发明名称 Rear fuselage of an aircraft
摘要 <p>Rear fuselage of an aircraft comprising a tail cone end and a rest of the real fuselage whereby the tail cone end is attached to the rest of the rear fuselage by means of an attachment system comprising two upper lugs, two lower lugs and a detachable balancer fitting. The balancer fitting is an adjustable fitting, being locked in a Z and Y directions of a Cartesian axis and being movable along an X direction of the Cartesian axis providing guidance for the tail cone end and the rest of the rear fuselage.</p>
申请公布号 EP2433861(A2) 申请公布日期 2012.03.28
申请号 EP20110380076 申请日期 2011.09.23
申请人 AIRBUS OPERATIONS S.L. 发明人 GARCIA PATINO, MARIA ARANZAZU;POSTIGO RODRIGUEZ, ANGEL;LOPEZ FERNANDEZ, DAVID
分类号 B64C1/06;B64D41/00 主分类号 B64C1/06
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