发明名称 AIRCRAFT FLIGHT TERMINATION SYSTEM AND METHOD
摘要 An aircraft (10) has a flight termination system (12) that allows flight of an unmanned aircraft to be quickly and efficiently terminated. The flight termination system separates one of the control surfaces (20) of the aircraft, such as a wing (32), from a fuselage (14) of the aircraft, while one or more other control surfaces connected to the fuselage. The separation may be accomplished by firing one or more explosive bolts to release a clamp that connects the control surface to the fuselage. The separation causes an asymmetry in configuration that results in a rapid crash of the aircraft. The flight termination system causes termination to be effected in small flight footprint, without use of powerful explosives, and without a large cost in weight or volume. The flight termination system may be used in unpowered or powered aircraft.
申请公布号 WO2009134513(A2) 申请公布日期 2009.11.05
申请号 WO2009US34441 申请日期 2009.02.19
申请人 RAYTHEON COMPANY;DIETRICH, MARK, C.;TREPANIER, CHARLES, N.;WERCH, TIMOTHY, R. 发明人 DIETRICH, MARK, C.;TREPANIER, CHARLES, N.;WERCH, TIMOTHY, R.
分类号 B64C1/32;B64C3/56;B64C19/00;B64C39/02 主分类号 B64C1/32
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