Seal-cover assembly for an aircraft or other structure and a method of assembling the same

Patent metadata

Field	Value
Publication number	US-11891189-B2
Application number	US-202117527056-A
Country	US
Kind code	B2
Filing date	Nov 15, 2021
Priority date	Nov 19, 2020
Publication date	Feb 6, 2024
Grant date	Feb 6, 2024

Abstract

A seal-cover assembly for a structure including a first side and a second side opposing the first side. The seal-cover assembly includes a cap defining a recess, and an insert fixed to the cap within the recess to form a cover unit. The cover unit is configured to be secured to the first side of the structure. The seal-cover assembly includes a fastener configured to be disposed through the structure from the second side of the structure. The fastener is attached to the cover unit relative to the second side without accessing the first side of the structure. Additionally, an aircraft includes the structure and the seal-cover assembly as discussed above. Furthermore, a method of assembling the seal-cover assembly to the structure includes the cover unit secured to the first side of the structure such that an interior of the cover unit is inaccessible from the first side.

First claim

What is claimed is:

1. A seal-cover assembly for a structure including a first side and a second side opposing the first side, the seal-cover assembly comprising:
a cap defining a recess;
an insert fixed to the cap within the recess to form a cover unit;
wherein the cover unit is configured to be secured to the first side of the structure; and
a fastener configured to be disposed through the structure from the second side of the structure, and the fastener is attached to the cover unit relative to the second side without accessing the first side of the structure.

2. The seal-cover assembly as set forth in claim 1 wherein the fastener is attached to the insert of the cover unit such that the cap conceals the fastener relative to the first side of the structure.

3. The seal-cover assembly as set forth in claim 2 wherein:
the insert includes an outer surface; and
the cap is formed of a nonconductive material that is permanently attached to the outer surface of the insert to form the cover unit.

4. The seal-cover assembly as set forth in claim 3 wherein:
the outer surface of the insert includes a grip feature; and
the nonconductive material of the cap is formed around the grip feature to permanently attach the cap to the outer surface of the insert.

5. The seal-cover assembly as set forth in claim 3 wherein the insert is formed of a metallic material that is different from the nonconductive material.

6. The seal-cover assembly as set forth in claim 2 wherein:
the cap includes an end face defining the recess that extends into the cap;
the cap includes an exterior surface that extends from the end face to surround the recess and the insert; and
the end face defines a groove spaced from the recess, and the groove surrounds the insert.

7. The seal-cover assembly as set forth in claim 1 :
further including a washer having an outer edge;
wherein the insert defines a first aperture disposed along a longitudinal axis and a second aperture disposed along the longitudinal axis adjacent to the first aperture;
wherein the fastener is disposed through both of the first aperture and the second aperture; and
wherein the washer is disposed inside of the second aperture of the insert, and the outer edge of the washer is secured to the insert inside of the second aperture.

8. The seal-cover assembly as set forth in claim 7 wherein:
the first aperture of the insert has a first diameter and the second aperture of the insert has a second diameter;
the first diameter is less than the second diameter; and
the fastener is threaded to the insert inside of the first aperture, and the washer is threaded to the insert inside of the second aperture.

9. The seal-cover assembly as set forth in claim 8 wherein:
the insert includes a first threaded portion that faces into the first aperture and a second threaded portion that faces into the second aperture;
the first threaded portion presents threads in a first direction;
the second threaded portion presents threads in a second direction; and
the first direction and the second direction are different from each other.

10. The seal-cover assembly as set forth in claim 1 wherein:
the cap includes an end face defining a groove; and
the groove is spaced from and surrounds the insert.

11. The seal-cover assembly as set forth in claim 1 :
wherein the insert defines a first aperture disposed along a longitudinal axis and a second aperture disposed along the longitudinal axis adjacent to the first aperture;
further including a washer having an inner edge defining a hole disposed along the longitudinal axis, and the fastener is disposed in the hole of the inner edge and disposed in the first aperture of the insert; and
wherein the washer has an outer edge opposing the inner edge, and the insert is threaded to the outer edge of the washer such that the washer is disposed inside of the second aperture.

12. The seal-cover assembly as set forth in claim 1 wherein:
the fastener is formed of a metallic material;
the cap is formed of a nonconductive material that is different from the metallic material of the fastener;
the insert includes an outer surface having a grip feature; and
the nonconductive material of the cap is formed around the grip feature to permanently attach the cap to the outer surface of the insert and the cap encloses an end portion of the fastener relative to the first side of the structure.

13. The seal-cover assembly as set forth in claim 1 wherein:
the insert includes an outer surface; and
the cap is formed of a nonconductive material that is permanently attached to the outer surface of the insert to form the cover unit.

14. An aircraft comprising:
a structure including a first side and a second side that opposes the first side;
a seal-cover assembly comprising:
a cap defining a recess;
an insert fixed to the cap within the recess to form a cover unit;
wherein the cover unit is secured to the first side of the structure; and
a fastener disposed through the structure from the second side of the structure, and the fastener is attached to the cover unit relative to the second side without accessing the first side of the structure.

15. The aircraft as set forth in claim 14 wherein:
the seal-cover assembly includes a washer secured to the first side of the structure, and the washer includes an outer edge;
the insert defines a first aperture and a second aperture disposed adjacent to the first aperture;
the outer edge of the washer is secured to the insert inside of the second aperture such that the cap abuts the first side of the structure to enclose the washer between the cover unit and the first side of the structure;
the fastener is secured to the insert inside of the first aperture; and
the cap encloses the insert and an end portion of the fastener relative to the first side of the structure such that the fastener is inaccessible from the first side of the structure.

16. The aircraft as set forth in claim 15 wherein:
the insert includes an outer surface;
the cap is formed of a nonconductive material that is permanently attached to the outer surface of the insert to form the cover unit;
the cap includes an end face that abuts the first side of the structure;
the insert includes a first threaded portion that faces into the first aperture and a second threaded portion that faces into the second aperture;
the first threaded portion presents threads in a first direction;
the second threaded portion presents threads in a second direction;
the first direction and the second direction are different from each other;
the outer edge of the washer and the second threaded portion of the insert are threaded together; and
the end portion of the fastener and the first threaded portion of the insert are threaded together without accessing the outer surface of the insert and without causing the cover unit to unthread from the washer.

17. A method of assembling a seal-cover assembly to a structure, the method comprising:
securing a cover unit to a first side of the structure such that an interior of the cover unit is inaccessible from the first side of the structure;
inserting a fastener through the structure relative to a second side of the structure; and
attaching the fastener to the interior of the cover unit relative to the second side of the structure without accessing the first side of the structure to attach the fastener to the cover unit.

18. The method as set forth in claim 17 :
further comprising securing a washer to the first side of the

Assignees

• Boeing Co

Inventors

• Cowan Daniel James
• Stevens Bart

Classifications

• B64D45/02 Primary

  Lightning protectors; Static dischargers · CPC title

• F16B33/004

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

• F16B37/14

  Cap nuts; Nut caps or bolt caps · CPC title