发明名称 System and method to stage primary zone airflow
摘要 A combustion air delivery system comprising a compressor operable to provide a stream of compressed air and a bypass duct positioned to divide the stream of compressed air into a bypass flow stream and a primary flow stream. A recuperator is operable to preheat the primary flow to produce a flow of preheated compressed air. A premix chamber receives the bypass flow stream and mixes the bypass flow stream with a flow of fuel to produce a fuel-air flow. A can member at least partially defines a primary zone that receives the fuel-air flow and includes an aperture sized to admit a predetermined portion of the flow of preheated compressed air. The fuel-air flow and predetermined portion of the flow of preheated compressed air mix in the primary zone to produce a combustible flow. An igniter is operable to ignite the combustible flow.
申请公布号 US6971227(B2) 申请公布日期 2005.12.06
申请号 US20030417016 申请日期 2003.04.16
申请人 INGERSOLL RAND ENERGY SYSTEMS, INC. 发明人 DOLAK ERIC;ARMSTRONG JEFFREY
分类号 F02C3/00;F02C7/00;F02C7/08;F02C7/10;F02C9/18;F23L15/00;F23L15/04;(IPC1-7):F02C7/10 主分类号 F02C3/00
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