Circular stapling device with offset spline tip

Information

  • Patent Grant
  • 10695069
  • Patent Number
    10,695,069
  • Date Filed
    Tuesday, July 17, 2018
    5 years ago
  • Date Issued
    Tuesday, June 30, 2020
    3 years ago
Abstract
A surgical stapling device includes an anvil assembly and a shell assembly. The anvil and shell assemblies each include splines that define guide channels. Each of the anvil splines defines a distally positioned triangular tip that is defined by an apex and first and second right cam surfaces. The cam surfaces of the anvil splines are configured to engage one of the shell splines to cam or rotate the anvil assembly into alignment with the shell assembly as the anvil assembly is moved in relation to the shell assembly to a clamped position.
Description
BACKGROUND
1. Technical Description

The present disclosure is directed to circular stapling devices, and more particularly, to circular stapling devices including splines having offset spline tips configured to prevent malformation of staples due to spline crashing.


2. Background of Related Art

Circular stapling devices are utilized by clinicians to apply one or more surgical fasteners, e.g., staples or two-part fasteners, to body tissue for the purpose of joining segments of body tissue together and/or for the creation of an anastomosis. Circular stapling devices generally include a shell assembly including a staple cartridge supporting a plurality of annular rows of staples and an anvil assembly operatively associated with the shell assembly and having annular arrays of staple receiving pockets. The staple receiving pockets are aligned with the annular rows of staples to provide a surface against which the plurality of annular rows of staples can be formed.


During a typical tissue fastening procedure, the anvil assembly of the stapling device is positioned within one segment of body tissue and the shell assembly is positioned in an adjacent segment of body tissue. The anvil assembly is then attached to the body portion of the stapling device and the stapling device is actuated to move the anvil assembly in relation to the staple cartridge of the shell assembly to clamp the body tissue segments together.


Typically, the anvil assembly includes an anvil shaft that includes splines that mate with splines formed within a shell housing of the shell assembly to align the staple forming pockets of the anvil assembly with staple receiving pockets of the staple cartridge of the shell assembly. The splines on the anvil shaft and on the shell housing of the shell assembly include first and second tapered ends that define an apex. When the tapered ends of the splines of the anvil assembly engage the tapered ends of the shell assembly, the anvil assembly is cammed into rotation to align the staple forming pockets of the anvil assembly with staple receiving pockets of the staple cartridge of the shell assembly. However, if the apexes of the splines of the anvil assembly and the shell assembly engage head on, i.e., crash, the splines of the anvil assembly and the shell assembly may be damaged such that proper alignment of the anvil and shell assemblies is prevented such that malformation of the staples may occur during firing of the stapling device.


A continuing need exists for a circular stapling device having a more reliable alignment structure for aligning the staple forming pockets of the anvil assembly with the staple receiving pockets of the staple cartridge of the shell assembly to minimize the occurrence of staple malformation.


SUMMARY

One aspect of the disclosure is directed to a surgical stapling device including an approximation assembly, a shell assembly, and an anvil assembly. The approximation assembly includes an anvil retainer. The shell assembly includes a staple cartridge and a shell housing having an inner housing portion defining a bore. The inner housing portion supports a plurality of shell splines positioned within the bore. Each of the plurality of shell splines defines a guide channel with an adjacent one of the plurality of shell splines. The staple cartridge is supported on the shell housing. The anvil assembly includes an anvil shaft having at least one anvil spline and an anvil head having an anvil surface defining a plurality of staple deforming recesses. The at least one anvil spline defines a longitudinal axis. The anvil shaft is configured to releasably engage the anvil retainer and the anvil head is supported on a distal portion of the anvil shaft. The at least one anvil spline includes first and second tapered surfaces that intersect at an apex that is offset to one side of the longitudinal axis. The first tapered surface has a surface area β and the second tapered surface has a surface area Ω that is different from surface area β.


Another aspect of the present disclosure is directed to an anvil assembly for a circular stapling device including an anvil shaft having at least one anvil spline and an anvil head having an anvil surface defining a plurality of staple deforming recesses. The at least one anvil spline defines a longitudinal axis. The anvil head is supported on a distal portion of the anvil shaft. The at least one anvil spline includes first and second tapered surfaces that intersect at an apex that is offset to one side of the longitudinal axis. The first tapered surface has a surface area β and the second tapered surface has a surface area Ω that is different from surface area β.


Another aspect of the disclosure is directed to a tool assembly including a shell assembly and an anvil assembly. The shell assembly includes a staple cartridge and a shell housing. The shell housing has an inner housing portion defining a bore and a plurality of shell splines supported on the inner housing portion within the bore. Each of the plurality of shell splines defines a guide channel with an adjacent one of the plurality of shell splines. The staple cartridge is supported on the shell housing. The anvil assembly includes an anvil shaft having at least one anvil spline and an anvil head having an anvil surface defining a plurality of staple deforming recesses. The at least one anvil spline defines a longitudinal axis. The anvil head is supported on a distal portion of the anvil shaft. The at least one anvil spline includes first and second tapered surfaces that intersect at an apex that is offset to one side of the longitudinal axis. The first tapered surface has a surface area β and the second tapered surface has a surface area Ω that is different from surface area β.


In embodiments, β is at least 1.5 times greater than Ω.


In some embodiments, β is at least 2 times greater than Ω.


In certain embodiments, the at least one anvil spline is formed from metal and the plurality of shell splines is formed from a polymer.


In embodiments, each of the plurality of shell splines defines a longitudinal axis and includes first and second tapered cam surfaces. The first and second tapered cam surfaces of each of the plurality of shell splines intersect at an apex.


In some embodiments, the apex of each of the plurality of shell splines is aligned with the longitudinal axis of the shell spline.


In certain embodiments, the first cam surface of each of the plurality of shell splines has a surface area that is equal to a surface area of the second cam surface of each of the plurality of shell splines.


In embodiments, at least one the anvil spline is formed to migrate into a respective shell spline of the plurality of the shell splines when the apex of the at least one anvil spline engages the apex of a respective one of the plurality of shell splines.





