发明名称 |
PULSE DETONATION COMBUSTOR VALVE FOR HIGH TEMPERATURE AND HIGH PRESSURE OPERATION |
摘要 |
A pulse detonation combustor valve assembly contains at least one pulse detonation combustor having an inlet portion through which air and/or fuel enters the chamber of the combustor. An annular rotating valve portion is positioned adjacent to an outer surface of the pulse detonation combustor and concentrically with the pulse detonation combustor so that the annular rotating valve portion can be rotated with respect to the combustor. The annular rotating valve portion contains at least one inlet portion through which air and/or fuel passes to enter the inlet portion of the pulse detonation combustor.
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申请公布号 |
US2009139199(A1) |
申请公布日期 |
2009.06.04 |
申请号 |
US20080271082 |
申请日期 |
2008.11.14 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
KENYON ROSS HARTLEY;JOSHI NARENDRA DIGAMBER;TANGIRALA VENKAT ESWARLU;DEAN ANTHONY JOHN;RASHEED ADAM;GLASER AARON JEROME;WIEDENHOEFER JAMES FREDRIC;CHAPIN DAVID;HINCKLEY KEVIN;PINARD PIERRE FRANCOIS |
分类号 |
F02C5/12 |
主分类号 |
F02C5/12 |
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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