发明名称 METHOD FOR MANUFACTURING A TURBOMACHINE FAN HAVING A REDUCED NOISE LEVEL AT MULTIPLE ROTATIONAL FREQUENCIES OF SAID TURBOMACHINE
摘要 The invention relates to a method (100) for manufacturing a turbomachine fan comprising a plurality of blades mounted on a disc extending along a longitudinal axis, said method comprising the following steps of: - measuring (102) at least one structural parameter of each of the blades in the cold state, and, for each of the blades, estimating (103) at least one structural parameter in operation relating to a blade from the structural parameter(s) measured on said blade in the cold state, - determining (104) an optimal sequence of the blades around the disc from the structural parameters estimated in operation for each of the blades, and - mounting (105) the blades on the disc in the optimal sequence thus determined.
申请公布号 WO2016198790(A1) 申请公布日期 2016.12.15
申请号 WO2016FR51377 申请日期 2016.06.08
申请人 SAFRAN AIRCRAFT ENGINES 发明人 LAFITTE, Anthony, Bernard, Germain;BRUHAT, Jean-Frédéric, Pierre, Joseph;POUZADOUX, Frédéric, Jean-Bernard;ROUX, Jean-Michel
分类号 F04D29/32;F01D5/02;F01D5/28;F04D29/64;F04D29/66 主分类号 F04D29/32
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