发明申请
US20140138480A1 HIGH LIFT SYSTEM FOR AN AIRCRAFT WITH TWO SEPARATE DRIVE UNITS
有权
具有两个独立驱动单元的飞机高升程系统
- 专利标题: HIGH LIFT SYSTEM FOR AN AIRCRAFT WITH TWO SEPARATE DRIVE UNITS
- 专利标题(中): 具有两个独立驱动单元的飞机高升程系统
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申请号: US13832483申请日: 2013-03-15
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公开(公告)号: US20140138480A1公开(公告)日: 2014-05-22
- 发明人: Martin Richter
- 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
- 优先权: DE102010047512.2 20101005
- 主分类号: B64C13/28
- IPC分类号: B64C13/28
摘要:
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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