发明名称 LANDING GEAR DOOR ASSEMBLY
摘要 <p>An aircraft landing gear door assembly has a plurality of doors. The doors include a first door (1) and a second door (2) adjacent to the first door when the doors are closed. The first door (1) is so mounted that its movement to its open position involves movement of at least part of the first door through space which is occupied by the second door (2) in its closed position and vacated by the second door (2) in its open position. Provision of the second door allows the axis of rotation (11) of the first door (1) to be disposed above the first door so that the door projects less far downwardly in its open position than would be the case if the first door (1) were hinged about its edge.</p>
申请公布号 WO2003089296(P1) 申请公布日期 2003.10.30
申请号 GB2003001382 申请日期 2003.03.28
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