AEROSPACE VEHICLE YAW GENERATING SYSTEMS AND ASSOCIATED METHODS
摘要
Aerospace vehicle yaw generating systems and associated methods are disclosed herein. One aspect of the invention is directed toward a yaw generating system that can include an aerospace vehicle having a fuselage with a first portion and a second portion. The system can further include a movable control surface coupled to the fuselage and extending generally in a horizontal plane. The control surface can be movable to a deflected position in which the control surface can be positioned to create a flow pattern proximate to the fuselage when the aerospace vehicle is located in a flow field. The flow pattern can be positioned to create a pressure differential between the first portion of the fuselage and the second portion of the fuselage. The first and second portions can be located so that the pressure differential produces a yawing moment on the aerospace vehicle.
申请公布号
WO2007001735(A2)
申请公布日期
2007.01.04
申请号
WO2006US21499
申请日期
2006.06.02
申请人
THE BOEING COMPANY;HARRIGAN, JEFFERY, S.;BEAUFRERE, HENRY, L.