Midshaft Rating for Turbomachine Engines

Midshaft Rating for Turbomachine Engines

TURBINE ENGINE INCLUDING TRANSFER GEARBOX AND ACCESSORY GEARBOX

FLEX COUPLER FOR HYBRID GAS TURBINE ENGINE POWERPLANT

UNIDIRECTIONAL FAN BRAKE FOR A GAS TURBINE ENGINE

Power transfer systems and methods for aircraft engines

Turbine engine including transfer gearbox and accessory gearbox

Supercharger assembly

Electrical propulsion system including a plurality of electric motors coupled to the same input shaft of a transmission system, aircraft including at least one such electrical propulsion assembly

Fan module comprising improved sealing means for a lubricant chamber

Flex coupler for hybrid gas turbine engine powerplant

TURBFAN ENGINE

Midshaft rating for turbomachine engines

Midshaft rating for turbomachine engines

Modularity of an aircraft turbomachine

Turbomachine lubrication system comprising a bypass for preferentially supplying lubricant to a low-speed reduction gear

Method of automatic load regulation, operation and protection for steam turbine and motor combined drive and power generation in converter saturated steam utilization

BLOWER SYSTEM

Midshaft rating for turbomachine engines

Midshaft rating for turbomachine engines

Assembly for aircraft turbine engine comprising an improved system for lubricating a fan drive reduction gear

Gas turbine engine

GAS TURBINES IN MECHANICAL DRIVE APPLICATIONS AND OPERATING METHODS THEREOF

Geared turbofan engine with a high ratio of thrust to turbine volume

Reverse-flow gas turbine engine

Aircraft turbomachine

Bypass turbine engine comprising at least one accessory or equipment

Accessory gearbox for a turbine engine

Electric machine within a turbine engine

Coupling guard for a rotating member

GAS TURBINE ENGINE INLET

Aircraft and direct drive engine under wing installation

Aircraft turbomachine arrangement comprising a lubrication pump driven by two oblique gears

Face seal arrangement for reduced force and pressure

ELECTRIC MACHINE, DRIVE SYSTEM, AND USE THEREOF

Fan rotor with tapered drive joint

Face seal arrangement for reduced force and pressure

TURBINE POSITIONING IN A GAS TURBINE ENGINE

Accessory gearbox for a turbine engine

Coupling and associated method of transferring torque

Turbine clutch control process

High speed rotorcraft propulsion configuration

Electric power generating apparatus for use in aircraft

Reverse-flow gas turbine engine

Geared turbofan engine with a high ratio of thrust to turbine volume

HYBRID SYNCHRONOUS CONDENSER AND POWER GENERATION UNIT

System and method for retrofitting a power generation system to incorporate clutchless synchronous condensing

ROTATIONAL SUPPORT FOR AN INTERDIGITATED ROTOR ASSEMBLY

Reverse-flow gas turbine engine

Cage for a turbomachine speed reducer with planetary gear set

Asymmetric propulsion system with heat recovery

Wind turbine drive control device, wind turbine power supply device, wind power generation device, and control method

Turbine positioning in a gas turbine engine

Blocking device of a fan

No pin compliant journal bearing shaft for one part carrier

Cage for a turbomachine speed reducer with planetary gear set

Shaft apparatus for a gas turbine engine

Gas turbine engine with scalable pumping system

SYSTEM AND METHOD FOR MANAGING POWER TO AN ENGINE CONTROLLER

Engine family platform design

Air turbine starter with decoupler

ENGINE, ROTARY DEVICE, POWER GENERATOR, POWER GENERATION SYSTEM, AND METHODS OF MAKING AND USING THE SAME

Turbomachine with fan rotor and reduction gearbox driving a low-pressure decompressor shaft

High speed rotorcraft propulsion configuration

Straightener vane and structural arm connected in a primary flow path

Failure mitigation and failure detection of intercooled cooling air systems

GAS TURBINE ENGINE SPOOL

Power source, adjusting power instructing apparatus, method, and recording medium for changing adjusting power

System for the rotational decoupling of shafts

Systems and methods of low spool power extraction

Auxiliary power unit with variable speed ratio

Method and device for connecting fan rotor to low pressure turbine rotor

MULTI-SHAFT GAS TURBINE ENGINE

Geared turbofan engine with a high ratio of thrust to turbine volume

Arm for turbomachine casing comprising a body and a removable part

Decoupler assembly for engine starter

System of variable stator vanes for a turbine engine

Spline ring for a fan drive gear flexible support

Air inlet for a gas turbine engine

Gas turbine having a high-speed low-pressure turbine and a turbine case

Method for coupling two sub-shafts

Transfer couplings

System and method for supplying lubrication fluid to at least one member of an aircraft propulsion assembly

Aircraft and direct drive engine under wing installation

Counter rotating turbine with reversing reduction gear assembly

Mechanically and electrically distributed propulsion

STUB SHAFT

GAS TURBINE ENGINE COMPRESSOR ARRANGEMENT

Multi-spool gas turbine engine

Floating vessel and method of operating a floating vessel

Twin shafts driving adjacent fans for aircraft propulsion

Gas turbine engine including a re-heat combustor and a shaft power transfer arrangement for transferring power between low and high pressure shafts