BRIEF DESCRIPTION OF THE DRAWINGS

Various embodiments of the presently disclosed circular stapling device are described herein below with reference to the drawings, wherein:



FIG. 1 is a side perspective view of an exemplary embodiment of the presently disclosed circular stapling device with a tool assembly in a clamped position;



FIG. 2 is a side perspective view of the surgical stapling device shown in FIG. 1 with shell and anvil assemblies of the tool assembly separated from the remaining portion of the stapling device;



FIG. 3 is a perspective view from a distal end of a “Prior Art” surgical stapling device with the anvil assembly of the tool assembly of the surgical stapling device separated from an anvil retainer (shown in phantom) of the surgical stapling device;



FIG. 4 is a schematic view of a spline configuration of the anvil assembly of the “Prior Art” surgical stapling device shown in FIG. 3;



FIG. 5 is a side perspective view of the anvil assembly of the surgical stapling device shown in FIG. 1;



FIG. 5A is a cross-sectional view taken along section line 5A-5A of FIG. 5;



FIG. 5B is an enlarged view of the indicated area of detail shown in FIG. 5;



FIG. 6 is a side view taken in the direction indicated by arrows 6-6 of FIG. 5;



FIG. 7 is a schematic view of the splines of the anvil and cartridge assemblies shown in FIG. 5 in a non-crash condition prior to engagement of the splines of the anvil assembly with the splines of the cartridge assembly;



FIG. 8 is a schematic view of the splines of the anvil and cartridge assemblies shown in FIG. 5 in a non-crash condition after engagement of the splines of the anvil assembly with the splines of the cartridge assembly as the splines of the anvil assembly are directed into the guide channels of the shell assembly;



FIG. 9 is a schematic view of the splines of the anvil and cartridge assemblies shown in FIG. 5 in a non-crash condition after engagement of the splines of the anvil assembly with the splines of the cartridge assembly, with the splines of the anvil assembly positioned within the guide channels of the shell assembly;



FIG. 10 is a cross-sectional view taken through the splines of the anvil and shell assemblies with the splines of the anvil assembly positioned within the guide channels of the shell assembly as shown in FIG. 9;



FIG. 11 is a schematic view of the splines of the anvil and cartridge assemblies shown in FIG. 5 in a crash condition as the apex of the splines of the anvil assembly initially engage the splines of the cartridge assembly;



FIG. 12 is a schematic view of the splines of the anvil and cartridge assemblies shown in FIG. 5 in a crash condition as the apex of the splines of the anvil assembly crash into the splines of the cartridge assembly;



FIG. 13 is a side view of one of the splines of the anvil assembly shown in FIG. 5 illustrating the crash forces applied to the anvil spline as the anvil spline crashes into one of the splines of the shell assembly;



FIG. 14 is a schematic view of the splines of the anvil and cartridge assemblies shown in FIG. 5 after engagement of the splines of the anvil assembly with the splines of the cartridge assembly, with the splines of the anvil assembly positioned within the guide channels of the shell assembly;



FIG. 15 is a cross-sectional view taken through the splines of the anvil and shell assemblies shown in FIG. 5 with the splines of the anvil assembly positioned within the guide channels of the shell assembly as shown in FIG. 14; and



FIG. 16 is a schematic view of the splines of the anvil and cartridge assemblies shown in FIG. 5 after engagement of the splines of the anvil assembly with the splines of the cartridge assembly, with the splines of the anvil assembly positioned within the guide channels of the shell assembly.





DETAILED DESCRIPTION OF EMBODIMENTS

The presently disclosed circular stapling device will now be described in detail with reference to the drawings in which like reference numerals designate identical or corresponding elements in each of the several views. However, it is to be understood that the disclosed embodiments are merely exemplary of the disclosure and may be embodied in various forms. Well-known functions or constructions are not described in detail to avoid obscuring the present disclosure in unnecessary detail. Therefore, specific structural and functional details disclosed herein are not to be interpreted as limiting, but merely as a basis for the claims and as a representative basis for teaching one skilled in the art to variously employ the present disclosure in virtually any appropriately detailed structure.


In this description, the term “proximal” is used generally to refer to that portion of the device that is closer to a clinician, while the term “distal” is used generally to refer to that portion of the device that is farther from the clinician. In addition, the term “clinician” is used generally to refer to medical personnel including doctors, nurses, and support personnel.


The presently disclosed surgical stapling device includes an anvil assembly and a shell assembly. The anvil and shell assemblies each include splines that define guide channels. The guide channels defined by the shell splines receive the anvil splines to properly align the anvil assembly with the shell assembly. Each of the shell splines defines a distally positioned triangular tip that is defined by an apex and first and second cam surfaces. The first and second cam surfaces of each shell spline are configured to engage one of the anvil splines to cam or rotate the anvil assembly into alignment with the shell assembly. Similarly, each of the anvil splines defines a proximally positioned triangular tip that is defined by an apex and first and second cam surfaces. The cam surfaces of the anvil splines are also configured to engage one of the shell splines to cam or rotate the anvil assembly into alignment with the shell assembly. The apex of each of the anvil splines is offset from a longitudinal axis of the anvil spline such that the first and second cam surfaces of the anvil splines have different surface areas. By providing anvil splines that have cam surfaces with a different surface areas, a greater force is applied to the cam surface of the anvil spline having the greater surface area when the splines of the anvil assembly and the shell assembly crash. As such, when crashing of the splines occurs the anvil splines will be pushed in one direction to rotate the anvil assembly in relation to the shell assembly out of the crashed position to direct the anvil splines into the guide channels defined by the shell splines to properly align the shell assembly with the anvil assembly.


Referring to FIGS. 1 and 2, the presently disclosed circular stapling device shown generally as stapling device 10 includes a handle assembly 12, an elongate body portion 14 that extends distally from the handle assembly 12, and a tool assembly 16 that is supported on a distal portion of the elongate body portion 14. The tool assembly 16 includes a shell assembly 18 that supports a staple cartridge 18a and an anvil assembly 20 that includes an anvil head 34 having an anvil surface 34a that defines a plurality of staple deforming recesses 20a (FIG. 2.) The handle assembly 12 includes an approximation knob 22 of an approximation assembly that is operable to move the anvil assembly 20 between unclamped and clamped positions in relation to the cartridge assembly 18, a firing trigger 24 that that operates a firing mechanism (not shown) to fire staples (not shown) from the staple cartridge 18a into tissue, and a firing trigger lockout 26 that is pivotally supported on the handle assembly 12 and is positioned to prevent inadvertent firing of the stapling device 10. For a detailed description of an exemplary circular stapling device including known approximation, firing, and lockout mechanisms, see U.S. Pat. No. 7,857,187 (“the '187 Patent”) which is incorporated herein by reference in its entirety.


Although the presently disclosed stapling device 10 is shown and described as being a manually powered device, it is envisioned that the stapling device 10 can also be an electrically powered device such as described in U.S. Patent Publication No. 2015/0048140 which is incorporated herein by reference in its entirety. A surgical stapling component according to any of the embodiments disclosed herein can be configured for use with a robotic surgical stapling system.


The staple cartridge 18a of the shell assembly 18 and the anvil surface 34a (FIG. 2) of the anvil assembly 20 have an annular configuration. The anvil assembly 20 is movable in relation to the shell assembly 18 between a spaced position and a clamped position to move the anvil surface 34a of the anvil head 34 into juxtaposed alignment with the staple cartridge 18a. The staple cartridge 18a defines staple receiving slots 28 (FIG. 1) that are aligned with the staple deforming recesses 20a (FIG. 2) of the anvil surface 34a when the staple cartridge 18a and the anvil surface 34a are properly aligned such that staples ejected from the staple receiving slots 28 are deformed within the staple deforming recesses 20a when the stapling device 10 is fired.


