DocumentCode :
2543470
Title :
Real-time detection of developing cracks in jet engine rotors
Author :
Eric, H.
Author_Institution :
Test Devices Inc., Hudson, MA
Volume :
6
fYear :
2000
fDate :
2000
Firstpage :
173
Abstract :
Test Devices has developed a unique method for detecting the existence of dangerous cracks in turbine engine disks. The system uses the data from two distinct sensors, a radial position sensor and an angular position reference signal. By combining these two data into a vector quantity, the system measures the displacement of the principal mass axis of the rotor. A reasoner system uses the change of principal mass axis to infer the presence of cracks. It does so by tracking changes in the unbalance as a function of the operating cycle count. The rate of change is compared with the known patterns of change produced by cracks as opposed to those produced by normal wear phenomena and other benign effects
Keywords :
aerospace engines; automatic testing; crack detection; diagnostic reasoning; fatigue testing; fault diagnosis; gas turbines; position measurement; rotors; NDT; Test Devices; angular position reference signal; cracks; displacement; high pressure turbine; jet engine rotors; power turbines; principal mass axis; radial position sensor; real time system; reasoner; turbine engine disks; vector quantity; wear; Cleaning; Coils; Eddy currents; Fluorescence; Inspection; Jet engines; Sensor systems; Testing; Thermal stresses; Vibration measurement;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference Proceedings, 2000 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
0-7803-5846-5
Type :
conf
DOI :
10.1109/AERO.2000.877893
Filename :
877893
Link To Document :
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