Trocar assembly with pneumatic sealing

• US 9,907,569 B2
• Filed: 07/11/2014
• Issued: 03/06/2018
• Est. Priority Date: 10/06/2006
• Status: Active Grant

• Current Assignee: Conmed Corporation (Jefferies Financial Group, Inc.)
• Original Assignee: Conmed Corporation (Jefferies Financial Group, Inc.)
• Inventors: Stearns, Ralph, Tang, Raymond Yue-Sing, Mastri, Dominick
• Primary Examiner(s): BOUCHELLE, LAURA A
• Application Number:
  US14/329,364
• Publication Number:
  US 20150025323A1
• Time in Patent Office: 1,334 Days
• CPC Class Codes: A61B 17/3423 Access ports, e.g. toroid shape introducers for instruments or hands access sites for liquids A61M39/0247
• CPC Class Codes: A61B 17/3462 with means for changing the diameter or the orientation of the entrance port of the cannula, e.g. for use with different-sized instruments, reduction ports, adapter seals expandable cannulas A61B17/3417
• CPC Class Codes: A61B 17/3474 Insufflating needles, e.g. Veress needles
• CPC Class Codes: A61B 2017/00477 Coupling A61B2017/0046 takes precedence
• CPC Class Codes: A61B 2017/3445 used as instrument channel for multiple instruments catheters A61B2017/22072
• CPC Class Codes: A61B 2217/007 with irrigation system

Abstract

A trocar assembly for creating a pneumatic seal during a minimally-invasive surgical procedure. The trocar assembly including an elongated body having a lumen extending therethrough. The proximal end portion of the body defining a housing. A fluid supply plenum is defined in the housing configured to deliver pressurized insufflation fluid to a nozzle. The nozzle configured for directing pressurized fluid into the lumen and creating a pneumatic seal. A fluid return plenum is defined in the housing configured to collect spent insufflation fluid from as patient'"'"'s abdominal cavity. The fluid return plenum including a plurality of axially and radially oriented elongate vanes configured to permit spent insufflation fluid to proceed between the vanes and direct spent insufflation fluid back to the fluid return plenum.

Claims

1. A nozzle assembly for generating a gaseous seal, comprising:

a) an upper nozzle portion including an annular body having an outer periphery and an inner periphery, the inner periphery defining a downwardly extending nozzle tube having a radially outer surface, wherein the radially outer surface of the nozzle tube includes a plurality of circumferentially spaced apart recessed surface areas defining a plurality of circumferentially spaced apart raised surface areas;

b) a lower nozzle portion including an annular body having an outer periphery and an inner periphery, the inner periphery defining a beveled surface area configured for intimate engagement with the plurality of circumferentially spaced apart raised surface areas of the nozzle tube, whereby the spaced apart recessed surface areas of the nozzle tube and the beveled surface area form a ring of circumferentially spaced apart jets for generating a gaseous seal; and

c) a locking assembly cooperatively associated with the outer periphery of the upper and lower nozzle portions for interlocking the nozzle portions together and maintaining a minimum axial spacing therebetween to form a high pressure interior plenum that communicates with the ring of circumferentially spaced apart jets, wherein the locking assembly includes a plurality of circumferentially spaced apart interfitting engagement lugs that define a plurality of circumferentially spaced apart passages in an outer periphery of the nozzle assembly that communicate with the high pressure interior plenum.

2. A nozzle assembly as recited in claim 1, wherein the lugs include a first set of lugs that extend downwardly from an outer periphery of the upper nozzle portion.

3. A nozzle assembly as recited in claim 2, wherein the lugs further include a second set of lugs that extend upwardly from an outer periphery of the lower nozzle portion.

4. A nozzle assembly as recited in claim 1, wherein the nozzle tube has a radially inwardly tapering lower outer circumferential edge for directing gas exiting the ring of circumferentially spaced apart jets radially inwardly.

5. A nozzle assembly as recited in claim 1, wherein the outer periphery of the upper and lower nozzle portion each include an annular groove for accommodating a seal.

6. A nozzle assembly for generating a gaseous seal, comprising:

a) an upper nozzle portion including an annular body having an outer periphery and an inner periphery, the outer periphery including a plurality of circumferentially spaced apart downwardly extending upper engagement lugs, the inner periphery defining a downwardly extending nozzle tube having a radially outer surface, wherein the radially outer surface of the nozzle tube includes a plurality of circumferentially spaced apart recessed surface areas defining a plurality of circumferentially spaced apart raised surface areas; and

b) a lower nozzle portion including an annular body having an outer periphery and an inner periphery, the outer periphery including a plurality of circumferentially spaced apart upwardly extending lower engagement lugs configured to interfit with the upper engagement lugs of the upper nozzle portion, the inner periphery defining a beveled surface area configured for intimate engagement with the plurality of circumferentially spaced apart raised surface areas of the nozzle tube, whereby the spaced apart recessed surface areas of the nozzle tube and the beveled surface area form a ring of circumferentially spaced apart jets for generating a gaseous seal, and wherein the plurality of circumferentially spaced apart interfitting engagement lugs are configured to maintain the upper and lower nozzle portions of the nozzle assembly in an axial spaced relationship so as to form a high pressure interior plenum therebetween that communicates with the ring of spaced apart jets and further define a plurality of circumferentially spaced apart passages in an outer periphery of the nozzle assembly that communicate with the high pressure interior plenum.

7. A nozzle assembly as recited in claim 6, wherein the nozzle tube has a radially inwardly tapering lower outer circumferential edge for directing gas exiting the ring of circumferentially spaced apart jets radially inwardly.

8. A nozzle assembly as recited in claim 6, wherein the outer periphery of the upper and lower nozzle portion each includes an annular groove for accommodating a seal.