发明名称 Fan blade retainer
摘要 An exemplary embodiment of the invention is a gas turbine engine retainer having a block, a retainer slot disposed through the block, and a shelf normal to and extending axially forward of the block below the retainer slot. A retainer wall depending radially inwardly from the block and the retainer wall has a retainer wall thickness smaller than a block thickness of the block. The shelf is disposed along a radially inner edge of the retainer wall and the retainer slot is disposed through the retainer wall along the shelf. The retainer slot is arced or curved sideways and may be rectangular in cross-section. The retainer slot may be rectangular in cross-section and the shelf may be a rectangular shelf that is rectangular in cross-section. The retainer slot may also be skewed sideways with respect to a shelf centerline extending axially down a middle of the shelf. A radially extending shelf aperture is disposed through the shelf.
申请公布号 US6457942(B1) 申请公布日期 2002.10.01
申请号 US20000723112 申请日期 2000.11.27
申请人 GENERAL ELECTRIC COMPANY 发明人 FORRESTER JAMES MICHAEL
分类号 F01D5/30;F01D5/32;(IPC1-7):F01D5/32 主分类号 F01D5/30
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