HIGH TEMPERATURE ANTI-ICE SYSTEMS FOR AIRCRAFT ENGINES

OPEN ROTOR WITH AERODYNAMICALLY ISOLATABLE FREE TURBINE

Combustion System with Pollution Abatement by Catalysts and Non-Thermal Plasma for Aircraft and Industrial Gas Turbines

AIR RECUPERATED ENGINE WITH AIR REINJECTION

TURBINE OVERSPEED PROTECTION

Aircraft engine having two radially offset turbines

Air recuperated engine with air reinjection

Compressor bypass bleed system for a ducted fan engine

Compressed N2 for energy storage

Crossover cooling flow for multi-engine systems

System and method for reconfiguring a bleed system

Multi-mode engine system with gas turbine engine and turbo-compressor

Turbomachine with device for cooling and pressurising a turbine

Aircraft and direct drive engine under wing installation

Secondary fuel flow demand fuel pumping system

Gas turbine engine having a turbomachine and an electric motor coupled to a propeller

TWO-SHAFT GAS TURBINE

Crossover cooling flow for multi-engine systems

GAS TURBINE ENGINE

Rotor including replaceable self-locking sealing assembly, turbine, and gas turbine including the same

SECONDARY FUEL FLOW DEMAND FUEL PUMPING SYSTEM

Compressed N2 for energy storage

Gas turbine engine with low pressure compressor stages

Auxiliary device for three air flow path gas turbine engine

Ducted gas turbine engine stability bleed valve with passive and active shutoff

Signal processing for variable geometry mechanism control

DUCT AND A GAS TURBINE ENGINE COMPRISING A DUCT

Adaptive engine with boost spool

Turbomachinery transition duct for wide bypass ratio ranges

Diversion of fan air to provide cooling air for gas turbine engine

Crossover cooling flow for multi-engine systems

Bleed air systems for use with aircraft and related methods

GAS TURBINE ENGINE AND TURBINE ARRANGEMENT

Process for retrofitting an industrial gas turbine engine for increased power and efficiency

Thermal gradient attenuation structure to mitigate rotor bow in turbine engine

Intercooled cooling air tapped from plural locations

Compressor stage EGR injection

MOBILE POWER GENERATION SYSTEM INCLUDING OPTICAL ALIGNMENT

Inlet guide vane assembly

Geared turbofan engine with high compressor exit temperature

Reverse core gear turbofan

Integrated fuel nozzle connection

INTER-TURBINE DUCTS WITH MULTIPLE SPLITTER BLADES

Aircraft and direct drive engine under wing installation

Systems and methods for controlling overboard bleed heat of a turbine inlet filter

Intercooled cooling air with dual pass heat exchanger

Engine driven by Sc0cycle with independent shafts for combustion cycle elements and propulsion elements

Turbine engine exhaust casing with improved lifetime

Systems and methods for reducing airflow imbalances in turbines

Intercooled cooling air with dual pass heat exchanger

Apparatus and process of retrofitting a combined cycle power plant

Engine bleed air with compressor surge management

Cooling air architecture for compact size and performance improvement

Aircraft turbine engine comprising a discharge device

Valved airflow passage assembly for adjusting airflow distortion in gas turbine engine

Process for retrofitting an industrial gas turbine engine for increased power and efficiency

Method and apparatus for optimizing the operation of a turbine system under flexible loads

System for generating steam and for providing cooled combustion gas to a secondary gas turbine combustor

Cyclonic separator for a turbine engine

Aircraft pneumatic system

Gas turbine engine with stream diverter

SYSTEM AND METHOD FOR DECOUPLING STEAM PRODUCTION DEPENDENCY FROM GAS TURBINE LOAD LEVEL

Compressor bleed auxiliary turbine

Engine driven by SC0cycle with independent shafts for combustion cycle elements and propulsion elements

Integrated turboshaft engine

Intercooled cooling air tapped from plural locations

Intercooled cooling air with plural heat exchangers

Intercooled cooling air with dual pass heat exchanger

Engine bypass valve

Self-contained power unit for implementing a method for optimizing the operability of an aircraft propulsive unit

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

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

Power generation system having compressor creating excess air flow and turbo-expander for cooling inlet air

