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.

Patent No.:

US 9682769 B1

PDF
Full Text
Expired
Date of Patent:
Jun. 20, 2017

Filed:

Mar. 15, 2013
Applicant:

Airbus Operations Gmbh, Hamburg, DE;

Inventor:

Martin Richter, Bremen, DE;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 13/28 (2006.01); B64C 13/30 (2006.01); B64D 45/00 (2006.01);
U.S. Cl.
CPC ...
B64C 13/28 (2013.01); B64C 13/30 (2013.01); B64D 45/0005 (2013.01); B64D 2045/001 (2013.01); Y02T 50/44 (2013.01);
Abstract

A high-lift system on a wing of an aircraft is provided. The wing includes a right-hand and a left-hand wing half with movably held high-lift flaps and the right-hand and left-hand wing half are attached to an aircraft fuselage, thus forming a wing root. Each wing half in a region in close proximity to the wing root, includes a drive unit. In each case this drive unit is joined to a transmission shaft mechanically connected to the respective drive unit, which transmission shaft extends from the drive unit in the direction of the end of the respective wing half and is designed to mechanically move the high-lift flaps arranged in the respective wing half. By means of such an arrangement it is possible to do without deflection gear arrangements from a central drive unit to the individual wing halves.


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Richter, Martin. (2017). High lift system for an aircraft with two separate drive units (U.S. Patent No. 9682769). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/9682769

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