发明名称 Transition duct for gas turbine engine
摘要 A transition duct having an inlet opening and an outlet opening and a body portion extending between the inlet and outlet openings at respective inlet and outlet ends. The inlet opening defines a generally circular cross-section for the body portion and has a geometric center, and the outlet opening defines a generally rectangular arc-like cross-section. The body portion has an internal profile substantially in accordance with coordinate values X, Y and Z at an angle &thetas;, as set forth in Table 1, where each of the X, Y and Z coordinate values are taken at a sweep angle &thetas; passing through the section origin and measured from a first plane defined by the inlet end and increasing toward a second plane defined by the outlet end.
申请公布号 US7810334(B2) 申请公布日期 2010.10.12
申请号 US20060581164 申请日期 2006.10.13
申请人 SIEMENS ENERGY, INC. 发明人 HSU JOHAN;MCQUIGGAN ANDREW G.;DAWSON ROBERT W.
分类号 F02C1/00;F02G3/00 主分类号 F02C1/00
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