Trocar seal system

Abstract
A seal assembly for reception of an elongated surgical instrument is provided which includes a body having at least one opening configured and dimensioned to permit entry of an elongated surgical instrument and defining a central longitudinal axis; a seal member formed of a resilient material and defining an aperture therein, the aperture being configured and dimensioned such that insertion of the surgical instrument into the aperture causes the resilient material defining the aperture to resiliently contact the outer surface of the surgical instrument in a substantially fluid tight manner; and a fabric layer juxtaposed relative to the resilient material. A coating may be applied to the seal member to reduce friction between the seal member and surgical instrumentation inserted therein. The coating is preferably a hydrocyclosiloxane membrane prepared by plasma polymerization process.
Description




BACKGROUND




1. Technical Field




The present disclosure relates to seal systems of the type adapted to allow the introduction of a surgical instrument into a patient's body. In particular, the disclosure relates to a seal system to be used in combination with a cannula assembly where the cannula assembly is intended for insertion into a patient's body and an instrument is inserted into the patient's body through the cannula.




2. Background of Related Art




Laparoscopic procedures are performed in the interior of the abdomen through a small incision, e.g., through narrow endoscopic tubes or cannulas inserted through a small entrance incision in the skin. Minimally invasive procedures are performed elsewhere in the body, e.g., in the chest, and are often generally referred to as “endoscopic” procedures. Minimally invasive or endoscopic procedures generally require that any instrumentation inserted into the body be sealed, i.e. provisions must be made to ensure that gases do not enter or exit the body through the endoscopic incision as, for example, in surgical procedures in which the surgical region is insufflated. Moreover, endoscopic procedures often require the surgeon to act on organs, tissues, and vessels far removed from the incision, thereby requiring that any instruments used in such procedures be relatively long and narrow.




For such procedures, the introduction of a tube into certain anatomical cavities such as the abdominal cavity is usually accomplished by use of a system incorporating a trocar and cannula assembly. A cannula assembly is formed of a cannula attached to a cannula housing which generally includes seal assembly adapted to maintain a seal across the opening of the seal assembly both with and without an instrument inserted therethrough. Since the cannula is in direct communication with the internal portion of the seal assembly, insertion of the cannula into an opening in the patient's body so as to reach the inner abdominal cavity should be adapted to maintain a fluid tight interface between the abdominal cavity and the outside atmosphere.




Since minimally invasive surgical procedures in the abdominal cavity of the body generally require insufflating gases to raise the cavity wall away from vital organs, the procedure is usually initiated by use of a Verres needle through which a gas is introduced into the body cavity. The gas provides a slight pressure which raises the wall surface of the peritoneum away from the vital organs thereby providing an adequate region in which to operate. Thereafter, a trocar assembly which includes a cannula and a trocar or obturator is inserted within the cannula to puncture the peritoneum, i.e. the inner lining of the abdominal cavity wall. The obturator is removed and laparoscopic or endoscopic surgical instruments may then be inserted through the cannula to perform surgery within the abdominal cavity. The cannula may also be utilized for introducing tubes into the body as for drainage purposes, for specimen removal, for diagnostic evaluations, or the like.




In view of the need to maintain the atmospheric integrity of the inner area of the cavity, a seal assembly for a cannula which permits introduction of an obturator and a wide range of surgical instruments and which maintains the atmospheric integrity of the inner area of the cavity is desirable. Generally, in the context of insufflatory, minimally invasive surgical procedures, cannula assemblies include structure(s) that satisfy two sealing requirements. The first requirement is to provide a substantially fluid tight seal when an instrument is not present in the cannula. The second requirement is to provide a substantially fluid tight seal when an instrument is being introduced into or already is present in the cannula. In this regard, there have been a number of attempts in the prior art to provide such sealing requirements.




U.S. Pat. No. 4,655,752 to Honkanen et al. teaches a cannula including a housing and first and second seal members. The first seal member is conically tapered toward the bottom of the housing and has a circular opening in its center, while the second seal is conically tapered and cup shaped. The second seal includes at least one slit to allow for the passage of instruments.




U.S. Pat. No. 4,929,235 to Merry et al. teaches a self-sealing catheter introducer having a sealing mechanism to prevent blood or fluid leakage. The sealing mechanism includes a planar sealing element having a slit and a conical sealing element. The sealing elements are each adapted to surround a tube.




