发明名称 Multi-turbofan system with separate core engine
摘要 This invention provides a multi-fan system separated core engine type turbofan engine in which high pressure air is used as the working fluid for a turbine which drives a fan, thereby reducing the manufacturing costs of the turbofan engine and simplifying the constitution thereof. A turbine for driving a fan 11 which is provided in a propulsion device 3 of the multi-fan system separated core engine type turbofan engine 1 is an air turbine 13 which is driven by the supply through a duct 9 of a part of high pressure air compressed in a compressor 5 of a core engine 2. Since the working fluid of the air turbine 13 for driving the fan 11 is not high temperature combustion gas, there is no need to use expensive heat-resistant material for the turbine, and thus the propulsion device 3 can be manufactured at low cost, the constitution thereof can be simplified, and operational control can be ameliorated. <IMAGE>
申请公布号 EP1331386(A2) 申请公布日期 2003.07.30
申请号 EP20030250235 申请日期 2003.01.15
申请人 NATIONAL AEROSPACE LABORATORY OF JAPAN 发明人 SAITO, YOSHIO;ENDO, MASANORI;MATSUDA, YUKIO;SUGIYAMA, NANAHISA;TAGASHIRA, TAKESHI
分类号 B64C29/00;F02C1/02;F02C3/10;F02C3/13;F02C6/08;F02C7/36;F02K3/00;F02K3/06;F02K3/075;F02K3/077;F02K3/12;(IPC1-7):B64C29/00 主分类号 B64C29/00
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