发明申请
- 专利标题: CENTRIFUGAL COMPRESSOR ASSEMBLY WITH STATOR VANE ROW
- 专利标题(中): 离心式压缩机总成与定子万向轮
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申请号: US13096295申请日: 2011-04-28
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公开(公告)号: US20120272663A1公开(公告)日: 2012-11-01
- 发明人: Zaher Milad Moussa , David Paul Miller , David Vickery Parker
- 申请人: Zaher Milad Moussa , David Paul Miller , David Vickery Parker
- 申请人地址: US NY Schenectady
- 专利权人: GENERAL ELECTRIC COMPANY
- 当前专利权人: GENERAL ELECTRIC COMPANY
- 当前专利权人地址: US NY Schenectady
- 主分类号: F02C3/04
- IPC分类号: F02C3/04 ; F01D9/04
摘要:
A compressor assembly for a gas turbine engine includes rotatable impeller with forward and aft ends, including: an annular hub defining a generally concave-curved cross-sectional inner flowpath surface at its radially outer periphery, the inner flowpath surface extending between an inlet and an exit; an annular array of airfoil-shaped inducer blades extending radially outward from the inner flowpath surface near the forward end; and an annular array of exducer blades extending outward from the inner flowpath surface, the array of exducer blades axially spaced apart from the array of inducer blades; a non-rotating shroud assembly surrounding the impeller and including a convex-curved outer flowpath surface, wherein the inner and outer flowpath surfaces cooperate to define a primary flowpath past the blades and the stator vanes; and an annular array of airfoil-shaped stator vanes extending radially inward from the outer flowpath surface into a space between the inducer and exducer blades.