IMPROVED PROPULSION ASSEMBLY FOR MULTI-ENGINE HYBRID AIRCRAFT

POWERPLANT WITH MULTIPLE INTEGRATED GAS TURBINE ENGINES

PLANT FOR HIGH-EFFICIENCY FUEL TO MECHANICAL ENERGY CONVERSION

Concentric introduction of the waste-gate mass flow into a flow-optimized axial diffusor

OPERATING AIRCRAFT PROPULSION SYSTEM DURING ENGINE-INOPERATIVE EVENT

Crossover cooling flow for multi-engine systems

Aircraft hybrid propulsion fan drive gear system dc motors and generators

SYSTEM AND METHOD OF OPERATING MULTI-ENGINE SYSTEM

System and method of operating multi-engine system

Method and system for governing an engine at low power

Turboshaft gas turbine engine

Turbofan with offset gas generator and auxiliary power core

Multi-engine system and power transfer between engines thereof

Gas turbine engine with low-pressure compressor bypass

Shaft-less twin rotor turbomachinery and the applications

Air system switching system to allow aero-engines to operate in standby mode

Method and system for governing an engine at low power

Turbine clutch control process

Cryogenic combined cycle power plant

Gearbox mechanically coupled fuel cell and COcombined cycle power generation

Aircraft hybrid propulsion fan drive gear system DC motors and generators

Arrangement of two turboshaft engines

Asymmetric propulsion system with heat recovery

Crossover cooling flow for multi-engine systems

Nuclear-powered turbine engine

Device for temporarily increasing turbomachine power

GAS TURBINE - ENERGY STORAGE HYBRID SYSTEM DESIGN

POWER SYSTEM FOR ROTARY WING AIRCRAFT

Method and a power plant for on-demand producing electricity from non-fossil power sources and from a renewable lignocellulosic biomass feedstock

Method for producing pure and highly concentrated carbon dioxide from a renewable lignocellulosic biomass feedstock

System and method for operating a multi-engine rotorcraft

System and method for operating a multi-engine rotorcraft for ice accretion shedding

System and method for purging a fuel manifold of a gas turbine engine using a pump

SYSTEM AND METHOD FOR OPERATING A ROTORCRAFT

System and method for operating multi-engine rotorcraft

Turbo cluster gas turbine system and activation method thereof

Air system switching system to allow aero-engines to operate in standby mode

Method and system for operating an engine in a multi-engine aircraft

MANUFACTURING METHOD

System and method for exiting an asymmetric engine operating regime

Work recovery system for a gas turbine engine utilizing an overexpanded, recuperated supercritical CO2 bottoming cycle

WORK RECOVERY SYSTEM FOR A GAS TURBINE ENGINE UTILIZING A RECUPERATED SUPERCRITICAL CO2 BOTTOMING CYCLE

Low noise gas turbine engine

AIRCRAFT ENGINE WITH HIGH PROPULSIVE AND THERMAL EFFICIENCY

Multi-engine system and method

Turboshaft gas turbine engine

Aircraft hybrid propulsion fan drive gear system DC motors and generators

Crossover cooling flow for multi-engine systems

Turbofan with bleed supercharged auxiliary engine

SYSTEMS AND METHODS FOR POWER PRODUCTION INCLUDING ION TRANSPORT COMPONENTS

Drive system for an aircraft

TURBOMACHINE TRAIN AND METHOD FOR COUPLING THE TURBOMACHINE TRAIN

Modular gas turbine system

Reverse core gear turbofan

SYSTEM AND METHOD FOR POWER PRODUCTION WITH SOLID FUEL COMBUSTION AND CARBON CAPTURE

Method for coupling two sub-shafts

AIRCRAFT PROPULSION ASSEMBLY COMPRISING A FAN CONJOINTLY DRIVEN BY TWO ENGINES

Combined two engine cycle with at least one recuperated cycle engine for rotor drive

Aircraft propulsion assembly comprising a thrust reverser

Aircraft comprising a propulsion assembly including a fan on the rear of the fuselage

System and method for dynamically controlling the operation of an aircraft

Multi-engine aircraft power plant with heat recuperation

Systems and methods for starting an engine

Systems and methods for power production including ion transport components

Controllable multi-spool gas turbine plant with independent generator speed control and hollow turbine-compressor separator

Device and method for controlling an auxiliary engine suitable for supplying thrust power to the rotor of a helicopter

Power plant management system for dual engine helicopter in single engine operation mode

Turbomachine arrangement

Mobile multi-mode power generation system with mode based adjustable drag configuration

Method for assisting a turboshaft engine in standby of a multiple-engine helicopter, and architecture of a propulsion system of a helicopter comprising at least one turboshaft engine that can be in standby

Compressor control device, compressor control system, and compressor control method

Method of regulating a three-engined power plant for a rotary wing aircraft

Multiple turboshaft engine control method and system for helicopters

Method for automatically controlling the operating speed of a helicopter turboshaft engine, corresponding control device and helicopter provided with such a device

Power generation system having compressor creating excess air flow and turbo-expander using same

Power generation system having compressor creating excess gas flow for supplemental gas turbine system

Power generation system having compressor creating excess air flow and turbo-expander to increase turbine exhaust gas mass flow

Method for operating a gas turbine arrangement

Power plant having a two-stage cooler device for cooling the admission air for a turboshaft engine

Sequential combustion with dilution gas

Combined two engine cycle with at least one recuperated cycle engine for rotor drive

Reverse core gear turbofan

Multi-stage turbocharger system

Two spool gas generator to create family of gas turbine engines

Aircraft propelled by a turbojet engine with contrarotating fans

Offset core engine architecture

External core gas turbine engine assembly

Sequential combustion with dilution gas mixer

Gas turbine engine with twin offset gas generators

Power plant including a secondary engine for compensating for losses of power from main engines in a rotary wing aircraft

Method and architecture for the optimized transfer of power between an auxiliary power motor and the main engines of a helicopter

Conjoined reverse core flow engine arrangement

Turbofan jet engine with low pressure shaft passing outside of core engine

Power generation apparatus, power generation method, decomposition-gas turbine and decomposition-gas boiler

SYSTEM AND METHOD FOR MODELING BOTTOMING CYCLE PERFORMANCE OF A COMBINED CYCLE POWER PLANT

Multi-engine power plant having an emergency fluid injection system, and an aircraft

Thrust efficient turbofan engine

Thrust efficient turbofan engine

Thrust efficient turbofan engine

Reheat burner arrangement having an increasing flow path cross-section

Damper arrangement for reducing combustion-chamber pulsation

Systems and methods for carbon dioxide capture in low emission combined turbine systems

Reverse core gear turbofan

Aerospace engine with augmenting turbojet

Single-casing steam turbine and combined cycle power plant of single-shaft type

Multiple turboshaft engine control method and system for helicopters

Gas turbine engine with auxiliary fan

Method and architecture for recombining the power of a turbomachine

Hybrid power plant

AIR COMPRESSION AND EXPANSION SYSTEM WITH SINGLE SHAFT COMPRESSOR AND TURBINE ARRANGEMENT

Method of Utilization of Gas Expansion Energy and Utilization Power Installation for Implementation of this Method

Methods for operating gas turbine engines

Turbine engine with modulated combustion and reheat chambers

Apparatus for operating gas turbine engines

Multiple turbine system with a single recuperator

Exhaust heat augmentation in a combined cycle power plant

Method of balancing the supply of bleed air from a plurality of engines

Turbofan or turbojet arrangement for vehicles, craft, aircraft and the like

Boost spool flow control and generator load matching via load compressor

System and method for automatically controlling one or multiple turbogenerators