a variety of end effectors. Following use, the adapter assembly may be disposed of along with the end effector. In some instances, the adapter assembly may be sterilized for reuse.


SUMMARY

An adapter assembly for operably connecting an end effector to a powered surgical instrument is provided. The adapter assembly includes a drive coupling assembly, a first drive assembly operably connected to the drive coupling assembly, a second drive assembly operably connected to the drive coupling assembly, and a third drive assembly operably connected to the drive coupling assembly. The first drive assembly includes a drive screw, the second drive assembly includes a first cam assembly, and, the third drive assembly includes a second cam assembly.


In embodiments, the second drive assembly may include a second drive member operably connected to the first cam assembly. The first cam assembly may be rotatable from a first orientation to a second to move the second drive member from a proximal position to a distal orientation. The third drive assembly may include a third drive member operably connected to the second cam assembly. The second cam assembly may be movable from a first orientation to a second orientation to move the third drive member from a proximal position to a distal position.


Each of the second and third drive members may include a tubular portion. The tubular portion of the third drive member may be slidably disposed within the tubular portion of the second drive member. Each of the second and third drive assemblies may include a guide member. Each of the second and third drive members may include a guide portion slidably disposed within the respective guide members. The first drive member may be slidably disposed within the tubular portion of the second drive member.


In embodiments, the drive coupling assembly may include a thruster plate and first, second, and third connector members. The first connector member may be operably connected to the drive screw. The second connector member may be operably connected to the first cam assembly. The third connector member may be operably connected to the second cam assembly.


The first cam assembly may include a drive shaft, a worm drive operably disposed on the drive shaft, a cam member, and a worm gear operably disposed on the cam member. The first cam assembly may include a cam member having an eccentric outer surface. The second drive member may include an engagement portion for engaging the eccentric outer surface. The eccentric outer surface of the cam member may include a first point a first distance from a central axis of the cam member and a second point a second distance from the central axis. The second distance may be greater than the first distance. A difference between the second distance and the first distance may be a distance of travel of the second drive member. Movement of the first drive member may perform a first function, movement of the second drive member may perform a second function, and movement of the third member may perform a third function.


In one embodiment, the adapter assembly includes a rotation assembly having a base and a rotation handle rotatably secured to the base. The adapter assembly may also include a sleeve fixedly secured to the rotation handle. The first, second, and third drive assemblies of the adapter assembly may be secured within the base.





BRIEF DESCRIPTION OF THE DRAWINGS

Embodiments of the present disclosure are described herein with reference to the accompanying drawings, wherein:



FIG. 1 is a perspective view of an adapter assembly, in accordance with an embodiment of the present disclosure, an exemplary electromechanical handle assembly, an exemplary extension assembly, and an exemplary end effector;



FIG. 2 is a perspective view of the adapter assembly of FIG. 1;



FIG. 3 is a perspective view of a drive mechanism of the adapter assembly of FIG. 1;



FIG. 4 is a perspective, separated view of the drive mechanism of FIG. 3;



FIG. 5 is a perspective side view of a first cam member of a second drive assembly of the drive mechanism of FIG. 3;



FIG. 6 is a perspective, side view of a second cam member of a third drive assembly of the drive mechanism of FIG. 3;



FIG. 7 is a perspective top view of a proximal end of the drive mechanism of FIG. 3, with each of the first, second, and third drive assemblies in their respective first positions;



FIG. 8 is side view of the drive mechanism of FIG. 3, with each of the first, second, and third drive assemblies in their first positions;



FIG. 9 is a cross-sectional top view of the drive assembly of FIG. 3 taken along section line 9-9 of FIG. 8 with each of the first, second, and third drive assemblies in their first positions;



FIG. 10 is a cross-sectional top view of the drive assembly of FIG. 3 taken along section line 9-9 of FIG. 8 with the first drive assembly in a second position, and each of the second and third drive assemblies in their first positions;



FIG. 11 is the perspective cross-sectional side view of the drive assembly of FIG. 3 taken along section line 11-11 in FIG. 10;



FIG. 12 is the perspective cross-sectional side view of the drive assembly of FIG. 3 taken along section line 12-12 in FIG. 10;



FIG. 13 is the perspective cross-sectional side view taken along section line 11-11 in FIG. 10, with the first and third drive assemblies in a second position and the second drive assembly in the first position; and



FIG. 14 is the perspective cross-sectional side view taken along section line 12-12 in FIG. 10, with the first, second, and third drive assemblies in their second position.





DETAILED DESCRIPTION OF EMBODIMENTS

Embodiments of the presently disclosed adapter assembly for surgical devices and/or handle assemblies are described in detail with reference to the drawings, in which like reference numerals designate identical or corresponding elements in each of the several views. As used herein the term “distal” refers to that portion of the adapter assembly or surgical device, or component thereof, farther from the user, while the term “proximal” refers to that portion of the adapter assembly or surgical device, or component thereof, closer to the user.


With reference to FIGS. 1 and 2, an adapter assembly in accordance with an embodiment of the present disclosure, shown generally as adapter assembly 100, is configured for selective connection to a powered handheld electromechanical instrument shown, generally as surgical device 10. As illustrated in FIG. 1, the surgical device 10 is configured for selective connection with the adapter assembly 100, and, in turn, the adapter assembly 100 is configured for selective connection with an extension assembly 20. The extension assembly 20 is configured for selective connection with a tool assembly or end effector, e.g. tool assembly 30, which may, in exemplary embodiments, include a loading unit 40 and an anvil assembly 50, for applying a circular array of staples (not shown) to tissue (not shown).


For a detailed description of the structure and function of an exemplary electromechanical instrument, please refer to commonly owned U.S. Pat. Appl. Publ. No. 2012/0253329, the content of which is incorporated by reference herein in its entirety.


With continued reference to FIG. 2, the adapter assembly 100 includes a proximal portion 102 and a distal portion 104. The proximal portion 102 includes a rotation assembly 106 having a base 108, and a rotation handle 110 rotatable relative to the base 108 about a longitudinal axis “x” of the adapter assembly 100. The distal portion 104 includes a sleeve 112 fixedly secured to the rotation handle 110. Rotation of the rotation handle 110 causes rotation of the sleeve 112. In this manner, an end effector, e.g. tool assembly 30 (FIG. 1), secured to the distal portion 104 of the adapter assembly 100, or an end effector secured to an extension assembly, e.g., extension assembly 20 (FIG. 1), which is secured to the distal portion 104 of the adapter assembly 100 is rotatable about the longitudinal axis “x” independent of movement of the surgical device 10 (FIG. 1) to which adapter assembly 100 is attached.


Still referring to FIG. 2, a latch 114 is mounted to the rotation handle 110 and selectively secures the rotation handle 110 in a fixed orientation about the longitudinal axis “x”. The latch 114 is configured to lock the rotation handle 110 relative to the base 108. Proximal movement of the latch 114 disengages the latch 114 from the base 108 to permit rotation of the rotation handle 110 relative to the base 108. For a detailed description of an exemplary rotation assembly and latch mechanism, please refer to commonly owned U.S. Provisional Patent Application Ser. No. 62/066,518, filed Oct. 21, 2014, the content of which is incorporated by reference herein in its entirety.


With additional reference to FIG. 3, the adapter assembly 100 includes a drive mechanism 115 (FIG. 3) for effecting actuation of an end effector, e.g., tool assembly 30 (FIG. 1), secured to the distal portion 104 of the adapter assembly 100 and/or an end effector, e.g., tool assembly 30, secured to an extension assembly, e.g., the extension assembly 20 (FIG. 1), which is secured to the distal portion 104 of the adapter assembly 100. The drive mechanism 115 is configured to transfer rotational motion from the surgical device 10 (FIG. 1) to linear motion to effect actuation of an end effector. More specifically, the drive mechanism 115 includes a drive coupling assembly 120 (FIG. 3), and first, second, and third drive assemblies 130, 140, 160 operably connected to the drive coupling assembly 120 for transferring rotation movement of respective first, second, and third drive shafts (not shown) of the surgical device 10 (FIG. 1) to respective first, second, and third linear movement for effecting first, second, and third actuations of an attached end effector, e.g. tool assembly 30 (FIG. 1), for performing respective first, second, and third operations of the tool assembly 30, e.g., clamping, stapling, and cutting.


