发明名称 |
SUPERSONIC COMPRESSOR STARTUP SUPPORT SYSTEM |
摘要 |
A supersonic compressor includes a fluid inlet, a fluid outlet, a fluid conduit extending therebetween, and at least one supersonic compressor rotor disposed within the fluid conduit and including a fluid flow channel that includes a throat portion. The supersonic compressor also includes a fluid control device coupled in fluid communication with at least one fluid source and an inlet of the fluid flow channel. The fluid control device channels a first fluid to the fluid flow channel inlet. The first fluid has a first plurality of fluid properties that facilitate attainment of supersonic flow of the first fluid in the throat portion during a first operational mode. The fluid control device further channels a second fluid to the fluid flow channel inlet. The second fluid has a second plurality of fluid properties that permit maintenance of supersonic flow of the second fluid in the throat portion. |
申请公布号 |
CA2753748(A1) |
申请公布日期 |
2012.04.08 |
申请号 |
CA20112753748 |
申请日期 |
2011.09.29 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
VYSOHLID, MARTIN;HOFER, DOUGLAS CARL |
分类号 |
F04D21/00;F04D27/00;F04D29/30 |
主分类号 |
F04D21/00 |
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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