Invention Grant
- Patent Title: High lift system for an aircraft and method for influencing the high lift characteristics of an aircraft
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Application No.: US14063536Application Date: 2013-10-25
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Publication No.: US09656739B2Publication Date: 2017-05-23
- Inventor: Xavier Hue , Bernhard Schlipf
- Applicant: Airbus Operations GmbH
- Applicant Address: DE
- Assignee: Airbus Operations GmbH
- Current Assignee: Airbus Operations GmbH
- Current Assignee Address: DE
- Agency: Lerner, David, Littenberg, Krumholz & Mentlik, LLP
- Priority: DE102011018906 20110428
- Main IPC: B64C9/22
- IPC: B64C9/22 ; B64C9/02 ; B64C9/14

Abstract:
A high lift system for an aircraft includes a basic body, a flap which is movably mounted on the basic body and has a flap edge, and a retaining element. The high lift system is set up to form a gap between the flap edge and the basic body. The retaining element is mounted on a region of the flap close to the flap edge and extends towards the basic body to restrict the distance between the flap edge and the basic body. The retaining element is preferably configured as a linear attachment means. Consequently, a gap dimension between a flap and a basic body can be influenced to restrict flexing effects during loading of the flap and of the basic body.
Public/Granted literature
- US20140048655A1 HIGH LIFT SYSTEM FOR AN AIRCRAFT AND METHOD FOR INFLUENCING THE HIGH LIFT CHARACTERISTICS OF AN AIRCRAFT Public/Granted day:2014-02-20
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