发明申请
US20070095970A1 Rotor wing aircraft having an adjustable tail nozzle 有权
转翼翼飞机具有可调式尾喷嘴

Rotor wing aircraft having an adjustable tail nozzle
摘要:
Aircraft including an airframe having a fuselage extending between a forward end and an aft end and a fixed wing extending laterally from the fuselage. The aircraft includes a power plant mounted on the airframe producing exhaust during operation. The aircraft includes a rotor/wing rotatably mounted on the airframe including a plurality of blades and an adjustable nozzle mounted on the airframe downstream from the power plant exhaust for selectively directing the power plant exhaust to exit the aircraft at a pre-selected angle with respect to the airframe within a range of angles extending from about horizontally rearward to about vertically downward.
公开/授权文献
信息查询
0/0