Research on measurement of infrared spectral radiant intensity of aero-engine exhaust system

Author

Yanmei Liu ; Li Fu ; Jianhui Xi ; Yan Ren

Author_Institution

Shenyang Aerosp. Univ., Shenyang, China

fYear

2014

fDate

May 31 2014-June 2 2014

Firstpage

1177

Lastpage

1180

Abstract

This paper presents a testing method for infrared radiation characteristics of the aircraft exhaust system. By using graphical programming language of virtual instrument development testing platform, infrared radiation characteristics of jet aircraft are studied. Infrared radiation can be achieved, displayed and so on. The virtual panel and block diagram are designed. The system designed mainly is composed of infrared radiometer calibration, data collection procedures and showing procedures. Simulation results show that the method is reliable and practical.

Keywords

aerospace computing; aircraft instrumentation; infrared spectra; jet engines; mechanical engineering computing; radiometry; virtual instrumentation; visual languages; aero-engine exhaust system; aircraft exhaust system; block diagram; data collection procedures; graphical programming language; infrared radiometer calibration; infrared spectral radiant intensity measurement; jet aircraft; showing procedures; testing method; virtual instrument development testing platform; virtual panel; Aircraft; Calibration; Exhaust systems; Instruments; Missiles; Radiometry; Testing; calibration; infrared radiation; testing platform; virtual panel;

fLanguage

English

Publisher

ieee

Conference_Titel

Control and Decision Conference (2014 CCDC), The 26th Chinese

Conference_Location

Changsha

Print_ISBN

978-1-4799-3707-3

Type

conf

DOI

10.1109/CCDC.2014.6852344

Filename

6852344