发明名称 Integral Powered Winged Aircraft for Infantry and Artillery Mobilization and Front Line Combat
摘要 Disclosed is a Powered Wing Aircraft. A generalized stabilizer/directional vent is used for providing a standard range of aeronautical control. It controls cross winds, directional velocity, directional control, and torque balancing in one simple easy to control device. It is attached to the axles. These improvements can apply to both military and civilian applications.
申请公布号 US2012049009(A1) 申请公布日期 2012.03.01
申请号 US201113118509 申请日期 2011.05.30
申请人 KISSEL, JR. WALDEMAR F. 发明人 KISSEL, JR. WALDEMAR F.
分类号 B64C39/06 主分类号 B64C39/06
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