Leading edge for an airfoil

US2017106969A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2017106969-A1
Application numberUS-201615295099-A
CountryUS
Kind codeA1
Filing dateOct 17, 2016
Priority dateOct 15, 2015
Publication dateApr 20, 2017
Grant date

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A leading edge for an airfoil comprising a torsion box, the leading edge comprising a leading plate and a first inflatable element suitable for being filled with air. The leading plate comprises a convex side and a concave side. The first inflatable element is in contact with at least part of the concave side, thus reinforcing the leading plate. An airfoil comprising such a leading edge is also provided.

First claim

Opening claim text (preview).

1 . A leading edge for an airfoil comprising a torsion box, the leading edge comprising: a leading plate with a convex side and a concave side, a first inflatable element configured to be filled with air, the first inflatable element being in contact with at least part of the concave side, thus reinforcing the leading plate. 2 . The leading edge according to claim 1 , further comprising an outer coverage, covering the leading plate, configured to further cover the t…

Assignees

Inventors

Classifications

  • Operations & Transport · mapped topic

  • B64C3/30Primary

    Operations & Transport · mapped topic

  • Operations & Transport · mapped topic

  • Operations & Transport · mapped topic

  • Cross-Sectional Technologies · mapped topic

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What does patent US2017106969A1 cover?
A leading edge for an airfoil comprising a torsion box, the leading edge comprising a leading plate and a first inflatable element suitable for being filled with air. The leading plate comprises a convex side and a concave side. The first inflatable element is in contact with at least part of the concave side, thus reinforcing the leading plate. An airfoil comprising such a leading edge is also…
Who is the assignee on this patent?
Airbus Operations Sl
What technology area does this patent fall under?
Primary CPC classification B64C3/30. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Thu Apr 20 2017 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). 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).