发明名称 |
Canard rotor/wing |
摘要 |
A dual-mode high speed rotorcraft is disclosed which combines the efficiency of a helicopter with the high-speed capability of a fixed wing aircraft. The rotorcraft includes a rotor for propulsion during low-speed flight and hover, which is stopped and locked to function as a fixed wing during a high-speed flight. Also included are a canard and a high-lift tail, which together function to provide substantially all of the lift for the rotorcraft during the transition between low and high-speed flight, so that the rotor may be unloaded while starting and stopping.
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申请公布号 |
US5454530(A) |
申请公布日期 |
1995.10.03 |
申请号 |
US19930068907 |
申请日期 |
1993.05.28 |
申请人 |
MCDONNELL DOUGLAS HELICOPTER COMPANY |
发明人 |
RUTHERFORD, JOHN W.;O'ROURKE, MATTHEW;MCDONNELL, WILLIAM R.;SMITH, BRIAN T. |
分类号 |
B64C27/24;(IPC1-7):B64C27/22;B64C39/12 |
主分类号 |
B64C27/24 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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