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[1]雷博娟,程树伟,边东伟.高压空气大流量现场校准装置设计与实现[J].火箭推进,2017,43(05):69-73.
　LEI Bojuan,CHENG Shuwei,BIAN Dongwei.Design and realization of calibration facility for high-pressure large flow air[J].Journal of Rocket Propulsion,2017,43(05):69-73.
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高压空气大流量现场校准装置设计与实现

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 43 期数: 2017年05期 页码: 69-73 栏目: 测控与实验 出版日期: 2017-10-15
Title:
Design and realization of calibration facility for high-pressure large flow air
作者:
雷博娟; 程树伟; 边东伟
西安航天动力研究所,陕西 西安 710100
Author(s):
LEI Bojuan; CHENG Shuwei; BIAN Dongwei
Xi'an Aerospace Propulsion Institute,Xi'an 710100,China
关键词:
高压大流量空气;  现场校准技术;  p.V.T.t法;  校准装置
Keywords:
high-pressure large flow air;  field calibration;  p.V.T.t method;  calibration facility
分类号:
V433-34
文献标志码:
A
摘要:
为满足新型吸气式发动机研制对于试验系统高压大流量超声速来流模拟条件下气体流量的准确测量和现场校准的迫切需求,设计了一套基于高压、大流量p.V.T.t法和比较法的流量现场校准装置(以下简称现场校准装置),通过原级p.V.T.t法与次级标准音速喷嘴相结合的方式,实现了压力3～23 MPa和流量1～60 kg/s条件下音速喷嘴流量系数的校准、溯源和试验系统空气流量准确测量,高压空气大流量现场校准装置扩展不确定度为0.84%。
Abstract:
A flow field calibration facility based on high pressure mass flow p.V.T.t method and the comparing method(hereafter referred to as on-line calibration facility)was designed to meet the urgent demand of air-breathing engine testing system to achieve accurate measurement and field calibration of high-pressure large flow supersonic air.By integrating the primary p.V.T.t method and the secondary standard-sonic nozzle,this facility effectuates calibration,traceability and accurate measurement of air flow coefficient of the sonic nozzle under the conditions of pressure range of 3～23 MPa and flow range of 1～60 kg/s.The extended uncertainty of the on-line calibration facility is 0.84%.

参考文献/References:

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备注/Memo

收稿日期:2017-05-30; 修回日期:2017-07-21 基金项目:国防军工技术基础2015年科研项目(JSJC2013203A001) 作者简介: 雷博娟(1988—)女,工程师,研究领域为冲压发动机介质试验工艺

更新日期/Last Update: 2017-11-10