发明授权
- 专利标题: High-lift system for a wing of an aircraft
- 专利标题(中): 飞机机翼高升系统
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申请号: US13855995申请日: 2013-04-03
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公开(公告)号: US09376204B2公开(公告)日: 2016-06-28
- 发明人: Christoph Winkelmann
- 申请人: AIRBUS OPERATIONS GMBH
- 申请人地址: DE Hamburg
- 专利权人: AIRBUS OPERATIONS GMBH
- 当前专利权人: AIRBUS OPERATIONS GMBH
- 当前专利权人地址: DE Hamburg
- 代理机构: Ingrassia Fisher & Lorenz, P.C.
- 优先权: DE102010047540 20101005
- 主分类号: B64C5/10
- IPC分类号: B64C5/10 ; B64C13/34 ; B64D45/00
摘要:
A high-lift system for a wing of an aircraft is provided. The high-lift system includes movably held high-lift flaps, at least one drive unit, at least one transmission shaft connected to the drive unit, and several actuator devices, distributed on the transmission shaft and connected to the high-lift flaps, for moving the high-lift flaps. The actuator devices each comprise a driven element and a torque limiting means. In one example, the driven elements of two adjacent actuator devices are interconnected in a non-rotational manner with the use of a separate torque transmitting means. If one actuator device is blocked, for example as a result of a defective tooth arrangement or some other defect, the torque to be produced by the intact actuator device increases and triggers its torque limiting means. This ensures synchronous operation and in the case of malfunction prevents damage to or detachment of a flap.
公开/授权文献
- US20130277498A1 HIGH-LIFT SYSTEM FOR A WING OF AN AIRCRAFT 公开/授权日:2013-10-24
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