航空发电机综合测试系统的研制
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摘要
本文介绍一种航空发电机测试系统。该系统将单片机技术和虚拟仪器技术相结合,能完成航空发电机规定项目的检测、运行状况的数据记录。用于航空发电机装机前测试、定期检查以及故障诊断,并可以推广到常规机电设备性能检测系统的应用中去。
系统硬件由阻性交流电子负载模块、数据采集与记录模块、数据通信模块三部分组成。针对对飞机用电设备的模拟,并考虑飞机用电设备的不同及地面模拟的实际需要,设计了基于PWM、单片机技术的大功率数字化可调的阻性交流电子负载系统;针对航空发电机电参数实时检测的要求,在考虑测试标准满足用户要求的前提下,设计了基于单片机的多路数据采集系统;为了适应航空发电机多种运行参数高速记录数据存储的要求,设计了基于SD卡技术的存储容量为16MB的单片机应用系统;为了满足系统抗干扰的要求,解决现有系统人为操作带来的随意性,设计了基于CAN总线转RS-232总线技术的数据通信模块。同时设计了两种电压输出的电源模块,并分析了系统的抗干扰设计。
系统计算机应用软件以Lab Windows/CVI 6.0为开发平台,设计了航空发电机数据采集处理程序,实现了对阻性交流电子负载系统、数据采集记录系统的控制,规范了检测方法与步骤,消除了人为因素的干扰;利用双线程技术实现了整个检测系统的控制、数据采集与处理的并行运行,提高了整个检测系统的实时性。最后完成了对实验结果数据的存储、运行曲线显示、报表以及打印输出等功能。
研制的航空发电机综合测试系统的阻性交流电子负载、测试数据记录计算机系统等部分设备已经投入使用。系统运行稳定、可靠,基本达到了预期的功能和精度指标。
This paper introduces an Aero-Generator testing system. Integrating virtual instrument technology with microcontroller technology, the system completes the test of regulation project and the recode of operation condition for Aero-Generator. The test system not only can use on test, regular check and fault detection for Aero-Generator, but also can apply to the normal mechatronics detection system.
The hardware of this system is made of 3 parts. They are AC electronic load module, data acquisition and storage module, and data transmission module. Considering different equipment and practical need of simulation on the ground, an AC electronic load system has been designed for the Aero-Generator basing on PWM Technology, MCU and high power. In provide of satisfying the users, basing on MCU, an airborne data acquisition system has been designed to count the real time gathering circuit. In order to satisfy the need of high speed data storage for airborne equipment, an application system has been designed with 16MB storage capacity basing on MCU. The data transmission module has also been designed to satisfy the data transfer with the controlling software and hardware. Can bus transformation RS-232 bus has been used in the transmission module. Meantime, we design two kinds of power supply module and analyze the anti-disturbance design of system.
Taking Lab Windows/CVI 6.0 as developing tool, the Aero-Generator software system is designed, realizing the control of AC electronic load, data collection and record. The software of this system solves the problems and improves the nature for the ant jamming by human. Meanwhile the technology of multi-threading can be used to realize the concurrent processing and improve the ability of real-time. Surely, the technology of multi-threading can be used to realize the concurrent processing and improve the ability of real-time. In the end, this paper accomplishes the function of effective data storage, printing testing reports and characteristic curve, and so on.
The AC electronic load, data collection, and recording module have been deployed. The system which runs stably and reliably achieves the expected functions and precisions.
