Vibrations experienced in PT6 and JT15D installations are reviewed. The JT15D turbojet vibrations are due primarily to rotor unbalances which may produce significant responses at some of the critical speeds. The PT6 turboprop vibrations are mainly caused by the propeller and, therefore, occur at low frequencies. PT6 gearbox vibrations at very high frequencies are of interest in the production process. Typical vibration problems are discussed. (Peters)
Vibration aspects of small turbine engines in aircraft installations
Schwingungen kleiner Turbomaschinen in Flugzeugen
1980
8 Seiten, 13 Bilder, 12 Quellen
Conference paper
English
Vibration Aspects of Small Turbine Engines in Aircraft Installations
SAE Technical Papers | 1980
|Small turbine engine integration in aircraft installations
Tema Archive | 1979
|Engineering Index Backfile | 1948