公开(公告)号：US20120151896A1

公开(公告)日：2012-06-21

申请号：US12974085

申请日：2010-12-21

申请人： VENKAT ESWARLU TANGIRALA ,  NARENDRA DIGAMBER JOSHI ,  ADAM RASHEED ,  Brian Gene Brzek ,  Douglas Carl Hofer ,  Thomas Michael Lavertu ,  Fuhua MA

发明人： VENKAT ESWARLU TANGIRALA ,  NARENDRA DIGAMBER JOSHI ,  ADAM RASHEED ,  Brian Gene Brzek ,  Douglas Carl Hofer ,  Thomas Michael Lavertu ,  Fuhua MA

IPC分类号： F02C5/00

CPC分类号： F02C5/02 ,  F02C7/18 ,  F02C9/18 ,  F05D2260/205 ,  F23C15/00

摘要： The flow through the core of a hybrid pulse detonation combustion system is passed through a compressor and then separated into a primary flow, that passes directly to the combustor, and a bypass flow, which is routed to a portion of the system to be used to cool components of the system. The bypass flow is routed to a nozzle of the pulse detonation combustor. The flow is then passed back into the primary flow through the core downstream of where it was extracted.

摘要翻译： 通过混合脉冲爆震燃烧系统的核心的流动通过压缩机，然后分离成直接通向燃烧器的主流，以及旁路流，其被路由到系统的一部分以用于 系统的酷组件。 旁路流被引导到脉冲爆震燃烧器的喷嘴。 然后将流体通过芯被提取的下游的核心传回初级流中。