发明名称 |
HELICE NON CARENEE A PALES A CALAGE VARIABLE POUR UNE TURBOMACHINE |
摘要 |
The propeller has propeller blades rotatably mounted around axes of a housing (36) of a radial annular element (34), where the rotation of each blade is carried by a plate (238). A cylindrical body (282) is engaged in the housing of the radial annular element, and is centered and guided in rotation by a laminated abutment (200). The laminated abutment comprises a stack of elastomeric metal rings. The laminated abutment is elastically deformable in torsion about a longitudinal axis over a predetermined angular range, which is equal to the angular range of the propeller blades. |
申请公布号 |
FR2993919(B1) |
申请公布日期 |
2014.07.11 |
申请号 |
FR20120057207 |
申请日期 |
2012.07.25 |
申请人 |
SNECMA |
发明人 |
FABRE ADRIEN, JACQUES, PHILIPPE |
分类号 |
F01D5/30;F02K3/02;F16F1/40 |
主分类号 |
F01D5/30 |
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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