DocumentCode :
2903638
Title :
Fault diagnostics on jet engine starting
Author :
Liu, H.Z. ; Wang, H.M. ; Ni, X.Q.
Author_Institution :
Beijing Univ. of Aeronaut. & Astronaut., China
fYear :
1991
fDate :
27-31 Oct 1991
Firstpage :
392
Lastpage :
396
Abstract :
To investigate jet engine starting, a series of engine parameters must be evaluated. The measurements of rotor speed, fuel flow rate, fuel combustion, and gas temperature must be taken in real time. A dynamic measurement system was used to evaluate the starting performance, and to diagnose faults during starting. The dynamic measurement system contained a photoelectric system and a fast thermocouple used to detect and inspect the fault symptoms during starting. As a result, the starting operation quality to be assessed can be determined and improved. The experiment was completed on a sea-level test bench for a small single spool jet engine
Keywords :
aerospace engines; aerospace testing; combustion; fault location; flames; photodetectors; starting; combustion; dynamic measurement; fault diagnosis; flame signal; fuel combustion; fuel flow rate; gas temperature; ignition; jet engine starting; photoelectric system; real time; rotor speed; sea-level test bench; single spool jet engine; thermocouple; Aerodynamics; Combustion; Extraterrestrial measurements; Fires; Frequency; Fuels; Ignition; Jet engines; Phototransistors; Testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Instrumentation in Aerospace Simulation Facilities, 1991. ICIASF '91 Record., International Congress on
Conference_Location :
Rockville, MD
Type :
conf
DOI :
10.1109/ICIASF.1991.186262
Filename :
186262
Link To Document :
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