发明名称 Thrust reverser with movable deflector
摘要 The present invention relates to a thrust reverser system for a turbofan-type turbojet engine having thrust reverser doors with movable deflectors. The deflectors are movably attached to an upstream edge of the thrust reversing doors and are movable between retracted and extended positions. When the thrust reversing door is closed and the turbojet engine operates in its normal thrust mode, the deflectors are retracted thereby enabling the difference between the inner surface of the thrust reversing door and the theoretical aerodynamic flow line to be reduced or eliminated. When the thrust reversing door is in the thrust reversing position, the deflector is extended so as to protrude beyond the inner surface of the door so as to direct the air flow in a more forward direction to increase the thrust reversing capabilities of the system. The deflectors are mounted on the thrust reversing door such that they are automatically extended when the thrust reversing door moves to the thrust reversing position.
申请公布号 US4894985(A) 申请公布日期 1990.01.23
申请号 US19880223021 申请日期 1988.07.22
申请人 SOCIETE ANONYME DITE: HISPANO SUIZA 发明人 DUBOIS, CLAUDE A. G.;LORE, XAVIER R. Y.
分类号 F02K1/70 主分类号 F02K1/70
代理机构 代理人
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