发明名称 |
TURBINE SECTION ARCHITECTURE FOR GAS TURBINE ENGINE |
摘要 |
A turbine section of a gas turbine engine is described, which includes an aftmost rotor extending, an aftmost stator located upstream of the aftmost rotor, and a second to last aftmost rotor located upstream of the aftmost stator. The second to last aftmost rotor being spaced apart a first axial distance from the aftmost stator. A turbine exhaust case is located downstream of the aftmost rotor and includes an inner radial wall and an outer radial wall defining a main gas path duct downstream of the aftmost rotor. The turbine exhaust case being axially spaced apart from the aftmost rotor a second axial distance that is greater than the first axial distance. |
申请公布号 |
CA2713316(A1) |
申请公布日期 |
2011.02.17 |
申请号 |
CA20102713316 |
申请日期 |
2010.08.17 |
申请人 |
PRATT & WHITNEY CANADA CORP. |
发明人 |
LEFEBVRE, GUY;DUROCHER, ERIC |
分类号 |
F01D25/30;F01D5/06;F01D21/14;F01D25/24;F02K1/00;F02K1/78 |
主分类号 |
F01D25/30 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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