MITIGATION OF ROTATING STALL IN TURBINE EXHAUST SECTION USING FLOW CONTROL VANES

MITIGATION OF ROTATING STALL IN TURBINE EXHAUST SECTION USING SEGMENTED AUXILIARY STRUTS

Variable tandem fan outlet guide vanes

Variable outlet guide vanes

Adaptive case for a gas turbine engine

System and method for detecting inlet temperature distortion of an engine

Methods and apparatus for reducing flow distortion at engine fans of nacelles

Method for separated flow detection

Stability margin and clearance control using power extraction and assist of a gas turbine engine

Methods and apparatus for reducing flow distortion at engine fans of nacelles

Aircraft comprising a turbine engine incorporated into the rear fuselage with variable supply

Gas turbine engine with progressive stall recovery

Secondary airflow passage for adjusting airflow distortion in gas turbine engine

Takeoff power management system and method for gas turbine engines

Controlling a Gas Turbine Engine to Account for Airflow Distortion

Turbofan engine and method of reducing air flow separation therein

Thrust reversal for turbofan gas turbine engine

Non-axisymmetric fan flow path

GAS TURBINE HAVING AN EXHAUST GAS DIFFUSER AND SUPPORTING FINS

Continuous-flow machine with at least one guide vane ring

Protecting the operating margin of a gas turbine engine having variable vanes from aerodynamic distortion

Compressor inlet manifold for a gas turbine engine

Method for injecting water into a multistage axial compressor of a gas turbine

COMPRESSOR HAVING A GUIDE VANE ASSEMBLY WITH A RADIALLY VARIABLE OUTFLOW

Compressor

Closed-loop control for a gas turbine with actively stabilized compressor

Apparatus and method for controlling a compressor

Controlling operation of a compressor to avoid surge