Fluid-tight mechanical fastening system and associated structural assembly

Patent metadata

Field	Value
Publication number	US-10329008-B2
Application number	US-201615191819-A
Country	US
Kind code	B2
Filing date	Jun 24, 2016
Priority date	Jun 24, 2016
Publication date	Jun 25, 2019
Grant date	Jun 25, 2019

Abstract

A structural assembly including a first member having an external side and an internal side, the first member defining a first member through-bore, a second member having an external side and an internal side, the second member defining a second member through-bore aligned with the first member through-bore, and a mechanical fastening system including a bushing at least partially received in the first member through-bore, the bushing defining a bushing through-bore and including a flange, wherein the flange is positioned in a gap between the internal side of the first member and the external side of the second member, a nut plate connected to the internal side of the second member, the nut plate defining a clearance bore aligned with the second member through-bore and the bushing through-bore, the nut plate including a nut, and a bolt extending through the bushing through-bore and into threaded engagement with the nut.

First claim

What is claimed is:

1. A structural assembly comprising:
a first member comprising an external side and an internal side, said first member defining a first member through-bore;
a second member comprising an external side and an internal side, said second member defining a second member through-bore aligned with said first member through-bore; and
a mechanical fastening system comprising:
a bushing at least partially received in said first member through-bore, said bushing defining a bushing through-bore and comprising a flange, wherein said flange is positioned in a gap between said internal side of said first member and said external side of said second member;
a nut plate connected to said internal side of said second member, said nut plate defining an enclosed clearance bore aligned with said second member through-bore and said bushing through-bore, said nut plate comprising a nut, wherein said enclosed clearance bore extends from a first end portion adjacent to said second member to a second end portion opposite said first end portion, wherein said first end portion is an open end and said second end portion is a closed end; and
a bolt extending through said bushing through-bore and into threaded engagement with said nut.

2. The structural assembly of claim 1 further comprising a first seal sealing an interface between said flange and said internal side of said first member.

3. The structural assembly of claim 2 wherein said first seal comprises a fillet seal.

4. The structural assembly of claim 1 further comprising a second seal positioned between said flange and said external side of said second member.

5. The structural assembly of claim 4 wherein said second seal comprises an O-ring, and wherein said O-ring is received in a groove formed in said bushing.

6. The structural assembly of claim 1 further comprising a third seal positioned between said nut plate and said internal side of said second member.

7. The structural assembly of claim 6 wherein said third seal comprises an O-ring, and wherein said O-ring is received in a groove formed in said nut plate.

8. The structural assembly of claim 1 further comprising an outer bushing at least partially received in said first member through-bore, said outer bushing defining an outer bushing through-bore aligned with said bushing through-bore of said bushing.

9. The structural assembly of claim 8 wherein said first member through-bore comprises a countersink, and wherein said outer bushing is seated in said countersink.

10. The structural assembly of claim 8 wherein said outer bushing is formed from a metallic material.

11. The structural assembly of claim 10 wherein said bushing and said nut plate are formed from a polymeric material.

12. The structural assembly of claim 1 wherein said nut is press-fit into said clearance bore.

13. The structural assembly of claim 1 wherein said nut plate is connected to said internal side of said second member with mechanical fasteners.

14. An aircraft comprising said structural assembly of claim 1 .

15. The aircraft of claim 14 wherein said first member comprises an aircraft wing skin panel and said second member comprises a rib.

16. A structural assembly comprising:
a first member comprising an external side and an internal side, said first member defining a first member through-bore;
a second member comprising an external side and an internal side, said second member defining a second member through-bore aligned with said first member through-bore; and
a mechanical fastening system comprising:
an outer bushing at least partially received in said first member through-bore proximate said external side of said first member, said outer bushing defining an outer bushing through-bore;
an inner bushing at least partially received in said first member through-bore proximate said internal side of said first member, said inner bushing defining an inner bushing through-bore and comprising a flange positioned in a gap between said internal side of said first member and said external side of said second member, wherein said flange is in sealing engagement with said external side of said second member;
a fillet seal sealing an interface between said flange and said internal side of said first member;
a nut plate in sealing engagement with said internal side of said second member, said nut plate defining an enclosed clearance bore and comprising a nut received in said clearance bore, wherein said enclosed clearance bore extends from a first end portion adjacent to said second member to a second end portion opposite said first end portion, wherein said first end portion is an open end and said second end portion is a closed end; and
a bolt extending through said outer bushing through-bore and said inner bushing through-bore, and into threaded engagement with said nut.

17. The structural assembly of claim 16 wherein said outer bushing is formed from a metallic material and said inner bushing is formed from a polymeric material.

18. A method for assembling a first member and a second member comprising:
forming a first member through-bore in said first member and a second member through-bore in said second member;
inserting a bushing into said first member through-bore, said bushing defining a bushing through-bore and comprising a flange, wherein said flange abuts an internal side of said first member;
connecting a nut plate to an internal side of said second member, wherein said nut plate defines an enclosed clearance bore aligned with said second member through-bore and comprises a nut received in said clearance bore, wherein said enclosed clearance bore extends from a first end portion adjacent to said second member to a second end portion opposite said first end portion, wherein said first end portion is an open end and said second end portion is a closed end;
aligning said bushing through-bore with said second member through-bore; and
inserting a bolt through said bushing through-bore and threading said bolt into engagement with said nut.

19. The method of claim 18 further comprising:
applying a first seal to an interface between said flange and said internal side of said first member;
applying a second seal to said flange such that said second seal seals an interface between said flange and an external side of said second member; and
applying a third seal to said nut plate such that said third seal seals an interface between said nut plate and said internal side of said second member.

20. The method of claim 18 further comprising trimming said flange prior to said step of inserting said bolt.

Assignees

• Boeing Co

Inventors

• Walker Steven P
• Plass Christopher E
• Klein Michael K
• Salmi John V

Classifications

• F16B5/02

  by means of fastening members using screw-thread ({F16B5/0004 takes precedence}; construction of screw-threaded connections F16B25/00 - F16B39/00) · CPC title

• B64C3/26 Primary

  Construction, shape, or attachment of separate skins, e.g. panels · CPC title

• F16B37/14

  Cap nuts; Nut caps or bolt caps · CPC title

• B64F5/10 Primary

  Manufacturing or assembling aircraft, e.g. jigs therefor · CPC title

• F16B33/004

  Sealing; Insulation (by means of washers F16B43/001) · CPC title