Invention Grant
US08814082B2 Aircraft high lift system and method for determining an operating condition of an aircraft high lift system
有权
用于确定飞机高升程系统的运行状态的飞机高升程系统和方法
- Patent Title: Aircraft high lift system and method for determining an operating condition of an aircraft high lift system
- Patent Title (中): 用于确定飞机高升程系统的运行状态的飞机高升程系统和方法
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Application No.: US12778743Application Date: 2010-05-12
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Publication No.: US08814082B2Publication Date: 2014-08-26
- Inventor: Bernd Schievelbusch , Bernhard Hauber
- Applicant: Bernd Schievelbusch , Bernhard Hauber
- Applicant Address: DE Lindenberg/Allgaeu
- Assignee: Liebherr-Aerospace Lindenberg GmbH
- Current Assignee: Liebherr-Aerospace Lindenberg GmbH
- Current Assignee Address: DE Lindenberg/Allgaeu
- Agency: Alleman Hall McCoy Russell & Tuttle LLP
- Priority: DE102009020840 20090512
- Main IPC: B64C13/16
- IPC: B64C13/16 ; B64D45/00
Abstract:
The present disclosure relates to an aircraft high lift system with at least one load station for actuating a flap of a wing, preferably a landing flap and/or a leading-edge flap, at least one transmission with transmission portions located between branch transmissions, wherein by means of the branch transmissions actuating energy can be branched off from the transmission to the load station, and to a method for determining an operating condition of an aircraft high lift system.
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