DocumentCode :
2903212
Title :
Conception of a UHB engine simulator for the essential characteristics of a true-scale engine
Author :
Bolms, H.T. ; Braunling, W.
Author_Institution :
Deutsche Forschungsanstalt fuer Luft- und Raumfahrt, Gottingen
fYear :
1991
fDate :
27-31 Oct 1991
Firstpage :
190
Lastpage :
195
Abstract :
Turbine powered simulators (TPSs) usually are not able to simulate the whole spectrum of characteristic features of an original engine correctly and simultaneously. The difficulties in scaling down an engine are the reasons for these deficiencies. The order of magnitude of the errors resulting from these problems is shown for a turbine powered simulator set up conventionally. A revised simulator concept that avoids most of the significant deficiencies of conventional simulators is presented considering a typical UHB (ultra high bypass) engine. A correct simulation, which permits the full transmission of simulation results to the real engine, requires the correct simulation of the secondary cycle, the primary nozzle flow, and the inlet flow. Contrary to a conventional TPS, the new concept, besides the correct simulation of the specific thrust, also allows the correct simulation of the thrust partition between the secondary and the primary cycle
Keywords :
aerospace engines; aerospace simulation; aircraft; turbogenerators; UHB engine simulator; advanced ducted propfan engine; aircraft engine; inlet flow; primary cycle; primary nozzle flow; secondary cycle; thrust partition; turbine powered simulator; turbofan engine; ultra high bypass engine; Aerodynamics; Airplanes; Analytical models; Angular velocity; Engines; Fuel economy; Manufacturing; Power generation economics; Temperature; Turbines;
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.1991.186239
Filename :
186239
Link To Document :
بازگشت