发明名称 |
Suspension device for a turboprop engine |
摘要 |
A device for suspending a turboprop engine from a structural element of an aircraft comprises a suspension pylon parallel to the longitudinal axis of the engine and fixed to the structural element, resilient connections between the engine and the pylon and an arch fixed to the pylon, and a torsion bar carried by the arch so that the bar can pivot freely about its own axis, the opposite ends of the torsion bar being connected to opposite sides of the engine by respective lever and link rod assemblies so that the torsion bar takes up the reaction torque about the longitudinal axis of the engine.
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申请公布号 |
US5806792(A) |
申请公布日期 |
1998.09.15 |
申请号 |
US19960698070 |
申请日期 |
1996.08.15 |
申请人 |
SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION "SNECMA" |
发明人 |
BROSSIER, PASCAL NOEL;MIRAUCOURT, CARMEN |
分类号 |
B64D27/18;B64D27/26;F02C7/20;(IPC1-7):B64D27/26 |
主分类号 |
B64D27/18 |
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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