[1]卿绿军,晁文雄,周创辉,等.无人机燃油系统增压泵性能测试系统设计[J].工业仪表与自动化装置,2025,(05):31-35.[doi:10.19950/j.cnki.CN61-1121/TH.2025.05.006]
　QING Lvjun,CAO Wenxiong,ZHOU Chuanghui,et al.Performance measurement system for centrifugal pump in UAV fuel system[J].Industrial Instrumentation & Automation,2025,(05):31-35.[doi:10.19950/j.cnki.CN61-1121/TH.2025.05.006]
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无人机燃油系统增压泵性能测试系统设计()

《工业仪表与自动化装置》[ISSN:1000-0682/CN:61-1121/TH]

卷:
期数:
2025年05期
页码:
31-35
栏目:
出版日期:
2025-10-15

文章信息/Info

Title:
Performance measurement system for centrifugal pump in UAV fuel system
文章编号:
1000-0682（2025）05-0031-05
作者:
卿绿军1; 晁文雄1; 周创辉1; 许 睿2
1.西安航空学院 液压技术研究院, 陕西 西安 710077;2. 西安航空学院 机械工程学院, 陕西 西安 710077
Author(s):
QING Lvjun1; CAO Wenxiong1; ZHOU Chuanghui1; XU Rui2
1. School of Automation, Nanjing University of Science and Technology,Jiangsu Nanjing 210094,China;2. Suzhou Konig Electronic Technology Co., Ltd.,Jiangsu Changshu 215562,China
关键词:
无人机; 燃油增压泵; LabVIEW; 性能测试
Keywords:
UAV;  fuel centrifugal pump;  LabVIEW;  measurement
分类号:
TH137
DOI:
10.19950/j.cnki.CN61-1121/TH.2025.05.006
文献标志码:
A
摘要:
针对无人机用高性能增压泵的研制需求，开发了一套无人机燃油系统增压泵性能测试系统。通过分析试验台组成及其工作原理，确定了测试系统的总体方案；以USB-4711多功能数据采集卡为核心，搭建了测试系统的硬件系统；采用LabVIEW软件，开发了基于PID算法的测试系统上位软件；以DCW2-1828离心泵为被测试验件，对所搭建测试系统的功能进行了验证，其结果表明：该测试系统信号采集、信号处理、信号输出、数据显示等功能均能正常工作，其压力控制误差小于2%，验证了测试系统的有效性，为高性能增压泵研制提供实验基础。
Abstract:
To meet the development requirements of high-performance centrifugal pump for UAV fuel system, a performance measurement system for centrifugal pumps is designed. The working principle of the centrifugal pump performance measurement system is first analyzed, leading to the determination of the overall system design. The hardware system is then constructed using the USB-4711 multifunctional data acquisition card as the core component. The performance measurement system for the centrifugal pump is subsequently developed using LabVIEW software, enabling the collection of performance parameters, adjustment of operating conditions, data processing, and the display and storage of data during the testing process. Finally, through the experimental test on the centrifugal pump performance, it is shown the system can meet the performance measurement requirements for centrifugal pumps in UAV fuel systems, and the feasibility of the system is verified. The results show that the signal acquisition, signal processing, signal output, data display and other functions of the testing system can work normally, and the pressure control error is less than 2%, which verifies the effectiveness of the testing system and provides experimental foundation for the development of high-performance centrifugal pump.

参考文献/References:

[1] 刘洋,孙博,吴晓丹,等.燃油离心泵可靠性仿真[J/OL].航空发动机,1-6[2025-04-22].http://kns.cnki.net/kcms/detail/21.1359.V.20241225.2003.010.html.

[2] 魏志强,王晶.大型固定翼无人机跟随民航机的尾流安全评估方法[J].安全与环境学报,2024,24(12):4533-4541.
[3] 范田昊,张士卫,薛小伟,等.低成本可消耗无人机极限不可用燃油量确定方法研究[J].航空科学技术,2024,35(09):29-34.
[4] 仲世杰,符江锋,刘显为,等.基于超参数双调和方程代理模型的航空燃油离心泵多目标优化[J].推进技术,2024,45(12):107-119.
[5] 陈璇,李嘉,李斌,等.基于Kriging的多阶段加点策略及离心叶轮汽蚀优化[J].西北工业大学学报,2024,42(03):467-476.
[6] 符江锋,仲世杰,刘显为,等.耦合双层参数更新的改进PCE模型在燃油离心泵不确定性分析中的应用[J].航空学报,2024,45(21):194-212.
[7] 张岭,杨兴,李一鸣,等.液环式航空燃油离心泵自吸性能[J].排灌机械工程学报,2024,42(04):342-349.
[8] 李婉琦,黎义斌,汪波,等.航空燃油离心泵高空吸油特性数值研究[J].推进技术,2024,45(12):255-266.
[9] 刘荣升,张岭,李一鸣,等.燃油离心泵内流特性分析[J].工程机械,2023,54(12):88-96+10.
[10] 张同,陈聪.飞机燃油系统组态监控设计[J].工业控制计算机,2023,36(06):22-24+27.
[11] 邹品文,马高长,严社斌,等.基于燃油离心泵叶轮轴向力测试技术的研究[J].应用力学学报,2024,41(03):509-515.
[12] 蒋辉,黄昆,赵辉.某型直升机离心式燃油增压泵增压值设计[J].南京航空航天大学学报,2022,54(02):233-238.
[13] 李嘉,李华聪,张伟,等.高压燃油离心泵压力脉动及非定常流动分析[J].西北工业大学学报,2022,40(01):199-205.
[14] 王科雷,周洲,马悦文,等.垂直起降固定翼无人机技术发展及趋势分析[J].航空工程进展,2022,13(05):1-13.
[15] 唐庆,单金光,周振华,等.航空燃油离心泵内流特性分析[J].液压与气动,2021,45(08):183-188.
[16] 杨红英.燃油增压泵燃油润滑油掺混故障的分析[J].机械制造,2021,59(05):82-87.
[17] KUMAR D, SINGH RANAWAT N, KUMAR KANKAR P, et al. InceptionV3 based blockage fault diagnosis of centrifugal pump [J]. Advanced Engineering Informatics, 2025(65), 103181.
[18] MANSOUR M, THéVENIN D. Impact of blade twisting and tip clearance on centrifugal pump performance under air–water two-phase flow [J]. International Journal of Heat and Fluid Flow, 2025(112), 109682.

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备注/Memo

备注/Memo:
收稿日期：2025-05-06基金项目：陕西省自然科学基础研究计划项目2023-JC-YB-407、校级科研基金项目2022KY0206和2024KY0222。第一作者：卿绿军（1987—），男，汉族，四川绵阳，博士，讲师。研究方向为航空机电液测控系统研究。
更新日期/Last Update: 1900-01-01