U.S. Pat. Nos. 4,874,377 and 5,064,416 to Newgard et al. relate to a self-occluding intravascular cannula assembly in which an elastomeric valving member is positioned transversely to a housing and is peripherally compressed to cause displacement, distortion and/or rheological flow of the elastomeric material. A frustoconical dilator projection cooperates with the elastomeric valving member in moving the valving member to a non-occluding position.




U.S. Pat. No. 5,300,033 to Miller suggests a valve construction including an elastic body having a cylindrical wall with first and second walls formed integrally with the cylindrical wall. The second wall includes a slit to permit passage of a surgical instrument and first and second leaflets which define the slit. The leaflets are thicker in cross section to provide an additional closing force at the slit.




A disadvantage of several known seal systems for cannulas concerns the difficulty encountered in inserting and advancing the surgical instrument through the seal unit. In particular, since known elastomeric seal members are designed to form and maintain a fluid tight seal about the instrument, the aperture or slit within the seal through which the instrument is passed is of relatively small or narrow dimension. Further, portions of the seal member defining the aperture are generally thick in cross-section to provide a sufficient closing force of the seal about the instrument. see, e.g., U.S. Pat. No. 5,300,033. As a consequence of these design considerations, the level of force needed to insert and advance the instrument through the seal aperture is increased, thereby requiring awkward maneuvering on the surgeon's behalf to appropriately position the instrument for the desired surgery. Moreover, known seal systems are generally ineffectual in accommodating instruments of differing diameter while maintaining acceptable insertion forces and facilitating the range of desired surgical manipulations, e.g., angular instrument movements and specimen removal.




Accordingly, the present disclosure obviates the disadvantages of the prior art by providing a seal unit or assembly for a cannula assembly, which is capable of forming and maintaining a tight seal about instruments of varying diameters inserted through the cannula and which incorporates structure to enhance and facilitate passage of the instrument through the seal unit.




SUMMARY




The present disclosure provides a seal assembly for reception of an elongated surgical instrument, which comprises a body having at least one opening configured and dimensioned to permit entry of an elongated surgical instrument and defining a central longitudinal axis; a seal member formed of a resilient material and defining an aperture therein, the aperture being configured and dimensioned such that insertion of the surgical instrument into the aperture causes the resilient material defining the aperture to resiliently contact the outer surface of the surgical instrument in a substantially fluid tight manner; and a fabric layer juxtaposed relative to the resilient material.




The seal assembly may further include a coating applied to the seal member to reduce friction between the seal member and surgical instrumentation inserted therein. The coating is preferably a hydrocyclosiloxane membrane prepared by plasma polymerization process.




In one aspect of the presently disclosed seal assembly a ring member is secured to the seal member and includes a dampening element disposed between a surface of the ring member and a surface of the body.











BRIEF DESCRIPTION OF THE DRAWINGS




Various embodiments are described herein below with reference to the drawings wherein:





FIG. 1

is a perspective view of one embodiment of a seal assembly constructed in accordance with the present disclosure;





FIG. 2

is a perspective view with parts separated showing the various structural components of the seal assembly embodiment of

FIG. 1

;





FIG. 3

is a perspective view of a fabric portion for incorporation into the seal element of the embodiment of

FIG. 1

;





FIG. 4

is a cross-sectional view taken along section line


4





4


of

FIG. 3

;





FIG. 5

is a perspective view of a fully formed seal member for the seal assembly of

FIG. 1

;





FIG. 6

is a cross-sectional view taken along section line


6





6


of

FIG. 5

;





FIG. 6A

is an alternative embodiment of the seal element of

FIG. 6

;





FIG. 7

is a cross-sectional view of the seal assembly of

FIG. 1

;





FIG. 8

is a perspective view of a trocar assembly having the seal assembly of

FIG. 1

removably installed thereon;





FIG. 9

is a partial cross-sectional view showing the seal body housing. taken along section line


9





9


of

FIG. 8

;





FIG. 10

is an alternative embodiment of the seal assembly of the present disclosure;





FIG. 11

is a cross-sectional view of a further embodiment of the seal assembly constructed in accordance with the present disclosure;





FIG. 12

is a perspective view of the seal assembly of

FIG. 11

;





FIG. 13

is a perspective view with parts separated of the seal assembly embodiment of

FIG. 11

;





FIG. 14

is a cross-sectional view of a further embodiment of the seal assembly constructed in accordance with the present disclosure; and





FIG. 15

is a perspective view of the seal member of the seal assembly of FIG.


