发明名称 FLUGZEUG MIT STÖRKLAPPEN LEDIGLICH AN DER OBERSEITE
摘要 An aircraft with swept back wings and spoilers inlaid into the top surface near the tips of the wings. The aircraft also includes an elevator 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.
申请公布号 DE602004003376(D1) 申请公布日期 2007.01.04
申请号 DE20046003376T 申请日期 2004.05.26
申请人 NORTHROP GRUMMAN CORP. 发明人 CLARK, D.
分类号 B64C1/00;B64C5/08;B64C9/12;B64C9/32;B64C9/34;B64C39/02 主分类号 B64C1/00
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