发明名称 Air-discharge device for an airplane turbofan engine
摘要 <p>The device (20) has a rotating door (24) comprising inner and outer flaps (26, 28) secured and articulated around a pivot axle (58) that is remote from the inner flap in a direction from the outer flap to the inner flap when the door is in closing position so that upstream and downstream ends of the inner and outer flaps protrude from inner and outer sides relative to inner and outer surfaces (12, 14) of a fixed structure (22) in opening position. The inner flap is spaced from the structure to provide an air passage between the inner flap and the structure in downstream of the inner flap.</p>
申请公布号 EP2433864(A1) 申请公布日期 2012.03.28
申请号 EP20110181789 申请日期 2011.09.19
申请人 AIRBUS OPERATIONS 发明人 BULIN, GUILLAUME;SURPLY, THIERRY
分类号 B64C9/32;F02K1/70;F02K1/82;F02K3/06 主分类号 B64C9/32
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