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交错六旋翼飞行器地效影响下的着陆特性研究

朱赫 韦少雄 聂宏 魏小辉 杜俞浩

航空科学技术2025,Vol.36Issue(8):27-33,7.
航空科学技术2025,Vol.36Issue(8):27-33,7.DOI:10.19452/j.issn1007-5453.2025.08.004

交错六旋翼飞行器地效影响下的着陆特性研究

Analysis on Vertical Landing Stability for Intermeshing Hexacopter Under Ground Effects

朱赫 1韦少雄 2聂宏 3魏小辉 4杜俞浩2

作者信息

  • 1. 南京航空航天大学,江苏 南京 210016||直升机动力学全国重点实验室,江苏 南京 210016||飞行器先进设计技术国防重点学科实验室,江苏 南京 210016
  • 2. 南京航空航天大学,江苏 南京 210016
  • 3. 直升机动力学全国重点实验室,江苏 南京 210016||飞行器先进设计技术国防重点学科实验室,江苏 南京 210016
  • 4. 飞行器先进设计技术国防重点学科实验室,江苏 南京 210016||航空航天结构力学及控制全国重点实验室,江苏 南京 210016
  • 折叠

摘要

Abstract

The intermeshing rotorcraft often encounters ground effects during the landing process,which generate additional lift and disturbance forces on the rotors,leading to dynamic rebound or even tipping of the aircraft,severely threatening landing safety.This paper analyzes the variation of lifts on a hexacopter with intermeshing rotors under different rotational speeds and altitudes above the ground through ground effect experiments.A theoretical model of lift for the intermeshing hex rotor was derived using potential flow and image method,and a dynamic landing dynamics model was established,considering the initial landing height of the aircraft,the foot-to-ground friction force,and landing velocity.The simulation results indicate that the rotorcraft is significantly affected by ground effects at high rotational speeds,requiring a certain initial descent velocity for landing.There exists an optimal descent velocity that minimizes the structural forces on the aircraft now of touchdown.It provides a theoretical basis for the safe and stable landing of hexacopter under complex ground effects.

关键词

气动干扰/地面效应/多旋翼飞行器/着陆稳定性/数值仿真

Key words

aerodynamic interference/ground effect/multirotor aircraft/landing stability/numerial simulation

分类

航空航天

引用本文复制引用

朱赫,韦少雄,聂宏,魏小辉,杜俞浩..交错六旋翼飞行器地效影响下的着陆特性研究[J].航空科学技术,2025,36(8):27-33,7.

基金项目

国家自然科学基金(52202443,52275114) (52202443,52275114)

航空科学基金(2023Z010052002) (2023Z010052002)

中国博士后科学基金(2023M731656) (2023M731656)

直升机动力学全国重点实验室基金(2023-JCJQ-LB-067-05e) (2023-JCJQ-LB-067-05e)

江苏省自然科学基金(BK20220898) National Natural Science Foundation of China(52202443,52275114) (BK20220898)

Aeronautical Science Foundation of China(2023Z010052002) (2023Z010052002)

China Postdoctoral Science Foundation(2023M731656) (2023M731656)

National Key Laboratory of Helicopter Aeromechanics Foundation(2023-JCJQ-LB-067-05e) (2023-JCJQ-LB-067-05e)

Natural Science Foundation of Jiangsu Province(BK20220898) (BK20220898)

航空科学技术

1007-5453

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