Hybrid metallic/composite joint with integral bearing

Patent metadata

Field	Value
Publication number	US-11534984-B2
Application number	US-201916379649-A
Country	US
Kind code	B2
Filing date	Apr 9, 2019
Priority date	Apr 9, 2019
Publication date	Dec 27, 2022
Grant date	Dec 27, 2022

Abstract

A metallic-composite joint fitting is provided. The fitting may comprise a composite structure, an integral bearing comprising a first frustoconical portion and a second frustoconical portion each having a complimentary shape to the composite structure, a sleeve comprising a third frustoconical portion coupled to a cylindrical bearing surface of the integral bearing, and a metallic end fitting coupled to the third frustoconical portion, wherein the metallic end fitting comprises a bearing portion contacted with the cylindrical bearing surface.

First claim

What is claimed is:

1. A metallic-composite joint fitting, comprising:
a composite structure for receiving a metallic end structure, the composite structure comprising:
an integral bearing comprising a first frustoconical portion and a second frustoconical portion each having a complimentary shape to the composite structure; and
a sleeve comprising a bearing surface portion, a third frustoconical portion at a first end of the bearing surface portion, and a flange at a second end of the bearing surface portion opposite to the first end, wherein a first surface of the bearing surface portion is coupled to a cylindrical bearing surface of the integral bearing; and

the metallic end fitting coupled to the third frustoconical portion of the sleeve, wherein the metallic end fitting comprises a bearing portion in contact with a second surface opposite the first surface of the bearing surface portion of the sleeve.

2. The metallic-composite joint fitting of claim 1 , wherein the composite structure is wrapped over the integral bearing.

3. The metallic-composite joint fitting of claim 2 , wherein the composite structure comprises a cylindrical portion and a flared end portion, wherein the flared end portion has a complimentary shape to each of the first frustoconical portion, the second frustoconical portion, and the third frustoconical portion.

4. The metallic-composite joint fitting of claim 1 , wherein the bearing portion of the metallic end fitting comprises a flange.

5. The metallic-composite joint fitting of claim 1 , wherein the metallic end fitting comprises an externally threaded portion coupled to the third frustoconical portion at an internally threaded surface of the third frustoconical portion of the sleeve.

6. The metallic-composite joint fitting of claim 5 , wherein the externally threaded portion has a relatively smaller diameter than the bearing portion.

7. The metallic-composite joint fitting of claim 5 , wherein a relative length ratio of the externally threaded portion to the bearing portion is 1:3 or less.

8. The metallic-composite joint fitting of claim 1 , wherein the integral bearing comprises at least one of a steel, a stainless steel, a titanium, a titanium alloy, an aluminum, an aluminum alloy, a bearing metal, a composite, a plastic, a thermoplastic, a glass, or a ceramic.

9. A landing gear system, comprising:
a shock strut coupled to an axle;
a wheel coupled to the axle; and
a metallic-composite joint fitting, comprising:
a composite structure for receiving a metallic end structure, the composite structure comprising:
an integral bearing comprising a first frustoconical portion and a second frustoconical portion each having a complimentary shape to the composite structure; and
a sleeve comprising a bearing surface portion, a third frustoconical portion at a first end of the bearing surface portion, and a flange at a second end of the bearing surface portion opposite to the first end, wherein a first surface of the bearing surface portion is coupled to a cylindrical bearing surface of the integral bearing; and

the metallic end fitting coupled to the third frustoconical portion of the sleeve, wherein the metallic end fitting comprises a bearing portion in contact with a second surface opposite the first surface of the bearing surface portion of the sleeve.

10. The landing gear system of claim 9 , wherein the composite structure is wrapped over the integral bearing.

11. The landing gear system of claim 10 , wherein the composite structure comprises a cylindrical portion and a flared end portion, wherein the flared end portion has a complimentary shape to each of the first frustoconical portion, the second frustoconical portion, and the third frustoconical portion.

12. The landing gear system of claim 9 , wherein the bearing portion of the metallic end fitting comprises a flange.

13. The landing gear system of claim 9 , wherein the metallic end fitting comprises an externally threaded portion coupled to the third frustoconical portion at an internally threaded surface of the third frustoconical portion of the sleeve.

14. The landing gear system of claim 13 , wherein the externally threaded portion has a relatively smaller diameter than the bearing portion.

15. The landing gear system of claim 13 , wherein a relative length ratio of the externally threaded portion to the bearing portion is 1:3 or less.

16. A method of joining a composite structure and a metallic end fitting, comprising:
coupling an integral bearing about a sleeve, wherein the sleeve comprises a bearing surface portion, a frustoconical portion at a first end of the bearing surface portion, and a flange at a second end of the bearing surface portion opposite to the first end and wherein a first surface of the bearing surface portion is coupled to a cylindrical bearing surface of the integral bearing;
wrapping the composite structure about the integral bearing to form a flared end portion of the composite structure;
inserting a coupling portion of the metallic end fitting into the sleeve; and
engaging a bearing portion of the coupling portion with a second surface opposite the first surface of the bearing surface portion of the sleeve and coupling an externally threaded portion of the coupling portion to an internally threaded portion of the frustoconical portion of the sleeve.

Assignees

• Goodrich Corp

Inventors

• Baird Bradley William
• Allen Jason Bradley

Classifications

• F16L19/065

  the wedging action being effected by means of a ring · CPC title

• F16L19/08

  with metal rings which bite into the wall of the pipe {(F16L19/045 takes precedence)} · CPC title

• B64C25/60

  Oleo legs · CPC title

• F16C7/026 Primary

  made of fibre reinforced resin · CPC title

• B64C25/32

  characterised by elements which contact the ground or similar surface  (arrester hooks B64C25/68) · CPC title