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[1]王 堃,李纯飞,董 苑.挤压式供应系统气瓶压力仿真[J].火箭推进,2013,39(02):79-82.
　WANG Kun,LI Chun-fei,DONG Yuan.Simulation of gas pressure inside high pressure vessel of pressure-fed propellant feed system[J].Journal of Rocket Propulsion,2013,39(02):79-82.
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挤压式供应系统气瓶压力仿真

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 39 期数: 2013年02期 页码: 79-82 栏目: 测控与试验 出版日期: 2013-04-30
Title:
Simulation of gas pressure inside high pressure vessel of pressure-fed propellant feed system
文章编号:
1672-9374(2013)02-0063-04
作者:
王 堃1; 李纯飞2; 董 苑2
1. 海装西安局，陕西 西安 710089；2. 西安航天动力研究所，陕西 西安 710100
Author(s):
WANG Kun1;  LI Chun-fei2;  DONG Yuan2
1. Xi’an Military Representative Bureau of Naval Equipment Department, Xi’an 710089, China; 2. Xi’an Aerospace Propulsion Institute, Xi’an 710100, China
关键词:
液体火箭发动机; 推进剂供应系统; 气瓶压力; 仿真模型; AMESim
Keywords:
liquid rocket engine;  propellant feed system;  gas pressure inside high pressure vessel;  simulation model;  AMESim
分类号:
V434+.23
文献标志码:
A
摘要:
以挤压式液体火箭发动机为研究对象，对发动机推进剂供应系统工作过程进行了理论分析，利用AMESim软件建立了仿真平台，计算了发动机工作过程气瓶压力。将仿真计算结果与试车数据进行对比，结果表明仿真计算结果与试车数据一致性较好，验证了仿真模型建模思路的正确性，为气瓶压力计算提供了一种方法。
Abstract:
Taking the gas pressure-fed liquid rocket engine with high pressure vessel as a study object, the working process of propellant feed system in the engine was analyzed theoretically. An emulator was established with AMESim. With the emulator, the gas pressure in the vessel was computed while the engine was working. The calculated result was compared with the data obtained in the test. The compared results indicate that the trend curve of the calculated result can maintain consistency with the test date. It verified the correctness of the way to establish the emulator. The method can be used to calculate the gas pressure in high pressure vessel.

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备注/Memo

收稿日期：2012-12-１4；修回日期：2013-01-15
基金项目：0901工程项目（2005AA722062）
作者简介：王堃（1983—），男，工程师，研究领域为导弹发动机总体设计

更新日期/Last Update: 1900-01-01