Fastener and method for fastening to associated structural assembly

Patent metadata

Field	Value
Publication number	US-9895750-B2
Application number	US-201615214139-A
Country	US
Kind code	B2
Filing date	Jul 19, 2016
Priority date	Jul 19, 2016
Publication date	Feb 20, 2018
Grant date	Feb 20, 2018

Abstract

A fastener for fastening a drill jig to overlapping work pieces and clamping the overlapping work pieces for facilitating accurate drilling of the overlapping work pieces including a fastener body and a damper assembly operatively connected to the fastener body. The damper assembly is configured to enable application of a first load to the drill jig, and the fastener body is configured to enable application of a second load to the overlapping work pieces when the fastener fastens the drill jig to the overlapping work pieces. The first load is less than the second load. The first load is sufficient to hold the drill jig to the overlapping work pieces during drilling but without causing significant deformation of the drill jig. The second load is sufficient to reduce the formation of burrs during drilling of a hole through the overlapping working pieces.

First claim

What is claimed is:

1. A fastener for fastening a drill jig to overlapping work pieces and clamping the overlapping work pieces for facilitating accurate drilling of the overlapping work pieces, said fastener comprising:
a fastener body; and
a damper assembly,
wherein said damper assembly is operatively connected to said fastener body,
wherein said damper assembly is configured to enable application of a first load to said drill jig and said fastener body is configured to enable application of a second load to said overlapping work pieces when said fastener fastens the drill jig to the overlapping work pieces,
wherein said first load is less than said second load,
wherein said first load is sufficient to hold the drill jig to the overlapping work pieces during drilling but without causing significant deformation of the drill jig, and
wherein said second load is sufficient to reduce the formation of burrs during drilling of a hole through said overlapping working pieces.

2. The fastener of claim 1 further comprising a housing, wherein said damper assembly comprises a damper, wherein said housing houses said damper.

3. The fastener of claim 1 wherein said damper assembly comprises a wave spring.

4. The fastener of claim 3 further comprising a housing, wherein said housing houses said wave spring, wherein said damper assembly comprises an adjusting device, wherein said adjusting device is configured to adjust the axial length of said housing.

5. The fastener of claim 1 wherein said fastener body defines a through-bore, wherein said overlapping work pieces comprise a pilot hole, wherein said drill jig comprises a drill bushing, wherein said fastener body is configured to extend through said drill bushing such that said through-bore is aligned with said pilot hole, a sleeve, wherein said sleeve partially extends into said through-bore and engages said fastener body, wherein said sleeve is configured to extend through said pilot hole and engage said work pieces, a bolt, wherein said bolt extends through said through-bore and into threaded engagement with said sleeve.

6. The fastener of claim 1 wherein said damper assembly comprises a casing, wherein said casing extends around said fastener body, wherein said fastener body comprises a flange, wherein said damper assembly comprises an adjusting ring, wherein said flange, said casing and said adjusting ring define a housing for housing said damper, wherein said adjusting ring is configured to adjust the axial length of said housing.

7. The fastener of claim 6 further comprising a retaining ring, wherein said retaining ring comprises an outer portion, wherein said casing comprises a circumferential groove that receives said outer portion of said retaining ring to retain the damper assembly to the damper body.

8. The fastener of claim 6 wherein said adjusting ring is positioned between said damper body and said casing and extends around said damper body, wherein said adjusting ring is in threaded engagement with said casing such that rotation of said adjusting ring around said damper body adjusts the axial length of said housing.

9. A structural assembly comprising:
a drill jig, wherein the drill jig comprises a drill bushing;
overlapping work pieces, wherein said overlapping work pieces comprise a pilot hole; and
a fastener, wherein said fastener extends through said drill bushing and said pilot hole to fasten said drill jig to said overlapping work pieces and clamp the overlapping work pieces together for facilitating accurate drilling of the overlapping work pieces, wherein said fastener comprises:
a fastener body; and
a damper assembly, wherein said damper assembly is connected to said fastener body,
wherein said damper assembly enables application of a first load to said drill jig and said fastener body enables application of a second load to said overlapping work pieces, wherein said first load is less than said second load, wherein said first load is sufficient to hold the drill jig to the overlapping work pieces during drilling but without causing significant deformation of the drill jig, wherein said second load is sufficient to reduce the formation of burrs during drilling of a hole through said overlapping working pieces.

10. The structural assembly of claim 9 wherein one of said overlapping work pieces is formed from a metallic material and another one of said overlapping work pieces is formed from a composite material.

11. The structural assembly of claim 9 wherein one of said overlapping work pieces is formed from an aluminum material and another one of said overlapping work pieces is formed from a carbon fiber reinforced plastic material.

12. The structural assembly of claim 9 wherein said drill jig is formed of a material that has a hardness that is less than the hardness of the material of the overlapping work pieces.

13. The structural assembly of claim 9 wherein said overlapping work pieces are part of an aircraft.

14. The structural assembly of claim 9 wherein said damper assembly comprises a wave spring.

15. The structural assembly of claim 14 wherein said fastener body defines a through-bore, wherein said fastener body extends through said drill bushing such that said through-bore is aligned with said pilot hole, a sleeve, wherein said sleeve partially extends into said through-bore and engages said fastener body, wherein said sleeve extends through said pilot hole and engages said work pieces, a bolt, wherein said bolt extends through said through-bore and into threaded engagement with said sleeve.

16. The structural assembly of claim 9 wherein said damper assembly comprises a casing, where said casing extends around said fastener body, wherein said fastener body comprises a flange, wherein said damper assembly comprises an adjusting ring, wherein said adjusting ring is positioned between said damper body and said casing and extends around said damper body, wherein said flange, said casing and said adjusting ring define a housing for housing said damper, wherein said adjusting ring is in threaded engagement with said casing such that rotation of said adjusting ring around said damper body adjusts the axial length of said housing.

17. A method for fastening a drill jig to said overlapping work pieces and clamping said overlapping work pieces together for facilitating accurate drilling of said overlapping work pieces comprising:
positioning said drill jig onto said overlapping work pieces such that a drill bushing of said drill jig is aligned over a pilot hole in said overlapping work pieces;
inserting a fastener through said drill bushing and said pilot hole, wherein said fastener comprises a fastener body and damper assembly, wherein said damper assembly is operatively connected to said fastener body;
driving said fastener to a predetermined position such that a first load is applied via said damper assembly to said drill jig and a second load is applied via said fastener body to said overlapping work pieces, wherein said first load is less than said second load, wherein said first load is sufficient to hold the drill jig to the overlapping work pieces during drilling but without causing significant deformation of the drill jig, wherein said second load is sufficient to reduce burring during drilling of a hole through said overlapping working pieces.

18. The method of claim 17 wherein said fastener comprises a bolt and a sleeve, wherein said fastener body defines a through-bore, wherein said sleeve partially extends into said through-bore and engages said fastener body, wher

Assignees

• Boeing Co

Inventors

• Craig Brent F
• Dillon Patrick K
• Roberts Matthew K

Classifications

• B23B47/28 Primary

  Drill jigs for workpieces (equipment for setting or guiding the drill B23B49/00) · CPC title

• Y10T408/563

  Work-gripping clamp · CPC title

• B23B2215/04

  Aircraft components · CPC title

• B23B2260/136

  Springs · CPC title

• B23B2247/08

  Jigs for drilling overlapping or interfering holes · CPC title