发明名称 Jet engine provided with a thrust reverser
摘要 A jet engine for an aircraft has a thrust reverser including one or more doors which define at least a part of the throat of the engine's nozzle. The engine further includes a latch mechanism for retaining the doors in a stowed position. The doors may be deployed for reversal of engine thrust, but are also capable while stowed of being pivoted in a limited way to change the cross-section area of the throat of the nozzle.
申请公布号 US5192023(A) 申请公布日期 1993.03.09
申请号 US19900573481 申请日期 1990.08.24
申请人 THE DEE HOWARD COMPANY 发明人 FAGE, ETIENNE;LAIR, JEAN-PIERRE
分类号 F02K1/11;F02K1/60 主分类号 F02K1/11
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