With particular reference to FIGS. 3 and 4, the drive coupling assembly 120 is operably supported within the base 108 (FIG. 2) of the rotation assembly 106 (FIG. 2) and includes a thruster plate 122, and first, second, and third connector members 124, 126, 128 rotatably supported through the thruster plate 122. Proximal ends 124a, 126a, 128a of the respective first, second, and third connector members 124, 126, 128 are configured for operable connection with the respective first, second, and third drive shafts (not shown) of a surgical device, e.g., the surgical device 10 (FIG. 1). A flange 122a (FIG. 4) extends distally from the thruster plate 122 and includes first and second pivot members 123a, 123b (FIG. 4).


The first drive assembly 130 includes a drive screw 132 integrally formed with or fixedly coupled to the first connector member 124 of the drive coupling assembly 120 and extending distally therefrom, and a first drive member 134 longitudinally movable relative to the drive screw 132. Specifically, a proximal end 134a of the first drive member 134 defines a threaded longitudinal opening 135 (FIG. 10) through which the drive screw 132 is received. Rotation of the drive screw 132 in a first direction causes the first drive member 134 to move proximally, i.e., retract, and rotation of the drive screw 132 in a second direction causes the first drive member 134 to move in a distal direction, i.e., advance. As will be described in further detail below, a distal end 134b of the first drive member 134 is operably connectable to a drive member (not shown) of an anvil assembly, e.g., the anvil assembly 50 (FIG. 1), of an end effector, e.g., tool assembly 30 (FIG. 1), to perform a first function, e.g., clamping of tissue.


Still referring to FIGS. 3 and 4, the second drive assembly 140 (FIG. 3) includes a second drive member 142, and a first cam assembly 150 operably disposed between the second connector member 126 of the drive coupling assembly 120 and the second drive member 142. The second drive member 142 includes a tubular portion 144 and a guide portion 146 secured to the tubular portion 144. An engagement portion 146a extends proximally from the guide portion 146 and engages a cam member 158 of a first cam assembly 150. The guide portion 146 of the second drive member 142 may be slidably disposed within a first guide member (not shown), or within a first groove (not shown) of the sleeve 112 (FIG. 2), to maintain the second drive member 142 in axial alignment with the longitudinal axis “x” (FIG. 2) of the adapter assembly 100 (FIG. 2) as operation of the first cam assembly 150 longitudinally translates the second drive member 142 within the sleeve 112. The tubular portion 144 of the second drive member 142 defines a longitudinal opening 141 through which the first drive member 134 of the first drive assembly 130 is received. The second drive member 142 is biased in a proximal direction by a spring 145 (FIG. 4) or other biasing means.


With particular reference to FIG. 4, the first cam assembly 150 includes a drive shaft 152 integrally formed with or fixedly coupled to the second connector member 126 of the drive coupling assembly 120, a worm drive 154 disposed adjacent a distal end 152b of the drive shaft 152, and a cam member 158 rotatably supported relative to the drive shaft 152 on the first pivot member 123a extending from the flange 122a of the thruster plate 122. The cam member 158 includes a worm gear 160 integrally formed with or fixedly coupled thereto. The cam member 158 and the drive shaft 152 are positioned such that teeth 160a of the worm gear 160 operably engage a thread 154a of the worm drive 154. Rotation of the drive shaft 152 in a first direction causes rotation of the cam member 158 in a counter-clockwise direction and rotation of the drive shaft 152 in a second direction causes rotation of the cam member 158 in a clockwise direction.


With particular reference to FIG. 5, the cam member 158 of the first cam assembly 150 (FIG. 3) defines a central axis “C1” and includes an eccentric outer surface 158a. More particularly, a first point “A1” on the eccentric outer surface 158a of the cam member 158 is a first distance “M1” from the central axis “C1” of the cam member 158 and a second point “B1” on the eccentric outer surface 158a of the cam member 158 is a second distance “N1” from the central axis “C1”. The second distance “N1” is greater than the first distance “M1”. As shown in FIG. 5, when viewed in a clockwise direction, the distance between the eccentric outer surface 158a of the cam member 158 and the central axis “C1” of the cam member 158 gradually increases from the first point “A1” to the second point “B1”.


As will become apparent, the difference between the first distance “M1” and the second distance “N1” is the distance in which the second drive member 142 is moved during actuation of the first cam assembly 150. This distance coincides with a distance required to move, for example, a cutting assembly (not shown) of the loading unit 40 (FIG. 1) to cause the cutting of tissue. The eccentric outer surface 158a of the cam member 158 defines a transition zone 159 between the first point “A1” and the second point “B1” in the counter-clockwise direction.


As will be described in further detail below, the second drive member 142 is in a proximal-most position when the engagement portion 146a of the second drive member 142 engages the eccentric outer surface 158a of the cam member 158 within the transition zone 159. As the cam member 158 rotates in a counter-clockwise direction, as indicated by arrow “D” in FIG. 7, the second drive member 142 moves from the proximal-most position (FIG. 7) when in the transition zone 159, to a distal-most position (FIG. 8) to effect a second function, i.e., cutting of tissue.


With continued reference to FIGS. 3 and 4, the third drive assembly 160 includes a third drive member 162, and a second cam assembly 170 operably disposed between the third connector member 128 of the drive coupling assembly 120 and the third drive member 162. The third drive member 162 includes a tubular portion 164 and a guide portion 166 secured to the tubular portion 164. An engagement portion 166a extends proximally from the guide portion 166 and engages a cam member 178 of the second cam assembly 170. The guide portion 166 of the third drive member 162 may be slidably disposed within a second guide member (not shown), or within a second groove (not shown) of the sleeve 112 (FIG. 2), to maintain the third drive member 162 in axial alignment with the longitudinal axis “x” (FIG. 2) of the adapter assembly 100 (FIG. 2) as operation of the second cam assembly 170 longitudinally translates the second drive member 162 within the sleeve 112. The tubular portion 164 of the third drive member 162 defines a longitudinal opening 161 through which the first and second drive members 134, 142 of the respective first and second drive assemblies 130, 140 are received and a longitudinal slot 163 through with the guide portion 146 of the second drive member 142 is received. The third drive member 162 is biased in a proximal direction by a spring 165 or other biasing means.


The second cam assembly 170 includes a drive shaft 172 integrally formed with or fixedly coupled to the third connector member 128 of the drive coupling assembly 120, a worm drive 174 disposed adjacent a distal end 172b of the drive shaft 172, a bearing assembly 176 rotatably supporting the distal end 172b of the drive shaft 172, and a cam member 178 rotatably supported relative to the drive shaft 172 on the second pivot member 123b (FIG. 4) extending from the flange 122a of the thruster plate 122. The cam member 178 includes a worm gear 180 integrally formed with or fixedly coupled thereto. The cam member 178 and the drive shaft 172 are positioned such that teeth 180a (FIG. 6) of the worm gear 180 operably engage a thread 174a of the worm drive 174. Rotation of the drive shaft 172 in a first direction causes rotation of the cam member 178 in a counter-clockwise direction and rotation of the drive shaft 172 in a second direction causes rotation of the cam member 178 in a clockwise direction.


