Emission-capturing apparatus and method for capturing emissions from an ejection port
US-10457384-B2 · Oct 29, 2019 · US
US9102403B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9102403-B2 |
| Application number | US-201314094009-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 2, 2013 |
| Priority date | Dec 2, 2013 |
| Publication date | Aug 11, 2015 |
| Grant date | Aug 11, 2015 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
Systems are disclosed to allow for the landing gear doors to be opened in the event of an emergency gravity free-fall landing gear deployment with little or no contact with the landing gear tires. The emergency gear extension systems according to the embodiments disclosed herein thus permit the free-fall movement of the landing gear to be synchronized with the opening of the associated gear doors. That is, according to the embodiments disclosed herein deployment of the landing gear assembly is time-delayed relative to the opening of the associated gear door(s). In such a manner, the landing gear assembly is synchronously released only after the associated gear door is in a safe position during its opening sequence thereby avoiding the risk that the gear door will jam the full extension of the landing gear during an emergency gear deployment due to contact between the landing gear tires and the gear door.
Opening claim text (preview).
What is claimed is: 1. An emergency gravity free-fall landing gear deployment system for aircraft comprising: a landing gear assembly moveable between retracted and extended positions; a landing gear door having a closed condition when the landing gear assembly is in the retracted position and movable into an opened condition to allow the landing gear assembly to be moved into the extended position; a landing gear uplock mechanism which includes an uplock actuator having a pre…
Related publications grouped by family.
Free tools are coming soon. Tell us what you want to track and we'll notify you.
Answers are generated from the same data shown on this page.