Load apparatus and method for bolt-loaded compact tension test specimen

• US 5,598,738 A
• Filed: 04/03/1995
• Issued: 02/04/1997
• Est. Priority Date: 04/03/1995
• Status: Expired due to Fees

• Current Assignee: Battelle Energy Alliance LLC (Battelle Memorial Institute)
• Original Assignee: Lockheed Idaho Technologies Company
• Inventors: Epstein, Jonathan S., Ward, Michael B., Buescher, Brent J. Jr., Lloyd, W. Randolph
• Primary Examiner(s): Chilcot, Richard
• Assistant Examiner(s): NOORI, MAX H
• Application Number:
  US08/415,879
• Time in Patent Office: 673 Days
• Field of Search: 73/761, 73/768, 73/774, 73/799, 73/826, 73/856
• US Class Current: 73/761
• CPC Class Codes: F16B 31/025 with a gauge pin in a longitudinal bore in the body of the bolt
• CPC Class Codes: G01L 5/0028 Force sensors associated with force applying means G01L5/0052, G01L5/0057, G01L5/0061 take precedence
• CPC Class Codes: G01N 2203/0017 Tensile
• CPC Class Codes: G01N 2203/0037 involving a rotating movement, e.g. gearing, cam, eccentric, or centrifuge effects
• CPC Class Codes: G01N 2203/0066 Propagation of crack
• CPC Class Codes: G01N 3/16 applied through gearing G01N3/18 takes precedence

Abstract

A bolt-loaded compact tension test specimen load apparatus includes: a) a body having first and second opposing longitudinal ends, the first end comprising an externally threaded portion sized to be threadedly received within the test specimen threaded opening; b) a longitudinal loading rod having first and second opposing longitudinal ends, the loading rod being slidably received in a longitudinal direction within the body internally through the externally threaded portion and slidably extending longitudinally outward of the body first longitudinal end; c) a force sensitive transducer slidably received within the body and positioned to engage relative to the loading rod second longitudinal end; and d) a loading bolt threadedly received relative to the body, the loading bolt having a bearing end surface and being positioned to bear against the transducer to forcibly sandwich the transducer between the loading bolt and loading rod. Also disclosed is a method of in situ determining applied force during crack propagation in a bolt-loaded compact tension test specimen.

Claims

1. A bolt-loaded compact tension test specimen load apparatus, the specimen having a notch and a threaded opening extending to and positioned transversely relative to the notch for receiving a threaded bolt for applying an opening force to the notch, the load apparatus comprising:

a body having first and second opposing longitudinal ends, the first end comprising an externally threaded portion sized to be threadedly received within the test specimen threaded opening;

a longitudinal loading rod having first and second opposing longitudinal ends, the loading rod being slidably received in a longitudinal direction within the body internally through the externally threaded portion and slidably extending longitudinally outward of the body first longitudinal end;

a force sensitive transducer slidably received within the body and positioned to engage relative to the loading rod second longitudinal end; and

a loading bolt threadedly received relative to the body, the loading bolt having a bearing end surface and being positioned to bear against the transducer to forcibly sandwich the transducer between the loading bolt bearing end and second end of the loading rod.

2. The load apparatus of claim 1 wherein the body externally threaded portion has a minor thread diameter, the loading rod first longitudinal end having a diameter which is less than the minor thread diameter.

3. The load apparatus of claim 1 wherein the body externally threaded portion has a minor thread diameter, the loading rod first longitudinal end having a diameter which is one-half or less than the minor thread diameter.

4. The load apparatus of claim 1 wherein the bearing end of the loading bolt is radiused, thereby reducing contact area between the bolt and transducer as compared to a flat bearing end.

5. The load apparatus of claim 1 wherein,

the test specimen notch has an open notch spacing and the specimen threaded opening has a length from the exterior of the specimen to the notch, the spacing and length having a sum defining a first distance;

and

the body comprises a main body portion and the externally threaded portion comprises a longitudinal extension extending from the main body portion, the main body comprising a bearing surface adjacent the longitudinal extension, the longitudinal extension extending longitudinally from the main body bearing surface to a second distance, the second distance being effectively less than the first distance to enable contacting of the main body bearing surface against the exterior of the test specimen when the longitudinal extension is fully threaded inwardly relative to the test specimen threaded opening.

6. The load apparatus of claim 5 wherein the bearing surface is formed on an annular ring which encircles the longitudinal extension.

7. The load apparatus of claim 1 wherein,

the body comprises a main body portion having a first longitudinal threaded opening at the first end, the main body first threaded opening being of the same diameter as the test specimen threaded opening;

and

the externally threaded portion comprises a discrete longitudinally elongated body which is threadedly received within the main body first threaded opening.

8. The load apparatus of claim 1 wherein,

the test specimen notch has an open notch spacing and the specimen threaded opening has a length from the exterior of the specimen to the notch, the spacing and length having a sum defining a first distance;

the body comprises a main body portion having a first longitudinal threaded opening at the first end and an adjacent lateral bearing surface, the main body first threaded opening being of the same diameter as the test specimen threaded opening; and

the externally threaded portion comprises a discrete longitudinally elongated body which is threadedly received within the main body first threaded opening, the discrete body extending longitudinally from the main body bearing surface to a second distance, the second distance being effectively less than the first distance to enable contacting of the main body bearing surface against the exterior of the test specimen when the longitudinal extension is fully threaded inwardly relative to the test specimen threaded opening.

