发明名称 |
REACTION TURBINE AND HYBRID IMPULSE REACTION TURBINE |
摘要 |
<p>A reaction turbine has channels formed in the top surface of a disc to create nozzles. The channels can be covered by a membrane sealed to the disc or by the housing extended from a combustor. Each channel may have a first section extending radially outwardly from an inlet of the reaction turbine and a second curved section extending from the first section to a periphery of the disc. A reaction turbine may also receive input from an impulse turbine. Fluid flows through the impulse turbine and fluid from the impulse turbine enters an inlet of the reaction turbine. The reaction turbine may have cooling channels and cooling fins to lower the temperature of the disc during operation.</p> |
申请公布号 |
WO2013063115(A1) |
申请公布日期 |
2013.05.02 |
申请号 |
WO2012US61691 |
申请日期 |
2012.10.24 |
申请人 |
HYBRID TURBINE GROUP |
发明人 |
PURDUM, HOWARD E.;DOWNS, WILLIAM L.;DOWNS, L. VANN |
分类号 |
F01D1/00 |
主分类号 |
F01D1/00 |
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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