发明名称 LOCKING SPACER ASSEMBLY
摘要 A locking spacer assembly for securing adjacent rotor blades includes a first end piece configured to fit into a space between the platforms of adjacent rotor blades. The first end piece comprises an outer surface and an inner surface. The outer surface has a profile that is adapted to project into the attachment slot. A second end piece is configured to fit into a space between the platforms. The second end piece comprises an outer surface and an inner surface. The outer surface has a profile that is adapted to project into the attachment slot. The inner surfaces of the first and second end pieces generally face each other. The first end piece and the second end piece are bonded together either directly or via a spacer block that is inserted between the inner surfaces.
申请公布号 US2015101350(A1) 申请公布日期 2015.04.16
申请号 US201314055114 申请日期 2013.10.16
申请人 General Electric Company 发明人 Healy Michael James;Potter Brian Denver
分类号 F01D5/30 主分类号 F01D5/30
代理机构 代理人
主权项 1. A locking spacer assembly for insertion into a circumferential attachment slot between platforms of adjacent rotor blades, comprising: a first end piece configured to fit into a space between platforms of adjacent rotor blades, said first end piece comprising an outer surface and an inner surface, said outer surface having a profile adapted to project into an attachment slot; a second end piece configured to fit into said space between said platforms, said second end piece comprising an outer surface and an inner surface, said outer surface having a profile adapted to project into said attachment slot, wherein said inner surfaces of said first and second end pieces generally face each other; and a spacer block configured to be inserted between said inner surfaces of said first and second end pieces, wherein said spacer block is bonded to each of said first end piece and said second end piece.
地址 Schenectady NY US