发明名称 Integrated bypass turbojet engines for aircraft and other vehicles
摘要 Turbojet engines and aircraft configurations for advantageous use of the turbojet engines; the turbojet engines utilizing ram air turbine units that centrifugally compress air isothermally for use in various combustion configurations designed for stoichiometric combustion, wherein a stream of by-pass ram air jets is mixed with combustion gas jets for discharge in a common discharge nozzle.
申请公布号 US2003192303(A1) 申请公布日期 2003.10.16
申请号 US20020292829 申请日期 2002.11.12
申请人 PAUL MARIUS A. 发明人 PAUL MARIUS A.
分类号 B64C29/00;B64D27/16;F02C3/045;F02C3/08;F02K3/02;F02K3/04;F02K3/077;(IPC1-7):F02K3/02 主分类号 B64C29/00
代理机构 代理人
主权项
地址