王晓光, 林麒
收稿日期:
2018-01-30
修回日期:
2018-05-08
出版日期:
2018-10-15
发布日期:
2018-05-11
通讯作者:
王晓光
E-mail:xgwang@xmu.edu.cn
基金资助:
WANG Xiaoguang, LIN Qi
Received:
2018-01-30
Revised:
2018-05-08
Online:
2018-10-15
Published:
2018-05-11
Supported by:
摘要: 新型飞行器的研制越发强调先进的飞行性能,这对风洞试验模型支撑技术提出了高的要求,为扩展风洞试验的能力,迫切需要研究新型的智能支撑技术。绳牵引并联支撑是基于机器人技术的一种新型机构,具有刚度较大,动态性能良好等优点,为风洞试验提供了一种新的手段。首先,全面论述了绳系支撑在风洞试验中的应用,并给出动态分析;进一步根据绳牵引并联支撑技术的特点,将其分为可实现受迫运动的冗余约束支撑,以及可实现受迫+自由运动的欠约束支撑;其次,重点阐述了冗余约束与欠约束两类支撑系统的若干关键技术问题及其研究进展;最后,指出绳牵引并联支撑技术的发展方向是具有可重构性和智能化。可为绳牵引并联支撑技术在风洞试验中的工程应用提供一定的理论指导与技术支持。
中图分类号:
王晓光, 林麒. 风洞试验绳牵引并联支撑技术研究进展[J]. 航空学报, 2018, 39(10): 22064-022064.
WANG Xiaoguang, LIN Qi. Progress in wire-driven parallel suspension technologies in wind tunnel tests[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(10): 22064-022064.
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