Diversion of fan air to provide cooling air for gas turbine engine

Gas turbine, gas-turbine control device, and gas turbine operation method

Engine system with intake bypass device

Method to operate a combustor of a gas turbine

Ducted cowl support for a gas turbine engine

Inner diffuser case cone and skirt

Method of Operation of a Gas Turbine Engine

Bleed valve resonance augmentations

Gas turbine engine and method of assembling the same

Geared turbofan engine with high compressor exit temperature

Gas turbine engine having an annular core bleed

Gas turbine engine with distributed fans and bypass air mixer

Gas turbine engine driven by supercritical power generation system

Geared turbofan engine with high compressor exit temperature

Reverse core gear turbofan

Two spool gas generator with improved air porting

Gas turbine engine with variable speed turbines

Turbine cooling system using an enhanced compressor air flow

Aircraft gas turbine having a core engine casing with cooling-air tubes

Auxiliary device for three air flow path gas turbine engine

System and method for generating electric energy

Inner diffuser case struts for a combustor of a gas turbine engine

Method of operating a gas turbine assembly and the gas turbine assembly

ULTRA HIGH OVERALL PESSURE RATIO GAS TURBINE ENGINE

Bleed air systems for use with aircrafts and related methods

Passive cooling system for control valve actuators within a negative pressure turbine enclosure using ambient cooling air

Compressed-air energy-storage system

Gas turbine power plant with non-homogeneous input gas

GEARED TURBOFAN ENGINE WITH HIGH COMPRESSOR EXIT TEMPERATURE

Gas turbine engine with stream diverter

Bleed air systems for use with aircrafts and related methods

Axial-flow turbine and power plant including the same

LPC flowpath shape with gas turbine engine shaft bearing configuration

Aircraft power system

Gas turbine engine with compressor inlet guide vane positioned for starting

System and method for expanding a compressor bleed flow

System and method for a multi-wall turbine combustor

System and method for recirculating and recovering energy from compressor discharge bleed air

Modular louver system

Reverse core gear turbofan

Aerospace engine with augmenting turbojet

GAS TURBINE ENGINE WITH COMPRESSOR INLET GUIDE VANE POSITIONED FOR STARTING

Bleed air systems for use with aircrafts and related methods

Flushing the exhaust gas recirculation lines of a gas turbine

Turbine component cooling with closed looped control of coolant flow

Gas turbine engine having a multi-variable closed loop controller for regulating tip clearance

Method for optimizing the operability of an aircraft propulsive unit, and self-contained power unit for implementing same

Method and apparatus for optimizing the operation of a turbine system under flexible loads

Apparatus for aircraft with high peak power equipment

Power plant including an exhaust gas recirculation system for injecting recirculated exhaust gases in the fuel and compressed air of a gas turbine engine

Gas turbine engine with aft core driven fan section

Method for operating a gas turbine power plant with exhaust gas recirculation

Variable cycle gas turbine engine

Self-actuating bleed valve for a gas turbine engine

Integrated variable geometry flow restrictor and heat exchanger

Gas turbine engine with turbine cooling arrangement

Combustion turbine cooling media supply method

Blocked nozzle detection and remedial method and system

Combustion turbine cooling media supply method

Gas turbine engine

LIGHTWEIGHT START SYSTEM FOR A GAS TURBINE ENGINE

Bleed structure for a bleed passage in a gas turbine engine

Cooling of turbine components using combustor shell air

Turbine engine having two off-axis spools with valving-enabled modulation between high and low power modes

PARALLEL TURBINE ARRANGEMENT AND METHOD

Rear propulsor for a variable cycle gas turbine engine

Auxiliary propulsor for a variable cycle gas turbine engine

Aircraft combination engines exhaust thrust recovery

Nozzle with yaw vectoring vane

Dual volute turbocharger

Combustion turbine cooling media supply method

Bleed structure for a bleed passage in a gas turbine engine

High performance method for throttling of closed gas turbine cycles

Gas turbine engine

Method and apparatus for enabling engine turn down

Compressor having integral EGR valve and mixer

Gas turbine engine and method of operating same

BLEED STRUCTURE FOR A BLEED PASSAGE IN A GAS TURBINE ENGINE

Method and system for balancing bleed flows from gas turbine engines

Thrust vectoring aft FLADE engine

Multi-stage turbocharging system with efficient bypass

Gas turbine engine bleed air power assist system and method

Methods and apparatus for assembling gas turbine engines

Gas-turbine installation

Production process of gas turbine

Pre-heating aircraft engine in standby mode