发明名称 Thrust nozzle for jet propulsion engine - is located inside engine body, behind accelerator chamber and in front of second combustion and accelerator chamber with jet directed outwards
摘要 The thrust nozzle is located at the end of the jet engine, and its jet is directed outwards. The nozzle is located inside the body of the engine, behind the accelerator chamber and in front of second combustion and accelerator chambers. The thrust nozzle may consist of a combination of inner and outer nozzles, which are connected by a guide chamber. USE - The thrust nozzle is for an engine, to generate reactive forces.
申请公布号 DE4324794(A1) 申请公布日期 1994.01.13
申请号 DE19934324794 申请日期 1993.07.23
申请人 SCHAEFER, ALEXANDER, 75175 PFORZHEIM, DE 发明人 SCHAEFER, ALEXANDER, 75175 PFORZHEIM, DE
分类号 F02K3/08;F02K3/10;(IPC1-7):F02K1/40 主分类号 F02K3/08
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