14


.











DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS




Referring now in detail to the drawing figures in which like reference numerals identify similar or identical elements, a first embodiment of the seal assembly of the present disclosure is illustrated in

FIGS. 1-9

, and is designated generally as seal assembly


100


.




The presently disclosed seal assembly embodiments contemplate the introduction of various types of surgical instruments adapted for insertion through an elongated trocar assembly. Examples of such instruments include clip appliers, graspers, dissectors, retractors, staplers, laser fibers, photographic devices, endoscopes and laparoscopes, tubes, and the like. Such instruments are collectively referred to herein as “instruments”.




A two part ring assembly which includes ring members


120


and


122


are snap fitted together on either side of seal member


118


. Ring member


120


is disposed adjacent the distally facing surface of seal member


118


and ring member


122


is disposed on the proximally facing side of seal member


118


. Ring


120


is provided with holes


120




b


and posts


120




a


which are alternately disposed around the ring and are aligned with holes


118




a


on seal member


118


. Ring


122


is provided with posts


122




b


and holes


122




a


which mate with holes


120




a


and posts


120




b


of ring member


120


, respectively by snap fitting together thereby surrounding inner section


118




b


. Although rings


120


and


122


are shown having alternating holes and posts, one of the rings could have all holes formed therein while the other ring could have all posts aligned with the holes of the other ring. Additionally, greater or fewer holes and posts may be utilized to secure the two rings together.




A seal clamp


124


is provided within the housing component


114


and


116


and serves to secure the outer periphery of seal member


118


within seal assembly


100


(as best shown in FIG.


7


). Seal clamp


124


is provided with four projecting posts


124




a


which fit within openings (

FIG. 7

) formed on the proximal side of lower housing


116


. Seal clamp


124


also serves to secure a proximal flange of a lower seal


126


which is provided at the distal end of lower housing member


116


. Lower seal


126


assists in the securement of seal assembly


100


to cannula assembly


110


.




Referring now to

FIGS. 3-6

, seal member


118


includes a fabric disc-shaped portion


128


which is preferably disposed on both the proximal and distal sides of inner section


118




b


of seal member


118


. Alternatively, fabric section


128


may be disposed on just one of either the proximally facing surface or the distally facing surface of inner portion


118




b,


as desired. Fabric portion


128


may be of any suitable fabric, for example, a SPANDEX material containing 20% LYCRA available from Milliken.




In one method of forming the composite seal member


118


with fabric portion


128


a raw, i.e., uncured polyisoprene plug is first compressed into a flat state, e.g., a flat sheet of polyisoprene. A single layer of fabric is positioned on top of the flattened polyisoprene sheet and compressed into the uncured rubber by any suitable compression process such as, for example, calendering. If it is desired to have fabric on both sides of seal member


118


, this process is repeated on the other side of the polyisoprene sheet. The fabric polyisoprene composite is die cut into circular slugs having an outer diameter and an inner diameter which forms a central aperture. The slugs are placed in a hot compression mold to cure the polyisoprene. This step also serves to extrude the outer portions of seal member


118


which extend outwardly from inner section


118




b.






During the above-described process the bleed-through of the polyisoprene material into and/or through the fabric layers is regulated by the density of the fabric selected. A greater degree of bleed-through of polyisoprene provides greater resistance to fraying of the fabric upon repeated insertion of instruments through the seal. However, too much bleed-through of the polyisoprene through the fabric will increase friction forces upon instruments being inserted through seal member


118


.




Referring to

FIG. 6A

, an alternative embodiment of seal member


118


is shown as seal member


418


. Seal member


418


is the same as seal member


118


in most aspects except that inner section


418




b


is formed to have fabric layer


428


enveloped between upper and lower polyisoprene layers


418




c


and


418




d.






In order to reduce friction between instruments and the seal member, e.g. seal member


118


or seal member


418


, as instruments are inserted through seal assembly


100


, a coating may be applied to the seal member. One coating which has been found particularly effective is a hydrocyclosiloxane membrane prepared by plasma polymerization process. Such a coating is available from Innerdyne, Inc. of Salt Lake City, Utah, U.S.A., and is disclosed in U.S. Pat. No. 5,463,010 which issued to Hu et al. on Oct. 31, 1995, the entire contents of which are hereby incorporated by reference.




