发明名称 Blade assembly for a turbomachine
摘要 Gas turbine engines are used as powerplants for aircraft. When the aircraft are parked on the ground, the wind can blow through the engines and set fans and rotors into motion, i.e., windmill them. Given that the blades of the fans and rotors are loosely fastened to their rotors, the low speed rotation caused by windmilling causes the blades to clatter or clank, thus causing wear. The present invention provides means for clamping blades into position during this low speed rotation for reducing clanking.
申请公布号 US4483661(A) 申请公布日期 1984.11.20
申请号 US19830490820 申请日期 1983.05.02
申请人 GENERAL ELECTRIC COMPANY 发明人 MANHARTH, GARY B.;CORNELL, JAY L.
分类号 F01D5/26;F01D5/30;(IPC1-7):F01D5/32 主分类号 F01D5/26
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