Method of making a device for monitoring fatigue life

• US 4,639,997 A
• Filed: 07/18/1985
• Issued: 02/03/1987
• Est. Priority Date: 01/23/1984
• Status: Expired due to Term

• Current Assignee: Material Technologies, Inc.
• Original Assignee: Tensiodyne Scientific Corporation
• Inventors: Brull, Maurice A.
• Primary Examiner(s): NOT, DEFINED
• Application Number:
  US06/756,419
• Time in Patent Office: 565 Days
• Field of Search: 29/557, 29/412, 29/407, 29/415, 29/417, 73/762, 73/786, 73/787, 73/794, 73/802
• US Class Current: 29/407.01
• CPC Class Codes: G01L 1/06 by measuring the permanent deformation of gauges, e.g. of compressed bodies
• CPC Class Codes: G01N 2203/027 Specimens with holes or notches
• CPC Class Codes: G01N 2203/0282 Two dimensional, e.g. tapes, webs, sheets, strips, disks or membranes
• CPC Class Codes: G01N 3/062 with mechanical indicating or recording means
• CPC Class Codes: Y10T 29/49764 with testing or indicating
• CPC Class Codes: Y10T 29/49794 Dividing on common outline
• CPC Class Codes: Y10T 29/49995 Shaping one-piece blank by removing material

Abstract

A device for monitoring the fatigue life of a structural member is comprised of at least one and preferably a plurality of substantially flat, elongated coupons which are fabricated of the same material as that of the member being monitored. The coupons are secured in parallel to the member so that they all experience the same strain history as the member. Each of the coupons includes a different stress concentrating notch pattern so that the application of the same strain to all of the coupons results in the development of different stress concentrations within the coupons. The development of different stress concentrations within the coupons causes each coupon to have a different fatigue life, the fatigue life of each coupon being a predetermined percentage of the fatigue life of the structural member being monitored.

Claims

1. A method of making a device for monitoring the fatigue life of a member fabricated of a particular material comprising the steps of:

obtaining a thin sheet of the material from which the member is fabricated;

cutting a plurality of generally parallel elongated coupons from the thin sheet of material;

cutting a predetermined stress concentrating notch pattern comprised of at least one pair of notches into each coupon, one notch of the notch pair being disposed on each of the longitudinal sides of a coupon, the notches of the notch pair being substantially geometrically the same and substantially aligned with each other, the notch pattern of each of the coupons varying in intensity from mild in which the edge surfaces of the notches are generally smooth and continuously curved, to severe, in which the edge surface of each of the notches exhibits a sudden change to form two portions which are in different planes, the two portions meeting to form a line so that upon the application of the same strain to all of the coupons, each coupon has a different fatigue life, the fatigue life of each coupon being a percentage of the fatigue life of the member being monitored.

2. The method as recited in claim 1 further including the steps of:

testing each of the coupons to develop and S-n endurance curve for each coupon which indicates the number of cycles required to develop fatigue failure within the coupon; and

comparing the S-n curves for the different coupons to determine whether the separation between the fatigue failure of the coupons is adequate to provide a desired separation of the fatigue failure warnings.

3. The method as recited in claim 1 wherein at least one of the coupons has a notch pattern comprised of at least one pair of wedge angle V-shaped notches, the wedge angle of the V-shaped notches being varied.

4. The method as recited in claim 1 wherein the orientation angle of the notches is varied.

5. The method as recited in claim 1 wherein the number of notch pairs for each coupon is varied.