系统硬件由阻性交流电子负载模块、数据采集与记录模块、数据通信模块三部分组成。针对对飞机用电设备的模拟,并考虑飞机用电设备的不同及地面模拟的实际需要,设计了基于PWM、单片机技术的大功率数字化可调的阻性交流电子负载系统;针对航空发电机电参数实时检测的要求,在考虑测试标准满足用户要求的前提下,设计了基于单片机的多路数据采集系统;为了适应航空发电机多种运行参数高速记录数据存储的要求,设计了基于SD卡技术的存储容量为16MB的单片机应用系统;为了满足系统抗干扰的要求,解决现有系统人为操作带来的随意性,设计了基于CAN总线转RS-232总线技术的数据通信模块。同时设计了两种电压输出的电源模块,并分析了系统的抗干扰设计。
系统计算机应用软件以Lab Windows/CVI 6.0为开发平台,设计了航空发电机数据采集处理程序,实现了对阻性交流电子负载系统、数据采集记录系统的控制,规范了检测方法与步骤,消除了人为因素的干扰;利用双线程技术实现了整个检测系统的控制、数据采集与处理的并行运行,提高了整个检测系统的实时性。最后完成了对实验结果数据的存储、运行曲线显示、报表以及打印输出等功能。
研制的航空发电机综合测试系统的阻性交流电子负载、测试数据记录计算机系统等部分设备已经投入使用。系统运行稳定、可靠,基本达到了预期的功能和精度指标。
This paper introduces an Aero-Generator testing system. Integrating virtual instrument technology with microcontroller technology, the system completes the test of regulation project and the recode of operation condition for Aero-Generator. The test system not only can use on test, regular check and fault detection for Aero-Generator, but also can apply to the normal mechatronics detection system.
The hardware of this system is made of 3 parts. They are AC electronic load module, data acquisition and storage module, and data transmission module. Considering different equipment and practical need of simulation on the ground, an AC electronic load system has been designed for the Aero-Generator basing on PWM Technology, MCU and high power. In provide of satisfying the users, basing on MCU, an airborne data acquisition system has been designed to count the real time gathering circuit. In order to satisfy the need of high speed data storage for airborne equipment, an application system has been designed with 16MB storage capacity basing on MCU. The data transmission module has also been designed to satisfy the data transfer with the controlling software and hardware. Can bus transformation RS-232 bus has been used in the transmission module. Meantime, we design two kinds of power supply module and analyze the anti-disturbance design of system.
Taking Lab Windows/CVI 6.0 as developing tool, the Aero-Generator software system is designed, realizing the control of AC electronic load, data collection and record. The software of this system solves the problems and improves the nature for the ant jamming by human. Meanwhile the technology of multi-threading can be used to realize the concurrent processing and improve the ability of real-time. Surely, the technology of multi-threading can be used to realize the concurrent processing and improve the ability of real-time. In the end, this paper accomplishes the function of effective data storage, printing testing reports and characteristic curve, and so on.
