发明名称 Angled cooling air bypass slots in honeycomb seals
摘要 A labyrinth seal having a static honeycomb land and a toothed rotary land, an angled passage is formed in the honeycomb land to communicate cooling air from the static vane region of the interstage HP section of the turbine into the aft cavity which is bounded by the rotating stage two blade whereby the exiting cooling air will acquire a velocity component which is in the same direction as the rotating stage two blade.
申请公布号 US5215435(A) 申请公布日期 1993.06.01
申请号 US19910783462 申请日期 1991.10.28
申请人 GENERAL ELECTRIC COMPANY 发明人 WEBB, ALAN L.;ECKERT, TERRY T.
分类号 F01D5/08;F01D11/02 主分类号 F01D5/08
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