Deployment mechanisms for surgical instruments

Patent metadata

Field	Value
Publication number	US-9724153-B2
Application number	US-201414542858-A
Country	US
Kind code	B2
Filing date	Nov 17, 2014
Priority date	Nov 17, 2014
Publication date	Aug 8, 2017
Grant date	Aug 8, 2017

Abstract

A deployment mechanism for selectively deploying and retracting an energizable member and/an insulative member relative to an end effector assembly of a surgical instrument includes one or more actuators, a clutch assembly, and a drive assembly. The clutch assembly is configured to couple to the actuator(s) to provide rotational motion in the first direction in response to such rotation of the actuator(s) and to decouple from the actuator(s) in response to rotation thereof in the second direction. The drive assembly is operably coupled to the clutch assembly and is configured to convert the rotational motion provided by the clutch assembly into longitudinal motion to translate the energizable member and/or insulative member from a storage position to a deployed position and to translate the energizable member and/or the insulative member from the deployed position back to the storage position.

First claim

What is claimed is:

1. A deployment mechanism for selectively deploying and retracting at least one of an energizable member or an insulative member relative to an end effector assembly of a surgical instrument, the deployment assembly comprising:
at least one actuator rotatable in a first direction from an un-actuated position to an actuated position and rotatable in a second direction from the actuated position back to the un-actuated position;
a clutch assembly associated with the at least one actuator, the clutch assembly configured to couple to the at least one actuator to provide rotational motion in the first direction in response to rotation of the at least one actuator in the first direction, the clutch assembly configured to decouple from the at least one actuator in response to rotation of the at least one actuator in the second direction; and
a drive assembly operably coupled to the clutch assembly and the at least one of the energizable member or the insulative member, the drive assembly configured to convert the rotational motion provided by the clutch assembly into longitudinal motion to translate the at least one of the energizable member or the insulative member from a storage position to a deployed position and to translate the at least one of the energizable member or the insulative member from the deployed position back to the storage position.

2. The deployment mechanism according to claim 1 , wherein the clutch assembly includes a clutch gear and wherein the drive assembly includes at least one drive gear operably coupled to the clutch gear for transferring rotational motion of the clutch gear to the at least one drive gear.

3. The deployment mechanism according to claim 2 , further including an intermediate gear operably disposed between the clutch gear and the at least one drive gear.

4. The deployment mechanism according to claim 1 , wherein the clutch assembly includes a first pulley wheel, wherein the drive assembly includes at second pulley wheel, and wherein a pulley belt is operably coupled between the first and second pulley wheels for transferring rotational motion of the first pulley wheel to the second pulley wheel.

5. The deployment mechanism according to claim 1 , wherein the drive assembly further includes an arm operably coupled between the clutch assembly and the at least one of the energizable member or the insulative member, the arm continuously rotatable in one direction such that rotation of the arm through a first portion of a revolution translates the at least one of the energizable member or the insulative member from the storage position to the deployed position, and such that rotation of the arm through a second portion of the revolution translates the at least one of the energizable member or the insulative member from the deployed position back to the storage position.

6. The deployment mechanism according to claim 5 , wherein the deployment mechanism is configured to define a ratio of a degree of rotation of the at least one actuator relative to a degree of rotation of the arm of less than or equal to about 1:3.

7. The deployment mechanism according to claim 5 , wherein the arm includes a hand disposed at a free end thereof and wherein the drive assembly further includes:
an upright member defining a slot that extends in generally perpendicular orientation relative to an axis of translation of the at least one of the energizable member or the insulative member, wherein the hand of the arm is engaged within the slot; and
a slider coupled to the upright member and the at least one of the energizable member or the insulative member,
wherein rotation of the arm in response to the rotational motion provided by the clutch assembly moves the hand along the slot and urges the upright member to translate the slider to thereby translate the at least one of the energizable member or the insulative member from the storage position to the deployed position and to translate the at least one of the energizable member or the insulative member from the deployed position back to the storage position.

8. The deployment mechanism according to claim 5 , wherein the drive assembly further includes:
a linkage bar having a first end and a second end, the first end pivotably coupled to a free end of the arm;
a slider pivotably coupled to the second end of the linkage bar and coupled to the at least one of the energizable member or the insulative member,
wherein rotation of the arm in response to the rotational motion provided by the clutch assembly moves the linkage to translate the slider to thereby translate the at least one of the energizable member or the insulative member from the storage position to the deployed position and to translate the at least one of the energizable member or the insulative member from the deployed position back to the storage position.

9. The deployment mechanism according to claim 1 , wherein the clutch assembly and drive assembly are operably mounted on at least one support member.

10. The deployment mechanism according to claim 9 , wherein the at least one support member includes a guide configured to guide translation of the at least one of the energizable member or the insulative member between the storage position and the deployed position.

11. The deployment mechanism according to claim 9 , wherein the at least one support member includes at least one locking member, each locking member configured to releasably lock the at least one of the energizable member or the insulative member in one of the storage position or the deployed position.

12. A surgical instrument, comprising:
a housing;
a shaft extending distally from the housing;
an end effector assembly disposed at a distal end of the shaft;
a deployable assembly including at least one of an energizable member or an insulative member, the deployable assembly selectively movable relative to the end effector assembly between a storage condition and a deployed condition; and
a deployment mechanism for selectively moving the deployable assembly between the storage condition and the deployed condition, the deployment mechanism including:
at least one actuator rotatable mounted on the housing, the at least one actuator rotatable in a first direction from an un-actuated position to an actuated position and rotatable in a second direction from the actuated position back to the un-actuated position;
a clutch assembly associated with the at least one actuator, the clutch assembly configured to couple to the at least one actuator to provide rotational motion in the first direction in response to rotation of the at least one actuator in the first direction, the clutch assembly configured to decouple from the at least one actuator in response to rotation of the at least one actuator in the second direction;
a gear system including a first gear operably coupled to the clutch assembly, an intermediate gear, and a second gear, the first, intermediate, and second gears operably coupled to one another; and
a drive assembly operably coupled between the second gear and the deployable assembly, the drive assembly configured to convert the rotational motion provided by the clutch assembly into longitudinal motion to move the deployable assembly from the storage condition to the deployed condition and to move the deployable assembly from the deployed condition back to the storage condition.

13. The surgical instrument according to claim 12 , wherein the deployment mechanism further includes at least one support member operably mounting the clutch assembly, gear system, and drive assembly thereon.

14. The surgical instrument according t

Assignees

• Covidien Lp

Inventors

• Jadhav Amarsinh D

Classifications

• A61B17/320016

  Endoscopic cutting instruments, e.g. arthroscopes, resectoscopes (A61B10/0233, A61B17/29, A61B17/3207 take precedence) · CPC title

• F16H19/06

  comprising {flexible members, e.g. an} endless flexible member · CPC title

• A61B2018/1253

  monopolar · CPC title

• A61B2018/00196

  reciprocating lengthwise · CPC title

• A61B2017/2912

  transmission of forces to actuating rod or piston · CPC title