Attachment of composite lug to composite structural tube

Patent metadata

Field	Value
Publication number	US-11536306-B2
Application number	US-202117192451-A
Country	US
Kind code	B2
Filing date	Mar 4, 2021
Priority date	May 22, 2015
Publication date	Dec 27, 2022
Grant date	Dec 27, 2022

Abstract

A landing gear system includes a composite tube. The composite tube comprises at least one of (i) a filament wound composite tube, (ii) a filament braided tube, and (iii) a composite tube of laid up filament. The landing gear system further comprises a first lug cluster mounted to the composite tube and a second lug cluster mounted to the composite tube. The first lug cluster and the second lug cluster are oriented at an angle to one another.

First claim

What is claimed is:

1. A landing gear system comprising:
a composite tube comprising at least one of:
a filament wound composite tube;
a filament braided tube; or
a laid up filament;

a first lug cluster mounted to the composite tube; and
a second lug cluster mounted to the composite tube;
wherein the first lug cluster and the second lug cluster are oriented at an angle to one another; and
the first lug cluster comprises:
a first side comprising a first flange comprising a first side groove receiving a first fiber filament according to a first filament path;
a second side comprising a second flange comprising a second side groove receiving the first fiber filament according to the first filament path; and
a first saddle comprising:
a first floor member formed to follow a contour of the composite tube; and
a first upper infill member resting on the first floor member and positioned between the first side and the second side.

2. The landing gear system according to claim 1 , wherein the second lug cluster comprises:
a third side comprising a third flange comprising a third side groove receiving a second fiber filament according to a second filament path;
a fourth side comprising a fourth flange comprising a fourth side groove receiving the second fiber filament according to the second filament path; and
a second saddle comprising:
a second floor member formed to follow the contour of the composite tube;
a second upper infill member resting on the second floor member and positioned between the third side and the fourth side.

3. The landing gear system according to claim 2 , wherein the composite tube comprises a landing gear strut.

4. The landing gear system according to claim 2 , wherein the second lug cluster is secured in compression against the composite tube via the second fiber filament.

5. The landing gear system according to claim 2 , wherein the third side groove is disposed in an outer periphery of the third side and the fourth side groove in disposed in an outer periphery of the fourth side.

6. The landing gear system according to claim 1 , wherein the first floor member comprises a tube contour edge comprising an arc corresponding to a partial circumference of the composite tube.

7. The landing gear system according to claim 6 , wherein the composite tube comprises a first radius, and the tube contour edge comprises a second radius equal to the first radius of the composite tube.

8. The landing gear system according to claim 1 , wherein the first lug cluster is secured in compression against the composite tube via the first fiber filament.

9. The landing gear system according to claim 1 , wherein the first side groove is disposed in an outer periphery of the first side and the second side groove in disposed in an outer periphery of the second side.

Assignees

• Goodrich Corp

Inventors

• Luce William E

Classifications

• F16B5/125 Primary

  one of the auxiliary fasteners is comprising wire or sheet material or is made thereof · CPC title

• B29L2031/3076

  Aircrafts (blades, propellers B29L2031/08) · CPC title

• B29K2715/00

  Condition, form or state of preformed parts, e.g. inserts · CPC title

• B29C70/683

  Pretreatment of the preformed part, e.g. insert · CPC title

• B29C70/84

  by moulding material on preformed parts to be joined {(joining plastic parts by moulding B29C65/70)} · CPC title