Determination of Gas-Generator Fuel Capacity for Hybrid Aerial Underwater Vehicles with Airfoil Cavity-Forming System

V. P. Makhrov; V. A. Sorokin; A. I. Yur’ev

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Determination of Gas-Generator Fuel Capacity for Hybrid Aerial Underwater Vehicles with Airfoil Cavity-Forming System

机译：用翼型腔成形系统测定混合空中水下车辆的气体发电机燃料能力

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We determine the behavior of onboard gas-generator flowrate for generating the cavitation flow around a hybrid aerial underwater vehicle by using an annular wing on the underwater trajectory section.

机译：我们通过在水下轨迹部分上使用环形翼部分，确定船上气体发生器流量的行为，用于通过在水下轨迹部分上使用环形翼来产生混合鸟水下车辆周围的空化流动。

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来源
《Russian Aeronautics》 |2017年第4期|共5页
作者
V. P. Makhrov; V. A. Sorokin; A. I. Yur’ev;
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作者单位

Moscow Aviation Institute (National Research University);

Moscow Aviation Institute (National Research University);

Moscow Aviation Institute (National Research University);

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原文格式 PDF
正文语种 eng
中图分类航空;
关键词
cavitation flow; annular wing; gas flowrate;

机译：空化流动;环形翼;气体流量;

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专利

1. Determination of Gas-Generator Fuel Capacity for Hybrid Aerial Underwater Vehicles with Airfoil Cavity-Forming System [J] . V. P. Makhrov, V. A. Sorokin, A. I. Yur’ev Russian Aeronautics . 2017,第4期

机译：用翼型腔成形系统测定混合空中水下车辆的气体发电机燃料能力
2. A High-Efficiency Double DC-DC Conversion System for a Fuel Cell/Battery Hybrid Power Propulsion System in Long Cruising Range Underwater Vehicles [J] . Wang Bin, Hu Qiao, Wang Zhiyu Energy & fuels . 2020,第7期

机译：用于长巡航范围水下车辆的燃料电池/电池混合动力推进系统的高效双DC-DC转换系统
3. A sizing-design methodology for hybrid fuel cell power systems and its application to an unmanned underwater vehicle [J] . Q. Cai, D.J.L. Brett, D. Browning, Journal of power sources . 2010,第19期

机译：混合燃料电池动力系统的尺寸设计方法及其在无人水下航行器中的应用
4. Effect of Operating Parameters on a Hybrid Propulsion System with High Efficiency Fueled by Kerosene for High Altitude Long Endurance Unmanned Aerial Vehicles [C] . Zhixing Ji, Jiang Qin, Fafu Guo, AIAA/SAE/ASEE joint propulsion conference;AIAA propulsion and energy forum . 2018

机译：工作参数对高海拔长航程无人机高效率煤油燃料混合动力系统的影响
5. Power Management for Fuel Cell and Battery Hybrid Unmanned Aerial Vehicle Applications. [D] . Strele, Thomas. 2016

机译：燃料电池和电池混合动力无人机应用的电源管理。
6. Airfoil Selection Procedure Wind Tunnel Experimentation and Implementation of 6DOF Modeling on a Flying Wing Micro Aerial Vehicle [O] . Taimur Ali Shams, Syed Irtiza Ali Shah, Ali Javed, 2020

机译：翼型微型飞行器的机翼选择程序风洞实验和6DOF建模实现
7. A Feasibility Study for a Stratospheric Long-endurance Hybrid Unmanned Aerial Vehicle using a Regenerative Fuel Cell System [O] . Seong-Hyun Cho, Moon-Yong Cha, Minjin Kim, 2016

机译：利用再生燃料电池系统的平流层长耐久性混合空中航空公司的可行性研究
8. Preliminary Design and Prototyping Results of an Encapsulated Underwater Launch System for Micro Unmanned Aerial Vehicles (UAVs) [R] . Buescher, J., Mailey, C., Stenson, R., 2008

机译：用于微型无人机（UaV）的封装水下发射系统的初步设计和原型设计结果

Determination of Gas-Generator Fuel Capacity for Hybrid Aerial Underwater Vehicles with Airfoil Cavity-Forming System

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