The AC electronic load, data collection, and recording module have been deployed. The system which runs stably and reliably achieves the expected functions and precisions.
引文
[1] 蒋志扬等. 飞机供电系统(修订版). 北京:国防工业出版社,1990.15～20
[2] 刘建英等. 飞机电源系统. 北京:兵器工业出版社,2004.8～15
[3] 谢军. 航空电机学. 北京:国防工业出版社,2004.102～103
[4] 飞机交流电源系统编写组. 飞机交流电源系统. 北京:国防工业出版社,1979.35～41
[5] Electrical Power system Analysis and System Logic Preliminary Report,Doc. No. 871660
[6] 樊晓光等. 航空发电机性能试验系统的设计与实现. 测控技术,1999,18(8):32～34
[7] 刘君华. 现代检测技术与测试系统设计. 西安:西安交通大学出版社,1999.154～158
[8] 张保冰. 基于虚拟仪器的飞机电源系统自动测试技术研究:[学位论文]. 南京:南京航空航天大学,2005
[9] 秦树人. 虚拟仪器. 北京:中国计量出版社,2003.6~7
[10] 孙世贵. 航空测控技术现状及其发展. 测控技术,1995,2:35～37
[11] 陆绮荣等. 电子负载的设计. 桂林工学院学报,1999,14(7):14～16
[12] 刘凯. 对大功率脉冲变压器的几点分析. 国际电子变压器,2000,10:56～58
[13] C. E. Lin, C. L. Cheng, C. L. Huang and J. C. Yeh, “Investigation of Magnetizing Inrush Current in Transformers. I. Numerical Simulation,” IEEE Trans. Power Delivery, vol. 8, pp. 246-254, Jan. 1993
[14] http://www.21ic.com ATmega48 data book, 2000
[15] 康华光等. 电子技术基础(模拟部分)第四版. 北京:高等教育出版社,1999.325～330
[16] 毛继红等. 现代电子测试技术. 北京:国防工业出版社,1999.125～130
[17] 刘君华. 现代检测技术与测试系统设计. 西安:西安交通大学出版社,1999.56～68
[18] 朱飞. 新型飞机供电参数测试系统的研究与设计:[学位论文]. 西安:西北工业大学,2003
[19] L. Cristaldi, A. Ferrero. A method and related digital instrument for the measurement of the electric power quality. IEEE Transactions on Power Delivery, 1995,10(3):1183～1189
[20] 中华人民共和国国家军用标准 GJBS189-2003. 飞机供电特性参数测试方法,2003
[21] http://www.hitrendtech.com/cn ATT7022 data book
[22] http://www.21ic.com SD data book,2000
[23] http://www.xhl.com.cn/downfile/e-c8051f33x.pdf
[24] 马宁等. 基于 CAN 总线的通用串口适配器的设计. 测控技术,2006,25(2):32～34
[25] 邬宽明. CAN 总线原理和应用系统设计. 北京:机械工业出版社,1996,124～128
[26] PHILIPS. PCA82C250 CAN controller interface.Philips Semiconductors. 2000. Jan 13
[27] National Semiconductor Data sheet. ASM1117,2004
[28] Ivo Barbiet. al. Buck Quasi-Resonant Converter Operating at Constant Frequent; Analysis, Design and Experimentation, IEEE Trans. On Power Electronics, High Frequency Power Conversion Conference Proceedings, 1991
[29] 宋宇峰等. Lab Windows/CVI 逐步深入与开发实例. 北京: 机械工业出版社,2003,135～146
[30] 李华良等. 虚拟仪器技术及其在航空测试领域中的应用. 现代电子技术,2002,7:52～53
[31] 冯一. 飞机供电参数测试系统的研制:[学位论文],西安:西北工业大学,2006
[32] Chakradhar S T. Toward massively parallel automatic test generation. IEEE Trans, 1999
[33] 张怀相等. 基于虚拟仪器技术的多线程数据采集系统. 中国仪器仪表,2003,4:4~7
[34] 刑瑞川等. 多线程技术在数据采集中的应用. 包头钢铁学院学报,2001,20(2):157~160
[35] 张凤均等. Lab Windows/CVI 开发入门和进阶. 北京:北京航空航天大学出版社,2002
[36] 杰拉尔德. 应用数值分析(第七版). 北京:机械工业出版社,2006
[37] 赵峻彦等. 单片机系统的抗干扰设计.长春大学学报,2005,15(2):21～24
[38] 梁志荣. 单片机应用系统的抗干扰技术. 现代电子技术,2003,24:32～34
