发明名称 Bleed housing
摘要 A gas turbine engine compressor has a number of shroud rings, at least a bleed one of which defines a number of bleed ports. A structural hub is downstream of the shroud rings and secured relative to the shroud rings. A structural hub case extends from an aft joint with the structural hub to a fore joint with a joined one of the shroud rings and has a number of valve ports. At least a portion of the structural case extends structurally between the fore and aft joints. A valve element is shiftable between first and second conditions for respectively blocking and not blocking communication through the valve ports.
申请公布号 US2005106009(A1) 申请公布日期 2005.05.19
申请号 US20030713641 申请日期 2003.11.13
申请人 CUMMINGS KEVIN J.;DEMERS CHRISTOPHER G.;HODGSON JAMES C.;SUCIU GABRIEL;MERRY BRIAN 发明人 CUMMINGS KEVIN J.;DEMERS CHRISTOPHER G.;HODGSON JAMES C.;SUCIU GABRIEL;MERRY BRIAN
分类号 F01D17/16;F01D17/10;F01D17/14;F02C6/08;F04D27/02;F04D29/54;(IPC1-7):F01D17/00 主分类号 F01D17/16
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