公开(公告)号：US20160376016A1

公开(公告)日：2016-12-29

申请号：US15110670

申请日：2015-01-07

Applicant: SNECMA

Inventor： Mathieu Ange POISSON ,  Francois Robert BELLABAL ,  Nicolas FLORENT

IPC: B64D27/26 ,  B64D33/02

CPC classification number: B64D27/26 ,  B64D33/02 ,  B64D2027/005 ,  B64D2027/262 ,  F02C6/206 ,  F05D2220/325 ,  F05D2240/14 ,  Y02T50/44 ,  Y02T50/66 ,  Y02T50/671

Abstract: A suspension structure for suspending a turboprop including two unducted propellers from a structural element of an aircraft, the structure including a suspension frame for fastening to a structural element of the aircraft and including a main beam extending parallel to a longitudinal axis of the turboprop, the suspension frame being fastened to an air intake structure of the turboprop by an attachment frame.

Abstract translation: 一种悬挂结构，用于悬挂涡轮螺旋桨飞机，其包括来自飞行器的结构元件的两个未被引导的螺旋桨，该结构包括用于紧固到飞行器的结构元件的悬架，并且包括平行于涡轮螺旋桨发生器的纵向轴线延伸的主梁 悬挂框架通过附接框架紧固到涡桨螺旋桨的进气结构。