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大加速度环境下板式贮箱内极限导流特性

杨琦 肖汀兰 彭若玲 李德友 刘锦涛 李益

空间控制技术与应用2024,Vol.50Issue(4):87-94,8.
空间控制技术与应用2024,Vol.50Issue(4):87-94,8.DOI:10.3969/j.issn.1674-1579.2024.04.010

大加速度环境下板式贮箱内极限导流特性

Limit Diversion Characteristics of a Vane-type Tank under High Acceleration Conditions

杨琦 1肖汀兰 1彭若玲 1李德友 1刘锦涛 2李益3

作者信息

  • 1. 哈尔滨工业大学,哈尔滨 150001
  • 2. 北京控制工程研究所,北京 100094
  • 3. 星箭科技股份有限公司,宁波 315153
  • 折叠

摘要

Abstract

The future propulsion system needs to adapt to large acceleration environment and have the refueling ca-pacity with large filling volume.Therefore,it is very important for the overall design of aircraft to research the pro-pellant management characteristic of spacecraft tank at a large acceleration environment.In this paper,the limit management performance of a vane-type surface tension tank is studied by numerical methods.The gas-liquid distri-bution in the tank and the liquid level curves of the propellant are analyzed.The diversion capacity of parallel vanes under a large acceleration is calculated,and the influence of vane width and clearance distance on the diversion performance is studied.The numerical simulation results show that increasing the vane width and decreasing the clearance distance between the vane and tank shell can improve the diversion effect at 10-2 g acceleration.The re-search results of this paper can provide theoretical reference for the optimal design of vane-type surface tension tanks.

关键词

表面张力贮箱/平行导流板/重力加速度/数值模拟/极限导流能力

Key words

surface tension tank/parallel vanes/gravitational acceleration/numerical simulation/limit diversion capacity

分类

航空航天

引用本文复制引用

杨琦,肖汀兰,彭若玲,李德友,刘锦涛,李益..大加速度环境下板式贮箱内极限导流特性[J].空间控制技术与应用,2024,50(4):87-94,8.

基金项目

北京控制工程研究所先进空间推进技术实验室和北京市高效能及绿色宇航推进工程技术研究中心开放基金(LabASP-2023-01) Advanced Space Propulsion Laboratory of BICE and Beijing Engineering Research Center of Efficient and Green Aero-space Propulsion Technology(LabASP-2023-01) (LabASP-2023-01)

空间控制技术与应用

OA北大核心CSTPCD

1674-1579

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