一种液力涡轮与泵共用混合蜗壳

By using a shared mixing volute design for the hydraulic turbine and pump, and optimizing the intersection angle and outlet angle, the problem of medium mixing and flow loss when the hydraulic turbine and pump share an outlet is solved, thereby improving the efficiency and structural compactness of the turbopump system.

CN117627959BActive Publication Date: 2026-07-17BEIJING AEROSPACE PROPULSION INST

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
BEIJING AEROSPACE PROPULSION INST
Filing Date
2023-11-24
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

In a hydraulic turbine-driven turbopump system, when the hydraulic turbine and the pump share the same outlet, the flow loss due to medium mixing is large, which affects the work capacity of both the turbine and the pump.

Method used

A hybrid volute design for a hydraulic turbine and pump is adopted, including a first volute and a second volute, which are coaxial and rotate in the same direction. The base circle of the second volute is smaller than that of the first volute. The second volute is surrounded in the helical space formed by the first volute. The outlet diffuser sections of the first and second volutes intersect. By optimizing parameters such as the intersection angle, the outlet section angle, and the medium flow velocity, flow loss is reduced.

Benefits of technology

It effectively reduces flow losses due to media mixing, improves the efficiency of the entire system, reduces flow impact, simplifies the structure, and improves space utilization.

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Abstract

本发明涉及一种液力涡轮与泵共用混合蜗壳,该蜗壳包括第一蜗壳与第二蜗壳,第一蜗壳与第二蜗壳共轴,旋向相同,第二蜗壳的基圆小于第一蜗壳基圆,第二蜗壳被包围在第一蜗壳形成的螺旋空间内,第一蜗壳与第二蜗壳出口扩散段相交,第一蜗壳用于泵,第二蜗壳用于液力涡轮,或者第一蜗壳用于液力涡轮,第二蜗壳用于泵。本发明创新性地提出一种液力涡轮与泵共用混合蜗壳的设计方法,相比于不采用混合蜗壳的设计,本发明的方法能有效降低液力涡轮与泵出口介质掺混的流动损失,从而提升整个系统的效率。
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