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

School of Power and Energy

Northwestern Polytechnical University Xian

Research output: Contribution to journal › Article › peer-review

3 Scopus citations

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.

Original language	English
Pages (from-to)	154-158+181
Journal	Tuijin Jishu/Journal of Propulsion Technology
Volume	30
Issue number	2
State	Published - Apr 2009

Keywords

High altitude flight
Pilotless aircraft
System parameter
Turbofan engine

Cite this

@article{b25c574348be4e36962f294235065057,

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",

issn = "1001-4055",

publisher = "Journal of Propulsion Technology",

number = "2",

}

TY - JOUR

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

Abstract

Keywords

Other files and links

Fingerprint

Cite this