发明名称 DEVICE FOR SUSPENDING A CASING, A TURBINE ENGINE AND A PROPULSION ASSEMBLY
摘要 The invention relates to a device (1) for suspending a casing (2) of a turbine engine (3) to the structure (12) of an aircraft, characterized in that it comprises a suspension ring (4), said suspension ring (4) comprising; a plurality of attachment surfaces (33) positioned so as to protrude on the circumference of the suspension ring (4) and having attachment holes (6), for attachment to the structure (12),a circumferential flange (5) comprising a plurality of holes (35) for attaching the suspension ring (4) to the casing (2);one or several hanging surfaces (10) for hanging at least one piece of equipment (15) , positioned so as to protrude on the circumference of the suspension ring (4), and having holes (8) for hanging the piece of equipment (15) to the ring (4).;The invention also relates to a turbine engine and to a propulsion assembly comprising such a device.
申请公布号 US2015075177(A1) 申请公布日期 2015.03.19
申请号 US201414489649 申请日期 2014.09.18
申请人 SNECMA 发明人 NATAL Maria;PLE Arnaud
分类号 B64D27/26;F16M1/04 主分类号 B64D27/26
代理机构 代理人
主权项 1. A device for suspending a casing of a turbine engine to the structure of an aircraft, said device comprising a suspension ring, said suspension ring comprising; a plurality of attachment surfaces positioned so as to protrude on the a circumference of the suspension ring and having attachment holes, for attachment to the structure, a circumferential flange comprising a plurality of holes for attaching the suspension ring to the casing; one or several hanging surfaces for hanging at least one piece of equipment, positioned so as to protrude on the circumference of the suspension ring, and having holes for hanging the piece of equipment to the ring.
地址 Paris FR