Force sensing apparatus and robot arm including the same

• US 9,186,797 B2
• Filed: 04/20/2012
• Issued: 11/17/2015
• Est. Priority Date: 10/31/2011
• Status: Active Grant

• Current Assignee: Samsung Electronics Co. Ltd.
• Original Assignee: Samsung Electronics Co. Ltd.
• Inventors: Kim, Jun-hyung, Choi, Hyun-do, Kim, Yeon-ho, Park, Chang-bae
• Primary Examiner(s): CAPUTO, LISA M
• Assistant Examiner(s): Hopkins, Brandi N
• Application Number:
  US13/452,071
• Publication Number:
  US 20130104672A1
• Time in Patent Office: 1,306 Days
• Field of Search: None
• US Class Current: 1/1
• CPC Class Codes: A61B 2090/064 for measuring force, pressure or mechanical tension
• CPC Class Codes: A61B 34/30 Surgical robots
• CPC Class Codes: B25J 13/085 Force or torque sensors B25J13/082, B25J13/084 take precedence
• CPC Class Codes: G01L 1/246 using integrated gratings, e.g. Bragg gratings
• CPC Class Codes: G01L 5/166 using photoelectric means

Abstract

A multi-axis force sensing apparatus that is installed at an operational end of a surgery robot and is capable of measuring force acting upon the operational end and a robot arm including the force sensing apparatus includes a body that is elastically deformable and has a pipe form extending along an axial direction of the body, an optical fiber strain gauge attached to a surface of the body to measure a tension and compression of the body in at least three directions. The optical fiber strain gauge may include at least three fiber Bragg gratings (FBGs) that are attached to the surface of the body and extended in an axial direction of the body, a light source providing light to each of the FBGs, and a light detector detecting light reflected by the FBGs or light that has passed through the FBGs.

Claims

1. A force sensing apparatus, comprising:

a body that is elastically deformable and has a pipe form extending along an axial direction of the body;

at least three fiber Bragg gratings (FBGs) attached to a surface of the body;

an opening in the body between each two adjacent FBGs so that a plane perpendicular to the axial direction of the body intersects the opening and the two adjacent FBGs;

a light source configured to provide light to each of the FBGs; and

a light detector configured to detect light reflected by each of the FBGs or light that has passed through each of the FBGs.

2. The force sensing apparatus of claim 1, wherein the at least three FBGs are arranged to extend along the axial direction of the body.

3. The force sensing apparatus of claim 1, wherein the at least three FBGs are attached to the surface of the body at at least three different positions at predetermined intervals along an azimuth angle direction.

4. The force sensing apparatus of claim 1, wherein the FBGs are attached to an external surface or an inner surface of the body.

5. The force sensing apparatus of claim 1, wherein the body comprises plastic material.

6. The force sensing apparatus of claim 1, further comprising:

a plurality of bolt holes in an upper portion and a lower portion of the body;

wherein an extension line between a center of two adjacent bolt holes and a center of the opening is at a 45-degree angle with respect to a horizontal surface.

7. The force sensing apparatus of claim 1, wherein when an operational end of the force sensing apparatus is assumed to be an upper portion of the body, a center of the opening is at a position lower than a center of two adjacent FBGs.

8. A force sensing apparatus comprising:

a body that is elastically deformable and has a pipe form extending along an axial direction of the body;

at least three fiber Bragg gratings (FBGs) attached to a surface of the body;

a light source configured to provide light to each of the FBGs; and

a light detector configured to detect light reflected by each of the FBGs or light that has passed through each of the FBGs;

wherein the body comprises;

an upper portion and a lower portion separated from each other;

at least three elastic beams that connect the upper portion and the lower portion of the body and are extended in a direction perpendicular to an axis of the body;

gaps between one of the elastic beams and the upper portion of the body and between one of the elastic beams and the lower portion of the body; and

a stopper between each two adjacent elastic beams so that a plane perpendicular to the axial direction of the body intersects the stopper and one of the at least three FBGs between the two adjacent elastic beams.

9. The force sensing apparatus of claim 8, wherein the body comprises metal.

10. The force sensing apparatus of claim 8, wherein a first end portion of the elastic beams is connected to the upper portion of the body, and

wherein a second end portion of the elastic beams opposite to the first end portion is connected to the lower portion of the body.

11. The force sensing apparatus of claim 8, wherein the stopper comprises:

a first protrusion that protrudes and extends from the lower portion of the body toward the upper portion of the body in the axial direction of the body; and

a second protrusion that protrudes and extends from the upper portion of the body toward the lower portion of the body in the axial direction of the body to surround the first protrusion.

12. The force sensing apparatus of claim 11, wherein the first protrusion comprises an intermediate portion having a first width and an end portion having a second width,

wherein the second protrusion comprises an intermediate portion having a third width and an end portion having a fourth width,

wherein the first protrusion and the second protrusion are engaged with each other in a complementary form,

wherein the first width is smaller than the second width, and

wherein the third width is smaller than the fourth width.

13. The force sensing apparatus of claim 12, wherein the gaps extend between the first protrusion and the second protrusion.

14. The force sensing apparatus of claim 11, wherein the at least three elastic beams and the stopper between each two adjacent elastic beams are formed in a monolithic manner by forming at least three gaps in the body by using a wire electrical discharge machining (EDM) method,

wherein two end sides of each of the at least three gaps extend in a direction perpendicular to the axial direction of the body, and

wherein centers of each of the gaps are curved to form the stopper between each two adjacent elastic beams.

15. The force sensing apparatus of claim 14, wherein two adjacent gaps of the at least three gaps are separated in the axial direction of the body and are partially overlapped with each other in an azimuth angle direction, and

wherein both side portions of each of the two adjacent gaps are in parallel to a side portion of another one of the two adjacent gaps such that a respective one of the at least three elastic beams is between the two adjacent gaps.

16. The force sensing apparatus of claim 14, wherein the body further comprises an opening at each of two end portions of each of the gaps.

17. The force sensing apparatus of claim 8, wherein one of the FBGs is attached to the body across the stopper between each two adjacent elastic beams.

18. The force sensing apparatus of claim 8, wherein the FBGs are attached to the body across the elastic beams.

19. A robot arm, comprising:

a body that is elastically deformable and has a pipe form extending along an axial direction of the body;

at least three fiber Bragg gratings (FBGs) attached to a surface of the body;

an opening in the body between each two adjacent FBGs so that a plane perpendicular to the axial direction of the body intersects the opening and the two adjacent FBGs;

a light source configured to provide light to each of the FBGs; and

a light detector configured to detect light reflected by each of the FBGs or light that has passed through each of the FBGs.

20. The robot arm of claim 19, wherein the body of the force sensing apparatus is the same with a body of the robot arm.

21. The robot arm of claim 19, further comprising grippers installed at an operational end of the body.

22. A method to sense a force applied to an elastically deformable body, the method comprising:

attaching at least three optical fiber strain gauges to the body;

forming an opening in the body between two adjacent optical fiber strain gauges of the at least three optical fiber strain gauges so that a plane perpendicular to an axial direction of the elastically deformable body intersects the opening and the two adjacent optical fiber strain gauges;

providing light to each of the at least three optical fiber strain gauges;

detecting the light from each of the at least three optical fiber strain gauges; and

calculating the force applied to the body based on the detected light.