Hybrid brake system
US-12179912-B2 · Dec 31, 2024 · US
Brake rod assembly
US2016264235A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016264235-A1 |
| Application number | US-201615067963-A |
| Country | US |
| Kind code | A1 |
| Filing date | Mar 11, 2016 |
| Priority date | Mar 12, 2015 |
| Publication date | Sep 15, 2016 |
| Grant date | — |
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- Title
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- Abstract
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Abstract
Official abstract text for this publication.
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
Opening claim text (preview).
1 . A brake rod assembly for an aircraft landing gear, the brake rod assembly comprising: a first brake rod comprising a first pivot point and a second pivot point, the first and second pivot points are longitudinally spaced apart along a portion of the first brake rod; a second brake rod coupled to the second pivot point; a shock absorbing strut coupled to the first pivot point. 2 . A brake rod assembly according to claim 1 wherein the portion of the first brake rod is not parallel to the remainder of the first brake rod. 3 . A 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 . A brake rod assembly according to claim 1 wherein the rotation axes of the first pivot point and the second pivot point are parallel. 5 . A 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 .
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Frequently asked questions
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- What does patent US2016264235A1 cover?
- 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 po…
- Who is the assignee on this patent?
- Messier-Dowty Ltd, Messier Bugatti Dowty
- What technology area does this patent fall under?
- Primary CPC classification B64C25/44. Mapped technology areas include Operations & Transport.
- When was this patent published?
- Publication date Thu Sep 15 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). Legal status and post-grant events are not shown on this page.
- What related patents are in patentsdb?
- We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).