发明名称 |
Methods and apparatus for supplying air to turbine engine combustors |
摘要 |
A combustor for a gas turbine engine that facilitates reducing combustor chamber dump pressure losses to improve combustor and engine performance is described. The combustor includes a diffuser that diffuses airflow directed into the combustor. The diffuser includes an outer wall, an inner wall, and a plurality of splitter vanes between the outer wall and the inner wall. The splitter vanes are spaced radially apart, and each is spaced radially from a respective diffuser wall such that an outer passage, an inner passage, and a central passage are defined by the splitter vanes.
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申请公布号 |
US2002092303(A1) |
申请公布日期 |
2002.07.18 |
申请号 |
US20010760167 |
申请日期 |
2001.01.12 |
申请人 |
AL-ROUB MARWAN;CREEVY CLIFFORD STEPHEN;ROBERTS HUBERT SMITH;GREENWOOD ANTHONY PAUL |
发明人 |
AL-ROUB MARWAN;CREEVY CLIFFORD STEPHEN;ROBERTS HUBERT SMITH;GREENWOOD ANTHONY PAUL |
分类号 |
F02C7/04;F23R3/04;F23R3/10;(IPC1-7):F02C7/00 |
主分类号 |
F02C7/04 |
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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