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公开(公告)号：US09682769B2
公开(公告)日：2017-06-20
申请号：US13832483
申请日：2013-03-15
发明人： Martin Richter
CPC分类号： B64C13/28 , B64C13/30 , B64D45/0005 , B64D2045/001 , Y02T50/44
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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公开(公告)号：US20140138480A1
公开(公告)日：2014-05-22
申请号：US13832483
申请日：2013-03-15
发明人： Martin Richter
IPC分类号： B64C13/28
CPC分类号： B64C13/28 , B64C13/30 , B64D45/0005 , B64D2045/001 , Y02T50/44
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.
摘要翻译： 提供飞机机翼上的高升程系统。 机翼包括右手和左手翼半部，其具有可移动的高举襟翼，右侧和左侧翼半部连接到飞机机身，从而形成翼根。 靠近翼根的区域中的每个翼半部包括驱动单元。 在每种情况下，该驱动单元连接到机械地连接到相应驱动单元的传动轴，该传动轴从驱动单元沿着相应的翼半部的端部的方向延伸，并被设计成机械地移动高升降翼 布置在相应的翼半部。 通过这种布置，可以在没有偏转齿轮装置的情况下从中心驱动单元到单个翼片半部进行。
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