发明名称 GAS TURBINE ANTI-ICING SYSTEM
摘要 Embodiments of the present disclosure are directed towards a system having a compressor bleed air recirculation system. The compressor bleed air recirculation system includes a compressor bleed air line extending from a compressor to an air intake, wherein the compressor bleed air line is configured to flow a compressor bleed air flow, and the air intake is configured to supply an air flow to the compressor. The compressor bleed air recirculation system further includes an eductor disposed along the compressor bleed air line between the compressor and the air intake, wherein the eductor is configured to receive and mix the compressor bleed air flow and a first ambient air flow to form a first air mixture.
申请公布号 US2013327012(A1) 申请公布日期 2013.12.12
申请号 US201213493989 申请日期 2012.06.11
申请人 MAHABUB MOHAMMAD;KHAN IMRAN A.;NGUYEN THO VANKHANH;GENERAL ELECTRIC COMPANY 发明人 MAHABUB MOHAMMAD;KHAN IMRAN A.;NGUYEN THO VANKHANH
分类号 F02C7/047 主分类号 F02C7/047
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