With particular reference to FIG. 6, the cam member 178 of the second cam assembly 170 defines a central axis “C2” and includes an eccentric outer surface 178a. More particularly, a first point “A2” on the eccentric outer surface 178a of the cam member 178 is a first distance “M2” from the central axis “C2” of the cam member 178 and a second point “B2” on the eccentric outer surface 178a is a second distance “N2” from the central axis “C2”. The second distance “N2” is greater than the first distance “M2”. When viewed in a counter-clockwise direction, the distance between the eccentric outer surface 178a of the cam member 178 and the central axis “C2” of the cam member 178 gradually increases from the first point “A2” to the second point “B2”. The difference between the first distance “M2” and the second distance “N2” is the distance required to, for example, move a stapling assembly (not shown) of the loading unit 40 (FIG. 1) to cause the stapling of tissue. The eccentric outer surface 178a of the cam member 178 defines a transition zone 179 between the first point “A2” and the second point “B2” in the counter-clockwise direction.


Although shown as having different configurations, it is envisioned that the first and second cam members 158, 178 of the respective first and second cam assemblies 150, 170 may be the same size and/or configuration. It is further envisioned that each of the first and second cam assemblies 150, 170 may be modified to adjust the rate at which the respective second and third drive members 142, 162 move relative to each other. For example, the thread 154a of the worm drive 154 of the first cam assembly 150 may include a different pitch than the thread 174a of the worm drive 174 of the second cam assembly 170 and/or the number of teeth 160a of the worm gear 160 of the first cam assembly 150 may be different than the number of teeth 180a of the worm gear 180 of the second cam assembly 170 such that the first and second cams 158, 178 rotate at different rates.


With continued reference to FIG. 4, the drive mechanism 115 further includes a seal assembly 190 disposed on a distal end of the second drive member 142 of the second drive assembly 140. The seal assembly 190 includes a seal member 192, and a seal housing 194 for supporting the seal member 192. A pair of fasteners, e.g., screws 196a, 196b, secure the seal assembly 190 to the second drive member 142 of the second drive assembly 140.


The operation of the drive mechanism 115 will now be described with reference to the figures. Referring initially to FIGS. 7-9, the drive mechanism 115 is shown with the first, second, and third drive assemblies 130, 140, 170 in first or initial positions. In the first positions, the first drive member 134 of the first drive assembly 130 is in a distal-most or fully-extended position, and each of the second and third drive members 142, 162 are in a proximal-most or fully-retracted position. When, for example, the anvil assembly 50 (FIG. 1) of the tool assembly 30 (FIG. 1) is operably secured to the first drive member 134, in the first position, the anvil assembly 50 is spaced from the loading unit 40 (FIG. 1), as shown in FIG. 1.


Although shown and described with the first drive member 134 of the first drive assembly 130 in a distal-most position when the first drive assembly 130 is in the first position, it is envisioned that the operation of an end effector (not shown) secured to the adapter assembly 100 (FIG. 1) may require the first drive member 134 of the first drive assembly 130 to be in a proximal-most or fully-retracted position, or at a location somewhere between the distal-most and proximal-most positions, when the first drive assembly 130 is in the first position. Similarly, although shown and described with the second and third drive members 142, 162 of the respective second and third drive assemblies 140, 160 in a proximal-most position when the second and third drive assemblies 140, 160 are in the first position, it is envisioned that the operation of an end effector secured to the adapter assembly 100 (FIG. 1) may require either or both of the second and third drive members 142, 162 of the respective second and third drive assemblies 140, 160 to be in a distal-most position, or at a location somewhere between the proximal-most and distal-most positions, when the second and/or third drive assemblies 140, 160 are in the first position.


With reference still to FIGS. 11 and 12, when the second and third drive assemblies 140, 160 are in the retracted position, the cam members 158, 178 of the respective first and second cam assemblies 150, 170 are oriented such that the engagement portions 146a, 166a of the respective second and third drive members 142, 162 engage the cam members 158, 178, respectively, along the respective transition zones 159, 179. When the engagement portions 146a, 166a of the respective second and third drive members 142, 162 of the respective second and third drive assemblies 140, 160 engage the respective transition zones 159, 179 of the respective cam members 158, 178, the second and third drive members 142, 162 are in their proximal-most position.


Turning now to FIG. 10, movement of the first drive member 134 of the first drive assembly 130 from the first position to a second position is effected by operation of the surgical device 10 (FIG. 1). Specifically, rotation of a first drive shaft (not shown) of the surgical device 10 (FIG. 1) causes rotation of the first connector member 124 of the drive coupling assembly 120, as indicated by arrow “A” in FIG. 10. As the first connector member 124 rotates in a first direction, the drive screw 132 integrally formed with the first connector member 124 rotates in the same first direction within the threaded passage 135 of the first drive member 134. Rotation of the drive screw 132 within the thread passage 135 of the first drive member 134 causes the first drive member 134 to move proximally, i.e., retract, as indicated by arrow “B”. Conversely, when the first connector member 124 is rotated in a second direction, the drive screw 132 rotates in the second direction to cause the first drive member 134 to move distally, i.e., advance.


Proximal movement of the first drive member 134 effectuates a first function of an end effector operably secured the adapter assembly 100 (FIG. 1). If, for example, the tool assembly 30 (FIG. 1) is operably secured to the adapter assembly 100 and the anvil assembly 50 (FIG. 1) is operably secured to the distal end 134b of the first drive member 134, proximal movement of the first drive member 134 effectuates clamping of tissue between the anvil assembly 50 and the loading unit 40 (FIG. 1).


Turing now to FIG. 13, movement of the third drive assembly 160 from the first position to a second, advanced position is effected by operation of the surgical device 10 (FIG. 1). Specifically, rotation of a third drive shaft (not shown) of the surgical device 10 (FIG. 1) causes rotation of the third connector member 128 (FIG. 4) of the drive coupling assembly 120 (FIG. 3). As the third connector member 128 rotates in a first direction, the threads 174a (FIG. 4) of the worm drive 174 (FIG. 4) engage the teeth 180a (FIG. 6) of the worm gear 180 (FIG. 6) causing the cam member 178 to rotate in a clockwise direction, as indicated by arrow “C” in FIG. 13. As the cam member 178 rotates, the engagement portion 166a of the third drive member 162 engages the eccentric surface 178a of the cam member 178 causing the third drive member 162 of the third drive assembly 160 to move distally, i.e., advance, as indicated by arrows “D” in FIG. 13.


Conversely, when the third connector member 128 is rotated in a second direction, the drive shaft 172 rotates in the second direction to cause the cam member 178 to turn in a counter-clockwise direction causing the third drive member 174 to move proximally, i.e., retract. As noted above, in embodiments, a guide member (not shown) or a groove (not shown) within the sleeve 112 (FIG. 1) maintains the third drive member 162 in axial alignment with the longitudinal axis “x” (FIG. 2) of the adapter assembly 100 (FIG. 2) during translation of the third drive member 162.


Distal movement of the third drive member 162 effectuates a second function of an end effector operably secured to the adapter assembly 100 (FIG. 2). If, for example, the tool assembly 30 (FIG. 1) is operably secured to the adapter assembly 100 with the loading unit 40 (FIG. 1) is operably secured to the third drive member 162, distal movement of the third drive member 162 advances a pusher assembly (not shown) to effectuate the stapling of tissue. The third drive member 162 is at a distal-most position when the engagement portion 166a engages point “B2” (FIG. 6) of the eccentric surface 178a of the cam member 178.


Continued rotation of the cam member 178 in the clockwise direction causes the engagement portion 166a of the third drive member 162 to engage the transition portion 179 of the cam member 178. When the engagement portion 166a of the third drive member 162 engages the transition portion 179 of the cam member 178, the spring 165 (FIG. 4) biases the third drive member 162 to the proximal-most position to reset the third drive member 162. Alternatively, the third drive member 162 is reset to the proximal-most position by rotating the cam member 178 in the counter-clockwise direction. It will be recognized that any of the drive members can also be reset by being captured in a cam groove rather than being pressed against the cam surface by a spring.


