Aircraft actuator with no-back, load detent assembly
US-2017313409-A1 · Nov 2, 2017 · US
Aerodynamic body with an ancillary flap
US8925869B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-8925869-B2 |
| Application number | US-201313750020-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 25, 2013 |
| Priority date | Jul 26, 2010 |
| Publication date | Jan 6, 2015 |
| Grant date | Jan 6, 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.
An aerodynamic body, with at least one ancillary flap arranged such that it can be moved on the aerodynamic body with the aid of a guide mechanism, and with a drive device for purposes of actuating the ancillary flap, the guide mechanism having a pivotal articulation, by which the ancillary flap is articulated on the aerodynamic body such that it can be extended, and which is arranged in a rear region of the ancillary flap as viewed in the flow direction.
First claim
Opening claim text (preview).
The invention claimed is: 1. An aerodynamic body, with at least one ancillary flap arranged such that the at least one ancillary flap is movable on the aerodynamic body with aid from a guide mechanism, and with a drive device for purposes of actuating the ancillary flap, wherein the guide mechanism comprises: a pivotal articulation, by which the ancillary flap is articulated on the aerodynamic body such that it is extendable wherein when the ancillary flap is retracted, the pivota…
Assignees
Inventors
Classifications
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 US8925869B2 cover?
- An aerodynamic body, with at least one ancillary flap arranged such that it can be moved on the aerodynamic body with the aid of a guide mechanism, and with a drive device for purposes of actuating the ancillary flap, the guide mechanism having a pivotal articulation, by which the ancillary flap is articulated on the aerodynamic body such that it can be extended, and which is arranged in a rear…
- Who is the assignee on this patent?
- Airbus Operations Gmbh
- What technology area does this patent fall under?
- Primary CPC classification B64C5/10. Mapped technology areas include Operations & Transport.
- When was this patent published?
- Publication date Tue Jan 06 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).