Referring to

FIGS. 7 and 8

, seal assembly


100


is used in combination with a conventional trocar assembly which includes a cannula assembly


110


and a trocar obturator


112


. Examples of trocar assemblies in which the present seal assembly may be utilized are disclosed in U.S. Pat. No. 5,603,702 which issued on Feb. 18, 1997 to Smith et al. and U.S. application Ser. No. 08/546,009 filed Oct. 20, 1995 by Smith et al., the entire contents of each of these disclosures are hereby incorporated by reference.




Seal assembly


100


, either alone or in combination with a seal unit/seal assembly internal to cannula assembly


110


, provides a substantial seal between a body cavity of a patient and the outside atmosphere both during and subsequent to insertion of an instrument through the cannula. In this manner, insufflation gases are prevented from escaping through the trocar assembly to the outside environment. Seal assembly


100


is capable of accommodating instruments of varying diameter, e.g., from about 5 mm to about 12 mm, while providing a fluid tight seal with the outer diameter of each instrument. The versatility of the presently disclosed seal assembly embodiments greatly facilitate endoscopic surgery, wherein a variety of instruments having different diameters are often needed during a single surgical procedure.




Seal assembly


100


is preferably detachably mountable to the proximal end of cannula assembly


110


. Thus, the surgeon can remove the seal assembly


100


from the cannula assembly


110


at any time during the surgical procedure and, similarly, mount the seal assembly


100


to the cannula when desired in order to provide a sealing engagement with an instrument to be inserted through the cannula. In addition, seal assembly


100


may be readily adapted for mounting to conventional cannulas of differing structures. The detachability of seal assembly


100


from cannula assembly


110


facilitates specimen removal through cannula assembly


110


. Seal assembly


100


includes a housing which is formed by the snap fitting together of end cap


114


and lower housing member


116


. Preferably the housing components of seal assembly


100


are formed of a polycarbonate material such as ABS available from the General Electric Company.





FIG. 9

shows an instrument having a shaft


130


inserted through seal assembly


100


and a duck bill valve or “zero” seal valve


132


which prevents the escape of insufflation gases in the absence of an instrument in the trocar assembly. As shown in

FIG. 9

, seal member


118


provides a seal about the periphery of shaft


130


.




Referring to

FIG. 10

, an alternate embodiment of seal assembly


100


is designated generally as seal assembly


150


. Seal assembly


150


is the same as seal assembly


100


except that an inner planar seal member


152


is disposed in the distal end of seal assembly


100


to provide additional sealing capability for instruments having larger diameters. Seal element


152


has an aperture


154


which has a diameter larger than the diameter of aperture


156


of seal member


118


. A further feature illustrated in

FIG. 10

is a dampening member such as pad


158


which is secured to the proximal surface of ring


122


to dampen the sound created by the impact of the proximal surface of ring


122


with the inner distal facing surface of housing component


114


. Other dampening member configurations are also contemplated. For example, ring


122


may be over-molded with material such as polyisoprene so as to envelope part or all of the ring thereby forming a bumper between the ring and the housing component.




Referring to

FIGS. 11-13

, a further embodiment of a seal assembly generally designated as seal assembly


200


is shown throughout the several views. Seal member


218


is configured in an hourglass shape and preferably includes the fabric portion


228


formed as part of seal member


218


in a similar manner as described above. The friction reducing coating of a hydrocyclosiloxane membrane prepared by plasma polymerization process noted above may also be utilized to coat the surfaces of seal member


218


.




Referring now to

FIGS. 14 and 15

, a further embodiment of the seal assembly generally designated as seal assembly


300


is shown. Seal member


318


is similar to seal member


118


except that inner portion


318




b


is formed in a conical shape with a wider opening directed towards a proximal end of seal assembly


300


and a narrower opening directed towards distal end of seal assembly


300


. The friction reducing coating of a hydrocyclosiloxane membrane prepared by plasma polymerization process noted above may also be utilized to coat the surfaces of seal member


318


.