The anvil assembly 20 is releasably supported on an anvil retainer 30 (FIG. 2) of the stapling device 10. The anvil retainer 30 in conjunction with the rotation knob 22 forms part of the approximation mechanism of the stapling device 10 and includes a distal portion 30a and a proximal portion 30b (FIG. 2). The distal portion 30a of the anvil retainer 30 extends from a distal end of the elongate body portion 14 of the stapling device 10 and through the shell assembly 18 to a position to engage the anvil assembly 20. The proximal portion 30b of the anvil retainer 30 is operatively connected to the approximation knob 22 via an approximation linkage 37 (FIG. 2) such that rotation of the approximation knob 22 causes the anvil retainer 30 to move within the shell assembly 18 to move the anvil assembly 20 in relation to the staple cartridge 18a between the spaced position and the clamped position.


The shell assembly 18 includes an annular knife (not shown) that is movable from a retracted position to an advanced position within the shell assembly 18 during firing of the stapling device 10 to transect tissue clamped between the staple cartridge 18a and the anvil surface 34a. (See the '187 Patent.) In some embodiments, the shell assembly 18 is releasably coupled to a distal portion of the elongate body 14 of the stapling device 10 to facilitate replacement of the shell assembly 18 after each firing of the stapling device 10. Mechanisms for releasably coupling the shell assembly 18 to the elongate body portion 14 of the stapling device 10 are described in U.S. Patent Publication Nos. 2016/0310141, 2016/0192938, and 2016/0192934 which are incorporated herein in their entirety by reference. Alternately, the shell assembly 18 can be fixedly secured to the distal portion of the elongate body 14.


Referring to FIG. 3, prior art circular stapling devices 100 include an anvil assembly 120 having an anvil head 122 and an anvil shaft or center rod 124, and a shell assembly 118 having a staple cartridge 118a and a shell housing 126 having an inner housing portion 128 that defines a through bore 128a. The anvil head 122 defines an anvil surface 122a that defines an annular array of staple deforming recesses 122b and the staple cartridge 118a defines an annular array of staple receiving slots 118b. An anvil retainer 130 (shown in phantom) includes a distal end that is configured to releasably engage the anvil shaft 124 of the anvil assembly 120. The anvil retainer 130 is received within the through bore 128a of the shell housing 126 and is movable between retracted and advanced positions. When the anvil shaft 124 is coupled to the anvil retainer 130 and the anvil retainer 130 is retracted (via actuation of the approximation knob 22, FIG. 1), the anvil shaft 124 is drawn into the through bore 128a of the inner housing portion 128 of the shell housing 126.


The anvil assembly 120 includes splines 134 formed on the anvil shaft 124 and the shell assembly 118 includes splines formed along the inner housing portion 128 of the shell housing 126. In order to align the staple deforming recesses 122b of the anvil surface 122a of the anvil assembly 120 with the staple receiving slots 118b of the staple cartridge 118a of the shell assembly 118, the splines 134 on the anvil shaft 124 including adjacent splines 134a, 134b (FIG. 4) are received in channels 148 defined between the splines 136 formed along an inner wall of the inner housing portion 128 (FIG. 3) of the shell housing 126. Each of the splines 134 of the anvil assembly 120 defines a central axis “Z” and first and second tapered cam surfaces 138a, 138b positioned on opposite sides of the central axis “Z” as viewed in FIG. 4. The tapered surfaces 138a, 138b meet at their proximal ends at an apex 140. Similarly, each of the splines 136 of the shell assembly 118 defines a central axis “X” and first and second tapered cam surfaces 142a, 142b positioned on opposite sides of the central axis “X”. The tapered surfaces 142a, 142b meet at their distal ends at an apex 144. As shown, the first and second tapered cam surfaces 138a, 138b have substantially equal surface areas. Similarly, the first and second tapered cam surfaces 142a, 142b of the shell splines 136 have substantially equal surface areas.


When the anvil assembly 120 is attached to the anvil retainer 130 (FIG. 3) and the anvil retainer 130 and anvil assembly 120 are retracted into the through bore 128a (FIG. 3) of the inner housing portion 128 of the shell housing 126, the anvil splines 134 of the anvil assembly 120 move towards the shell splines 136 of the shell assembly 118. If the anvil splines 134 are misaligned with channels 148 defined between the shell splines 136, the apexes 140 of the anvil splines 134a, 134b will engage one of the cam surfaces 142a, 142b of the shell splines 136. When the apexes 140 of the anvil splines 134a, 134b (only two are shown) engage the first tapered cam surface 142a of the splines 136, the engagement urges or cams the anvil assembly 120 to rotate in the direction indicated by arrow “S” (FIG. 4) to realign the anvil splines 134a, 134b so that the anvil splines 134a, 134b enter into the channels 148 defined between the shell splines 136. However, if the apexes 140 of the anvil splines 134a-b are aligned with the apexes 144 of the shell splines 136 such that the apexes 140 and 144 meet head on or “crash”, the apexes 140 and 144 may be damaged to that extent that the anvil assembly 120 will not rotate into alignment with the shell assembly 118. When this occurs, alignment between the staple receiving slots 118b of the staple cartridge 118a and the staple deforming recesses 122b of the anvil assembly 120 when the staples are fired. This may result staple malformation.


Referring to FIGS. 5-6, in the exemplary embodiment of the presently disclosed stapling device 10, the anvil assembly 20 includes the anvil head 34 and an anvil shaft 36. The anvil shaft 36 supports a plurality of splines 38. Each of the splines 38 defines a longitudinal axis “W” and includes a proximally positioned tip 40 that is defined by a first tapered surface 42 and a second tapered surface 44. The first and second tapered surfaces 42, 44 intersect at an apex 46 that is offset to one side of the longitudinal axis “W”. The first tapered surface 42 defines a long edge 42a and has a surface area β. The second tapered surface 44 defines a short edge 44a and a second surface area Ω. In embodiments, β is greater than Ω. In some embodiments, β is at least 1.5 times greater than Ω. In other embodiments, β is at least 2 times greater than Ω. In embodiments, the anvil splines 38 are formed from a hard material such as metal.


Referring again to FIG. 5, the shell assembly 18 includes a shell housing 50 having an inner housing portion 52 including an inner wall surface 54 that defines a central bore 56. The central bore 56 is receives the anvil retainer 30 and the anvil shaft 36 of the anvil assembly 20. The inner wall surface 54 of the inner housing portion 52 of the shell housing 50 supports a plurality of shell splines 60. Each of the shell splines 60 defines a guide channel 61 with an adjacent shell spline 60. In embodiments, the shell splines 60 are formed from a polymeric material such as polyethylene.


Referring to FIG. 7, each of the shell splines 60 defines a longitudinal axis “Y” and includes first and second tapered cam surfaces 62 and 64. The first and second tapered cam surfaces 62 and 64 intersect at an apex 66 that is aligned with the longitudinal axis “Y” of the spline 60 such that the area of the first cam surface 62 is substantially equal to the area of the second cam surface 64.


