发明名称 |
Integrated guide vane assembly |
摘要 |
An integrated outlet guide vane assembly for turbomachinery typically includes at least one outlet guide vane and at least one bifurcation having a leading edge and a trailing edge. The turbomachinery has a central axis of rotation and a defined direction of rotation about the axis. The guide vane comprises an airfoil having a leading edge and a trailing edge and has a non-zero angle of lean in the direction of rotation and a non-zero sweep angle relative to a line perpendicular to the central axis. The leading edge of the bifurcation has a non-zero angle of lean in the direction of rotation and a non-zero sweep angle relative to a line perpendicular to the central axis. The trailing edge of the vane is faired into the leading edge of the bifurcation.
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申请公布号 |
US8221071(B2) |
申请公布日期 |
2012.07.17 |
申请号 |
US20080241842 |
申请日期 |
2008.09.30 |
申请人 |
WOJNO JOHN P.;PRENTICE IAN FRANCIS;GIRIDHARAN MANAMPATHY;GENERAL ELECTRIC COMPANY |
发明人 |
WOJNO JOHN P.;PRENTICE IAN FRANCIS;GIRIDHARAN MANAMPATHY |
分类号 |
F03B1/00;F03B11/02;F03D5/00 |
主分类号 |
F03B1/00 |
代理机构 |
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