发明名称 Supersonic compressor startup support system
摘要 A supersonic compressor (10) includes a fluid inlet (26), a fluid outlet (28), a fluid conduit (32) extending therebetween, and at least one supersonic compressor rotor (40) disposed within the fluid conduit and including a fluid flow channel (80) that includes a throat portion (124). The supersonic compressor also includes a fluid control device (308) coupled in fluid communication with at least one fluid source (302/304/306) and an inlet (76) 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 EP2439414(A2) 申请公布日期 2012.04.11
申请号 EP20110184251 申请日期 2011.10.07
申请人 GENERAL ELECTRIC COMPANY 发明人 VYSOHLID, MARTIN;HOFER, DOUGLAS CARL
分类号 F04D27/02;F04D21/00 主分类号 F04D27/02
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