发明名称 parte traseira de aeronave, compreendendo uma estrutura de suporte de motores atravessando a fuselagem e ligada a este por pelo menos uma biela.
摘要 A rear part of an aircraft including a support structure for supporting engines, extending through the fuselage, through a first opening and a second opening. A connection structure connects the support structure to the fuselage, including a first connection mechanism connecting the support structure to a first casing forming the first opening and a second connection mechanism connecting the support structure to a second casing forming the second opening. The connection structure also includes at least one effort recovery connecting rod, the first end of which is mounted on the support structure and the opposite end is mounted on the fuselage, at a distance from the first and second openings.
申请公布号 BRPI0918643(A2) 申请公布日期 2015.12.01
申请号 BR2009PI18643 申请日期 2009.09.16
申请人 AIRBUS OPERATIONS SAS 发明人 DELPHINE JALBERT;ETHIENNE BARDOU;FRÉDÉRIC JOURNADE;LAURENT LAFONT
分类号 B64D27/14;B64D27/20;B64D27/26 主分类号 B64D27/14
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