Turing now to FIG. 14, movement of the second drive assembly 140 from the first position (FIG. 8) to a second, advanced position is effected by operation of the surgical device 10 (FIG. 1). Specifically, rotation of the second shaft (not shown) of the surgical device 10 (FIG. 1) causes rotation of the second connector member 126 of the drive coupling assembly 120. The threads 154a (FIG. 4) of the worm drive 154 (FIG. 4) engage the teeth 160a (FIG. 5) of the worm gear 160 (FIG. 6) causing the cam member 158 to rotate in a counter-clockwise direction, as indicated by arrow “E” in FIG. 14. As the cam member 158 rotates, the engagement portion 146a of the second drive member 142 engages the eccentric surface 158a of the cam member 158 causing the second drive member 142 of the second drive assembly 140 to move distally, i.e., advance, as indicated by arrow “F” in FIG. 14.


Conversely, when the second connector member 126 is rotated in a second direction, the drive shaft 152 rotates in the second direction to cause the cam member 158 to turn in a clockwise direction causing the second drive member 154 to move proximally, i.e., retract. As noted above, in embodiments, a guide member (not shown) or a groove (not shown) within the sleeve 112 (FIG. 1) maintains the second drive member 142 in axial alignment with the longitudinal axis “x” (FIG. 2) of the adapter assembly 100 (FIG. 2) during translation of the second drive member 142.


Distal movement of the second drive member 142 effectuates a third function. If, for example, the tool assembly 30 (FIG. 1) is operably secured to the adapter assembly 100 (FIG. 2) and the loading unit 40 (FIG. 1) is operably secured to the second drive member 142, distal movement of the second drive member 142 advances a knife assembly (not shown) to effectuate the cutting of tissue. The second drive member 142 of the second drive assembly 140 is at a distal-most position when the engagement portion 146a engages point “B1” of the eccentric surface 158a of the cam member 158.


Continued rotation of the cam member 158 in the counter-clockwise direction causes the engagement portion 146a of the second drive member 142 to engage the transition portion 159 of the cam member 158. When the engagement portion 146a of the second drive member 142 engages the transition portion 159 of the cam member 158, the spring 145 (FIG. 4) biases the second drive member 142 to the proximal-most position to reset the second drive member 142. Alternatively, the second drive member 142 is reset to the proximal-most position by rotating the cam member 158 in the clockwise direction.


Although the drive mechanism 115 (FIG. 3) of the adapter assembly 100 (FIG. 1) has been shown and described as relates to operation of the tool assembly 30 (FIG. 1) including the loading unit 40 (FIG. 1) and the anvil assembly 50 (FIG. 1), the drive mechanism 115 may be modified for operation with end effectors having different configurations. For example, the drive mechanism 115 may be modified for use with an end effector having only a single actuation, e.g., linear stapling.


Any of the components described herein may be fabricated from either metals, plastics, resins, composites or the like taking into consideration strength, durability, wearability, weight, resistance to corrosion, ease of manufacturing, cost of manufacturing, and the like.


Persons skilled in the art will understand that the devices and methods specifically described herein and illustrated in the accompanying drawings are non-limiting exemplary embodiments. It is envisioned that the elements and features illustrated or described in connection with one exemplary embodiment may be combined with the elements and features of another without departing from the scope of the present disclosure. As well, one skilled in the art will appreciate further features and advantages of the disclosure based on the above-described embodiments. Accordingly, the disclosure is not to be limited by what has been particularly shown and described, except as indicated by the appended claims.

Claims
  • 1. An adapter assembly for operably connecting an end effector to a surgical instrument, the adapter assembly comprising: a drive coupling assembly;a first drive assembly operably connected to the drive coupling assembly, the first drive assembly including a drive screw;a second drive assembly operably connected to the drive coupling assembly, the second drive assembly including a first cam assembly and a second drive member, the first cam assembly including a first eccentric cam member in operable engagement with the second drive member; anda third drive assembly operably connected to the drive coupling assembly, the third drive assembly including a second cam assembly and a third drive member, wherein at least one of the first or second drive assemblies operates independently from the third drive assembly and the drive screw, the second drive member, and the third drive member are coaxial.
  • 2. The adapter assembly of claim 1, wherein the second drive member is operably connected to the first cam assembly, the first cam assembly being movable from a first orientation to a second orientation to move the second drive member from a proximal position to a distal position.
  • 3. The adapter assembly of claim 2, wherein the third drive member is operably connected to the second cam assembly, the second cam assembly being movable from a first orientation to a second orientation to move the third drive member from a proximal position to a distal position.
  • 4. The adapter assembly of claim 3, wherein each of the second and third drive members includes a tubular portion, the tubular portion of the third drive member being slidably disposed within the tubular portion of the second drive member.
  • 5. The adapter assembly of claim 4, wherein the first drive assembly further includes a first drive member in operable engagement with the drive screw, the first drive member being slidably disposed within the tubular portion of the second drive member.
  • 6. The adapter assembly of claim 1, wherein the drive coupling assembly includes a thruster plate and first, second, and third connector members.
  • 7. The adapter assembly of claim 6, wherein the first connector member is operably connected to the drive screw, the second connector member is operably connected to the first cam assembly, and the third connector member is operably connected to the second cam assembly.
  • 8. The adapter assembly of claim 1, wherein the first cam assembly further includes a first drive shaft, a first worm drive operably disposed on the first drive shaft, and a first worm gear operably disposed on the first eccentric cam member.
  • 9. The adapter assembly of claim 2, wherein the first eccentric cam member includes an eccentric outer surface and the second drive member includes an engagement portion for engaging the eccentric outer surface of the first eccentric cam member.
  • 10. The adapter assembly of claim 9, wherein the eccentric outer surface of the first eccentric cam member includes a first point a first distance from a central axis of the cam member and a second point a second distance from the central axis, the second distance being greater than the first distance.
  • 11. The adapter assembly of claim 10, wherein a difference between the second distance and the first distance is a distance of travel of the second drive member.
  • 12. The adapter assembly of claim 5, wherein movement of the first drive member performs a first function, movement of the second drive member performs a second function, and movement of the third member performs a third function.
  • 13. The adapter assembly of claim 1, further including a rotation assembly including a base and a rotation handle rotatably secured to the base.
  • 14. The adapter assembly of claim 13, further including a sleeve fixedly secured to the rotation handle.
  • 15. The adapter assembly of claim 14, wherein the first, second, and third drive assemblies are secured within the base.
  • 16. An adapter assembly for operably connecting an end effector to a surgical instrument, the adapter assembly comprising: a drive coupling assembly;a drive screw operably connected to the drive coupling assembly;a first drive assembly operably connected to the drive coupling assembly, the first drive assembly including a first cam assembly and a first drive member operably connected to the first cam assembly; anda second drive assembly operably connected to the drive coupling assembly, the second drive assembly including a second cam assembly and a second drive member operably connected to the second cam assembly, wherein each of the first and second drive members includes a tubular portion, the tubular portion of the second drive member being slidably disposed within and coaxial with the tubular portion of the first drive member, wherein the first drive assembly, the second drive assembly, and the drive screw operate independently from one another.
  • 17. The adapter assembly of claim 1, wherein each of the first, second, and third drive assemblies operate independently from one another.
  • 18. The adapter assembly of claim 9, wherein the second cam assembly includes a second drive shaft, a second worm drive operably disposed on the second drive shaft, a second eccentric cam member, and a second worm gear operably disposed on the second eccentric cam member.
  • 19. The adapter assembly of claim 18, wherein the second eccentric cam member includes an eccentric outer surface, and the third drive member includes an engagement portion for engaging the eccentric outer surface of the second eccentric cam member.
  • 20. The adapter assembly of claim 16, wherein the first cam assembly includes a first eccentric cam member.
  • 21. The adapter assembly of claim 20, wherein the second cam assembly includes a second eccentric cam assembly.
CROSS-REFERENCE TO RELATED APPLICATIONS

This application claims the benefit of and priority to U.S. Provisional Patent Application No. 62/261,469, filed Dec. 1, 2015, the entire disclosure of which is incorporated by reference herein.

