AERO GAS TURBINE ENGINE WITH COMPRESSOR AND ASSOCIATED METHOD
AERO GAS TURBINE ENGINE WITH COMPRESSOR AND ASSOCIATED METHOD
- New search for: STOCKWELL MARK
- New search for: STOCKWELL MARK
There is disclosed an aero gas turbine engine comprising a compressor and an array of variable inlet guide vanes for the compressor. The angle of the variable inlet guide vanes is controlled by scheduling, the scheduling comprising a first component invoked for engine ground start and a second component invoked for engine in-flight windmill start at least under particular flight conditions. The angle of the variable inlet guide vanes required by at least a portion of the second component is greater than the angle of the variable inlet guide vanes required by at least a portion of the first component.
Document information
AERO GAS TURBINE ENGINE WITH COMPRESSOR AND ASSOCIATED METHOD
FLUGZEUG-GASTURBINENTRIEBWERK MIT VERDICHTER UND ZUGEHÖRIGES VERFAHREN
MOTEUR DE TURBINE À GAZ AÉRIENNE AVEC COMPRESSEUR ET MÉTHODE ASSOCIÉE
2019-09-04
Patent
Electronic Resource
English
| IPC: | F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS / B64C AEROPLANES , Flugzeuge / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS |
Similar titles
Gas Turbine Aero Engine Compressor Blade Erosion and Heat Resistant Coatings
| British Library Conference Proceedings | 2011
Gas Turbine Aero Engine Compressor Blade Erosion and Heat Resistant Coatings
| British Library Conference Proceedings | 2011
Specification for Aero and Aero-Derived Gas Turbine Engine Lubricants
SAE Technical Papers | 2013