发明名称 Centrifugal rocket motor pump with open impeller - has open impeller blades with inlet at base near central drive shaft, and associated outlet with fixed diffuser
摘要 The unit contains an open impeller blade (5) furnished with blades (6) placed inside a housing (1,2). An inlet (3) is defined at the base of the blades near the central drive shaft (22) plus its associated outlet (4) provided with a fixed diffuser (7) situated in the region of the periphery of the blades. A system of active axial equilibrium (51,71,14,15) of the assembly is integrated with the impeller. It consists of a balancing chamber (14) between the rear face of the impeller body and the rear section (2) of the housing, with the impeller itself acting as the balancing plate. The inlet to the chamber is via the adjusting gap (8) formed by the fixed piece (71) and the tip (51) of the impeller, and the outlet is via the gap (15) to a channel connecting to the suction. USE/ADVANTAGE - High-performance centrifugal pump for rocket motors using an open impeller where balancing features make for fewer stages needed.
申请公布号 FR2698667(A1) 申请公布日期 1994.06.03
申请号 FR19920014389 申请日期 1992.11.30
申请人 PROPULSION STE EUROPEENNE 发明人 LEHE JEAN-ROBERT;BEAURAIN ANDRE;BOSSON RENE C.;TIRET ETIENNE
分类号 F04D29/22;(IPC1-7):F04D29/66;F02K9/46 主分类号 F04D29/22
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