10. The load apparatus of claim 1 wherein the body comprises a longitudinal threaded opening, the apparatus further comprising an externally threaded plug threadedly received within the body longitudinal threaded opening, the plug having internal threads sized to receive the loading bolt, the loading bolt being longitudinally threaded into the plug with the loading bolt bearing end surface extending out of the plug.

9. A bolt-loaded compact tension test specimen load apparatus, the specimen having a notch and a threaded opening extending to and positioned transversely relative to the notch for receiving a threaded bolt for applying an opening force to the notch, the load apparatus comprising:

a body having first and second opposing longitudinal ends, the first end comprising an externally threaded portion sized to be threadedly received within the test specimen threaded opening;

a longitudinal loading rod having first and second opposing longitudinal ends, the loading rod being slidably received in a longitudinal direction within the body internally through the externally threaded portion and slidably extending longitudinally outward of the body first longitudinal end;

a force sensitive transducer slidably received within the body and positioned to engage relative to the loading rod second longitudinal end;

a force transfer plate slidably positioned within the body between the loading bolt and the transducer; and

a loading bolt threadedly received relative to the body, the loading bolt having a bearing end surface and being positioned to bear against the transducer to forcibly sandwich the transducer between the loading bolt and loading rod.

11. The load apparatus of claim 9 wherein the bearing end of the loading bolt is radiused, thereby reducing contact area between the bolt and transducer as compared to a flat bearing end.

12. The load apparatus of claim 9 wherein,

the body externally threaded portion has a minor thread diameter, the loading rod first longitudinal end having a diameter which is less than the minor thread diameter;

and

the bearing end of the loading bolt is radiused, thereby reducing contact area between the bolt and transducer as compared to a flat bearing end.

13. The load apparatus of claim 9 wherein,

the body externally threaded portion has a minor thread diameter, the loading rod first longitudinal end having a diameter which is one-half or less than the minor thread diameter;

and

the bearing end of the loading bolt is radiused, thereby reducing contact area between the bolt and transducer as compared to a flat bearing end.

14. The load apparatus of claim 9 wherein,

the body externally threaded portion has a minor thread diameter, the loading rod first longitudinal end having a diameter which is one-half or less than the minor thread diameter;

the bearing end of the loading bolt is radiused, thereby reducing contact area between the bolt and transducer as compared to a flat bearing end; and

the body comprises a longitudinal threaded opening, the apparatus further comprising an externally threaded plug threadedly received within the body longitudinal threaded opening, the plug having internal threads sized to receive the loading bolt, the loading bolt being longitudinally threaded into the plug with the loading bolt bearing end surface extending out of the plug.

15. The load apparatus of claim 9 wherein,

the test specimen notch has an open notch spacing and the specimen threaded opening has a length from the exterior of the specimen to the notch, the spacing and length having a sum defining a first distance;

the bearing end of the loading bolt is radiused, thereby reducing contact area between the bolt and transducer as compared to a flat bearing end; and

the body comprises a main body portion and the externally threaded portion comprises a longitudinal extension extending from the main body portion, the main body comprising a bearing surface adjacent the longitudinal extension, the longitudinal extension extending longitudinally from the main body bearing surface to a second distance, the second distance being effectively less than the first distance to enable contacting of the main body bearing surface against the exterior of the test specimen when the longitudinal extension is fully threaded inwardly relative to the test specimen threaded opening.

16. The load apparatus of claim 15 wherein the bearing surface is formed on an annular ring which encircles the longitudinal extension.

17. The load apparatus of claim 9 wherein,

the test specimen notch has an open notch spacing and the specimen threaded opening has a length from the exterior of the specimen to the notch, the spacing and length having a sum defining a first distance;

the bearing end of the loading bolt is radiused, thereby reducing contact area between the bolt and transducer as compared to a flat bearing end;

the body comprises a main body portion having a first longitudinal threaded opening at the first end, the main body first threaded opening being of the same diameter as the test specimen threaded opening; and

the externally threaded portion comprises a discrete longitudinally elongated body which is threadedly received within the main body first threaded opening.

18. The load apparatus of claim 9 wherein,

the test specimen notch has an open notch spacing and the specimen threaded opening has a length from the exterior of the specimen to the notch, the spacing and length having a sum defining a first distance;

the bearing end of the loading bolt is radiused, thereby reducing contact area between the bolt and transducer as compared to a flat bearing end;

the body comprises a main body portion having a first longitudinal threaded opening at the first end and an adjacent lateral bearing surface, the main body first threaded opening being of the same diameter as the test specimen threaded opening;

the externally threaded portion comprises a discrete longitudinally elongated body which is threadedly received within the main body first threaded opening, the discrete body extending longitudinally from the main body bearing surface to a second distance, the second distance being effectively less than the first distance to enable contacting of the main body bearing surface against the exterior of the test specimen when the longitudinal extension is fully threaded inwardly relative to the test specimen threaded opening; and

the load apparatus further comprising a force transfer plate slidably positioned within the body between the loading bolt and the transducer.

19. A method of in situ determination of applied force during crack propagation in a bolt-loaded compact tension test specimen, the method comprising the following steps:

providing a rod in a transversely slidable orientation relative to a notch in a bolt-loaded compact tension test specimen, the rod having first and second opposing ends, the first end being positioned and adapted for bearing against one transverse surface of the test specimen exposed by the notch;

providing a force sensitive transducer operatively against the second end of the loading rod;

threading a bolt operatively against the transducer to force the first rod end against the one transverse surface of the test specimen to load the test specimen; and

determining applied force on the test specimen as a function of time from readings obtained from the force sensitive transducer.