发明名称 Inlet Bleed Heat System with Integrated Air Knife/Silencer Panels
摘要 The present application provides an inlet bleed heat system for supplying a flow of bleed air to a flow of incoming air into a compressor of a gas turbine engine. The inlet bleed heat system may include an air knife and a silencer panel. The air knife may include a compressor bleed air port in communication with the flow of bleed air and a discharge gap to discharge the flow of bleed air into the flow of incoming air. The air knife may and the silencer panel may form an integrated air knife/silencer panel.
申请公布号 US2014123674(A1) 申请公布日期 2014.05.08
申请号 US201213669478 申请日期 2012.11.06
申请人 GENERAL ELECTRIC COMPANY 发明人 HAO YONGJIANG;BYRD DOUGLAS SCOTT;ZHANG HUA;KIPPEL BRADLY AARON;ZHANG JIANMIN
分类号 F01D25/08;F02C7/04 主分类号 F01D25/08
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