Pinned lug joint
US-9150302-B2 · Oct 6, 2015 · US
Apparatus and system for preventing wear to a component
US9278752B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9278752-B2 |
| Application number | US-201414216283-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 17, 2014 |
| Priority date | Mar 17, 2014 |
| Publication date | Mar 8, 2016 |
| Grant date | Mar 8, 2016 |
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- Title
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- Abstract
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Abstract
Official abstract text for this publication.
In an embodiment, a system may include an aircraft clevis comprising two opposite sides and a longitudinal axis located between the two opposite sides. The longitudinal axis may be parallel to the two opposite sides. The system may include a slider positioned within the aircraft clevis and along the longitudinal axis. The system may include a clip configured to prevent the slider from rotating about the longitudinal axis by having at least a first portion of the clip coupled to one of the two opposite sides of the aircraft clevis and at least a second portion of the clip in contact with the slider.
First claim
Opening claim text (preview).
What is claimed is: 1. An apparatus, comprising: a first member and a second member for positioning the apparatus between a first arm and a second arm of an aircraft clevis, the first member and the second member each positioned on opposite sides of a longitudinal axis, the longitudinal axis being parallel to at least a portion of the first member and the second member and being substantially midway between the first member and the second member, the first member and the second me…
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Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
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Frequently asked questions
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- What does patent US9278752B2 cover?
- In an embodiment, a system may include an aircraft clevis comprising two opposite sides and a longitudinal axis located between the two opposite sides. The longitudinal axis may be parallel to the two opposite sides. The system may include a slider positioned within the aircraft clevis and along the longitudinal axis. The system may include a clip configured to prevent the slider from rotating …
- Who is the assignee on this patent?
- Osvog Andrew J, Lockheed Corp
- What technology area does this patent fall under?
- Primary CPC classification B64C9/02. Mapped technology areas include Operations & Transport.
- When was this patent published?
- Publication date Tue Mar 08 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
- What related patents are in patentsdb?
- We list 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).