145649 ⎘
Control; Purpose of the control system to cope with, or avoid, compressor flow instabilities; Compressor surge or stall caused by working fluid flow velocity profile distortion due to high angle of attack of aircraft
Methods and apparatus for reducing flow distortion at engine fans of nacelles
#2Methods and apparatus for reducing flow distortion at engine fans of nacelles
#3Takeoff power management system and method for gas turbine engines
#4Protecting the operating margin of a gas turbine engine having variable vanes from aerodynamic distortion
#5Double-ducted fan
#6Closed-loop control for a gas turbine with actively stabilized compressor
#7Apparatus and method for controlling a compressor
#8Fan nacelle flow control