Referring to FIGS. 7-10, when the anvil assembly 20 is secured to the anvil retainer 30 (FIG. 10) and the anvil retainer 30 and the anvil shaft 36 (FIG. 10) of the anvil assembly 20 are withdrawn into the central bore 56 of the inner housing portion 52 of the shell housing 50 (FIG. 10) in the direction indicated by arrow “A” in FIG. 7, the anvil splines 38 are moved towards and into engagement with the shell splines 60. When the apex 46 of each of the anvil splines 38 is offset from the apex 66 of the respective shell splines 60 such that the apex 46 of the anvil splines 38 engage one of the right or left tapered surfaces 62, 64 of the shell splines 60, the anvil assembly 20 (FIG. 1) is cammed in either a clockwise or counterclockwise direction to guide the anvil splines 38 into one of the guide channels 61 (FIG. 10) positioned between the shell splines 60. For example, when the apex 46 of the anvil splines 38 engage one of the left tapered surfaces 62, 64 of the respective shell splines 60, the anvil assembly 20 is cammed in the direction indicated by arrow “B” in FIG. 8 to direct the anvil splines 38 into the guide channels 61 (FIG. 10) positioned between adjacent shell splines 60. This movement properly aligns the anvil assembly 20 in relation to the shell assembly 18 for firing of the stapling device 10.


Referring to FIGS. 11-16, when the anvil assembly 20 is secured to the anvil retainer 30 (FIG. 15) and the anvil retainer 30 and the anvil shaft 36 of the anvil assembly 20 are withdrawn into the central bore 56 of the inner housing portion 52 of the shell housing 50 (FIG. 15) in the direction indicated by arrow “C” in FIG. 12, the anvil splines 38 are moved towards and into engagement with the shell splines 60. When the apex 46 of each of the anvil splines 38 is aligned with a respective apex 66 of the shell splines 60, the apex 46 of each of the anvil splines 38 crashes into the apex 66 of the shell splines 60. When the apex 46 of the metal anvil splines 38 engage the polymeric shell splines 60 and the anvil shaft 36 is withdrawn further into the central bore 56 of the inner housing portion 52 of the shell housing 50, the anvil splines 38 migrate or penetrate into the shell splines 60 (FIG. 12).


As shown in FIG. 13, as the anvil splines 38 migrate into the shell splines 60, the forces applied by the tapered surface 42 defined by the long edge and having the greater surface area β applies a higher force on one side of the shell spline 60 to cam or urge the anvil assembly 20 (FIG. 1) into rotation in the direction indicated by arrow “D” in FIG. 15. As the anvil assembly 18 rotates in relation to the shell assembly 18, the anvil splines 38 break through the respective shell splines 60 and are directed into the guide channels 61 positioned between the shell splines 60 of the shell assembly 20 (FIG. 16). The short edge 44a and a second surface area Ω of the left tapered surface 44 engage an adjacent shell spline 60a (FIG. 16) to prevent the anvil splines 38 from migrating into the adjacent shell splines.


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. A surgical stapling device comprising: an approximation assembly including an anvil retainer;a shell assembly including a staple cartridge and a shell housing, the shell housing having an inner housing portion defining a bore, a plurality of shell splines supported on the inner housing portion within the bore, each of the plurality of shell splines defining a guide channel with an adjacent one of the plurality of shell splines, the staple cartridge being supported on the shell housing; andan anvil assembly including an anvil shaft having at least one anvil spline and an anvil head having an anvil surface defining a plurality of staple deforming recesses, the at least one anvil spline defining a longitudinal axis, the anvil shaft being configured to releasably engage the anvil retainer and the anvil head being supported on a distal portion of the anvil shaft, wherein the at least one anvil spline includes first and second tapered surfaces that intersect at an apex that is offset to one side of the longitudinal axis, the first tapered surface having a surface area β and the second tapered surface having a surface area Ω that is different from surface area β.
  • 2. The surgical stapling device of claim 1, wherein β is at least 1.5 times greater than Ω.
  • 3. The surgical stapling device of claim 1, wherein β is at least 2 times greater than Ω.
  • 4. The surgical stapling device of claim 1, wherein the at least one anvil spline is formed from metal and the plurality of shell splines is formed from a polymer.
  • 5. The surgical stapling device of claim 1, wherein each of the plurality of shell splines defines a longitudinal axis and includes first and second tapered cam surfaces, the first and second tapered cam surfaces of each of the plurality of shell splines intersecting at an apex.
  • 6. The surgical stapling device of claim 5, wherein the apex of each of the plurality of shell splines is aligned with the longitudinal axis of the shell spline.
  • 7. The surgical stapling device of claim 6, wherein the first cam surface of each of the plurality of shell splines has a surface area that is equal to a surface area of the second cam surface of each of the plurality of shell splines.
  • 8. The surgical stapling device of claim 1, wherein at least one the anvil spline is formed to migrate into a respective shell spline of the plurality of the shell splines when the apex of the at least one anvil spline engages the apex of a respective one of the plurality of shell splines.
  • 9. An anvil assembly for a circular stapling device comprising: an anvil shaft having at least one anvil spline and an anvil head having an anvil surface defining a plurality of staple deforming recesses, the at least one anvil spline defining a longitudinal axis, the anvil head being supported on a distal portion of the anvil shaft, wherein the at least one anvil spline includes first and second tapered surfaces that intersect at an apex that is offset to one side of the longitudinal axis, the first tapered surface having a surface area β and the second tapered surface having a surface area Ω that is different from surface area β.
  • 10. The anvil assembly of claim 9, wherein β is at least 1.5 times greater than Ω.
  • 11. The anvil assembly of claim 9, wherein β is at least 2 times greater than Ω.
  • 12. The anvil assembly of claim 9, wherein the at least one anvil spline is formed from metal.
  • 13. A tool assembly comprising: a shell assembly including a staple cartridge and a shell housing, the shell housing having an inner housing portion defining a bore, a plurality of shell splines supported on the inner housing portion within the bore, each of the plurality of shell splines defining a guide channel with an adjacent one of the plurality of shell splines, the staple cartridge being supported on the shell housing; andan anvil assembly including an anvil shaft having at least one anvil spline and an anvil head having an anvil surface defining a plurality of staple deforming recesses, the at least one anvil spline defining a longitudinal axis, the anvil head being supported on a distal portion of the anvil shaft, wherein the at least one anvil spline includes first and second tapered surfaces that intersect at an apex that is offset to one side of the longitudinal axis, the first tapered surface having a surface area β and the second tapered surface having a surface area Ω that is different from surface area β.
  • 14. The surgical stapling device of claim 13, wherein β is at least 1.5 times greater than Ω.
  • 15. The surgical stapling device of claim 14, wherein β is at least 2 times greater than Ω.
  • 16. The surgical stapling device of claim 13, wherein the at least one anvil spline is formed from metal and the plurality of shell splines is formed from a polymer.
  • 17. The surgical stapling device of claim 13, wherein each of the plurality of shell splines defines a longitudinal axis and includes first and second tapered cam surfaces, the first and second tapered cam surfaces of each of the plurality of shell splines intersecting at an apex.
  • 18. The surgical stapling device of claim 17, wherein the apex of each of the plurality of shell splines is aligned with the longitudinal axis of the shell spline.
  • 19. The surgical stapling device of claim 18, wherein the first cam surface of each of the plurality of shell splines has a surface area that is equal to a surface area of the second cam surface of each of the plurality of shell splines.
  • 20. The surgical stapling device of claim 13, wherein at least one the anvil spline is formed to migrate into a respective shell spline of the plurality of the shell splines when the apex of the at least one anvil spline engages the apex of a respective one of the plurality of shell splines.
CROSS-REFERENCE TO RELATED APPLICATIONS

