发明名称 |
Fixed part for receiver of turboshaft engine of aircraft, has crossing holes, where each hole defines passage for set of routing constraints, and each crossing hole is crossed by one of routing constraints of turboshaft engine |
摘要 |
<p>The part (31) has a fixed hollow shaft (57) that is centered on a longitudinal axis (3) of a turboshaft engine. A supporting ring (91) is arranged with an axis (93) that is approximately parallel with the axis of the turboshaft engine. The supporting ring is arranged with a set of crossing holes that is arranged separately from each other. Each crossing hole defines a passage for a set of routing constraints, and each crossing hole is crossed by one of the routing constraints of the turboshaft engine. Independent claims are also included for the following: (1) a turboshaft engine (2) a method for assembly of a fixed part of a receiver of a turboshaft engine.</p> |
申请公布号 |
FR3001498(A1) |
申请公布日期 |
2014.08.01 |
申请号 |
FR20130050766 |
申请日期 |
2013.01.30 |
申请人 |
SNECMA |
发明人 |
HUGON NADEGE;CHARIER GILLES, ALAIN |
分类号 |
F02K3/072 |
主分类号 |
F02K3/072 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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