| 直升机旋翼锥体及动平衡设备校验系统的研究 |
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| 引用本文： | 薛伟松,邢士喜,郑牧,董良. 直升机旋翼锥体及动平衡设备校验系统的研究[J]. 测控技术, 2006, 25(3): 4-7,19 |
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| 作者姓名： | 薛伟松 邢士喜 郑牧 董良 |
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| 作者单位： | 哈飞航空产品开发部设计试验室,黑龙江,哈尔滨,150066;总参陆航研究所,黑龙江,哈尔滨,150066 |
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| 基金项目： | 黑龙江省杰出青年科学基金 |
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| 摘 要： | 主要介绍了直升机旋翼锥体、动平衡测量设备的基本原理及校验系统的硬件和软件结构,详细阐述了该系统的具体设计方法.本系统主要由HRDS型旋翼锥体仿真试验器和HBMC型高精度标准信号源两部分组成,信号源部分主要采用PC104微型计算机作为主控计算机,利用宝石公司设计的RU-BY-MM-416型PC104接口的4通道16位D/A模拟输出卡和自行设计的滤波及放大电路作为信号输出部分,以及自行编写的软件组合而成的校验系统.
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| 关 键 词： | 直升机 旋翼锥体 动平衡 微型计算机 校验系统 |
| 文章编号： | 1000-8829（2006）03-0004-04 |
| 收稿时间： | 2005-07-01 |
| 修稿时间： | 2005-07-01 |
Research on Checkout System for Track-Height and Dynamic Balance Equipment of Helicopter |
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| XUE Wei-song,XING Shi-xi,ZHENG Mu,DONG Liang. Research on Checkout System for Track-Height and Dynamic Balance Equipment of Helicopter[J]. Measurement & Control Technology, 2006, 25(3): 4-7,19 |
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| Authors: | XUE Wei-song XING Shi-xi ZHENG Mu DONG Liang |
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| Affiliation: | 1. Design Test Lab Harbin Aviation Industry Group, Harbin 150066, China; 2. Army Aviation Research Institute, Harbin 150066, China |
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| Abstract: | The basic principle for the measure system which is designed to checkout track-height and dynamic balance equipment of the helicopter, and the hardware and software structure for the checkout system are described. The design ways for this system are expatiated in detail. This system includes mostly two parts, trackheight simulative tester HRDS and high precision normal signal fountain HBMC. The host computer of the signal fountain is a microcomputer PC104. It uses four PC104 output blocks RUBY-MM-416 designed by Stone Ltd., which has 16 bits D/A output, and the filter and amplifier are designed by ourselves, which are used for the signal output. The software of the system is designed by ourselves too. |
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| Keywords: | helicopter track-height dynamic balance microcomputer checkout system |
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