This application claims the benefit of and priority to U.S. Provisional Patent Application Ser. No. 62/549,266 filed Aug. 23, 2017, the entire disclosure of which is incorporated by reference herein.

US Referenced Citations (499)
Number Name Date Kind
3193165 Akhalaya et al. Jul 1965 A
3388847 Kasulin et al. Jun 1968 A
3552626 Astafiev et al. Jan 1971 A
3638652 Kelley Feb 1972 A
3771526 Rudie Nov 1973 A
4198982 Fortner et al. Apr 1980 A
4207898 Becht Jun 1980 A
4289133 Rothfuss Sep 1981 A
4304236 Conta et al. Dec 1981 A
4319576 Rothfuss Mar 1982 A
4350160 Kolesov et al. Sep 1982 A
4351466 Noiles Sep 1982 A
4379457 Gravener et al. Apr 1983 A
4473077 Noiles et al. Sep 1984 A
4476863 Kanshin et al. Oct 1984 A
4485817 Swiggett Dec 1984 A
4488523 Shichman Dec 1984 A
4505272 Utyamyshev et al. Mar 1985 A
4505414 Filipi Mar 1985 A
4520817 Green Jun 1985 A
4550870 Krumme et al. Nov 1985 A
4573468 Conta et al. Mar 1986 A
4576167 Noiles Mar 1986 A
4592354 Rothfuss Jun 1986 A
4603693 Conta et al. Aug 1986 A
4606343 Conta et al. Aug 1986 A
4632290 Green et al. Dec 1986 A
4646745 Noiles Mar 1987 A
4665917 Clanton et al. May 1987 A
4667673 Li May 1987 A
4671445 Barker et al. Jun 1987 A
4700703 Resnick et al. Oct 1987 A
4703887 Clanton et al. Nov 1987 A
4708141 Inoue et al. Nov 1987 A
4717063 Ebihara Jan 1988 A
4752024 Green et al. Jun 1988 A
4754909 Barker et al. Jul 1988 A
4776506 Green Oct 1988 A
4817847 Redtenbacher et al. Apr 1989 A
4873977 Avant et al. Oct 1989 A
4893662 Gervasi Jan 1990 A
4903697 Resnick et al. Feb 1990 A
4907591 Vasconcellos et al. Mar 1990 A
4917114 Green et al. Apr 1990 A
4957499 Lipatov et al. Sep 1990 A
4962877 Hervas Oct 1990 A
5005749 Aranyi Apr 1991 A
5042707 Taheri Aug 1991 A
5047039 Avant et al. Sep 1991 A
5104025 Main et al. Apr 1992 A
5119983 Green et al. Jun 1992 A
5122156 Granger et al. Jun 1992 A
5139513 Segato Aug 1992 A
5158222 Green et al. Oct 1992 A
5188638 Tzakis Feb 1993 A
5193731 Aranyi Mar 1993 A
5197648 Gingold Mar 1993 A
5197649 Bessler et al. Mar 1993 A
5205459 Brinkerhoff et al. Apr 1993 A
5221036 Takase Jun 1993 A
5222963 Brinkerhoff et al. Jun 1993 A
5253793 Green et al. Oct 1993 A
5261920 Main et al. Nov 1993 A
5271543 Grant et al. Dec 1993 A
5271544 Fox et al. Dec 1993 A
5275322 Brinkerhoff et al. Jan 1994 A
5282810 Allen et al. Feb 1994 A
5285944 Green et al. Feb 1994 A
5285945 Brinkerhoff et al. Feb 1994 A
5292053 Bilotti et al. Mar 1994 A
5309927 Welch May 1994 A
5312024 Grant et al. May 1994 A
5314435 Green et al. May 1994 A
5314436 Wilk May 1994 A
5330486 Wilk Jul 1994 A
5333773 Main Aug 1994 A
5344059 Green et al. Sep 1994 A
5346115 Perouse et al. Sep 1994 A
5348259 Blanco et al. Sep 1994 A
5350104 Main et al. Sep 1994 A
5355897 Pietrafitta et al. Oct 1994 A
5360154 Green Nov 1994 A
5368215 Green et al. Nov 1994 A
5392979 Green et al. Feb 1995 A
5395030 Kuramoto et al. Mar 1995 A
5403333 Kaster et al. Apr 1995 A
5404870 Brinkerhoff et al. Apr 1995 A
5411508 Bessler et al. May 1995 A
5425738 Gustafson et al. Jun 1995 A
5433721 Hooven et al. Jul 1995 A
5437684 Calabrese et al. Aug 1995 A
5439156 Grant et al. Aug 1995 A
5443198 Viola et al. Aug 1995 A
5447514 Gerry et al. Sep 1995 A
5454825 Van Leeuwen et al. Oct 1995 A
5464415 Chen Nov 1995 A
5470006 Rodak Nov 1995 A
5474223 Viola et al. Dec 1995 A
5497934 Brady et al. Mar 1996 A
5503635 Sauer et al. Apr 1996 A
5522534 Viola et al. Jun 1996 A
5533661 Main et al. Jul 1996 A
5588579 Schnut et al. Dec 1996 A
5609285 Grant et al. Mar 1997 A
5626591 Kockerling et al. May 1997 A
5632433 Grant et al. May 1997 A
5639008 Gallagher et al. Jun 1997 A
5641111 Ahrens et al. Jun 1997 A
5658300 Bito et al. Aug 1997 A
5669918 Balazs et al. Sep 1997 A
5685474 Seeber Nov 1997 A
5709335 Heck Jan 1998 A
5715987 Kelley et al. Feb 1998 A
5718360 Green et al. Feb 1998 A
5720755 Dakov Feb 1998 A
5732872 Bolduc et al. Mar 1998 A
5749896 Cook May 1998 A
5758814 Gallagher et al. Jun 1998 A
5799857 Robertson et al. Sep 1998 A
5814055 Knodel et al. Sep 1998 A
5833698 Hinchliffe et al. Nov 1998 A
5836503 Ehrenfels et al. Nov 1998 A
5839639 Sauer et al. Nov 1998 A
5855312 Toledano Jan 1999 A
5860581 Robertson et al. Jan 1999 A
5868760 McGuckin, Jr. Feb 1999 A
5881943 Heck Mar 1999 A
5915616 Viola et al. Jun 1999 A
5947363 Bolduc et al. Sep 1999 A
5951576 Wakabayashi Sep 1999 A
5957363 Heck Sep 1999 A
5993468 Rygaard Nov 1999 A
6024748 Manzo et al. Feb 2000 A
6050472 Shibata Apr 2000 A
