Nut retention system

Patent metadata

Field	Value
Publication number	US-10465740-B2
Application number	US-201615354676-A
Country	US
Kind code	B2
Filing date	Nov 17, 2016
Priority date	Nov 17, 2016
Publication date	Nov 5, 2019
Grant date	Nov 5, 2019

Abstract

A nut retention arrangement may comprise a first nut comprising a first threaded aperture and a first retention aperture, a second nut comprising a second threaded aperture and a second retention aperture, and a tensile member having a first end extending through the first retention aperture and a second end extending through the second retention aperture such that rotation in a direction toward loosening of either the first nut or the second nut causes rotation in a direction toward tightening of the other of the first nut or the second nut.

First claim

What is claimed is:

1. A nut retention arrangement comprising:
a first nut comprising:
a first annular wall defining a first threaded aperture extending along a rotational axis of the first nut, the first annular wall configured to engage a first threaded fastener via the first threaded aperture;
a first flange circumferentially disposed about the first annular wall; and
a first retention aperture disposed in the first flange, wherein the first retention aperture extends through the first flange without breaching the first threaded aperture;

a second nut comprising:
a second annular wall defining a second threaded aperture extending along a rotational axis of the second nut, the second annular wall configured to engage a second threaded fastener via the second threaded aperture;
a second flange circumferentially disposed about the second annular wall; and
a second retention aperture disposed in the second flange, wherein the second retention aperture extends through the second flange without breaching the second threaded aperture; and

a tensile member having a first end extending through the first retention aperture and a second end extending through the second retention aperture such that rotation in a direction toward loosening of either the first nut or the second nut causes rotation in a direction toward tightening of the other of the first nut or the second nut.

2. The nut retention arrangement of claim 1 , further comprising:
a first threaded fastener; and
a second threaded fastener,
wherein the first nut is coupled to the first threaded fastener, the first threaded aperture engaging the first threaded fastener, and
the second nut is coupled to the second threaded fastener, the second threaded aperture engaging the second threaded fastener.

3. The nut retention arrangement of claim 2 , wherein the tensile member prevents the first nut from rotating with respect to the first threaded fastener and prevents the second nut from rotating with respect to the second threaded fastener.

4. The nut retention arrangement of claim 1 , further comprising:
a first ferrule coupled to the first end; and
a second ferrule coupled to the second end.

5. The nut retention arrangement of claim 4 , wherein the first ferrule prevents the first end from translating through the first retention aperture.

6. The nut retention arrangement of claim 1 , wherein the first retention aperture extends in a direction orthogonal to the rotational axis of the first nut.

7. The nut retention arrangement of claim 1 , wherein the tensile member comprises:
a first strand twisted together with a second strand,
wherein the first strand extends through the first retention aperture, and
one of the first strand or the second strand extends through the second retention aperture.

8. The nut retention arrangement of claim 7 , wherein the first end of the tensile member terminates with the first strand twisted together with the second strand.

9. The nut retention arrangement of claim 7 , wherein the second end of the wire terminates with the first strand coupled to the second strand at a bend in the tensile member.

10. A method of servicing an aircraft to prevent threaded fasteners from loosening comprising:
replacing a first threaded fastener on an aircraft with a first anti-loosening nut, comprising:
a first annular wall defining a first threaded aperture extending along a rotational axis of the first nut, the first annular wall configured to engage a first threaded fastener via the first threaded aperture;
a first flange circumferentially disposed about the first annular wall; and
a first retention aperture disposed in the first flange, wherein the first retention aperture extends through the first flange without breaching the first threaded aperture;

replacing a second threaded fastener on the aircraft with a second anti-loosening nut, comprising:
a second annular wall defining a second threaded aperture extending along a rotational axis of the second nut, the second annular wall configured to engage a second threaded fastener via the second threaded aperture;
a second flange circumferentially disposed about the second annular wall; and
a second retention aperture disposed in the second flange, wherein the second retention aperture extends through the second flange without breaching the second threaded aperture; and

connecting a tensile member between the first anti-loosening nut and the second anti-loosening nut by extending a first end of the tensile member through the first retention aperture and a second end of the tensile member through the second retention aperture, such that rotation in a direction toward loosening of either the first anti-loosening nut or the second anti-loosening nut causes rotation in a direction toward tightening of the other of the first anti-loosening nut or the second anti-loosening nut.

11. The method of claim 10 , wherein the tensile member comprises at least one of a wire or a cable.

12. A nut comprising:
an annular wall defining a threaded aperture extending along a rotational axis of the nut, the annular wall configured to engage a threaded fastener via the threaded aperture;
a flange circumferentially disposed about the annular wall; and
a first retention aperture disposed in the flange, wherein the first retention aperture extends through the flange without breaching the threaded aperture.

13. The nut of claim 12 , wherein the first retention aperture extends in a direction perpendicular to the rotational axis.

14. The nut of claim 13 , wherein the first retention aperture is configured to receive a tensile member.

15. The nut of claim 14 , further comprising:
a second retention aperture disposed in the flange.

16. The nut of claim 15 , wherein the first retention aperture and the second retention aperture are circumferentially spaced about the flange.

17. The nut of claim 15 , wherein the flange extends from the annular wall at a terminus of the nut.

Assignees

• Goodrich Corp

Inventors

• Freshour Thomas

Classifications

• B64C25/42

  Arrangement or adaptation of brakes · CPC title

• F16B39/28 Primary

  by special members on, or shape of, the nut or bolt (F16B39/26 takes precedence; locknuts F16B39/12) · CPC title

• B64C25/34

  wheeled type, e.g. multi-wheeled bogies · CPC title

• F16B39/101 Primary

  with a plate, spring, wire or ring holding two or more nuts or bolt heads which are mainly in the same plane · CPC title