Towards an integrated framework for propulsion, aerothermal heating, and control for hypersonic UAVs

建立高超音速无人机推进、气动加热和控制的集成框架

• 批准号: 577269-2022
• 负责人: Hickey, JeanPierreJP
• 金额: $ 1.46万
• 依托单位: University of Waterloo
• 依托单位国家: 加拿大
• 项目类别: Alliance Grants
• 财政年份: 2022
• 资助国家: 加拿大
• 起止时间: 2022-01-01 至 2023-12-31
• 项目状态: 已结题
• 来源: https://www.nserc-crsng.gc.ca/ase-oro/Details-Detailles_eng.asp?id=760349
• 关键词: Towards; integrated; framework; propulsion; aerothermal

Commercial Unmanned Aerial Vehicles (UAVs) are purpose-built vehicles that are tailored to the intended applications and use cases. As the use cases for UAVs continue to grow, so do the needs for new, bespoke vehicle designs. This is especially true in the use of UAVs for high-speed reconnaissance and surveillance where speed and agility must be balanced with reliability, efficiency and environmental impact. To meet the specific performance requirements, the novel UAV designs ultimately revolve around the selection and integration of the propulsion system, while considering aerothermal heating effects and control systems. The current research program seeks develop an integrated framework for the design of a novel class of hypersonic UAVs. This work will help UVAD develop and commercialize the first, designed-in-Canada hypersonic UAV to compete on the global market.

商业无人机（UAVS）是针对预期的应用和用例量身定制的专用车辆。随着无人机的用例继续增长，新定制车辆设计的需求也是如此。在使用无人机进行高速侦察和监视的情况下，尤其如此，速度和敏捷性必须与可靠性，效率和环境影响保持平衡。 为了满足特定的性能要求，新颖的无人机设计最终围绕着推进系统的选择和整合，同时考虑了航空热的加热效果和控制系统。当前的研究计划正在寻求为设计新型超音速无人机设计的设计综合框架。这项工作将有助于UVAD开发和商业化第一个在加拿大高音无人机上设计的，以在全球市场上竞争。