发明名称 MEASUREMENT INSTALLATION FOR BLADE FAILURE TESTING IN A TURBOMACHINE
摘要 Turbomachine fitted with a device for gathering the information recorded during operation of the former by a strain gauge positioned on a fan blade borne by a fan disc of said turbomachine, said device comprising a hollow cylindrical pipe positioned inside one of the rotating shafts of said turbomachine in order to guide at least one wire for transmitting this information, characterized in that said device further comprises a part for attaching said pipe to said rotating shaft.
申请公布号 US2014105727(A1) 申请公布日期 2014.04.17
申请号 US201314051749 申请日期 2013.10.11
申请人 SNECMA 发明人 ROUSSELIN STEPHANE;ADNOT JEAN-FRANCOIS;MARCELLIN PATRICK
分类号 F01D21/00 主分类号 F01D21/00
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