FASTENER GRIP LENGTH SELECTOR

• US 20060090363A1
• Filed: 11/02/2004
• Published: 05/04/2006
• Est. Priority Date: 11/02/2004
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Hoeckelman, Leslie A., Luner, Jeffery J., Kleine, David W.
• Granted Patent: US 7,065,897 B2
• Time in Patent Office: Days
• US Class Current: 33/833
• CPC Class Codes: F16B 5/0642 the plates being arranged one on top of the other and in full close contact with each other
• CPC Class Codes: G01B 3/28 Depth gauges
• CPC Class Codes: Y10T 29/49771 Quantitative measuring or gauging

Abstract

A fastener grip length selector includes a housing having a first section and a second section, and a gauge fitted with the second section of the housing and including a spindle that reaches into the first section of the housing. The fastener grip length selector enables the precise determination of a grip length of a fastener to be installed in a particular fastener hole while a temporary fastener is installed in that particular fastener hole. The fastener grip length selector is suitable for, but not limited to, applications in the aerospace industry. The fastener grip length selector may be used, for example, during the installation process of an aircraft airframe assembly. Using the method for precisely measuring a thickness of an assembly in clamped-up condition enables the determination of the length of a blind fastener hole with high accuracy while a temporary fastener is installed.

Claims

1. (canceled)

2. A fastener grip length selector, comprising:

an axis;

a housing extending along said axis and including a first section and a second section; and

a gauge fitted with said second section of said housing, said gauge including a spindle, wherein said spindle extends along said axis and reaches into said first section of said housing,

wherein said gauge further comprises a clamping shaft being in a fixed connection with said housing, wherein said spindle is inserted in said clamping shaft and is movable along said axis within said clamping shaft.

3. The fastener grip length selector of claim 2, wherein said gauge further comprised a spring, wherein said spring is in contact with said spindle.

4. The fastener grip length selector of claim 3, wherein said spindle compresses said spring.

5. The fastener grip length selector of claim 2, wherein said housing has a cylindrical shape, a top, and a bottom and wherein said first section is located at said bottom, and wherein said second section is located at said top.

6. The fastener grip length selector of claim 2, wherein the inside diameter of said first section is larger than the inside diameter of said second section.

7. The fastener grip length selector of claim 2, wherein the inside diameter of said first section is large enough to fit over a temporary fastener.

8. The fastener grip length selector of claim 2, wherein said gauge further includes a display.

9. The fastener grip length selector of claim 8, wherein said display is a digital display.

10. The fastener grip length selector of claim 8, wherein said display is an analog display.

11. A fastener grip length selector, comprising:

an axis;

a cylindrical housing extending along said axis and including a first section and a second section; and

a gauge, including;

a clamping shaft, wherein said clamping shaft has a cylindrical shape and extends along said axis, and wherein said clamping shaft is in a fixed connection with said second section of said housing;

a spindle, wherein said spindle is inserted in said clamping shaft, wherein said spindle extends along said axis and reaches into said first section of said housing, and wherein said spindle is movable within said clamping shaft along said axis;

a spring, wherein said spring is in contact with said spindle, and wherein said spring is compressed with said spindle; and

a digital display, wherein said digital display displays a length corresponding to the movement of said spindle along said axis;

wherein said gauge translates the movement of said spindle into a length displayed in said digital display.

12. The fastener grip length selector of claim 11, wherein said display includes a reset button.

13. The fastener grip length selector of claim 11, wherein a gauge reading is displayed in said display, and wherein said gauge reading corresponds to the length compression of said spring.

14. The fastener grip length selector of claim 11, wherein said housing is placed over a temporary fastener, wherein said temporary fastener is installed along said axis in an assembly and provides a clamp-up force to said assembly.

15. The fastener grip length selector of claim 11, wherein said housing includes a top and a bottom, and wherein said gauge is in a fixed connection with said top of said housing, and wherein said bottom of said housing is in contact with an outer mold line of said assembly.

16. The fastener grip length selector of claim 11, wherein said spindle further includes a contact point, wherein said contact point is in contact with said temporary fastener.

17. A calibration system, comprising:

a reference standard;

wherein said reference standard includes;

a structure including a top surface and a bottom surface, wherein said structure has a known thickness measured from said top surface to said bottom surface; and

a fastener hole machined into said structure, wherein said fastener hole extends from said top surface to said bottom surface of said structure;

a temporary fastener installed in said fastener hole, wherein said temporary fastener includes a top; and

a fastener grip length selector placed over said temporary fastener, wherein said fastener grip length selector contacts said temporary fastener at said top, and wherein said fastener grip length selector contacts said top surface of said structure;

wherein said fastener grip length selector indicates a length.

