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