发明名称 Jet engine with turbine which can be coupled to drive shafts
摘要 It applies to any type of vehicle and in general to mechanisms which require movement. It includes a combustion chamber 1 whose outlet opening 7 is frustoconical so that the gases increase in speed in the zone where a nozzle 10 is coupled, which nozzle extends at an ascending vertical conduit 11 which is distributed in the form of an even number of branches arranged in the horizontal plane and finishing in nozzles oriented in the same direction of rotation in order to give rise to torques which generate rotation of the shaft 15 upon exit of the gases at high pressure. The gases strike the blades 18 of a turbine body 19 arranged in a coincident plane and which has secured to it an internally toothed crown 20 forming part of a planetary mechanism 21 whose output shaft 24 receives the combined movements both of the nozzle shaft 15 and of the actual turbine 19, rotating in the same direction. The free edges of the transverse C-section of the body of the turbine 19 are extended in the form of individual divergent annular flanges for better reception of the exhaust gases from the nozzles 17. <IMAGE>
申请公布号 ES2070697(A2) 申请公布日期 1995.06.01
申请号 ES19920002461 申请日期 1992.12.02
申请人 GIL VAZQUEZ SERAFIN 发明人 GIL VAZQUEZ SERAFIN
分类号 F02C3/00;F02K7/00;(IPC1-7):F02C3/00 主分类号 F02C3/00
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