公开(公告)号：WO2005023643A3

公开(公告)日：2005-07-14

申请号：PCT/US2004016588

申请日：2004-05-26

Applicant: NORTHROP GRUMMAN CORP

Inventor： CLARK WALTER D

IPC: B64C1/00 ,  B64C5/08 ,  B64C9/12 ,  B64C9/32 ,  B64C9/34 ,  B64C39/02

CPC classification number: B64C1/0009 ,  B64C5/08 ,  B64C9/12 ,  B64C9/32 ,  B64C9/323 ,  B64C9/34 ,  B64C39/024 ,  B64C2001/0045 ,  B64C2039/105 ,  B64C2201/028 ,  B64C2201/127 ,  B64C2201/22 ,  Y02T50/12 ,  Y02T50/32 ,  Y02T50/44

Abstract: An aircraft (10) with swept back wings (16, 18) and spoilers (30,32) inlaid into the top surface (36) near the tips of the wings. The aircraft also includes an elevator (34) formed in the center back portion of the aircraft, which is also aft of the spoilers. It is aft to allow an auxiliary control in the elevator signal to cancel the unwanted pitch up moment caused by the spoilers only going up and being aft of the center of gravity of the aircraft. Roll is achieved with these spoilers by the direct action of the lift dumping on one side or the other and by taking advantage of the transformation of yaw into roll by the sweep back of the wings.

Abstract translation: 具有靠近翼的尖端嵌入顶表面（36）的扫掠后翼（16,18）和扰流板（30,32）的飞机（10）。 飞机还包括形成在飞行器的中心后部的电梯（34），其也是扰流板的后部。 这是为了允许电梯信号中的辅助控制来消除由扰流板仅上升并且处于飞机重心的后方引起的不期望的俯仰上升时刻。 通过电梯倾倒在一侧或另一侧上的直接作用，并且通过翼的扫掠利用偏转转动的优点，利用这些扰流板实现滚动。