SYSTEM AND METHOD FOR DYNAMIC MECHANICAL POWER MANAGEMENT

Turbine engine having horizontally offset axes

Gas turbine engine with a geared turbofan arrangement

Control system for a cabin blower system

Reverse-flow gas turbine engine

Turbine shaft power take-off

Multi-spool gas turbine engine architecture

Multi-spool gas turbine engine architecture

ENGINE, ROTARY DEVICE, POWER GENERATOR, POWER GENERATION SYSTEM, AND METHODS OF MAKING AND USING THE SAME

Gas turbine engine shaft architecture and associated method of disassembly

Gear train architecture for a multi-spool gas turbine engine

Engine, rotary device, power generator, power generation system, and methods of making and using the same

Air turbine starter with decoupler

Turbomachine arrangement

Enhanced durability drive link for high load misalignment

Geared unison ring for variable vane actuation

35Geared unison ring for multi-stage variable vane actuation

Sliding gear actuation for variable vanes

Harmonic drive for shaft driving multiple stages of vanes via gears

Low hub-to-tip ratio fan for a turbofan gas turbine engine

DEVICE FOR ASSISTING A SOLID PROPELLANT PROPULSION SYSTEM OF A SINGLE-ENGINE HELICOPTER, SINGLE-ENGINE HELICOPTER COMPRISING SUCH A DEVICE

Turboshaft engine comprising a controlled mechanical coupling device, helicopter equipped with such a turboshaft engine, and method for optimising the zero-power super-idle speed of such a helicopter

Propulsion unit for an aircraft

Fluid turbine systems for harnessing light radiant energy, thermal energy and kinetic energy in vehicles and methods of operating thereof

Auxiliary power unit with variable speed ratio

Electric actuator for engine control

Transfer couplings

Integrated turboshaft engine

Transfer couplings

Gas turbine engine compressor arrangement

Common purpose apparatus for physical and chemical gas-solid reactions

Low hub-to-tip ratio fan for a turbofan gas turbine engine

Direct metering using a variable displacement vane pump

Split gear system for a gas turbine engine

Fuel System

Engine driven-shaft driven compressor utilizing infinitely variable transmission

GAS TURBINE

Method for coupling a steam turbine and a gas turbine at a desired differential angle

Gas turbine electrical machine arrangement

Spline ring for a fan drive gear flexible support

Turbofan engine with generator

Compressor bleed air supply for an aircraft environmental control system

Compressor of axial turbine engine with contra-rotating rotor

Damping system for a turbomachine slip ring

ACCELERATED FLUID MACHINE

Gas turbine engine system having a disengageable electric machine

Geared gas turbine engine with oil deaerator

Device for controlling a nozzle of variable cross-section of an aircraft

Gas turbine engine inlet

Low spool starter system for gas turbine engine

Stub shaft

Anti-rotational systems and methods

Geared turbofan engine with a high ratio of thrust to turbine volume

Fixed turbine engine receiver part comprising an assembly for holding ancillary systems in position inside a fixed hollow shaft

TURBINE SYSTEM WITH THREE TURBINES COUPLED TO A CENTRAL GEARBOX AND METHOD FOR OPERATING A WORK MACHINE

Low hub-to-tip ratio fan for a turbofan gas turbine engine

ACTUATOR ASSEMBLY

Adaptive fan system for a variable cycle turbofan engine

Turbine engine gearbox

Accessory gearbox device for a jet engine

Fluid Machine

TURBINE DRIVE-TRAIN APPARATUS

Method and system for controlling aircraft engine starter/generator

VARIABLE CAPACITY SUPERCHARGER FOR INTERNAL COMBUSTION ENGINE

Fluid Machine

Shrink disk connection for a wind turbine

Turbocompressor train and method for operation thereof and natural gas liquefaction plant having the turbocompressor train

System for controlling a plurality of functions of a turbojet engine

Turbine engine compressor

FUEL SUPPLY SYSTEM

Coupling assembly

Turbocharger

Tamperproof and calibration device, especially for a turbocharger with a variable nozzle device

Actuator arrangement for vectorable nozzles of gas turbine

Geared turbine machine for a machine train, machine train with and gear for geared turbine machine

Compressor variable stage remote actuation for turbine engine

Geared counter-rotating gas turbofan engine

Aircraft firewall

Variable bypass turbine fan

Gas turbine engine cold start mechanization

Attachment unit of driving shaft with tensioner nut

Narrow range variable frequency starter/generator system

Supercharger

Narrow range variable frequency starter/generator system

Power transfer systems and methods for aircraft engines

Gearbox assembly for an aircraft propulsion system

Planetary gear arrangement for carrying load and elliptical pin for supporting gear

Gas turbine engine and method of operating gas turbine engine to provide propulsion according to jet velocity ratio

Generator system