[39] http://www.21ic.com MAX1232 Microprocessor Monitor,2001
[40] 刘发明等. C++ Builder 开发的雷达天线近远场测量控制系统. 计算机自动测量与控制,2001,9
[2] 刘建英等. 飞机电源系统. 北京:兵器工业出版社,2004.8～15
[3] 谢军. 航空电机学. 北京:国防工业出版社,2004.102～103
[4] 飞机交流电源系统编写组. 飞机交流电源系统. 北京:国防工业出版社,1979.35～41
[5] Electrical Power system Analysis and System Logic Preliminary Report,Doc. No. 871660
[6] 樊晓光等. 航空发电机性能试验系统的设计与实现. 测控技术,1999,18(8):32～34
[7] 刘君华. 现代检测技术与测试系统设计. 西安:西安交通大学出版社,1999.154～158
[8] 张保冰. 基于虚拟仪器的飞机电源系统自动测试技术研究:[学位论文]. 南京:南京航空航天大学,2005
[9] 秦树人. 虚拟仪器. 北京:中国计量出版社,2003.6~7
[10] 孙世贵. 航空测控技术现状及其发展. 测控技术,1995,2:35～37
[11] 陆绮荣等. 电子负载的设计. 桂林工学院学报,1999,14(7):14～16
[12] 刘凯. 对大功率脉冲变压器的几点分析. 国际电子变压器,2000,10:56～58
[13] C. E. Lin, C. L. Cheng, C. L. Huang and J. C. Yeh, “Investigation of Magnetizing Inrush Current in Transformers. I. Numerical Simulation,” IEEE Trans. Power Delivery, vol. 8, pp. 246-254, Jan. 1993
[14] http://www.21ic.com ATmega48 data book, 2000
[15] 康华光等. 电子技术基础(模拟部分)第四版. 北京:高等教育出版社,1999.325～330
[16] 毛继红等. 现代电子测试技术. 北京:国防工业出版社,1999.125～130
[17] 刘君华. 现代检测技术与测试系统设计. 西安:西安交通大学出版社,1999.56～68
[18] 朱飞. 新型飞机供电参数测试系统的研究与设计:[学位论文]. 西安:西北工业大学,2003
[19] L. Cristaldi, A. Ferrero. A method and related digital instrument for the measurement of the electric power quality. IEEE Transactions on Power Delivery, 1995,10(3):1183～1189
[20] 中华人民共和国国家军用标准 GJBS189-2003. 飞机供电特性参数测试方法,2003
[21] http://www.hitrendtech.com/cn ATT7022 data book
[22] http://www.21ic.com SD data book,2000
[23] http://www.xhl.com.cn/downfile/e-c8051f33x.pdf
[24] 马宁等. 基于 CAN 总线的通用串口适配器的设计. 测控技术,2006,25(2):32～34
[25] 邬宽明. CAN 总线原理和应用系统设计. 北京:机械工业出版社,1996,124～128
[26] PHILIPS. PCA82C250 CAN controller interface.Philips Semiconductors. 2000. Jan 13
[27] National Semiconductor Data sheet. ASM1117,2004
[28] Ivo Barbiet. al. Buck Quasi-Resonant Converter Operating at Constant Frequent; Analysis, Design and Experimentation, IEEE Trans. On Power Electronics, High Frequency Power Conversion Conference Proceedings, 1991
[29] 宋宇峰等. Lab Windows/CVI 逐步深入与开发实例. 北京: 机械工业出版社,2003,135～146
[30] 李华良等. 虚拟仪器技术及其在航空测试领域中的应用. 现代电子技术,2002,7:52～53
[31] 冯一. 飞机供电参数测试系统的研制:[学位论文],西安:西北工业大学,2006
[32] Chakradhar S T. Toward massively parallel automatic test generation. IEEE Trans, 1999
[33] 张怀相等. 基于虚拟仪器技术的多线程数据采集系统. 中国仪器仪表,2003,4:4~7
[34] 刑瑞川等. 多线程技术在数据采集中的应用. 包头钢铁学院学报,2001,20(2):157~160
[35] 张凤均等. Lab Windows/CVI 开发入门和进阶. 北京:北京航空航天大学出版社,2002
[36] 杰拉尔德. 应用数值分析(第七版). 北京:机械工业出版社,2006
[37] 赵峻彦等. 单片机系统的抗干扰设计.长春大学学报,2005,15(2):21～24
[38] 梁志荣. 单片机应用系统的抗干扰技术. 现代电子技术,2003,24:32～34
[39] http://www.21ic.com MAX1232 Microprocessor Monitor,2001
[40] 刘发明等. C++ Builder 开发的雷达天线近远场测量控制系统. 计算机自动测量与控制,2001,9