- 专利标题: HIGH LIFT SYSTEM FOR AN AIRCRAFT AND METHOD FOR INFLUENCING THE HIGH LIFT CHARACTERISTICS OF AN AIRCRAFT
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申请号: EP12717709.5申请日: 2012-04-27
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公开(公告)号: EP2701975B1公开(公告)日: 2018-05-30
- 发明人: HUE, Xavier , SCHLIPF, Bernhard
- 申请人: Airbus Operations GmbH
- 申请人地址: Kreetslag 10 21129 Hamburg DE
- 专利权人: Airbus Operations GmbH
- 当前专利权人: Airbus Operations GmbH
- 当前专利权人地址: Kreetslag 10 21129 Hamburg DE
- 代理机构: LKGLOBAL Lorenz & Kopf PartG mbB Patentanwälte
- 优先权: DE102011018906 20110428; US201161479925P 20110428
- 国际公布: WO2012146712 20121101
- 主分类号: B64C9/22
- IPC分类号: B64C9/22
摘要:
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.
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