US Referenced Citations (483)
Number Name Date Kind
2224905 Franz Dec 1940 A
2586870 Shapiro Feb 1952 A
2777340 Hettwer et al. Jan 1957 A
2957353 Babacz Oct 1960 A
3070695 Lemmermann Dec 1962 A
3111328 Di Rito et al. Nov 1963 A
3242996 Wright Mar 1966 A
3688612 Hiroshi Sep 1972 A
3695058 Keith, Jr. Oct 1972 A
3734515 Dudek May 1973 A
3759336 Marcovitz et al. Sep 1973 A
3798983 Smith Mar 1974 A
3816218 Felten Jun 1974 A
3996697 Bailey Dec 1976 A
4080844 Killian Mar 1978 A
4162399 Hudson Jul 1979 A
4189950 Killian Feb 1980 A
4306671 Fisher Dec 1981 A
4606343 Conta et al. Aug 1986 A
4705038 Sjostrom et al. Nov 1987 A
4722685 de Estrada et al. Feb 1988 A
4823807 Russell et al. Apr 1989 A
4874181 Hsu Oct 1989 A
4876794 Myers Oct 1989 A
5054393 MacPhee Oct 1991 A
5054836 Schulz Oct 1991 A
5104005 Schneider, Jr. Apr 1992 A
5129118 Walmesley Jul 1992 A
5129570 Schulze et al. Jul 1992 A
5152744 Krause et al. Oct 1992 A
5281220 Blake, III Jan 1994 A
5301061 Nakada et al. Apr 1994 A
5312023 Green et al. May 1994 A
5326013 Green et al. Jul 1994 A
5350355 Sklar Sep 1994 A
5383874 Jackson et al. Jan 1995 A
5383880 Hooven Jan 1995 A
5389098 Tsuruta et al. Feb 1995 A
5395033 Byrne et al. Mar 1995 A
5400267 Denen et al. Mar 1995 A
5411508 Bessler et al. May 1995 A
5413267 Solyntjes et al. May 1995 A
5427087 Ito et al. Jun 1995 A
5433721 Hooven et al. Jul 1995 A
5467911 Tsuruta et al. Nov 1995 A
5476379 Disel Dec 1995 A
5487499 Sorrentino et al. Jan 1996 A
5518163 Hooven May 1996 A
5518164 Hooven May 1996 A
5526822 Burbank et al. Jun 1996 A
5529235 Boiarski et al. Jun 1996 A
5535934 Boiarski et al. Jul 1996 A
5535937 Boiarski et al. Jul 1996 A
5540375 Bolanos et al. Jul 1996 A
5540706 Aust et al. Jul 1996 A
5542594 McKean et al. Aug 1996 A
5549637 Crainich Aug 1996 A
5553675 Pitzen et al. Sep 1996 A
5562239 Boiarski et al. Oct 1996 A
5564615 Bishop et al. Oct 1996 A
5609560 Ichikawa et al. Mar 1997 A
5626587 Bishop et al. May 1997 A
5632432 Schulze et al. May 1997 A
5645209 Green et al. Jul 1997 A
5647526 Green et al. Jul 1997 A
5653374 Young et al. Aug 1997 A
5658300 Bito et al. Aug 1997 A
5662662 Bishop et al. Sep 1997 A
5667517 Hooven Sep 1997 A
5693042 Boiarski et al. Dec 1997 A
5704534 Huitema et al. Jan 1998 A
5713505 Huitema Feb 1998 A
5762603 Thompson Jun 1998 A
5779130 Alesi et al. Jul 1998 A
5782396 Mastri et al. Jul 1998 A
5782397 Koukline Jul 1998 A
5792573 Pitzen et al. Aug 1998 A
5797536 Smith et al. Aug 1998 A
5820009 Melling et al. Oct 1998 A
5863159 Lasko Jan 1999 A
5908427 McKean et al. Jun 1999 A
5954259 Viola et al. Sep 1999 A
5964774 McKean et al. Oct 1999 A
5993454 Longo Nov 1999 A
6009773 Kato Jan 2000 A
6010054 Johnson et al. Jan 2000 A
6017354 Culp et al. Jan 2000 A
6032849 Mastri et al. Mar 2000 A
6045560 McKean et al. Apr 2000 A
6090123 Culp et al. Jul 2000 A
6126651 Mayer Oct 2000 A
6129547 Cise et al. Oct 2000 A
6165169 Panescu et al. Dec 2000 A
6239732 Cusey May 2001 B1
6241139 Milliman et al. Jun 2001 B1
6264086 McGuckin, Jr. Jul 2001 B1
6264087 Whitman Jul 2001 B1
6302311 Adams et al. Oct 2001 B1
6315184 Whitman Nov 2001 B1
6321855 Barnes Nov 2001 B1
6329778 Culp et al. Dec 2001 B1
6343731 Adams et al. Feb 2002 B1
6348061 Whitman Feb 2002 B1
6368324 Dinger et al. Apr 2002 B1
6371909 Hoeg et al. Apr 2002 B1
6434507 Clayton et al. Aug 2002 B1
6443973 Whitman Sep 2002 B1
6461372 Jensen et al. Oct 2002 B1
6488180 Bayat Dec 2002 B1
6488197 Whitman Dec 2002 B1
6491201 Whitman Dec 2002 B1
6533157 Whitman Mar 2003 B1
6537280 Dinger et al. Mar 2003 B2
6610066 Dinger et al. Aug 2003 B2
6611793 Burnside et al. Aug 2003 B1
6645218 Cassidy et al. Nov 2003 B1
6654999 Stoddard et al. Dec 2003 B2
6673087 Chang Jan 2004 B1
6698643 Whitman Mar 2004 B2
6699177 Wang et al. Mar 2004 B1
6716233 Whitman Apr 2004 B1
6743240 Smith et al. Jun 2004 B2
6783533 Green et al. Aug 2004 B2
6792390 Burnside et al. Sep 2004 B1
6793652 Whitman et al. Sep 2004 B1
6817508 Racenet et al. Nov 2004 B1
6830174 Hillstead et al. Dec 2004 B2
6846308 Whitman et al. Jan 2005 B2
6846309 Whitman et al. Jan 2005 B2
6849071 Whitman et al. Feb 2005 B2
6860892 Tanaka et al. Mar 2005 B1
6899538 Matoba May 2005 B2
6905057 Swayze et al. Jun 2005 B2
6959852 Shelton, IV et al. Nov 2005 B2
6964363 Wales et al. Nov 2005 B2
6981628 Wales Jan 2006 B2
6981941 Whitman et al. Jan 2006 B2
6986451 Mastri et al. Jan 2006 B1
6988649 Shelton, IV et al. Jan 2006 B2
7032798 Whitman et al. Apr 2006 B2
RE39152 Aust et al. Jun 2006 E
7055731 Shelton, IV et al. Jun 2006 B2
7059508 Shelton, IV et al. Jun 2006 B2
7077856 Whitman Jul 2006 B2
7111769 Wales et al. Sep 2006 B2
7122029 Koop et al. Oct 2006 B2
7140528 Shelton, IV Nov 2006 B2
7141049 Stern et al. Nov 2006 B2
7143923 Shelton, IV et al. Dec 2006 B2
7143925 Shelton, IV et al. Dec 2006 B2
7143926 Shelton, IV et al. Dec 2006 B2
7147138 Shelton, IV Dec 2006 B2
7172104 Scirica et al. Feb 2007 B2
7225964 Mastri et al. Jun 2007 B2
7238021 Johnson Jul 2007 B1
7246734 Shelton, IV Jul 2007 B2
7252660 Kunz Aug 2007 B2
7328828 Ortiz et al. Feb 2008 B2
7364061 Swayze et al. Apr 2008 B2
7380695 Doll et al. Jun 2008 B2
7380696 Shelton, IV et al. Jun 2008 B2
7404508 Smith et al. Jul 2008 B2
7407078 Shelton, IV et al. Aug 2008 B2
7416101 Shelton, IV et al. Aug 2008 B2
7419080 Smith et al. Sep 2008 B2
7422139 Shelton, IV et al. Sep 2008 B2
7431189 Shelton, IV et al. Oct 2008 B2
7441684 Shelton, IV et al. Oct 2008 B2
7448525 Shelton, IV et al. Nov 2008 B2
7464846 Shelton, IV et al. Dec 2008 B2
7464847 Viola et al. Dec 2008 B2
7464849 Shelton, IV et al. Dec 2008 B2
