发明名称 Rotary engine driven by gas under pressure - has stages on each side of inlet formed by shaped recesses cut around circumference of cylindrical rotor
摘要 <p>The turbine has a rotor within a stator with a central inlet and two or more stages on each side of the inlet. The stages are formed by recesses cut in the rotor. Each state consists of four cavities spaced equally around the rotor. The outside of the rotor is domed (100) so that the stage has a larger diameter in its centre than at its axial ends. Each of the four cavities (102) has a base parallel to one of the transverse axes (O, P) of the rotor and two walls parallel to the other axis. Each cavity is divided internally by a partition (105) extending from the base of the cavity partly towards its outside. The thickness of the partition increases radially outwards.</p>
申请公布号 FR2367186(A1) 申请公布日期 1978.05.05
申请号 FR19740039347 申请日期 1974.12.02
申请人 FAGEOL RAYMOND 发明人
分类号 F02B53/00;F01D1/00;F01D3/02;(IPC1-7):01D1/00;02C7/00 主分类号 F02B53/00
代理机构 代理人
主权项
地址