GAS TURBINE ACCELERATION LIMIT BIASING FOR PREMATURE ASYMMETRIC OPERATING REGIME EXITS

BLENDED N-DOT AND RATIO UNIT REFERENCE ACCELERATION CONTROL ARCHITECTURE FOR GAS TURBINE ENGINE

Device for driving a generator of an aircraft turbomachine and method for regulating the speed of such a generator

GAS TURBINE ENGINE STALL MARGIN MANAGEMENT

Asymmetric propulsion system with heat recovery

Systems and methods for filling a fuel manifold of a gas turbine engine

Acceleration of a gas turbine

Active multi-effector control of high pressure turbine clearances

System and method for exiting an asymmetric engine operating regime

Transient operation control of a hybrid gas turbine engine

Method and system for setting an acceleration schedule for engine start

System and method for an engine controller based on inverse dynamics of the engine

TURBOMACHINE TRAIN AND METHOD FOR COUPLING THE TURBOMACHINE TRAIN

Propulsion system for an aircraft

Method and system for setting an acceleration schedule for engine start

System and method for an engine controller based on inverse dynamics of the engine

System and method for an engine controller based on acceleration power

Electrical augmentation of a gas turbine engine

Propulsion system

Method and a device for generating a command for the flow rate of fuel that is to be injected into a combustion chamber of a turbine engine

Fuel-air ratio control of gas turbine engines

Method and system for starting an aircraft turboengine

Method and apparatus for controlling gas turbine when gas turbine is started

Control system and method for controlling a gas turbine engine during transients

System and method for preventing an emergency over-speed condition in a rotating machine

Control of a gas turbine engine

Systems and methods for boundary control during steam turbine acceleration

Avionics method and device for monitoring a turbomachine at startup

Systems and Methods for Distributing Torque Contribution

Method of controlling speed transients in a turbine engine

Method of monitoring an electronic engine control (EEC) to detect a loss of fuel screen open area

Gas turbine startup control

Method for starting a turbomachine

Method for regulating the flow rate of fuel to a turboshaft engine in acceleration or in deceleration

ENGINE CONTROL SYSTEM

Method for starting a pressure storage plant

Approach to extending life of gas turbine engine

Method and apparatus for assessing gas turbine acceleration capability

Approach to extending life of gas turbine engine

Method and Apparatus for Prevention of Compressor Stall and Combustion Flameout in a Turbine Engine

Method for regulating the flow rate of fuel to a turboshaft engine in acceleration or in deceleration

Approach to extending life of gas turbine engine

Approach to extending life of gas turbine engine

Fault detection logic for engines

Time varying reslam logic for acceleration reference and maximum fuel flow rate