航天推进技术研究院主办
[1]王浩明,薛 翔,张银勇,等.空间闭式布雷顿循环旁路调节特性分析[J].火箭推进,2021,47(02):61-67.
WANG Haoming,XUE Xiang,ZHANG Yinyong,et al.Analysis of bypass regulation characteristics for spaceclosed Brayton cycle system[J].Journal of Rocket Propulsion,2021,47(02):61-67.
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WANG Haoming,XUE Xiang,ZHANG Yinyong,et al.Analysis of bypass regulation characteristics for spaceclosed Brayton cycle system[J].Journal of Rocket Propulsion,2021,47(02):61-67.
空间闭式布雷顿循环旁路调节特性分析
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
47
期数:
2021年02期
页码:
61-67
栏目:
研究与设计
出版日期:
2021-04-21
- Title:
- Analysis of bypass regulation characteristics for spaceclosed Brayton cycle system
- 文章编号:
- 1672-9374(2021)02-0000-07
- 分类号:
- V476.2
- 文献标志码:
- A
- 摘要:
- 闭式布雷顿循环是未来空间大功率热电转换的有效途径,而旁路调节是实现系统快速功率调节和转速控制的有效手段。通过对标美国普罗米修斯计划中的热电转换系统参数,进行了涡轮、压气机的气动设计和换热器性能计算,获得了包括组件特性、管道布局的热电转换系统动态仿真模型。基于该动态模型,对旁通阀不同响应时间、开度对系统功率、转速和循环温度、压力等参数影响进行仿真研究。空间闭式布雷顿循环系统在旁通阀开启后,系统功率和转速快速下降,其中功率出现了超调现象; 循环高压侧压力下降且低压侧压力上升; 回热器热侧入口温度增加而冷侧入口温度下降,热应力进一步提高。系统容积惯性的提高,在一定程度上可以降低系统对旁通阀调节的敏感性。
- Abstract:
- Closed Brayton cycle is an effective way of high-power thermo-electrical conversion in the future space mission, and the bypass adjustment is an effective way to realize fast power regulation and rotating speed control. Through the cycle parameters of thermo-electrical conversion system in Prometheus Project of US, the aerodynamic designs of turbine and compressor were finished as well as the performance of heat exchangers. Then, a dynamic simulation model was obtained based on the components characteristics and pipeline layout. Based on this dynamic model, the effort of different response time and opening degree of the bypass valve on the system power output, rotating speed, cycle temperature, pressure and other system parameters were simulated The results show that the power output and rotating speed of the closed apace Brayton cycle system decrease rapidly after the bypass valve opening, especially the power overshoot occurs in the process. The pressure in the high-pressure side decreases and it decreases in the low-pressure side. The inlet temperature of recuperator hot side increases, but the inlet temperature of cold side decrease, and the thermal stress of recuperator further increases. The sensibility for bypass regulation can be reduced by improving system volume inertia.
参考文献/References:
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备注/Memo
收稿日期:2020-10-11
基金项目:上海市科学技术委员会科研计划项目(19DZ1206502)
作者简介:王浩明(1985—),男,博士,研究领域为空间推进系统及大功率热电转换技术。
更新日期/Last Update:
1900-01-01