7481347 Roy Jan 2009 B2
7481824 Boudreaux et al. Jan 2009 B2
7487899 Shelton, IV et al. Feb 2009 B2
7549564 Boudreaux Jun 2009 B2
7565993 Milliman et al. Jul 2009 B2
7568603 Shelton, IV et al. Aug 2009 B2
7575144 Ortiz et al. Aug 2009 B2
7588175 Timm et al. Sep 2009 B2
7588176 Timm et al. Sep 2009 B2
7637409 Marczyk Dec 2009 B2
7641093 Doll et al. Jan 2010 B2
7644848 Swayze et al. Jan 2010 B2
7670334 Hueil et al. Mar 2010 B2
7673780 Shelton, IV et al. Mar 2010 B2
7699835 Lee et al. Apr 2010 B2
7721931 Shelton, IV et al. May 2010 B2
7738971 Swayze et al. Jun 2010 B2
7740159 Shelton, IV et al. Jun 2010 B2
7743960 Whitman et al. Jun 2010 B2
7758613 Whitman Jul 2010 B2
7766210 Shelton, IV et al. Aug 2010 B2
7770773 Whitman et al. Aug 2010 B2
7770775 Shelton, IV et al. Aug 2010 B2
7793812 Moore Sep 2010 B2
7799039 Shelton, IV et al. Sep 2010 B2
7802712 Milliman et al. Sep 2010 B2
7803151 Whitman Sep 2010 B2
7822458 Webster, III et al. Oct 2010 B2
7845534 Viola et al. Dec 2010 B2
7845537 Shelton, IV et al. Dec 2010 B2
7857185 Swayze et al. Dec 2010 B2
7870989 Viola et al. Jan 2011 B2
7900805 Shelton, IV et al. Mar 2011 B2
7905897 Whitman et al. Mar 2011 B2
7918230 Whitman et al. Apr 2011 B2
7922061 Shelton, IV et al. Apr 2011 B2
7922719 Ralph et al. Apr 2011 B2
7947034 Whitman May 2011 B2
7951071 Whitman et al. May 2011 B2
7954682 Giordano et al. Jun 2011 B2
7959051 Smith et al. Jun 2011 B2
7963433 Whitman et al. Jun 2011 B2
7967178 Scirica et al. Jun 2011 B2
7967179 Olson et al. Jun 2011 B2
7992758 Whitman et al. Aug 2011 B2
8011550 Aranyi et al. Sep 2011 B2
8016178 Olson et al. Sep 2011 B2
8016855 Whitman et al. Sep 2011 B2
8020743 Shelton, IV Sep 2011 B2
8025199 Whitman et al. Sep 2011 B2
8035487 Malackowski Oct 2011 B2
8052024 Viola et al. Nov 2011 B2
8114118 Knodel et al. Feb 2012 B2
8127975 Olson et al. Mar 2012 B2
8132705 Viola et al. Mar 2012 B2
8152516 Harvey et al. Apr 2012 B2
8157150 Viola et al. Apr 2012 B2
8157151 Ingmanson et al. Apr 2012 B2
8182494 Yencho et al. May 2012 B1
8186555 Shelton, IV et al. May 2012 B2
8186587 Zmood et al. May 2012 B2
8220367 Hsu Jul 2012 B2
8235273 Olson et al. Aug 2012 B2
8241322 Whitman et al. Aug 2012 B2
8272554 Whitman et al. Sep 2012 B2
8292150 Bryant Oct 2012 B2
8292888 Whitman Oct 2012 B2
8342379 Whitman et al. Jan 2013 B2
8348130 Shah et al. Jan 2013 B2
8348855 Hillely et al. Jan 2013 B2
8353440 Whitman et al. Jan 2013 B2
8357144 Whitman et al. Jan 2013 B2
8365633 Simaan et al. Feb 2013 B2
8365972 Aranyi et al. Feb 2013 B2
8371492 Aranyi et al. Feb 2013 B2
8372057 Cude et al. Feb 2013 B2
8391957 Carlson et al. Mar 2013 B2
8403926 Nobis et al. Mar 2013 B2
8418904 Wenchell et al. Apr 2013 B2
8424739 Racenet et al. Apr 2013 B2
8454585 Whitman Jun 2013 B2
8505802 Viola et al. Aug 2013 B2
8517241 Nicholas et al. Aug 2013 B2
8523043 Ullrich et al. Sep 2013 B2
8551076 Duval et al. Oct 2013 B2
8561871 Rajappa et al. Oct 2013 B2
8561874 Scirica Oct 2013 B2
8602287 Yates et al. Dec 2013 B2
8623000 Humayun et al. Jan 2014 B2
8627995 Smith et al. Jan 2014 B2
8632463 Drinan et al. Jan 2014 B2
8636766 Milliman et al. Jan 2014 B2
8647258 Aranyi et al. Feb 2014 B2
8652121 Quick et al. Feb 2014 B2
8657174 Yates et al. Feb 2014 B2
8657177 Scirica et al. Feb 2014 B2
8672206 Aranyi et al. Mar 2014 B2
8696552 Whitman Apr 2014 B2
8708213 Shelton, IV et al. Apr 2014 B2
8715306 Faller et al. May 2014 B2
8758391 Swayze et al. Jun 2014 B2
8806973 Ross et al. Aug 2014 B2
8808311 Heinrich et al. Aug 2014 B2
8820605 Shelton, IV Sep 2014 B2
8851355 Aranyi et al. Oct 2014 B2
8858571 Shelton, IV et al. Oct 2014 B2
8875972 Weisenburgh, II et al. Nov 2014 B2
8888762 Whitman Nov 2014 B2
8893946 Boudreaux et al. Nov 2014 B2
8899462 Kostrzewski et al. Dec 2014 B2
8905289 Patel et al. Dec 2014 B2
8910846 Viola Dec 2014 B2
8919630 Milliman Dec 2014 B2
8931680 Milliman Jan 2015 B2
8939344 Olson et al. Jan 2015 B2
8950646 Viola Feb 2015 B2
8960519 Whitman et al. Feb 2015 B2
8961396 Azarbarzin et al. Feb 2015 B2
8967443 McCuen Mar 2015 B2
8968276 Zemlok et al. Mar 2015 B2
8968337 Whitfield et al. Mar 2015 B2
8992422 Spivey et al. Mar 2015 B2
9016545 Aranyi et al. Apr 2015 B2
9023014 Chowaniec et al. May 2015 B2
9027423 Cui May 2015 B1
9033868 Whitman et al. May 2015 B2
9055943 Zemlok et al. Jun 2015 B2
9064653 Prest et al. Jun 2015 B2
9072515 Hall et al. Jul 2015 B2
9113847 Whitman et al. Aug 2015 B2
9113875 Viola et al. Aug 2015 B2
9113876 Zemlok et al. Aug 2015 B2
9113899 Garrison et al. Aug 2015 B2
9216013 Scirica et al. Dec 2015 B2
9241712 Zemlok et al. Jan 2016 B2
9282961 Whitman et al. Mar 2016 B2
9282963 Bryant Mar 2016 B2
9295522 Kostrzewski Mar 2016 B2
9307986 Hall et al. Apr 2016 B2
20010027321 Gellman Oct 2001 A1
20010031975 Whitman et al. Oct 2001 A1
20020049454 Whitman et al. Apr 2002 A1
20020165541 Whitman Nov 2002 A1
20030038938 Jung et al. Feb 2003 A1
20030165794 Matoba Sep 2003 A1
20040034369 Sauer et al. Feb 2004 A1
20040111012 Whitman Jun 2004 A1
20040133189 Sakurai Jul 2004 A1
20040153124 Whitman Aug 2004 A1
20040176751 Weitzner et al. Sep 2004 A1
20040193146 Lee et al. Sep 2004 A1
20050125027 Knodel et al. Jun 2005 A1
20050131442 Yachia et al. Jun 2005 A1
20050155443 Krozek Jul 2005 A1
20050235764 Johnson Oct 2005 A1
20060142656 Malackowski et al. Jun 2006 A1
20060142740 Sherman et al. Jun 2006 A1
20060142744 Boutoussov Jun 2006 A1
20060151567 Roy Jul 2006 A1
20060259073 Miyamoto et al. Nov 2006 A1
20060278680 Viola et al. Dec 2006 A1
20060284730 Schmid et al. Dec 2006 A1
20070023476 Whitman et al. Feb 2007 A1
