发明授权
- 专利标题: Helicopter blade assembly adapted to permit rapid forward flight
- 专利标题(中): 直升机叶片组件适于允许快速向前飞行
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申请号: US730871申请日: 1996-10-18
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公开(公告)号: US5931639A公开(公告)日: 1999-08-03
- 发明人: David Curt Morris
- 申请人: David Curt Morris
- 专利权人: Morris; David Curt
- 当前专利权人: Morris; David Curt
- 主分类号: B64C27/46
- IPC分类号: B64C27/46 ; B64C27/72 ; B64C27/39
摘要:
A helicopter blade assembly for permitting rapid forward flight in a helicopter having separate means for providing a forward impetus. The assembly has a set of rotatable blades attached to a substantially vertical mast. These blades slope downward near to their distal ends, thereby creating an inverted disk virtual air foil when the blades are rapidly rotated by the mast. In a preferred embodiment the camber of the blades and, therefore, the shape of the virtual air foil is controllable.
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