A multi cycle propulsion system for amphibious unmanned aerial vehicle with repeatable water exit

Jun TIAN; Yufan XIE; Fei LONG; Qin LIU

doi:10.13224/j.cnki.jasp.20210415

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A multi cycle propulsion system for amphibious unmanned aerial vehicle with repeatable water exit

Aerothermodynamics and Aeroengine Design | 更新时间：2025-03-14

- A multi cycle propulsion system for amphibious unmanned aerial vehicle with repeatable water exit
- Journal of Aerospace Power Vol. 37, Issue 9, Pages: 1793-1806(2022)
- 作者机构：
  
  1.中国航空工业集团有限公司中国特种飞行器研究所，湖北荆门 448035
  2.空军后勤部机场保障局，北京 100720
  3.南京普国科技有限公司，南京 210016
- 作者简介：
- 基金信息：
- DOI：10.13224/j.cnki.jasp.20210415
  CLC：
- 稿件说明：
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Jun TIAN, Yufan XIE, Fei LONG, et al. A multi cycle propulsion system for amphibious unmanned aerial vehicle with repeatable water exit[J]. Journal of Aerospace Power, 2022, 37(9): 1793-1806.
DOI：

Jun TIAN, Yufan XIE, Fei LONG, et al. A multi cycle propulsion system for amphibious unmanned aerial vehicle with repeatable water exit[J]. Journal of Aerospace Power, 2022, 37(9): 1793-1806. DOI： 10.13224/j.cnki.jasp.20210415.

摘要

针对一种可重复出水的两栖无人飞行器（UAV）总体方案及任务需求，提出一种水下采用泵喷水推进、出水采用液体火箭发动机推进、空中巡航采用涡扇发动机推进的多循环推进系统方案。根据推进系统技术发展现状、趋势，不同发动机循环特点、各阶段推力需求及多循环任务需求，开展了多循环方案设计方法研究，并计算出典型推进系统方案尺寸、质量、任务剖面燃油消耗质量等参数，验证了推进系统多循环方案及其设计方法的可行性，结果表明：综合未来飞行器及推进系统技术发展水平，所设计的多循环推进系统方案，能够实现无人飞行器可重复出水需求，其中能源需求占全机总质量的比例为26%左右。

Abstract

In view of the overall scheme and mission requirements of an amphibious unmanned aerial vehicle （UAV） with repeatable water exit

a multi‑cycle propulsion system using pump for water jet propulsion underwater

liquid rocket engine propulsion for water exit

and turbofan engine propulsion for air cruise was proposed.According to the development status and trends of propulsion system technology

the characteristics of different engine cycles

the thrust requirements of each stage and the requirements of multi‑cycle tasks

the study of multi cycle program design methods was carried out

and the typical propulsion system program size

mass

mission profile fuel consumption quality

etc

were calculated.The feasibility of the multi cycle propulsion system scheme and its design method were verified.The results showed that the multi cycle propulsion system scheme designed can meet the repeatable water demand of the unmanned aerial vehicle

in which the energy demand could account for about 26% of the total mass of the whole aerial vehicle.

关键词

Keywords

references

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