Airplane off ground advisory system
US-9221556-B2 · Dec 29, 2015 · US
Cantilevered differential motion sensor and associated frame
US9102418B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9102418-B2 |
| Application number | US-97711410-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 23, 2010 |
| Priority date | Oct 28, 2010 |
| Publication date | Aug 11, 2015 |
| Grant date | Aug 11, 2015 |
How to read this patent
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
- Title
What the patent document calls the invention.
- Abstract
A short plain-language summary of the technical disclosure.
- Assignees and inventors
Who owns or filed the patent and who is credited as inventor.
- Key dates
Filing, priority, publication, and grant dates set the timeline.
- First independent claim
The legal scope of protection — read this for what is actually claimed.
- CPC / IPC classifications
Technology tags used to group this patent with similar filings.
- Citations and related patents
Prior art links and similar publications in this corpus.
Abstract
Official abstract text for this publication.
The disclosed sensor includes a frame having a base and a plurality of arms integral with the base. The arms are biased to a relaxed position, which may be an extended position. A fuse is fastened between the arms to hold the arms in a non-relaxed position. When incorporated into an aircraft, for example, the disclosed sensor may be connected to a first panel, and a pin connected to a second panel may be positioned between the arms.
First claim
Opening claim text (preview).
What is claimed is: 1. A sensor for an aircraft, comprising: a frame including a base and a plurality of arms integrally formed with the base, the arms moveable between an relaxed position and a non-relaxed position, the arms being biased towards the relaxed position; and an electromechanical fuse fastened to the arms to hold the arms in the non-relaxed position, the fuse formed separately from the frame. 2. The sensor of claim 1 , wherein, when in the rel…
Assignees
Inventors
Classifications
- B64D45/0005Primary
Operations & Transport · mapped topic
Operations & Transport · mapped topic
Cross-Sectional Technologies · mapped topic
Patent family
Related publications grouped by family.
External sources
Next steps
Free tools are coming soon. Tell us what you want to track and we'll notify you.
Frequently asked questions
Answers are generated from the same data shown on this page.
- What does patent US9102418B2 cover?
- The disclosed sensor includes a frame having a base and a plurality of arms integral with the base. The arms are biased to a relaxed position, which may be an extended position. A fuse is fastened between the arms to hold the arms in a non-relaxed position. When incorporated into an aircraft, for example, the disclosed sensor may be connected to a first panel, and a pin connected to a second pa…
- Who is the assignee on this patent?
- Carbone Michael, Hamilton Sundstrand Corp
- What technology area does this patent fall under?
- Primary CPC classification B64D45/0005. Mapped technology areas include Operations & Transport.
- When was this patent published?
- Publication date Tue Aug 11 2015 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 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).