145280 ⎘
Application in turbines in gas turbines for a special turbine stage for a special compressor stage for an intermediate stage of a compressor
Compressor bleed pressure recovery
#2Variable speed boost compressor for gas turbine engine cooling air supply
#3Airfoil shape for second stage compressor stator vane
#4Airfoil shape for second stage compressor rotor blade
#5Airfoil shape for third stage compressor stator vane
#6Bleed air systems for use with aircraft and related methods
#7Radial cooling system for gas turbine engine compressors
#8Bleed ejector
#9Gas turbine and component-temperature adjustment method therefor
#10Intercooled cooling air with dual pass heat exchanger
#11Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the third stage of a turbine
#12Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the fifth stage of a turbine
#13Intercooled cooling air
#14Airfoil shape for second stage compressor rotor blade
#15Airfoil shape for tenth stage compressor rotor blade
#16Airfoil shape for fourth stage compressor rotor blade
#17Intercooled cooling air with dual pass heat exchanger
#18Variable speed boost compressor for gas turbine engine cooling air supply
#19Intercooled cooling air with dual pass heat exchanger
#20Hybrid compressor bleed air for aircraft use
#21Two spool gas generator with improved air porting
#22Gas turbine engine with supersonic compressor
#23Gas turbine engine
#24Active clearance control system and method for gas turbine
#25Compressor stator vane airfoils
#26Compressor stator vane airfoil
#27Compressor stator vane airfoils