发明名称 BLADE PRELOADING SYSTEM AND METHOD
摘要 A removable fan blade of a turbofan engine includes a blade root at one end thereof. A rotor disk has a retention slot having dimensions corresponding for receiving the root of the fan blade in the slot. An elongated resilient member extends within the retention slot in a lengthwise direction between the root of the fan blade and the bottom of the retention slot and an elongated member extends lengthwise between the root of the fan blade and the elastomeric member to compress the resilient member and provide a radial preload to the fan blade.
申请公布号 US2010189564(A1) 申请公布日期 2010.07.29
申请号 US20090358729 申请日期 2009.01.23
申请人 发明人 STONE PAUL
分类号 F01D5/30;B23P15/04 主分类号 F01D5/30
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