20070023477 Whitman et al. Feb 2007 A1
20070027469 Smith et al. Feb 2007 A1
20070029363 Popov Feb 2007 A1
20070055219 Whitman Mar 2007 A1
20070084897 Shelton et al. Apr 2007 A1
20070102472 Shelton May 2007 A1
20070152014 Gillum et al. Jul 2007 A1
20070175947 Ortiz et al. Aug 2007 A1
20070175949 Shelton et al. Aug 2007 A1
20070175950 Shelton et al. Aug 2007 A1
20070175951 Shelton et al. Aug 2007 A1
20070175955 Shelton et al. Aug 2007 A1
20070175961 Shelton et al. Aug 2007 A1
20070227850 Heravi Oct 2007 A1
20070270784 Smith et al. Nov 2007 A1
20080029570 Shelton et al. Feb 2008 A1
20080029573 Shelton et al. Feb 2008 A1
20080029574 Shelton et al. Feb 2008 A1
20080029575 Shelton et al. Feb 2008 A1
20080058801 Taylor et al. Mar 2008 A1
20080109012 Falco et al. May 2008 A1
20080110958 McKenna et al. May 2008 A1
20080147089 Loh et al. Jun 2008 A1
20080167736 Swayze et al. Jul 2008 A1
20080185419 Smith et al. Aug 2008 A1
20080188841 Tomasello et al. Aug 2008 A1
20080197167 Viola et al. Aug 2008 A1
20080208195 Shores et al. Aug 2008 A1
20080237296 Boudreaux et al. Oct 2008 A1
20080251561 Eades et al. Oct 2008 A1
20080255413 Zemlok et al. Oct 2008 A1
20080255607 Zemlok Oct 2008 A1
20080262654 Omori et al. Oct 2008 A1
20080308603 Shelton et al. Dec 2008 A1
20090012533 Barbagli et al. Jan 2009 A1
20090090763 Zemlok et al. Apr 2009 A1
20090099876 Whitman Apr 2009 A1
20090138006 Bales et al. May 2009 A1
20090171147 Lee et al. Jul 2009 A1
20090182193 Whitman et al. Jul 2009 A1
20090209946 Swayze et al. Aug 2009 A1
20090209990 Yates et al. Aug 2009 A1
20090254094 Knapp et al. Oct 2009 A1
20090299141 Downey Dec 2009 A1
20100023022 Zeiner et al. Jan 2010 A1
20100069942 Shelton, IV Mar 2010 A1
20100160821 Parihar Jun 2010 A1
20100193568 Scheib et al. Aug 2010 A1
20100211053 Ross et al. Aug 2010 A1
20100225073 Porter et al. Sep 2010 A1
20100320252 Viola Dec 2010 A1
20110071508 Duval et al. Mar 2011 A1
20110077673 Grubac et al. Mar 2011 A1
20110121049 Malinouskas et al. May 2011 A1
20110125138 Malinouskas et al. May 2011 A1
20110139851 McCuen Jun 2011 A1
20110155783 Rajappa et al. Jun 2011 A1
20110155786 Shelton, IV Jun 2011 A1
20110172648 Jeong Jul 2011 A1
20110174009 Lizuka et al. Jul 2011 A1
20110174099 Ross Jul 2011 A1
20110184245 Xia et al. Jul 2011 A1
20110204119 McCuen Aug 2011 A1
20110218522 Whitman Sep 2011 A1
20110247449 Parker Oct 2011 A1
20110276057 Conlon et al. Nov 2011 A1
20110290854 Timm et al. Dec 2011 A1
20110295242 Spivey et al. Dec 2011 A1
20110295269 Swensgard et al. Dec 2011 A1
20120000962 Racenet et al. Jan 2012 A1
20120074199 Olson et al. Mar 2012 A1
20120089131 Zemlok et al. Apr 2012 A1
20120104071 Bryant May 2012 A1
20120116368 Viola May 2012 A1
20120143002 Aranyi et al. Jun 2012 A1
20120172924 Allen, IV Jul 2012 A1
20120211542 Racenet Aug 2012 A1
20120215220 Manzo Aug 2012 A1
20120223121 Viola et al. Sep 2012 A1
20120245428 Smith et al. Sep 2012 A1
20120253329 Zemlok et al. Oct 2012 A1
20120265095 Fiebig Oct 2012 A1
20120310220 Malkowski et al. Dec 2012 A1
20120323226 Chowaniec et al. Dec 2012 A1
20120330285 Hartoumbekis et al. Dec 2012 A1
20130093149 Saur et al. Apr 2013 A1
20130181035 Milliman Jul 2013 A1
20130184704 Beardsley et al. Jul 2013 A1
20130214025 Zemlok et al. Aug 2013 A1
20130274722 Kostrzewski et al. Oct 2013 A1
20130282052 Aranyi et al. Oct 2013 A1
20130292451 Viola et al. Nov 2013 A1
20130313304 Shelton, IV et al. Nov 2013 A1
20130317486 Nicholas et al. Nov 2013 A1
20130319706 Nicholas et al. Dec 2013 A1
20130324978 Nicholas et al. Dec 2013 A1
20130324979 Nicholas et al. Dec 2013 A1
20130334281 Williams Dec 2013 A1
20140012236 Williams et al. Jan 2014 A1
20140012237 Pribanic et al. Jan 2014 A1
20140012289 Snow et al. Jan 2014 A1
20140025046 Williams et al. Jan 2014 A1
20140110455 Ingmanson et al. Apr 2014 A1
20140207125 Applegate et al. Jul 2014 A1
20140207182 Zergiebel et al. Jul 2014 A1
20140207185 Goble et al. Jul 2014 A1
20140236174 Williams et al. Aug 2014 A1
20140260720 Hartranft Sep 2014 A1
20140276932 Williams et al. Sep 2014 A1
20140277334 Yu et al. Sep 2014 A1
20140299647 Scirica et al. Oct 2014 A1
20140303668 Nicholas Oct 2014 A1
20140358129 Zergiebel et al. Dec 2014 A1
20140361068 Aranyi et al. Dec 2014 A1
20140365235 DeBoer et al. Dec 2014 A1
20140373652 Zergiebel et al. Dec 2014 A1
20150014392 Williams et al. Jan 2015 A1
20150035658 Provancher Feb 2015 A1
20150048144 Whitman Feb 2015 A1
20150076205 Zergiebel Mar 2015 A1
20150080912 Sapre Mar 2015 A1
20150112381 Richard Apr 2015 A1
20150122870 Zemlok et al. May 2015 A1
20150133224 Whitman et al. May 2015 A1
20150150547 Ingmanson et al. Jun 2015 A1
20150150574 Richard et al. Jun 2015 A1
20150157320 Zergiebel et al. Jun 2015 A1
20150157321 Zergiebel et al. Jun 2015 A1
20150164502 Richard et al. Jun 2015 A1
20150201931 Zergiebel et al. Jul 2015 A1
20150272577 Zemlok et al. Oct 2015 A1
20150297199 Nicholas et al. Oct 2015 A1
20150303996 Calderoni Oct 2015 A1
20150320420 Penna et al. Nov 2015 A1
20150327850 Kostrzewski Nov 2015 A1
20150342601 Williams et al. Dec 2015 A1
20150342603 Zergiebel et al. Dec 2015 A1
20150374366 Zergiebel et al. Dec 2015 A1
20150374370 Zergiebel et al. Dec 2015 A1
20150374371 Richard et al. Dec 2015 A1
20150374372 Zergiebel et al. Dec 2015 A1
20150374449 Chowaniec et al. Dec 2015 A1
20150380187 Zergiebel et al. Dec 2015 A1
20160095585 Zergiebel et al. Apr 2016 A1
20160095596 Scirica et al. Apr 2016 A1
20160106406 Cabrera et al. Apr 2016 A1
20160113648 Zergiebel et al. Apr 2016 A1
20160113649 Zergiebel et al. Apr 2016 A1
Foreign Referenced Citations (19)
