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倾转四旋翼机过渡状态操纵策略对结构载荷的影响分析

贺永涛 张夏阳 王鑫 郑礼雄

航空工程进展2025,Vol.16Issue(3):189-197,9.
航空工程进展2025,Vol.16Issue(3):189-197,9.DOI:10.16615/j.cnki.1674-8190.2025.03.20

倾转四旋翼机过渡状态操纵策略对结构载荷的影响分析

Analysis of the influence of transition state control strategy on structural load of quad-tiltrotor

贺永涛 1张夏阳 1王鑫 1郑礼雄1

作者信息

  • 1. 南京航空航天大学 直升机动力学全国重点实验室,南京 210016
  • 折叠

摘要

Abstract

There are complex structural load changes in the rotor during the tilt-transition of quad-tiltrotor aircraft,which can directly affect the life of the rotor.The control strategy analysis is beneficial to reveal the influence law of the rotor structural load,which can provide a conclusion basis for the future research on vibration suppression.In or-der to study the influence of tilt-transition control strategy on rotor dynamic characteristics,a comprehensive flight dynamics model of tiltrotor is established,two typical control strategies of tiltrotor transition state are designed,and the trim characteristics and aerodynamic load characteristics of the fixed tilt angle state are studied through nu-merical simulation,as well as the influence of the transition state control strategy on the dynamic characteristics of the rotor.By considering the influence of aerodynamics on structure,the aerodynamic loads are treated as external forces applied to the blade surface,and the blade dynamics equation is solved using finite element method.The Newmar k-β method is used to study the displacement response,and the influence of transition state control strate-gy on the rotor dynamic characteristics is studied.The results show that the periodic variable-pitch control during transition flight can reduce the aerodynamic loads on the rotor,so as to the rotor vibration response,which can achieve the load reduction on the rotor structure.

关键词

倾转四旋翼机/振动响应/操纵策略/配平特性

Key words

quad-tiltrotor/vibration response/control strategy/trim characteristic

分类

航空航天

引用本文复制引用

贺永涛,张夏阳,王鑫,郑礼雄..倾转四旋翼机过渡状态操纵策略对结构载荷的影响分析[J].航空工程进展,2025,16(3):189-197,9.

基金项目

国家自然科学基金(12472237) (12472237)

航空科学基金(2024Z010052002) (2024Z010052002)

中国科协青年人才托举工程(2022QNRC001) (2022QNRC001)

中国科协科技智库青年人才计划(XMSB20240710072) (XMSB20240710072)

江苏高校优势学科建设工程资助项目 ()

某专项项目(FKFB2023110833) (FKFB2023110833)

航空工程进展

1674-8190

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