It will be understood that various modifications may be made to the embodiments shown herein. Therefore, the above description should not be construed as limiting, but merely as exemplifications of preferred embodiments. Those skilled in the art will envision other modifications within the scope and spirit of the presently disclosed seal assemblies.



Claims
  • 1. A seal assembly for reception of an elongated surgical instrument, which comprises:a body having at least one opening configured and dimensioned to permit entry of an elongated surgical instrument and defining a central longitudinal axis; a seal member formed of a resilient material and defining an aperture therein, the aperture being configured and dimensioned such that insertion of the surgical instrument into the aperture causes the resilient material defining the aperture to resiliently contact the outer surface of the surgical instrument in a substantially fluid tight manner; and a fabric layer juxtaposed relative to the resilient material.
  • 2. A seal assembly for reception of an elongated surgical instrument according to claim 1, which further comprises a coating applied to the seal member to reduce friction between the seal member and surgical instrumentation inserted therein.
  • 3. A seal assembly for reception of an elongated surgical instrument according to claim 2, wherein the coating is a hydrocyclosiloxane membrane prepared by plasma polymerization process.
  • 4. A seal assembly for reception of an elongated surgical instrument according to claim 1, which further comprises a ring member secured to the seal member and having a dampening element disposed between a surface of the ring member and a surface of the body.
  • 5. A seal assembly comprising:a housing having a throughbore; and a seal member supported within the housing, the seal member being formed of a resilient material, the resilient material having a top surface and a bottom surface, the seal member having fabric material positioned adjacent the resilient material and having an opening formed therein aligned with the throughbore in the housing.
  • 6. A seal assembly according to claim 5, wherein the seal member has fabric material positioned on both the top and bottom surfaces of the resilient material.
  • 7. A seal assembly according to claim 5, wherein the resilient material is polyisoprene.
  • 8. A seal assembly according to claim 5, wherein the seal member includes a coating of material for reducing friction between the seal member and an instrument inserted through the seal member.
  • 9. A seal assembly according to claim 8, wherein the coating is a hydrocyclosiloxane membrane.
  • 10. A seal assembly according to claim 5, further including a ring assembly including a first ring member supported on the top surface of the seal member and a second ring member supported on the bottom surface of the seal member.
  • 11. A seal assembly according to claim 10, wherein the first and second ring members are adapted to be snap-fitted together.
  • 12. A seal assembly according to claim 5, wherein the housing includes an upper housing component and a lower housing component, the upper and lower housing components being positioned on opposite sides of the seal member.
  • 13. A seal assembly according to claim 5, wherein the fabric material is positioned between layers of resilient material.
  • 14. A seal assembly according to claim 5, wherein the seal assembly is adapted to releasably engage a cannula assembly.
  • 15. A seal assembly according to claim 5, wherein the seal member has an hourglass configuration.
  • 16. A seal assembly according to claim 5, wherein the seal member has a conical configuration.
  • 17. A seal assembly according to claim 5, further including a second seal member, the second seal member having an opening formed therein having a diameter which is larger than the opening in the first seal member.
  • 18. A seal assembly according to claim 10, further including a clamping element positioned between the ring assembly and the housing.
Parent Case Info

This application is a continuation of U.S. patent application Ser. No. 09/527,955, filed on Mar. 9, 2000, which claims priority from PCT International Application No. PCT/US98/08968, filed May 1, 1998, and U.S. Provisional Application Serial No. 60/045,412, filed May 2, 1997, all of which are incorporated herein by reference in their entirety.

