Dual valve gas pressure equalization system and method
US-2016368609-A1 · Dec 22, 2016 · US
US8997451B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-8997451-B2 |
| Application number | US-201013256308-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 12, 2010 |
| Priority date | Mar 13, 2009 |
| Publication date | Apr 7, 2015 |
| Grant date | Apr 7, 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.
An engine and pod assembly for an aircraft includes a pod receiving an engine having an air intake. A rotating nose cone extends on the nose cone, as well as a device for limiting the formation of ice. The device includes means for creating a circumferential heterogeneity of ice on the nose cone.
Opening claim text (preview).
The invention claimed is: 1. An engine and pod assembly for an aircraft, comprising: a pod receiving an engine with an air intake through which a rotating nose cone extends, the pod including a device for limiting the formation of ice on the nose cone, wherein the device includes means for creating a circumferential heterogeneity of ice on the nose cone, and wherein the pod includes a source of radiation able to at least prevent the formation of ice and directed to the nose co…
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.