发明名称 |
GAS TURBINE INTERMEDIATE STRUCTURE AND A GAS TURBINE ENGINE COMPRISING THE INTERMEDIATE STRUCTURE |
摘要 |
The invention relates to a gas turbine intermediate structure ( 14 ) for being arranged between a first and a second gas turbine structure ( 8 and 9 ) in an axial direction ( 18 ) of a gas turbine ( 1 ). The intermediate structure ( 14 ) comprises an gas duct ( 5 c) arranged for guiding a gas flow from a gas duct ( 5 a) in the first structure ( 8 ) to a gas duct ( 5 b) in the second structure ( 9 ). An inlet ( 19 ) of the intermediate structure gas duct ( 5 c) is substantially displaced in a radial direction in relation to an outlet ( 20 ) of the intermediate structure gas duct ( 5 c). At least one guide vane ( 28,29 ) is arranged in the intermediate structure gas duct ( 5 c) for guiding the gas flow. |
申请公布号 |
EP1799989(A4) |
申请公布日期 |
2014.07.09 |
申请号 |
EP20050792461 |
申请日期 |
2005.10.06 |
申请人 |
GKN AEROSPACE SWEDEN AB |
发明人 |
STRÖM, LINDA;LARSSON, JONAS |
分类号 |
F02K3/06;F01D9/02;F02C3/06 |
主分类号 |
F02K3/06 |
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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