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
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