Device for monitoring the fatigue life of a structural member and a method of making same

• US 5,425,274 A
• Filed: 02/08/1994
• Issued: 06/20/1995
• Est. Priority Date: 07/01/1992
• Status: Expired due to Term

• Current Assignee: EFS International SA, Tensiodyne Scientific, Inc.
• Original Assignee: Tensiodyne Scientific, Inc.
• Inventors: Creager, Matthew
• Primary Examiner(s): Williams, Hezron E.
• Assistant Examiner(s): Ashraf, Nashmiya
• Application Number:
  US08/193,342
• Time in Patent Office: 497 Days
• Field of Search: 73/775, 73/762, 73/799, 73/787, 73/808, 73/809, 73/810, 73/786, 73/787, 73/806
• US Class Current: 73/762
• CPC Class Codes: G01N 2203/0073 Fatigue
• CPC Class Codes: G01N 2203/0664 using witness specimens
• CPC Class Codes: G01N 3/32 by applying repeated or pulsating forces
• CPC Class Codes: G07C 3/00 Registering or indicating the condition or the working of machines or other apparatus, other than vehicles

Abstract

A device for monitoring the fatigue life of a structural member composed of a predetermined material, and a method of making same. The device is a substantially flat fuse composed of a material similar to the predetermined material and mountable on a structural member by adhesive during use. The fuse has cut out portions which define fuse elements and variable unbonded areas are formed about the fuse elements to effect failure at different times in sequence because of fatigue and prior to the failure of the monitored structural member when the fuse and the monitored structural member are subjected to substantially the same stress history.

Claims

1. A device for monitoring the fatigue life of a structural member composed of a predetermined material, the device comprising:

a substantially flat fuse blank composed of material similar to said predetermined material and mounted on the structural member during use of the device, said blank having means defining at least two fuse legs, a cut out portion on at least one side of each leg to define a fuse element therein and adhesive means applied to one surface of said blank to define variable unbonded areas around each of the fuse elements, whereby a configuration of the cut out portion and the unbonded areas for each fuse element effect a failure of the fuse elements at different percentages of the fatigue life of the structural member due to fatigue, prior to failure of the monitored structural member when the blank and the monitored structural member are subjected to a substantially similar stress history.

2. The device according to claim 1, wherein the variable unbonded areas have variable lengths.

3. The device according to claim 1, wherein the variable unbonded areas are disposed symmetrically about the cut out portions.

4. The device according to claim 1, wherein the variable unbonded areas are disposed asymmetrically about the cut out portions.

5. The device according to claim 1, wherein the variable unbonded areas are disposed symmetrically and asymmetrically about the cut out portions.

6. The device according to claim 1, wherein the cut out portions of the legs have different shapes and further comprising means effecting a reduced thickness of each of the fuse elements to effect failure of the fuse elements at different percentages of the fatigue life of the structural member.

7. The device according to claim 1, wherein the fuse elements have different reduced thicknesses relative to a remainder of the blank to effect failure of the fuse elements at different percentages of the fatigue life of the structural member.

8. The device according to claim 7, wherein the cut out portions have the same shape.

9. The device according to claim 1, wherein the predetermined material is a metal.

10. The device according to claim 6, wherein the means effecting a reduced thickness comprises a channel in the blank.

11. The device according to claim 10, wherein the channel is in a face of the blank.

12. A method of making a device for monitoring the fatigue life of a structural member composed of a predetermined material, the method comprising the steps of:

providing a substantially flat fuse blank composed of a material similar to said predetermined material, forming at least two fuse legs in the blank forming cut out portions in the fuse legs to define at least two fuse elements and applying adhesive to one surface of the blank to form variable unbonded areas around each of the fuse elements to effect a failure of each of the fuse elements at different percentages of the fatigue life of the structural member prior to a failure of the monitored structural member when the blank and the monitored structural member are subjected to a substantially similar stress history.

13. The method according to claim 12, wherein the variable unbonded areas have variable lengths.

14. The method according to claim 12, wherein the step of applying adhesive comprises applying adhesive symmetrically about the cut out portions.

15. The method according to claim 12, wherein the step of applying adhesive comprises applying adhesive asymmetrically about the cut out portions.

16. The method according to claim 12, wherein the step of applying adhesive comprises applying adhesive symmetrically and asymmetrically about the cut out portions.

17. The method according to claim 12, further comprising reducing a thickness of each fuse element by a different amount in the range of 10 to 90%.

18. The method according to claim 17, wherein the step of reducing comprises forming a channel in the blank.

19. The method according to claim 18, wherein the channel is in the one surface of the blank.

20. The method according to claim 12, further comprising bonding a flat member to the one surface of the blank on opposite sides of each fuse element prior to applying adhesive.