Research on Safety Control Strategy of Driving System for the Helicopter Wind Tunnel Test

被引：2

作者：

Peng Xianmin ^{[1
]}

Zhang Guichuan ^{[1
]}

Yin Xinfan ^{[1
]}

Che Binghui ^{[1
]}

Luo, Huan ^{[1
]}

Wei Yibo ^{[1
]}

机构：

[1] China Aerodynam Res & Dev Ctr, Mianyang 621000, Sichuan, Peoples R China

来源：

2020 5TH INTERNATIONAL CONFERENCE ON SMART GRID AND ELECTRICAL AUTOMATION (ICSGEA 2020) | 2020年

关键词：

helicopter wind tunnel test; driving system; safety protection; control strategy;

D O I：

10.1109/ICSGEA51094.2020.00028

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

Wind tunnel experiment for helicopter model involves forward and descent flight test under certain flow speeds. These tests are highly risky and test safety is the premise of successful tests. This paper is focused on the safety control mechanism of helicopter wind tunnel test. Safety control strategies for driving system of the test rig are described, including the main factors affecting test safety, the architecture of safety control and the flowchart of safety for the driving system. The proposed safety control strategies are applied on a coaxial rigid rotor test rig in the Phi 03.2m wind tunnel. Experimental application shows that proposed safety control strategies meets the requirements of helicopter wind tunnel test, and much progress was achieved in the improvement of test reliability.

引用

页码：94 / 101

页数：8

共 8 条

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[6] Xia Hong, 2010, EQUIPMENT FAULT DIAG
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[8] Yang Zhuo, 2011, MANUFACTURING AUTOMA, P56

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