6053390 Green et al. Apr 2000 A
6068636 Chen May 2000 A
6083241 Longo et al. Jul 2000 A
6102271 Longo et al. Aug 2000 A
6117148 Ravo et al. Sep 2000 A
6119913 Adams et al. Sep 2000 A
6126058 Adams et al. Oct 2000 A
6142933 Longo et al. Nov 2000 A
6149667 Hovland et al. Nov 2000 A
6176413 Heck et al. Jan 2001 B1
6179195 Adams et al. Jan 2001 B1
6193129 Bittner et al. Feb 2001 B1
6203553 Robertson et al. Mar 2001 B1
6209773 Bolduc et al. Apr 2001 B1
6241140 Adams et al. Jun 2001 B1
6253984 Heck et al. Jul 2001 B1
6258107 Balazs et al. Jul 2001 B1
6264086 McGuckin, Jr. Jul 2001 B1
6269997 Balazs et al. Aug 2001 B1
6273897 Dalessandro et al. Aug 2001 B1
6279809 Nicolo Aug 2001 B1
6302311 Adams et al. Oct 2001 B1
6338737 Toledano Jan 2002 B1
6343731 Adams et al. Feb 2002 B1
6387105 Gifford, III et al. May 2002 B1
6398795 McAlister et al. Jun 2002 B1
6402008 Lucas Jun 2002 B1
6439446 Perry et al. Aug 2002 B1
6443973 Whitman Sep 2002 B1
6450390 Heck et al. Sep 2002 B2
6478210 Adams et al. Nov 2002 B2
6488197 Whitman Dec 2002 B1
6491201 Whitman Dec 2002 B1
6494877 Odell et al. Dec 2002 B2
6503259 Huxel et al. Jan 2003 B2
6517566 Hovland et al. Feb 2003 B1
6520398 Nicolo Feb 2003 B2
6533157 Whitman Mar 2003 B1
6551334 Blatter et al. Apr 2003 B2
6578751 Hartwick Jun 2003 B2
6585144 Adams et al. Jul 2003 B2
6588643 Bolduc et al. Jul 2003 B2
6592596 Geitz Jul 2003 B1
6601749 Sullivan et al. Aug 2003 B2
6605078 Adams Aug 2003 B2
6605098 Nobis et al. Aug 2003 B2
6626921 Blatter et al. Sep 2003 B2
6629630 Adams Oct 2003 B2
6631837 Heck Oct 2003 B1
6632227 Adams Oct 2003 B2
6632237 Ben-David et al. Oct 2003 B2
6652542 Blatter et al. Nov 2003 B2
6659327 Heck et al. Dec 2003 B2
6676671 Robertson et al. Jan 2004 B2
6681979 Whitman Jan 2004 B2
6685079 Sharma et al. Feb 2004 B2
6695198 Adams et al. Feb 2004 B2
6695199 Whitman Feb 2004 B2
6698643 Whitman Mar 2004 B2
6716222 McAlister et al. Apr 2004 B2
6716233 Whitman Apr 2004 B1
6726697 Nicholas et al. Apr 2004 B2
6742692 Hartwick Jun 2004 B2
6743244 Blatter et al. Jun 2004 B2
6763993 Bolduc et al. Jul 2004 B2
6769590 Vresh et al. Aug 2004 B2
6769594 Orban, III Aug 2004 B2
6820791 Adams Nov 2004 B2
6821282 Perry et al. Nov 2004 B2
6827246 Sullivan et al. Dec 2004 B2
6840423 Adams et al. Jan 2005 B2
6843403 Whitman Jan 2005 B2
6846308 Whitman et al. Jan 2005 B2
6852122 Rush Feb 2005 B2
6866178 Adams et al. Mar 2005 B2
6872214 Sonnenschein et al. Mar 2005 B2
6874669 Adams et al. Apr 2005 B2
6884250 Monassevitch et al. Apr 2005 B2
6905504 Vargas Jun 2005 B1
6938814 Sharma et al. Sep 2005 B2
6942675 Vargas Sep 2005 B1
6945444 Gresham et al. Sep 2005 B2
6953138 Dworak et al. Oct 2005 B1
6957758 Aranyi Oct 2005 B2
6959851 Heinrich Nov 2005 B2
6978922 Bilotti et al. Dec 2005 B2
6981941 Whitman et al. Jan 2006 B2
6981979 Nicolo Jan 2006 B2
7032798 Whitman et al. Apr 2006 B2
7059331 Adams et al. Jun 2006 B2
7059510 Orban, III Jun 2006 B2
7077856 Whitman Jul 2006 B2
7080769 Vresh et al. Jul 2006 B2
7086267 Dworak et al. Aug 2006 B2
7114642 Whitman Oct 2006 B2
7118528 Piskun Oct 2006 B1
7122044 Bolduc et al. Oct 2006 B2
7128748 Mooradian et al. Oct 2006 B2
7141055 Abrams et al. Nov 2006 B2
7168604 Milliman et al. Jan 2007 B2
7179267 Nolan et al. Feb 2007 B2
7182239 Myers Feb 2007 B1
7195142 Orban, III Mar 2007 B2
7207168 Doepker et al. Apr 2007 B2
7220237 Gannoe et al. May 2007 B2
7234624 Gresham et al. Jun 2007 B2
7235089 McGuckin, Jr. Jun 2007 B1
RE39841 Bilotti et al. Sep 2007 E
7285125 Viola Oct 2007 B2
7303106 Milliman et al. Dec 2007 B2
7303107 Milliman et al. Dec 2007 B2
7309341 Ortiz et al. Dec 2007 B2
7322994 Nicholas et al. Jan 2008 B2
7325713 Aranyi Feb 2008 B2
7334718 McAlister et al. Feb 2008 B2
7335212 Edoga et al. Feb 2008 B2
7364060 Milliman Apr 2008 B2
7398908 Holsten et al. Jul 2008 B2
7399305 Csiky et al. Jul 2008 B2
7401721 Holsten et al. Jul 2008 B2
7401722 Hur Jul 2008 B2
7407075 Holsten et al. Aug 2008 B2
7410086 Ortiz et al. Aug 2008 B2
7422137 Manzo Sep 2008 B2
7422138 Bilotti et al. Sep 2008 B2
7431191 Milliman Oct 2008 B2
7438718 Milliman et al. Oct 2008 B2
7455676 Holsten et al. Nov 2008 B2
7455682 Viola Nov 2008 B2
7481347 Roy Jan 2009 B2
7494038 Milliman Feb 2009 B2
7506791 Omaits et al. Mar 2009 B2
7516877 Aranyi Apr 2009 B2
7527185 Harari et al. May 2009 B2
7537602 Whitman May 2009 B2
7540839 Butler et al. Jun 2009 B2
7546939 Adams et al. Jun 2009 B2
7546940 Milliman et al. Jun 2009 B2
