发明名称 TURBINE ENGINE ATTACHMENT STRUCTURE
摘要 An attachment structure for attaching a power plant including unducted propellers to a fuselage of an aircraft, the attachment structure being connected by first and second fasteners to respective front and rear spars penetrating into the fuselage and fastened to a carrier structure of the aircraft, and including a central longitudinal beam secured at its front end to a first frame, arranged in the plane of the front spar, that is secured at its rear end to a second rear frame, cantilevered out and arranged upstream from the unducted propellers, and that is secured to a third intermediate frame, arranged in the plane of the rear spar between the first and second frames. The first, second, and third frames are connected together by force-takeup beams, an assembly as constituted in this way forming a cradle for receiving the power plant via a standard attachment.
申请公布号 US2014130512(A1) 申请公布日期 2014.05.15
申请号 US201214128799 申请日期 2012.06.13
申请人 SNECMA 发明人 CHOUARD PIERRE-ALAIN JEAN-MARIE PHILIPPE HUGUES;VINCENT THOMAS ALAIN CHRISTIAN
分类号 B64D27/26 主分类号 B64D27/26
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