发明名称 Protection device for protecting control mechanism of inlet guide-vanes of turbojet engine
摘要 A protection device for protecting a control mechanism of inlet guide-vanes of a turbojet engine includes a narrowed section on a connecting rod. The connecting rod is for transmitting the movement of a spindle of a piston of the control mechanism or actuator to a control ring that directs all of the inlet guide-vanes. The narrowed section of the connecting rod is a frangible part.
申请公布号 US6398483(B1) 申请公布日期 2002.06.04
申请号 US20000589806 申请日期 2000.06.09
申请人 SNECMA MOTEURS 发明人 CONETE ERIC;MARLIN FRANCOIS MARIE PAUL
分类号 F02C7/00;F01D17/16;F02C7/057;(IPC1-7):F01D21/00 主分类号 F02C7/00
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