7547312 Bauman et al. Jun 2009 B2
7556186 Milliman Jul 2009 B2
7559451 Sharma et al. Jul 2009 B2
7585306 Abbott et al. Sep 2009 B2
7588174 Holsten et al. Sep 2009 B2
7600663 Green Oct 2009 B2
7611038 Racenet et al. Nov 2009 B2
7635385 Milliman et al. Dec 2009 B2
7669747 Weisenburgh, II et al. Mar 2010 B2
7686201 Csiky Mar 2010 B2
7694864 Okada et al. Apr 2010 B2
7699204 Viola Apr 2010 B2
7708181 Cole et al. May 2010 B2
7717313 Criscuolo et al. May 2010 B2
7721932 Cole et al. May 2010 B2
7726539 Holsten et al. Jun 2010 B2
7743958 Orban, III Jun 2010 B2
7744627 Orban, III et al. Jun 2010 B2
7770776 Chen et al. Aug 2010 B2
7771440 Ortiz et al. Aug 2010 B2
7776060 Mooradian et al. Aug 2010 B2
7793813 Bettuchi Sep 2010 B2
7802712 Milliman et al. Sep 2010 B2
7823592 Bettuchi et al. Nov 2010 B2
7837079 Holsten et al. Nov 2010 B2
7837080 Schwemberger Nov 2010 B2
7837081 Holsten et al. Nov 2010 B2
7845536 Viola et al. Dec 2010 B2
7845538 Whitman Dec 2010 B2
7857187 Milliman Dec 2010 B2
7886951 Hessler Feb 2011 B2
7896215 Adams et al. Mar 2011 B2
7900806 Chen et al. Mar 2011 B2
7909039 Hur Mar 2011 B2
7909219 Cole et al. Mar 2011 B2
7909222 Cole et al. Mar 2011 B2
7909223 Cole et al. Mar 2011 B2
7913892 Cole et al. Mar 2011 B2
7918377 Measamer et al. Apr 2011 B2
7922062 Cole et al. Apr 2011 B2
7922743 Heinrich et al. Apr 2011 B2
7931183 Orban, III Apr 2011 B2
7938307 Bettuchi May 2011 B2
7942302 Roby et al. May 2011 B2
7951166 Orban, III et al. May 2011 B2
7959050 Smith et al. Jun 2011 B2
7967181 Viola et al. Jun 2011 B2
7975895 Milliman Jul 2011 B2
8002795 Beetel Aug 2011 B2
8006701 Bilotti et al. Aug 2011 B2
8006889 Adams et al. Aug 2011 B2
8011551 Marczyk et al. Sep 2011 B2
8011554 Milliman Sep 2011 B2
8016177 Bettuchi et al. Sep 2011 B2
8016858 Whitman Sep 2011 B2
8020741 Cole et al. Sep 2011 B2
8025199 Whitman et al. Sep 2011 B2
8028885 Smith et al. Oct 2011 B2
8038046 Smith et al. Oct 2011 B2
8043207 Adams Oct 2011 B2
8066167 Measamer et al. Nov 2011 B2
8066169 Viola Nov 2011 B2
8070035 Holsten et al. Dec 2011 B2
8070037 Csiky Dec 2011 B2
8096458 Hessler Jan 2012 B2
8109426 Milliman et al. Feb 2012 B2
8109427 Orban, III Feb 2012 B2
8113405 Milliman Feb 2012 B2
8113406 Holsten et al. Feb 2012 B2
8113407 Holsten et al. Feb 2012 B2
8123103 Milliman Feb 2012 B2
8128645 Sonnenschein et al. Mar 2012 B2
8132703 Milliman et al. Mar 2012 B2
8136712 Zingman Mar 2012 B2
8146790 Milliman Apr 2012 B2
8146791 Bettuchi et al. Apr 2012 B2
8181838 Milliman et al. May 2012 B2
8192460 Orban, III et al. Jun 2012 B2
8201720 Hessler Jun 2012 B2
8203782 Brueck et al. Jun 2012 B2
8211130 Viola Jul 2012 B2
8225799 Bettuchi Jul 2012 B2
8225981 Criscuolo et al. Jul 2012 B2
8231041 Marczyk et al. Jul 2012 B2
8231042 Hessler et al. Jul 2012 B2
8257391 Orban, III et al. Sep 2012 B2
8267301 Milliman et al. Sep 2012 B2
8272552 Holsten et al. Sep 2012 B2
8276802 Kostrzewski Oct 2012 B2
8281975 Criscuolo et al. Oct 2012 B2
8286845 Perry et al. Oct 2012 B2
8308045 Bettuchi et al. Nov 2012 B2
8312885 Bettuchi et al. Nov 2012 B2
8313014 Bettuchi Nov 2012 B2
8317073 Milliman et al. Nov 2012 B2
8317074 Ortiz et al. Nov 2012 B2
8322590 Patel et al. Dec 2012 B2
8328060 Jankowski et al. Dec 2012 B2
8328062 Viola Dec 2012 B2
8328063 Milliman et al. Dec 2012 B2
8343185 Milliman et al. Jan 2013 B2
8353438 Baxter, III et al. Jan 2013 B2
8353439 Baxter, III et al. Jan 2013 B2
8353930 Heinrich et al. Jan 2013 B2
8360295 Milliman et al. Jan 2013 B2
8365974 Milliman Feb 2013 B2
8403942 Milliman et al. Mar 2013 B2
8408441 Wenchell et al. Apr 2013 B2
8413870 Pastorelli et al. Apr 2013 B2
8413872 Patel Apr 2013 B2
8418905 Milliman Apr 2013 B2
8418909 Kostrzewski Apr 2013 B2
8424535 Hessler et al. Apr 2013 B2
8424741 McGuckin, Jr. et al. Apr 2013 B2
8430291 Heinrich et al. Apr 2013 B2
8430292 Patel et al. Apr 2013 B2
8453910 Bettuchi et al. Jun 2013 B2
8453911 Milliman et al. Jun 2013 B2
8485414 Criscuolo et al. Jul 2013 B2
8490853 Criscuolo et al. Jul 2013 B2
8511533 Viola et al. Aug 2013 B2
8551138 Orban, III et al. Oct 2013 B2
8567655 Nalagatla et al. Oct 2013 B2
8579178 Holsten et al. Nov 2013 B2
8590763 Milliman Nov 2013 B2
8590764 Hartwick et al. Nov 2013 B2
8608047 Holsten et al. Dec 2013 B2
8616428 Milliman et al. Dec 2013 B2
8616429 Viola Dec 2013 B2
8622275 Baxter, III et al. Jan 2014 B2
8631993 Kostrzewski Jan 2014 B2
8636187 Hueil et al. Jan 2014 B2
8640940 Ohdaira Feb 2014 B2
