Hybrid metallic/composite joint with separate internal bearing

Patent metadata

Field	Value
Publication number	US-11512738-B2
Application number	US-201916381808-A
Country	US
Kind code	B2
Filing date	Apr 11, 2019
Priority date	Apr 11, 2019
Publication date	Nov 29, 2022
Grant date	Nov 29, 2022

Abstract

A metallic-composite joint fitting is provided. The fitting may comprise a frustoconical internal bearing having a bore, a conical sleeve configured to be disposed about the frustoconical internal bearing, a composite structure configured to couple between the frustoconical internal bearing and the conical sleeve, a metallic end fitting configured to be disposed within the bore and couple to the frustoconical internal bearing, and an external nut configured to couple to the metallic end fitting and the conical sleeve, wherein at least one of the frustoconical internal bearing or the conical sleeve comprises a flanged portion mutually configured to couple the conical sleeve to the frustoconical internal bearing via a locking ring.

First claim

What is claimed is:

1. A metallic-composite joint fitting, comprising:
a frustoconical internal bearing having a bore;
a conical sleeve configured to be disposed about the frustoconical internal bearing;
a composite structure configured to couple between the frustoconical internal bearing and the conical sleeve;
a metallic end fitting configured to be disposed within the bore and couple to the frustoconical internal bearing, wherein the metallic end fitting comprises a bearing portion configured to be disposed within the bore; and
an external nut configured to couple to the metallic end fitting and the conical sleeve,
wherein at least one of the frustoconical internal bearing or the conical sleeve comprises a flanged portion mutually configured to couple the conical sleeve to the frustoconical internal bearing via a locking ring.

2. The metallic-composite joint fitting of claim 1 , further comprising an internal bolt coupled within the bore, wherein the metallic end fitting is coupled to the internal bolt.

3. The metallic-composite joint fitting of claim 2 , wherein the composite structure comprises a cylindrical portion and a conical end portion.

4. The metallic-composite joint fitting of claim 3 , wherein the conical end portion is coupled relatively between the frustoconical internal bearing at a first conical bearing surface and the conical sleeve at a second conical bearing surface.

5. The metallic-composite joint fitting of claim 4 , wherein the conical end portion is flared.

6. The metallic-composite joint fitting of claim 1 , wherein the bearing portion contacts the frustoconical internal bearing at a cylindrical bearing surface.

7. The metallic-composite joint fitting of claim 1 , wherein the internal bolt is integral to the frustoconical internal bearing.

8. The metallic-composite joint fitting of claim 1 , wherein the metallic end fitting is coupled to the internal bolt at an internally threaded surface of the metallic end fitting.

9. The metallic-composite joint fitting of claim 1 , wherein the external nut is contacted with the conical sleeve via an end washer.

10. The metallic-composite joint fitting of claim 1 , wherein the conical sleeve comprises the flanged portion coupled to the frustoconical internal bearing via the locking ring.

11. 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 frustoconical internal bearing;
an internal bolt coupled within a bore of the frustoconical internal bearing;
a metallic end fitting coupled to the internal bolt, wherein the metallic end fitting comprises a bearing portion disposed within the bore;
a conical sleeve disposed about the frustoconical internal bearing; and
an external nut coupled to the metallic end fitting and the conical sleeve,
wherein the conical sleeve comprises a flanged portion coupled to the frustoconical internal bearing.

12. The landing gear system of claim 11 , wherein a composite structure is coupled between the frustoconical internal bearing and the conical sleeve.

13. The landing gear system of claim 12 , wherein the composite structure comprises a cylindrical portion and a conical end portion.

14. The landing gear system of claim 13 , wherein the conical end portion is coupled relatively between the frustoconical internal bearing at a first conical bearing surface and the conical sleeve at a second conical bearing surface.

15. The landing gear system of claim 14 , wherein the conical end portion is flared.

16. The landing gear system of claim 11 , wherein the bearing portion contacts the frustoconical internal bearing at a cylindrical bearing surface.

17. The landing gear system of claim 11 , wherein the internal bolt is integral to the frustoconical internal bearing.

18. The landing gear system of claim 11 , wherein the metallic end fitting is coupled to the internal bolt at an internally threaded surface of the metallic end fitting.

19. The landing gear system of claim 11 , wherein the flanged portion of the conical sleeve is coupled to the frustoconical internal bearing via a locking ring.

20. A method of joining a composite structure and a metallic end fitting, comprising:
coupling an internal bolt within a bore of a frustoconical internal bearing;
wrapping the composite structure over the frustoconical internal bearing to form a conical end portion;
disposing a conical sleeve over the conical end portion to enclose the conical end portion between a first conical bearing surface and a second conical bearing surface and coupling a flanged portion of the conical sleeve to the frustoconical internal bearing;
inserting a bearing portion of the metallic end fitting into the bore of the frustoconical internal bearing and coupling the internal bolt to an internally threaded surface of the metallic end fitting; and
coupling an external nut to an externally threaded surface of the metallic end fitting and contacting the external nut with the flanged portion of the conical sleeve.

Assignees

• Goodrich Corp

Inventors

• Baird Bradley William

Classifications

• F16B7/0406

  for rods or tubes being coaxial (F16B7/10 takes precedence) · CPC title

• B64C25/02

  Undercarriages · CPC title

• F16C7/026

  made of fibre reinforced resin · CPC title

• F16C2326/43

  Aeroplanes; Helicopters · CPC title

• F16D2001/0903

  the clamped shaft being hollow · CPC title