Aircraft
US-2016107744-A1 · Apr 21, 2016 · US
Wing of an aircraft
US8925871B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-8925871-B2 |
| Application number | US-201213464960-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 5, 2012 |
| Priority date | Nov 5, 2009 |
| Publication date | Jan 6, 2015 |
| Grant date | Jan 6, 2015 |
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- Title
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Abstract
Official abstract text for this publication.
A wing of an aircraft provided with a main wing and an arrangement of leading edge lifting bodies, which as seen with reference to the incident flow direction are arranged on the leading edge, which are adjustably arranged on the main wing one behind another as seen in the spanwise direction of the main wing by means of respectively two positioning devices spaced apart from one another in the spanwise direction of the main wing. The wing has a connecting device, which is coupled to each of two adjacent leading edge lifting bodies, wherein the connecting device is configured such that in the event of a fracture of a positioning device of a positioning body external forces acting on the latter are transferred via the respective connecting device to the leading edge lifting bodies coupled up via the latter.
First claim
Opening claim text (preview).
What is claimed is: 1. A wing of an aircraft comprising a main wing and an arrangement of leading edge lifting bodies, which as seen with reference to the flow direction are arranged on the leading edge, which are adjustably arranged on the main wing one behind another as seen in a spanwise direction of the main wing respectively by two positioning devices spaced apart from one another in the spanwise direction of the main wing, wherein the wing has a connecting device, which is c…
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Classifications
- B64C9/22Primary
Operations & Transport · mapped topic
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Frequently asked questions
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- What does patent US8925871B2 cover?
- A wing of an aircraft provided with a main wing and an arrangement of leading edge lifting bodies, which as seen with reference to the incident flow direction are arranged on the leading edge, which are adjustably arranged on the main wing one behind another as seen in the spanwise direction of the main wing by means of respectively two positioning devices spaced apart from one another in the s…
- Who is the assignee on this patent?
- Hue Xavier, Schlipf Bernhard, Airbus Operations Gmbh
- What technology area does this patent fall under?
- Primary CPC classification B64C9/22. 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).