Abstract The influence of thermocouple inertia compensation errors on the quality of channels selecting in multidimensional gas turbine engine control systems is analyzed. Based on the results obtained, the requirements to the accuracy of inertia thermocouple compensator realization are formulated. The study was carried out by means of mathematical modeling.
Development of requirements for accuracy of inertia compensation in gas temperature control loop of gas turbine engine control systems with a channel selector
Russian Aeronautics (Iz VUZ) ; 58 , 1 ; 71-77
2015-01-01
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch