Application of Fixed-Wings in Multi-Rotor Drones for Additional Lift

固定翼在多旋翼无人机附加升力中的应用

基本信息

  • 批准号:
    567789-2021
  • 负责人:
  • 金额:
    $ 7.29万
  • 依托单位:
  • 依托单位国家:
    加拿大
  • 项目类别:
    Alliance Grants
  • 财政年份:
    2021
  • 资助国家:
    加拿大
  • 起止时间:
    2021-01-01 至 2022-12-31
  • 项目状态:
    已结题

项目摘要

The durability of aerial vehicles are essential in the air mobility industry and drones operations. To this end, the aerodynamics efficiency and flight effectiveness of these systems are crucial in reducing drag and enhancing lift towards longer flight time. Multi-rotor drones, i.e., hexacopter, are designed for optimized maneuverability and effective landing/take-off in urban communities. However, this design is not efficient in cruising conditions, in which drones fly on a straight path with a constant tilt angle. Both the constant speed and tilt angle of the drones provide a suitable operating condition for fixed-wing aircraft to generate additional lift. Thus, we introduce the concept of a deployable Universal Lift Enhancement Device (ULED), in the form of a fixed or quasi-fixed wing, for multi-rotor drones. Using a combination of fundamental studies on unsteady wakes, aerodynamics of wings, and propeller downwash effects, this project aims to develop and test a prototype for an ULED under normal and maximum operating conditions for a hexacopter drone. This project combines numerical simulations using advanced in-house flow models and experimental studies in wind tunnels to optimize the design concept of ULED for deployment on a hexacopter. The final outcome of this project is well-trained engineers with unique skills in aerodynamics, aerospace and data analysis, as well as an operational ULED that enhances lift generation in multi-rotor drones. The latter has major implications in the air mobility industry, as well as civilian drones operations. The final outcome of this project is longer durability of drones, which has major impacts on the improved energy safety surveillance operations in northern Canada as well as lower emission air mobility. The knowledge gained and technology developed in this project (i.e., ULED) has significant indications on the renewable energy industry (wind and hydro-turbines), energy transportation industry (pipeline monitoring) and agriculture industry (crop production monitoring and optimization).
飞行器的耐用性在空中机动性行业和无人机操作中至关重要。为此,这些系统的空气动力学效率和飞行效率对于减少阻力和提高升力以延长飞行时间至关重要。多旋翼无人机,即六角战斗机,旨在优化机动性和在城市社区有效着陆/起飞。然而,这种设计在巡航条件下效率不高,在这种情况下,无人机在倾斜角度恒定的直线上飞行。无人机的恒速和倾角都为固定翼飞机产生额外升力提供了合适的运行条件。因此,我们引入了可展开的通用升力增强装置(ULED)的概念,其形式为固定或准固定机翼,用于多旋翼无人机。利用对非定常尾迹、机翼空气动力学和螺旋桨下洗效应的基础研究,该项目旨在开发和测试六角无人机在正常和最大工作条件下的ULED原型。该项目将先进的内部流动模型的数值模拟和风洞实验研究相结合,以优化六角飞行器上部署的ULED的设计理念。该项目的最终成果是训练有素的工程师,他们在空气动力学、航空航天和数据分析方面拥有独特的技能,以及一个可操作的ULED,可以增强多旋翼无人机的升力产生。后者在空中机动性行业以及民用无人机业务中具有重大影响。该项目的最终结果是无人机的耐用性更长,这对改善加拿大北部的能源安全监测行动以及降低排放空气流动性具有重大影响。在该项目中获得的知识和开发的技术(即ULED)对可再生能源行业(风力和水轮机)、能源运输行业(管道监测)和农业行业(作物生产监测和优化)具有重要的指示意义。

项目成果

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Hemmati, Arman其他文献

Why do anguilliform swimmers perform undulation with wavelengths shorter than their bodylengths?
  • DOI:
    10.1063/5.0040473
  • 发表时间:
    2021-03-01
  • 期刊:
  • 影响因子:
    4.6
  • 作者:
    Khalid, Muhammad Saif Ullah;Wang, Junshi;Hemmati, Arman
  • 通讯作者:
    Hemmati, Arman
Nonlinear response of passively flapping foils
  • DOI:
    10.1016/j.oceaneng.2022.112071
  • 发表时间:
    2022-08-10
  • 期刊:
  • 影响因子:
    5
  • 作者:
    Farooq, Hamayun;Khalid, Muhammad Saif Ullah;Hemmati, Arman
  • 通讯作者:
    Hemmati, Arman

Hemmati, Arman的其他文献

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{{ truncateString('Hemmati, Arman', 18)}}的其他基金

Vortex Interactions and Unsteady Wake Dynamics
涡相互作用和不稳定尾流动力学
  • 批准号:
    RGPIN-2020-03998
  • 财政年份:
    2022
  • 资助金额:
    $ 7.29万
  • 项目类别:
    Discovery Grants Program - Individual
Vortex Interactions and Unsteady Wake Dynamics
涡相互作用和不稳定尾流动力学
  • 批准号:
    RGPIN-2020-03998
  • 财政年份:
    2021
  • 资助金额:
    $ 7.29万
  • 项目类别:
    Discovery Grants Program - Individual
Reconfiguring In-Situ Thermal Oil Recovery facilities for Steam Assisted Geothermal Power (SAGP) Extraction
重新配置蒸汽辅助地热发电 (SAGP) 开采的原位热油回收设施
  • 批准号:
    556563-2020
  • 财政年份:
    2021
  • 资助金额:
    $ 7.29万
  • 项目类别:
    Alliance Grants
Vortex Interactions and Unsteady Wake Dynamics
涡相互作用和不稳定尾流动力学
  • 批准号:
    DGECR-2020-00490
  • 财政年份:
    2020
  • 资助金额:
    $ 7.29万
  • 项目类别:
    Discovery Launch Supplement
Vortex Interactions and Unsteady Wake Dynamics
涡相互作用和不稳定尾流动力学
  • 批准号:
    RGPIN-2020-03998
  • 财政年份:
    2020
  • 资助金额:
    $ 7.29万
  • 项目类别:
    Discovery Grants Program - Individual
Reconfiguring In-Situ Thermal Oil Recovery facilities for Steam Assisted Geothermal Power (SAGP) Extraction
重新配置蒸汽辅助地热发电 (SAGP) 开采的原位热油回收设施
  • 批准号:
    556563-2020
  • 财政年份:
    2020
  • 资助金额:
    $ 7.29万
  • 项目类别:
    Alliance Grants
Development of Reliable Wind Assessment Tool
开发可靠的风力评估工具
  • 批准号:
    530002-2018
  • 财政年份:
    2018
  • 资助金额:
    $ 7.29万
  • 项目类别:
    Connect Grants Level 1
Bio-inspired propulsors for efficient and high-speed locomotion, and energy harvesting
用于高效高速运动和能量收集的仿生推进器
  • 批准号:
    487807-2016
  • 财政年份:
    2017
  • 资助金额:
    $ 7.29万
  • 项目类别:
    Postdoctoral Fellowships
Investigating the unsteady lift and drag generation on oscillating airfoils, and their relationship with vortex structures in the surrounding flows
研究振荡翼型产生的非定常升力和阻力,及其与周围流中涡流结构的关系
  • 批准号:
    426863-2012
  • 财政年份:
    2012
  • 资助金额:
    $ 7.29万
  • 项目类别:
    Alexander Graham Bell Canada Graduate Scholarships - Master's

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