18. The calibration system of claim 17, wherein said fastener grip length selector includes a display, and wherein said display is set to zero.

19. The calibration system of claim 17, wherein said display is set to the known thickness of said reference standard.

20. A system for measuring an assembly thickness in a clamped-up condition, comprising:

an assembly including a plurality of panels, said assembly having an outer mold line and an inner mold line;

a fastener hole machined into said assembly;

a temporary fastener installed in said fastener hole, said temporary fastener including a top and providing a clamp-up force to said assembly holding said panels together; and

a fastener grip length selector including a housing, and a gauge including a spindle, said fastener grip length selector being placed over said installed temporary fastener, wherein said housing is in contact with said outer mold line of said assembly, wherein said spindle is in contact with said top of said temporary fastener, and wherein said gauge translates the movement of said spindle into a length.

21. The system for measuring an assembly thickness in a clamped-up condition of claim 20, wherein said gauge is selected from the group of a digital gauge, an analog gauge, a rotating micrometer head, and a sliding caliper.

22. The system for measuring an assembly thickness in a clamped-up condition of claim 20, wherein said gauge further includes a display displaying said length, and wherein the distance from said outer mold line to said inner mold line of said assembly is deduced from said displayed length.

23. The system for measuring an assembly thickness in a clamped-up condition of claim 20, wherein the gauge reading displayed in said display is digitally converted to a corresponding fastener grip length.

24. The system for measuring an assembly thickness in a clamped-up condition of claim 20, further including a reference standard calibrating said fastener grip length selector.

25. A system for measuring the thickness of an aircraft airframe assembly in clamped-up condition, comprising:

an aircraft airframe assembly including an outer mold line skin, a sealer, and a substructure, said assembly having an outer mold line an inner mold line, and a thickness;

a fastener hole machined into said aircraft airframe assembly, wherein said fastener hole is a blind hole not accessible from said inner mold line;

a temporary fastener installed in said fastener hole, said temporary fastener including a top and providing a clamp-up force to said aircraft airframe assembly holding said outer mold line skin, said sealer, and said substructure together;

a fastener grip length selector, comprising;

a gauge including a display, a spindle, and a spring in connection with said spindle, and a housing supporting said gauge; and

a reference standard having a known thickness and including a fastener hole, wherein said reference standard calibrates said fastener grip length selector;

wherein said fastener grip length selector is placed over said installed temporary fastener, wherein said housing of said fastener grip length selector is in contact with said outer mold line of said assembly, wherein said spindle is in contact with said top of said temporary fastener, and wherein said spindle compresses said spring; and

wherein said thickness of said aircraft airframe assembly is deduced from the gauge reading displayed in said display.

26. The system for measuring the thickness of an aircraft airframe assembly in clamped-up condition of claim 25, wherein said gauge further includes a cylindrical clamping shaft being in a fixed connection with said housing, wherein said spindle is inserted in said clamping shaft and is movable within said clamping shaft, and wherein said spring is inserted in said clamping shaft to be in contact with said spindle.

27. The system for measuring the thickness of an aircraft airframe assembly in clamped-up condition of claim 25, wherein said thickness of said aircraft airframe assembly is used to select the correct fastener to be installed permanently in said fastener hole.

28. A method for precisely measuring a thickness of an assembly in clamped-up condition, comprising the steps of:

calibrating a fastener grip length selector using a reference standard and a temporary fastener;

installing said temporary fastener in an assembly having a thickness;

placing said calibrated fastener grip length selector over said installed temporary fastener;

making contact between said fastener grip length selector, said temporary fastener, and said assembly;

reading a length displayed on said fastener grip length selector; and

deducing said thickness of said assembly from said reading.

29. The method of claim 28, further comprising the step of:

clamping said assembly by providing a clamp-up force to said assembly with said temporary fastener.

30. The method of claim 28, further comprising the steps of:

converting said reading to a correspondent grip length value of said fastener; and

selecting a correct fastener to be installed permanently in said assembly.

31. The method of claim 28, further comprising the steps of:

contacting said installed temporary fastener with a spindle of said fastener grip length selector;

moving said spindle while placing said calibrated fastener grip length selector over said installed temporary fastener;

displaying a gauge reading in a display of said gauge that corresponds to said movement of said spindle.