Number Date Country
2451558 Jan 2003 CA
1547454 Nov 2004 CN
1957854 May 2007 CN
101495046 Jul 2009 CN
102247182 Nov 2011 CN
103498904 Jan 2014 CN
103498905 Jan 2014 CN
102008053842 May 2010 DE
0705571 Apr 1996 EP
1563793 Aug 2005 EP
1769754 Apr 2007 EP
2316345 May 2011 EP
2446834 May 2012 EP
2668910 Dec 2013 EP
2333509 Feb 2010 ES
2005-125075 May 2005 JP
20120022521 Mar 2012 KR
2011108840 Sep 2011 WO
2012040984 Apr 2012 WO
Non-Patent Literature Citations (44)
Entry
European Search Report dated Mar. 30, 2017, issued in EP Application No. 16201370.
Extended European Search Report corresponding to counterpart International Application No. EP 14 18 4882.0 dated May 12, 2015.
Canadian Office Action corresponding to counterpart International Application No. CA 2640399 dated May 7, 2015.
Japanese Office Action corresponding to counterpart International Application No. JP 2011-197365 dated Mar. 23, 2015.
Japanese Office Action corresponding to counterpart International Application No. JP 2011-084092 dated May 20, 2015.
Japanese Office Action corresponding to counterpart International Application No. JP 2014-148482 dated Jun. 2, 2015.
Extended European Search Report corresponding to counterpart International Application No. EP 14 18 9358.6 dated Jul. 8, 2015.
Extended European Search Report corresponding to counterpart International Application No. EP 14 19 6148.2 dated Apr. 23, 2015.
Partial European Search Report corresponding to counterpart International Application No. EP 14 19 6704.2 dated May 11, 2015.
Australian Office Action corresponding to counterpart International Application No. AU 2010241367 dated Aug. 20, 2015.
Partial European Search Report corresponding to counterpart International Application No. EP 14 19 9783.3 dated Sep. 3, 2015.
Extended European Search Report corresponding to counterpart International Application No. EP 15 16 9962.6 dated Sep. 14, 2015.
Extended European Search Report corresponding to International Application No. EP 15 15 1076.5 dated Apr. 22, 2015.
Japanese Office Action corresponding to International Application No. JP 2011-084092 dated Jan. 14, 2016.
Extended European Search Report corresponding to International Application No. EP 12 19 7970.2 dated Jan. 28, 2016.
Chinese Office Action corresponding to International Application No. CN 201210560638.1 dated Oct. 21, 2015.
European Office Action corresponding to International Application No. EP 14 15 9056.2 dated Oct. 26, 2015.
Australian Examination Report No. 1 corresponding to International Application No. AU 2015200153 dated Dec. 11, 2015.
Australian Examination Report No. 1 corresponding to International Application No. AU 2014204542 dated Jan. 7, 2016.
Chinese Office Action corresponding to International Application No. CN 201310125449.6 dated Feb. 3, 2016.
Extended European Search Report corresponding to International Application No. EP 15 19 0245.9 dated Jan. 28, 2016.
Extended European Search Report corresponding to International Application No. EP 15 16 7793.7 dated Apr. 5, 2016.
European Office Action corresponding to International Application No. EP 14 18 4882.0 dated Apr. 25, 2016.
Extended European Search Report corresponding to International Application No. EP 14 19 6704.2 dated Sep. 24, 2015.
International Search Report and Written Opinion corresponding to Int'l Appln. No. PCT/US2015/051837, dated Dec. 21, 2015.
Extended European Search Report corresponding to International Application No. EP 14 19 7563.1 dated Aug. 5, 2015.
Partial European Search Report corresponding to International Application No. EP 15 19 0643.5 dated Feb. 26, 2016.
Extended European Search Report corresponding to International Application No. EP 15 16 6899.3 dated Feb. 3, 2016.
Extended European Search Report corresponding to International Application No. EP 14 19 9783.3 dated Dec. 22, 2015.
Extended European Search Report corresponding to International Application No. EP 15 17 38071 dated Nov. 24, 2015.
Extended European Search Report corresponding to International Application No. EP 15 19 0760.7 dated Apr. 1, 2016.
Extended European Search Report corresponding to International Application No. EP 15 17 3803.6 dated Nov. 24, 2015.
Extended European Search Report corresponding to International Application No. EP 15 17 3804.4 dated Nov. 24, 2015.
Extended European Search Report corresponding to International Application No. EP 15 18 8539.9 dated Feb. 17, 2016.
Extended European Search Report corresponding to International Application No. EP 15 17 3910.9 dated Nov. 13, 2015.
European Office Action corresponding to International Application No. EP 14 15 2236.7 dated Aug. 11, 2015.
Extended European Search Report corresponding to International Application No. EP 15 18 4915.5 dated Jan. 5, 2016.
Office Action corresponding to counterpart Int'l Appln. No. CN 201310369318.2 dated Jun. 28, 2016.
Chinese Office Action (with English translation), dated Jul. 4, 2016, corresponding to Chinese Patent Application No. 2015101559718; 23 total pages.
European Search Report EP 15 156 035.6 dated Aug. 10, 2016.
Australian Examination Report No. 1 corresponding to International Application No. AU 2013205872 dated Oct. 19, 2016.
Australian Examination Report from Appl. No. AU 2013205840 dated Nov. 3, 2016.
European Search Report corresponding to EP 15 184 915.5-1654 dated Sep. 16, 2016.
European Office Action dated May 10, 2019, issued in EP Appln. No. 16201370.
Related Publications (1)
Number Date Country
20170150965 A1 Jun 2017 US
Provisional Applications (1)
Number Date Country
62261469 Dec 2015 US