Abstract Hardware-in-the-loop testing technology for automatic control, condition monitoring and diagnostics systems of gas turbine engines is described. The technology proposed makes it possible to simulate combinations and chains of unexpected and gradual failures of engines, transducers and actuators.
Hardware-in-the-loop testing technology for integrated control and condition monitoring systems of aircraft gas turbine engines
Russian Aeronautics (Iz VUZ) ; 51 , 1 ; 47-52
2008-03-01
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Control of aircraft turbine engines
Engineering Index Backfile | 1968
|Sealing technology for aircraft gas turbine engines
AIAA | 1974
|Engineering Index Backfile | 1948