Brake rod assembly

Patent metadata

Field	Value
Publication number	US-10358209-B2
Application number	US-201615067963-A
Country	US
Kind code	B2
Filing date	Mar 11, 2016
Priority date	Mar 12, 2015
Publication date	Jul 23, 2019
Grant date	Jul 23, 2019

Abstract

A brake rod assembly for an aircraft landing gear. The brake rod assembly includes a support member, a first brake rod having a first pivot point and a second pivot point, and a second brake rod. The support member is coupled to the first pivot point, the second brake rod is coupled to the second pivot point, and the first and second pivot points are longitudinally spaced apart along a first portion of the first brake rod.

First claim

The invention claimed is:

1. A brake rod assembly for an aircraft landing gear, the brake rod assembly comprising:
a bogie beam rotatably connected to a shock absorbing strut;
a first brake assembly coupled to the bogie beam at a first end of the bogie beam;
a second brake assembly coupled to the bogie beam at a second end of the bogie beam;
a first brake rod comprising a first pivot point located between a second pivot point at a first end of the first brake rod and a first brake fixing point at a second end of the first brake rod, the first brake rod being coupled to the shock absorbing strut at the first pivot point and coupled to the first brake assembly at the first brake fixing point; and
a second brake rod coupled at a first end thereof to the first brake rod at the second pivot point and coupled at a second end thereof to the second brake assembly.

2. The brake rod assembly according to claim 1 wherein the second pivot point is laterally offset from the first pivot point.

3. The brake rod assembly according to claim 1 wherein the second pivot point is one of a pin joint, a clevis joint, a knuckle joint, or a universal joint.

4. The brake rod assembly according to claim 1 wherein the rotation axes of the first pivot point and the second pivot point are parallel.

5. The brake rod assembly according to claim 1 wherein the rotation axes of the first pivot point and the second pivot point are not parallel.

6. An aircraft landing gear including at least one brake rod assembly according to claim 1 .

7. An aircraft including at least one aircraft landing gear according to claim 6 .

Assignees

• Safran Landing Systems Uk Ltd

Inventors

• Sexton Matthew
• Schmidt Robert Kyle
• Halford Thomas

Classifications

• B64U70/60

  Take-off or landing of UAVs from a runway using their own power · CPC title

• B64C25/42 Primary

  Arrangement or adaptation of brakes · CPC title

• B64C25/44 Primary

  Actuating mechanisms · CPC title

• B64C25/58

  Arrangements or adaptations of shock-absorbers or springs (shimmy-dampers B64C25/50) · CPC title