发明名称 TURBOPUMP MACHINE WITH ISOLATED COOLING PASSAGE DISCHARGE
摘要 A turbopump machine includes a housing, a shaft rotatably supported in the housing on a set of bearings, an axial pump coupled with the shaft, a circumferential discharge volute fluidly coupled with the axial pump, and a turbine coupled with the shaft. The turbine includes a blade row disposed in an axial turbine flowpath that has an axial turbine flowpath discharge that is fluidly coupled with the circumferential discharge volute. A cooling passage is disposed between the housing and the shaft about the set of bearings. The cooling passage has a cooling passage discharge that is fluidly coupled with the circumferential discharge volute. The cooling passage discharge is adjacent the axial turbine flowpath discharge. A seal isolates the cooling passage discharge from the axial turbine flowpath discharge.
申请公布号 WO2016118208(A3) 申请公布日期 2016.09.09
申请号 WO2015US59173 申请日期 2015.11.05
申请人 AEROJET ROCKETDYNE, INC. 发明人 PHUI, Khin;CHILCOAT, Thaddeus
分类号 F04D13/04;F02K9/48;F04D29/046;F04D29/08;F04D29/42;F04D29/52;F04D29/58 主分类号 F04D13/04
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