发明名称
摘要 <p>A rear part of an aircraft, including a support structure for supporting engines, extending through the fuselage, through two openings distributed on either side of a vertical median plane of the aircraft. The support structure includes a first half-structure and a second half-structure respectively extending through the first and second fuselage openings, the first and second half-structures being joined to each other so that they can be disassembled in an inside space defined by the fuselage.</p>
申请公布号 JP2012502845(A) 申请公布日期 2012.02.02
申请号 JP20110527376 申请日期 2009.09.16
申请人 发明人
分类号 B64C1/16;B64D27/14 主分类号 B64C1/16
代理机构 代理人
主权项
地址