The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jan. 16, 2018

Filed:

Jan. 29, 2015
Applicant:

Airbus Operations Gmbh, Hamburg, DE;

Inventors:

Frieder Henning, Bremen, DE;

Tanno Zantz, Hamburg, DE;

Michael Brady, Hamburg, DE;

Assignee:

Airbus Operations GmbH, Hamburg, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 9/22 (2006.01); B64C 9/24 (2006.01); B64C 13/50 (2006.01); F03D 1/06 (2006.01); B64C 9/14 (2006.01);
U.S. Cl.
CPC ...
B64C 9/22 (2013.01); B64C 9/24 (2013.01); B64C 13/50 (2013.01); F03D 1/0641 (2013.01); B64C 2009/143 (2013.01); Y02E 10/721 (2013.01);
Abstract

A high lift system for an aircraft comprises a wing structure and a leading edge slat movably supported relative to a leading edge of the wing structure, the leading edge slat comprises a leading edge and a trailing edge, wherein the trailing edge is configured to take different positions to form a gap between the leading edge slat and the wing structure, a skin and enclosing an interior space of the leading edge slat, the skin having a flexible leading skin section facing away from the wing structure, a flexible trailing skin section facing towards the wing structure, at least one actuation arrangement arranged inside the interior space for selectively introducing a normal force onto at least one of the leading skin section and the trailing skin section.


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