作者: Guy Bernard Vauchel
DOI:
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摘要: A thrust reversal device (1) for a turbojet engine nacelle, in which: (i) the movable cowl (3) is provided with at least one driving lead screw (30) having peripheral groove over part of length thereof, whereby said can engage stationary guide means (31) nacelle so as to rotate during translational movement cowl; and (ii) associated transmitting (32, 35, 36) rotational thereof towards drive system (33, 34, 25) flap.