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倾转四旋翼机高效低噪旋翼外形优化设计

ZHANG Xiayang LUO Bin CHEN Xi YANG Tao

航空学报2025,Vol.46Issue(z1):38-56,19.
航空学报2025,Vol.46Issue(z1):38-56,19.DOI:10.7527/S1000-6893.2025.32183

倾转四旋翼机高效低噪旋翼外形优化设计

Optimization design of high-efficiency and low-noise rotor layout for quad-tiltrotor aircraft

ZHANG Xiayang 1LUO Bin 1CHEN Xi 1YANG Tao1

作者信息

  • 1. National Key Laboratory of Helicopter Aeromechanics,College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China
  • 折叠

摘要

Abstract

Quad-tiltrotor aircraft experience complex unsteady noise characteristics due to the presence of multi-vortex and multi-component aerodynamic interference among various components during typical flight modes.To obtain the high-efficiency and low-noise rotor shape combined with helicopter mode and fixed-wing mode,the computation meth-ods of rotor aerodynamic and noise considering the aerodynamic environment of the whole aircraft are established.The sensitivity analysis of the tip shape parameters to the aerodynamic and noise characteristics of the rotor is carried out.Based on the improved Latin hypercube sampling method and the genetic algorithm,the high-efficiency/low-noise shape design optimization process of the forward and rear rotors is established.A set of high-efficiency and low-noise forward and rear rotor shapes are obtained and are further compared with the reference ones.The results show that the aerodynamic and noise characteristics of the rotor are sensitive to the blade tip shape,which can severely affect the hover efficiency and cruise efficiency.After optimization,the hover efficiencies of the forward rotor and the rear ro-tor are increased by 1.5%and 1.0%,and the noise pressure level is reduced by 1.8 dB.In the fixed-wing mode,the cruise efficiencies of the forward rotor and the rear rotor are increased by 10.1%and 9.0%,and the noise pres-sure level is reduced by 2.2 dB.

关键词

倾转四旋翼机/气动干扰/气动性能/噪声特性/优化设计

Key words

quad-tiltrotor aircraft/aerodynamic interference/aerodynamic performance/noise characteristics/opti-mization design

分类

航空航天

引用本文复制引用

ZHANG Xiayang,LUO Bin,CHEN Xi,YANG Tao..倾转四旋翼机高效低噪旋翼外形优化设计[J].航空学报,2025,46(z1):38-56,19.

基金项目

国家自然科学基金(12472237,12032012) (12472237,12032012)

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

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

国家重点实验室基金(61422202201) (61422202201)

江苏高校优势学科建设工程 National Natural Science Foundation of China(12472237,12032012) (12472237,12032012)

Aeronautical Science Foundation of China(2024Z010052002) (2024Z010052002)

Young Elite Scientists Sponsorship Program by CAST(2022QNRC001) (2022QNRC001)

National Key Laboratory Foundation of China(61422202201) (61422202201)

Priority Academic Program Development of Jiangsu Higher Education Institutions ()

航空学报

OA北大核心

1000-6893

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