Takeoff Performance Analysis Based on Aeroengine EGT Trend Monitoring and Control

Fu Qiang; Fan Ding

doi:10.4028/www.scientific.net/AMM.680.307

Paper Titles

Development of Droplets Penetrating Roots Performance Test Device and Tests Applied this Device in Ultrasonic Aeroponic System
p.288

Simulation and Experimental Investigation of Springback in Air V-Bending Process Using Finite Element Method (FEM)
p.292

Kinematics Modelling and Simulation of Aero-Engine Fuel Piston Pump
p.299

A Design Method of Aero Fuel Centrifugal Pump with Integrated Inducer and Impeller
p.303

Takeoff Performance Analysis Based on Aeroengine EGT Trend Monitoring and Control
p.307

Positional Accuracy Based on a Load Identification Optimization on a Linear Motor Sheet Forming Feeder
p.311

Dynamic Analysis and Balance Design for a Constant Temperature Oscillator Based on ADAMS
p.315

Determining the Energy-Optimal Base Position of Industrial Robots by Means of the Modelica Multi-Physics Language
p.320

The Analysis of Displacements and the Load Distribution between Elements in a Planetary Roller Screw
p.326

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 680Takeoff Performance Analysis Based on Aeroengine...

Takeoff Performance Analysis Based on Aeroengine EGT Trend Monitoring and Control

Abstract:

Exhaust gas temperature (EGT) is an important parameter for aeroengine. By monitoring the change in trend, can effectively predict the engine take-off performance. The characteristics of takeoff EGT were introdeced firstly. Two methods of estimating takeoff performance were analyzed subsequently. According to the statistical data, EGT can be used for takeoff performance prediction.

You might also be interested in these eBooks

Materials Science, Mechanical Structures and Engineering

View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volume 680)

Pages:

307-310

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.680.307

Citation:

Cite this paper

Online since:

October 2014

Authors:

Fu Qiang*, Fan Ding

Keywords:

EGT, Monitoring, Performance, Takeoff, Trend

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

* - Corresponding Author

References

[1] ZHANG Jin, HONG Jie, CHEN Guang, Technology and development of modern aeroengine [M]. Beijing: Beijing University of Aeronautics and Astronautics Press, 2006. (in Chinese).

Google Scholar

[2] LIAN Xiaochun, WU Hu. Aeroengine priniple [M]. Xi'an: Northwestern Polytechnical University Press, 2001. (in Chinese).

Google Scholar

[3] Koen R W. GENEG-A program for calculating design and off-design performance for tuibojet and turbofan engine [R]. NASA-TND-6552, (1972).

Google Scholar

[4] Lewis Research Center Cleveland Ohio. Object-oriented approach for gas turbine engine simulation [R]. NASA-TM-106970. July (1995).

Google Scholar