PARTIAL-ADMISSION TURBINE ASSEMBLY FOR AN AIRCRAFT AND METHOD FOR CONTROLLING SAME

Epicyclic reduction gear for a turbomachine

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

Aircraft propulsion system with inter-turbine burner

Method for regulating the acceleration of a turbomachine

Two-shaft gas turbine control system and method

Electric power generation controller for use in aircraft

System and method for detecting and accommodating loss of torque on gas turbine engines

Gas turbine generator speed DC to DC converter control system

Method for controlling the speed and the power of a turbine engine propeller

Motor controller for electric blower motors

Control method of a compressor mechanically coupled to a turbine

Output ring gear for integrated drive generator

Gas turbine generator torque DC to DC converter control system

Gas turbine generator speed DC to DC converter control system

Turbine rotor assembly having a retaining collar for a bayonet mount

Gas turbine system and method of controlling the same

Integrated power generation and compression train, and method

Turbocharger assembly with oil carry-over protection

Dynamic flight command cross-feed for rotor speed droop reduction

Power plant thrust management system for turboprop engines

2-shaft gas turbine, and the control method of opening degree of inlet guide vane of the gas turbine

Control system for turbomachine complex and method of operating the same

Fuel control method for gas turbine, control device for executing said method, and gas turbine installation provided with said control device

Correction system and method for gas turbine proportional droop governor

Method and apparatus for operating an EC-fuel pump

Turboexpander and driven turbomachine system

Steam turbine governing system for maintaining synchronization and process for performing the same

Generating device for aircraft

Sealing arrangement of accessory to aircraft engine

TWIN-SHAFT GAS TURBINE

Rocket engine system for realizing high-speed response

Systems, methods, and apparatus for determining steady state conditions in a gas turbine

Twin-shaft gas turbine including a control system for adjusting the compressor inlet guide vane angle to optimize engine transient response

Aircraft electric generation system

Power station and method for its operation

Method for operating a power plant

Twin-shaft gas turbine including a control system for adjusting the compressor inlet guide vane angle to optimize engine transient response

Gas turbine control system

Gas energy conversion apparatus and method

Gas turbine control system