US Referenced Citations (100)
Number Name Date Kind
3421509 Fiore Jan 1969 A
3565078 Vailliancourt et al. Feb 1971 A
3853127 Spademan Dec 1974 A
3907310 Dufour Sep 1975 A
3994287 Turp et al. Nov 1976 A
4000739 Stevens Jan 1977 A
4112932 Chiulli Sep 1978 A
4173350 Sieghartner Nov 1979 A
4177814 Knepshield et al. Dec 1979 A
4177997 Cartwright Dec 1979 A
4240335 Stucka et al. Dec 1980 A
4240411 Hosono Dec 1980 A
4311315 Kronenberg Jan 1982 A
4334688 Spargo et al. Jun 1982 A
4338689 Zieg Jul 1982 A
4386756 Muchow Jun 1983 A
4387879 Tauschinski Jun 1983 A
4430081 Timmermans Feb 1984 A
4447237 Frisch et al. May 1984 A
4464178 Dalton Aug 1984 A
4473094 Harris Sep 1984 A
4553760 Reed et al. Nov 1985 A
4588195 Antonini et al. May 1986 A
4601710 Moll Jul 1986 A
4626245 Weinstein Dec 1986 A
4641842 Kataoka Feb 1987 A
4654030 Moll et al. Mar 1987 A
4655752 Honkanen et al. Apr 1987 A
4673393 Suzuki et al. Jun 1987 A
4705511 Kocak Nov 1987 A
4715360 Akui et al. Dec 1987 A
4723550 Bales et al. Feb 1988 A
4758225 Cox et al. Jul 1988 A
4842591 Luther Jun 1989 A
4844483 Iijima et al. Jul 1989 A
4844484 Antonini et al. Jul 1989 A
4857062 Russell Aug 1989 A
4869717 Adair Sep 1989 A
4874377 Newgard et al. Oct 1989 A
4874378 Hillstead Oct 1989 A
4889349 Muller Dec 1989 A
4909798 Fleischhacker et al. Mar 1990 A
4917668 Haindl Apr 1990 A
4929235 Merry et al. May 1990 A
4932633 Johnson et al. Jun 1990 A
4943280 Lander Jul 1990 A
4960412 Fink Oct 1990 A
4966588 Rayman et al. Oct 1990 A
4998740 Tellier Mar 1991 A
5000745 Guest et al. Mar 1991 A
5002557 Hasson Mar 1991 A
5015000 Perini May 1991 A
5038756 Kepley Aug 1991 A
5041095 Littrell Aug 1991 A
5053014 Van Heugten Oct 1991 A
5053016 Lander Oct 1991 A
5064416 Newgard et al. Nov 1991 A
5073169 Raiken Dec 1991 A
5104383 Shichman Apr 1992 A
5127626 Hilal et al. Jul 1992 A
5137520 Maxon et al. Aug 1992 A
5167636 Clement Dec 1992 A
5180373 Green et al. Jan 1993 A
5197955 Stephens et al. Mar 1993 A
5201714 Gentelia et al. Apr 1993 A
5209736 Stephens et al. May 1993 A
5209737 Ritchart et al. May 1993 A
5221264 Wilk et al. Jun 1993 A
5226891 Bushatz et al. Jul 1993 A
5242412 Blake, III Sep 1993 A
5290304 Storace Mar 1994 A
5299813 McKenna Apr 1994 A
5300033 Miller Apr 1994 A
5300036 Mueller et al. Apr 1994 A
5308336 Hart et al. May 1994 A
5342315 Rowe et al. Aug 1994 A
5350364 Stephens et al. Sep 1994 A
5385553 Hart et al. Jan 1995 A
5395342 Yoon Mar 1995 A
5407433 Loomas Apr 1995 A
5411483 Loomas et al. May 1995 A
5463010 Hu et al. Oct 1995 A
5496280 Vandenbroek et al. Mar 1996 A
5545142 Stephens et al. Aug 1996 A
5603702 Smith et al. Feb 1997 A
5613954 Nelson et al. Mar 1997 A
5628732 Antoon, Jr. et al. May 1997 A
5634908 Loomas Jun 1997 A
5709664 Vandenbroek et al. Jan 1998 A
5752938 Flatland et al. May 1998 A
5807338 Smith Sep 1998 A
5827228 Rowe Oct 1998 A
5865807 Blake, III Feb 1999 A
5868714 Danks Feb 1999 A
6004326 Castro et al. Dec 1999 A
RE36702 Green et al. May 2000 E
6079692 Powell Jun 2000 A
6228061 Flatland et al. May 2001 B1
6354602 Oldenburg Mar 2002 B1
6482181 Racenet et al. Nov 2002 B1
Foreign Referenced Citations (7)
Number Date Country
3217118 Aug 1983 DE
0051718 May 1982 EP
0113520 Jul 1984 EP
0312219 Apr 1989 EP
1482857 Aug 1977 GB
WO9304717 Mar 1993 WO
WO9853865 Dec 1998 WO
Provisional Applications (1)
Number Date Country
60/045412 May 1997 US
Continuations (1)
Number Date Country
Parent 09/527955 US
Child 10/165373 US