8662370 Takei Mar 2014 B2
8663258 Bettuchi et al. Mar 2014 B2
8672931 Goldboss et al. Mar 2014 B2
8678264 Racenet et al. Mar 2014 B2
8684248 Milliman Apr 2014 B2
8684250 Bettuchi et al. Apr 2014 B2
8684251 Rebuffat et al. Apr 2014 B2
8684252 Patel et al. Apr 2014 B2
8733611 Milliman May 2014 B2
20030111507 Nunez Jun 2003 A1
20040073090 Butler et al. Apr 2004 A1
20050051597 Toledano Mar 2005 A1
20050107813 Gilete Garcia May 2005 A1
20060000869 Fontayne Jan 2006 A1
20060011698 Okada et al. Jan 2006 A1
20060201989 Ojeda Sep 2006 A1
20070027473 Vresh et al. Feb 2007 A1
20070029363 Popov Feb 2007 A1
20070060952 Roby et al. Mar 2007 A1
20090236392 Cole et al. Sep 2009 A1
20090236398 Cole et al. Sep 2009 A1
20090236401 Cole et al. Sep 2009 A1
20100019016 Edoga et al. Jan 2010 A1
20100051668 Milliman et al. Mar 2010 A1
20100084453 Hu Apr 2010 A1
20100147923 D'Agostino et al. Jun 2010 A1
20100163598 Belzer Jul 2010 A1
20100224668 Fontayne et al. Sep 2010 A1
20100230465 Smith et al. Sep 2010 A1
20100258611 Smith et al. Oct 2010 A1
20100264195 Bettuchi Oct 2010 A1
20100327041 Milliman et al. Dec 2010 A1
20110011916 Levine Jan 2011 A1
20110114697 Baxter, III et al. May 2011 A1
20110114700 Baxter, III et al. May 2011 A1
20110144640 Heinrich et al. Jun 2011 A1
20110147432 Heinrich et al. Jun 2011 A1
20110192882 Hess et al. Aug 2011 A1
20120145755 Kahn Jun 2012 A1
20120193395 Pastorelli et al. Aug 2012 A1
20120193398 Williams et al. Aug 2012 A1
20120232339 Csiky Sep 2012 A1
20120273548 Ma et al. Nov 2012 A1
20120325888 Qiao et al. Dec 2012 A1
20130015232 Smith et al. Jan 2013 A1
20130020372 Jankowski et al. Jan 2013 A1
20130020373 Smith et al. Jan 2013 A1
20130032628 Li et al. Feb 2013 A1
20130056516 Viola Mar 2013 A1
20130060258 Giacomantonio Mar 2013 A1
20130105544 Mozdzierz et al. May 2013 A1
20130105546 Milliman et al. May 2013 A1
20130105551 Zingman May 2013 A1
20130126580 Smith et al. May 2013 A1
20130153630 Miller et al. Jun 2013 A1
20130153631 Vasudevan et al. Jun 2013 A1
20130153633 Casasanta, Jr. et al. Jun 2013 A1
20130153634 Carter et al. Jun 2013 A1
20130153638 Carter et al. Jun 2013 A1
20130153639 Hodgkinson et al. Jun 2013 A1
20130175315 Milliman Jul 2013 A1
20130175318 Felder et al. Jul 2013 A1
20130175319 Felder et al. Jul 2013 A1
20130175320 Mandakolathur Vasudevan et al. Jul 2013 A1
20130181035 Milliman Jul 2013 A1
20130181036 Olson et al. Jul 2013 A1
20130186930 Wenchell et al. Jul 2013 A1
20130193185 Patel Aug 2013 A1
20130193187 Milliman Aug 2013 A1
20130193190 Carter et al. Aug 2013 A1
20130193191 Stevenson et al. Aug 2013 A1
20130193192 Casasanta, Jr. et al. Aug 2013 A1
20130200131 Racenet et al. Aug 2013 A1
20130206816 Penna Aug 2013 A1
20130214027 Hessler et al. Aug 2013 A1
20130214028 Patel et al. Aug 2013 A1
20130228609 Kostrzewski Sep 2013 A1
20130240597 Milliman et al. Sep 2013 A1
20130240600 Bettuchi Sep 2013 A1
20130248581 Smith et al. Sep 2013 A1
20130277411 Hodgkinson et al. Oct 2013 A1
20130277412 Gresham et al. Oct 2013 A1
20130284792 Ma Oct 2013 A1
20130292449 Bettuchi et al. Nov 2013 A1
20130299553 Mozdzierz Nov 2013 A1
20130299554 Mozdzierz Nov 2013 A1
20130306701 Olson Nov 2013 A1
20130306707 Viola et al. Nov 2013 A1
20140008413 Williams Jan 2014 A1
20140012317 Orban et al. Jan 2014 A1
20160143641 Sapienza et al. May 2016 A1
20160157856 Williams et al. Jun 2016 A1
20160174988 D'Agostino et al. Jun 2016 A1
20160302792 Motai Oct 2016 A1
Foreign Referenced Citations (33)
Number Date Country
908529 Aug 1972 CA
2805365 Aug 2013 CA
1057729 May 1959 DE
3301713 Jul 1984 DE
0152382 Aug 1985 EP
0173451 Mar 1986 EP
0190022 Aug 1986 EP
0282157 Sep 1988 EP
0503689 Sep 1992 EP
1354560 Oct 2003 EP
2138118 Dec 2009 EP
2168510 Mar 2010 EP
2238926 Oct 2010 EP
2524656 Nov 2012 EP
3108825 Dec 2016 EP
3366234 Aug 2018 EP
1136020 May 1957 FR
1461464 Feb 1966 FR
1588250 Apr 1970 FR
2443239 Jul 1980 FR
1185292 Mar 1970 GB
2016991 Sep 1979 GB
2070499 Sep 1981 GB
2004147969 May 2004 JP
2013138860 Jul 2013 JP
7711347 Apr 1979 NL
1509052 Sep 1989 SU
8706448 Nov 1987 WO
8900406 Jan 1989 WO
9006085 Jun 1990 WO
9835614 Aug 1998 WO
0154594 Aug 2001 WO
2008107918 Sep 2008 WO
Non-Patent Literature Citations (1)
Entry
European Search Report dated Jan. 30, 2019, issued in EP Appln. No. 18190300.
Related Publications (1)
Number Date Country
20190059901 A1 Feb 2019 US
Provisional Applications (1)
Number Date Country
62549266 Aug 2017 US