Technological analysis for the turbofan engine of high altitude long endurance unmanned aerial vehicles

Gang Zhao; Yuan Hu Cai; Qiu Ye Tu; Zhan Xue Wang

Technological analysis for the turbofan engine of high altitude long endurance unmanned aerial vehicles

Gang Zhao
, Yuan Hu Cai
, Qiu Ye Tu
, Zhan Xue Wang

动力与能源学院

Northwestern Polytechnical University Xian

科研成果: 期刊稿件 › 文章 › 同行评审

3 引用（Scopus）

摘要

To develop the turbofan engine for high altitude, long endurance unmanned aerial vehicles (HALE UAV), the problems which will be run into at high altitude are discussed and analysed for high/low pressure compressor, combustion system, high/low pressure turbine, engine control system, lubrication system and internal air system. The solution for every problems are proposed.

源语言	英语
页（从-至）	154-158+181
期刊	Tuijin Jishu/Journal of Propulsion Technology
卷	30
期	2
出版状态	已出版 - 4月 2009

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引用此

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title = "Technological analysis for the turbofan engine of high altitude long endurance unmanned aerial vehicles",

abstract = "To develop the turbofan engine for high altitude, long endurance unmanned aerial vehicles (HALE UAV), the problems which will be run into at high altitude are discussed and analysed for high/low pressure compressor, combustion system, high/low pressure turbine, engine control system, lubrication system and internal air system. The solution for every problems are proposed.",

keywords = "High altitude flight, Pilotless aircraft, System parameter, Turbofan engine",

author = "Gang Zhao and Cai, \{Yuan Hu\} and Tu, \{Qiu Ye\} and Wang, \{Zhan Xue\}",

year = "2009",

month = apr,

language = "英语",

volume = "30",

pages = "154--158+181",

journal = "Tuijin Jishu/Journal of Propulsion Technology",

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publisher = "Journal of Propulsion Technology",

number = "2",

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T1 - Technological analysis for the turbofan engine of high altitude long endurance unmanned aerial vehicles

AU - Zhao, Gang

AU - Cai, Yuan Hu

AU - Tu, Qiu Ye

AU - Wang, Zhan Xue

PY - 2009/4

Y1 - 2009/4

N2 - To develop the turbofan engine for high altitude, long endurance unmanned aerial vehicles (HALE UAV), the problems which will be run into at high altitude are discussed and analysed for high/low pressure compressor, combustion system, high/low pressure turbine, engine control system, lubrication system and internal air system. The solution for every problems are proposed.

AB - To develop the turbofan engine for high altitude, long endurance unmanned aerial vehicles (HALE UAV), the problems which will be run into at high altitude are discussed and analysed for high/low pressure compressor, combustion system, high/low pressure turbine, engine control system, lubrication system and internal air system. The solution for every problems are proposed.

KW - High altitude flight

KW - Pilotless aircraft

KW - System parameter

KW - Turbofan engine

UR - https://www.scopus.com/pages/publications/65449125469

M3 - 文章

AN - SCOPUS:65449125469

SN - 1001-4055

VL - 30

SP - 154-158+181

JO - Tuijin Jishu/Journal of Propulsion Technology

JF - Tuijin Jishu/Journal of Propulsion Technology

IS - 2

ER -

Technological analysis for the turbofan engine of high altitude long endurance unmanned aerial vehicles

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