DUCTED TAIL ROTOR FOR ROTARY WING AIRCRAFT PROVIDING TORQUE REACTION AND YAW ATTITUDE CONTROL,申请号IL19920102700-传众专利搜索

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发明名称	DUCTED TAIL ROTOR FOR ROTARY WING AIRCRAFT PROVIDING TORQUE REACTION AND YAW ATTITUDE CONTROL
摘要
申请公布号	IL102700(D0)	申请公布日期	1993.02.21
申请号	IL19920102700	申请日期	1992.07.31
申请人	THE BOEING COMPANY	发明人
分类号	B64C27/45;B64C27/78;B64C27/82;(IPC1-7):B64C/	主分类号	B64C27/45
代理机构		代理人
主权项
地址

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