发明名称 AIRCRAFT TURBOJET ENGINE THRUST REVERSER WITH A LOWER NUMBER OF ACTUATORS
摘要 This cascade-type thrust reverser with one-piece moving cowl includes rails able to slide in guideways positioned on each side of a suspension pylon. This thrust reverser includes just two actuators positioned near the rails and able to cause this cowl to slide on the guideways between its direct-jet and reverse-jet positions. It also has means capable of compensating for forces that have a tendency to misalign the rails with respect to the guideways, thus preventing them from jamming in one another.
申请公布号 US2014131479(A1) 申请公布日期 2014.05.15
申请号 US201313875856 申请日期 2013.05.02
申请人 AIRCELLE;AIRCELLE 发明人 KERBLER OLIVIER;DEZEUSTRE NICOLAS;HURLIN HERVE
分类号 F02K1/56 主分类号 F02K1/56
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