Turbofan with offset gas generator and auxiliary power core

Method for coupling a hydroelectric power plant to the grid comprising at least two hydroelectric units

Gas turbine engine transfer efficiency

Architecture for a propulsion system of a helicopter including a hybrid turboshaft engine and a system for reactivating said hybrid turboshaft engine

MECHANICALLY DRIVEN AIR VEHICLE THERMAL MANAGEMENT DEVICE

Motoring synchronization for multiple engines

Multi-spool geared turbofan arrangement with integrated starter/generator

Splitter and guide vane arrangement for gas turbine engines

Low cost rocket

Toroidal lift force engine

Energy storage system and system enabling stable utilization of variable electric power

Gas turbine engine transfer efficiency

Turbo cluster gas turbine system and activation method thereof

Gas turbine engine with a double wall core casing

Air cycle machine connected to engine gearbox

Pre-start motoring synchronization for multiple engines

HIGH SPEED PROPULSION SYSTEM WITH INLET COOLING

Power system with a coordinated power draw

COMPRESSED GAS AND RECYCLED LIQUID TURBINE POWER SYSTEM

Gas turbine engine heaters

Multi-stage radial turboexpander

TURBOMACHINE TRAIN AND METHOD FOR COUPLING THE TURBOMACHINE TRAIN

Method for coupling two sub-shafts

Distributed fan lubrication system

Engine assembly with a dedicated voltage bus

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

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

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

Mechanically driven air vehicle thermal management device

Compound engine assembly with common inlet

Pre-start motoring synchronization for multiple engines

Gas turbine engine with distributed fans

Architecture for a propulsion system of a helicopter including a hybrid turboshaft engine and a system for reactivating said hybrid turboshaft engine

Aircraft with a propulsion unit comprising a fan at the rear of the fuselage

DRIVE CHAIN FOR A HELICOPTER INCORPORATING A PYROTECHNIC ASSISTANCE DRIVE MODULE AND HELICOPTER COMPRISING THE SAME

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

Compound engine assembly with common inlet

Rotary system

Reverse flow single spool core gas turbine engine

Decoupled gas turbine engine

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

MULTI-STAGE VOLUMETRIC FLUID EXPANSION DEVICE

High speed propulsion system with inlet cooling

Angled reverse core gas turbine engine with widened nozzle

Gas turbine engine with distributed fans

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

Rotary wing aircraft having two main engines together with a less powerful secondary engine, and a corresponding method

Conjoined reverse core flow engine arrangement

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

Two-shaft gas turbine

Variable cycle turbine engine

STEAM TURBINE FACILITY

Method and system for providing cooling and power

High-Pressure Fluid Compression System Utilizing Cascading Effluent Energy Recovery

Gas turbine engine with dual fans driven about a central core axis

High-pressure fluid compression system utilizing cascading effluent energy recovery

Method and system for operative reconversion of pairs of pre-existing steam turbo-units

Methods and apparatus for operating gas turbine engines

Gas-turbine installation

Re-circulating heat pump turbine