Method for joining at least two rotor elements of a turbomachine

Multi coordinate reference system for positioning bladed drum

Compression Apparatus

Compressor or Gas Extraction System

Lubrication device for a turbine engine

Outdoor fan motor driving device and air conditioner including an outdoor fan motor driving device

Gas turbine engine impact liner

Variable inlet guide vane scheduling

Tolerance resistance coverplates

GAS TURBINE ENGINE WITH AIRFOIL DAMPENING SYSTEM

Nut and rotary machine

Systems and methods for axial compressor with secondary flow

AXIAL COMPRESSOR WITH A MAGNETIC STEPPER OR SERVO MOTOR

Production methods of gas turbine

Turbomachine part with a non-axisymmetric surface

Multi-material turbine airfoil

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

Forward-swept impellers and gas turbine engines employing the same

Turbine engine with a turbo-compressor

Rotating component balance ring

Optimized circumferential groove casing treatment for axial compressors

Rotor for a thermal turbomachine

Geared Turbomachine

AXIAL COMPRESSOR CONFIGURATION

Gas turbine engine containment structures

BOAS thermal protection

Fan root endwall contouring

Gas turbine engines with internally stretched tie shafts

Fluid injector for cooling a gas turbine engine component

Gas turbine engine compressors having optimized stall enhancement feature configurations and methods for the production thereof

PRESSURE REGULATING SYSTEMS

Abradable Seal Material

Gas turbine engine with compressor disk deflectors

Reservoir egress fluid coupler

Compressor flowpath

COMPRESSOR AREA SPLITS FOR GEARED TURBOFAN

Cooling for gas turbine engine components

Integrally bladed rotor having axial arm and pocket

Encapsulated soft-lead capacitance probe for a gas turbine engine

ROTOR FOR A THERMAL TURBOMACHINE

Three spool geared turbofan with low pressure compressor drive gear system and mechanical controller

Split gear system for a gas turbine engine

Rotor for a thermal turbomachine

Non-axisymmetric fan flow path

NOZZLE FOR FOAM WASHING OF JET ENGINE

Flowpath boundary and rotor assemblies in gas turbines

Flowpath boundary and rotor assemblies in gas turbines

First stage turbine nozzle with erosion coating surface finish

Second stage turbine nozzle with erosion coating surface finish

Mixing plenum for spoked rotors

Compressing apparatus housing and compressing apparatus

Outer diffuser case for a gas turbine engine

Turbine engine assembly and method of manufacturing

Fiber reinforced spacer for a gas turbine engine

Geared turbofan engine gearbox arrangement

Bleed valve resonator drain

Three spool turbofan engine with low noise intermediate turbine rotor

Compact aero-thermo model based control system estimator starting algorithm

Angled Core Engine

Alternating Vane Asymmetry

Abradable composition and seal of an axial-flow turbomachine compressor casing

Rotor for a thermal turbomachine

Turbofan engine front section

Method for operating a turbomachine, wherein an efficiency characteristic value of a stage is determined, and turbomachine having a device for carrying out the method

Single-piece blisk for turbomachine fan comprising an upstream and/or downstream recess making its blades more flexible

Gas turbine engine and frame

Boosting system, and boosting method of gas

Sealing device

Corrected RPM calculation method for finding a corrected RPM of a compressor using a sound velocity of an inlet gas sucked into the compressor, and RPM of the compressor, and a reference state quantity

AIR INTAKE SLEEVE FOR AN AIRCRAFT TURBOPROP ENGINE

Turbofan engine front section

Aircraft engine with a compressor device

Secondary flowpath system for a gas turbine engine

Turbomachine rotors with thermal regulation

Panels of a fan of a gas turbine

Fan disk for a jet engine and jet engine

Coolant flow redirection component

Compressor rotor with anti-vortex fins

Gas turbine rotors

Fluid-cooled seal arrangement for a gas turbine engine

Gas turbine engine with axial compressor with internal cooling pathways

Gas turbine engine axial compressor rear hub

Turbofan engine bearing and gearbox arrangement

Compact aero-thermo model based engine material temperature control

Compact aero-thermo model based degraded mode control

Serrated outer surface for vortex initiation within the compressor stage of a gas turbine

Pretrenched rotor for gas turbine engine

Gas turbine blade array with reduced acoustic output

Method for assembling compressor, and bundle guide device

Compact aero-thermo model based control system

Compact aero-thermo model stabilization with compressible flow function transform

Compact aero-thermo model based tip clearance management

Compact aero-thermo model based engine power control

Wheel of a Turbine, Compressor or Pump

Compact aero-thermo model base point linear system based state estimator

Compact aero-thermo model real time linearization based state estimator

Double snapped cover plate for rotor disk

Rotor and gas turbine engine including same

Low speed fan for gas turbine engines

Gas takeoff isolation system

Guide vane ring, guide vane, inner ring and turbomachine

TURBO TYPE FLUID MACHINE

Method for inspecting a turbine engine rotor with a rotor disc cavity inspection apparatus

Geared turbofan engine gearbox arrangement

Fastening system for rotor hubs

Method for balancing and assembling a turbine rotor

Turbine or compressor stage including an interface part made of ceramic material

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

Dampers for fan spinners of aircraft engines

Gas turbine engine cooling arrangement

Turbine cap for turbo-molecular pump

Hybrid spinner support

Non-integral fan blade platform

Endwall contouring

BLEED TUBE ATTACHMENT

Endwall contouring

Vacuum pump having fastening element for securing rotor part to rotor shaft and deformed safety element projecting in axial direction for preventing relative rotation between the rotor part and rotor shaft

FAN ASSEMBLY

Fan blade platform flap seal

Inlet shroud assembly

Vacuum pump and rotor thereof

TEMPERATURE GRADIENT MANAGEMENT ARRANGEMENT FOR A TURBINE SYSTEM AND METHOD OF MANAGING A TEMPERATURE GRADIENT OF A TURBINE SYSTEM

Bladed rotor for a turbomachine

Systems and methods to control flow in a rotor wheel

Rotor balancing method

Compressor power and torque transmitting hub

Fan rotor and associated turbojet engine

Cooling device for a jet engine

Gas turbine engine compressor stator seal

Gas turbine compressor with bleed path

Thermal management system for a gas turbine engine

Apparatus and method for purging a gas turbine rotor

Variable length compressor rotor pumping vanes

Balancing of rotors

Axisymmetric part for an aviation turbine engine rotor

GAS TURBINE SYSTEM

Compressor disk bleed air scallops

Gas turbine engine with high speed low pressure turbine section and bearing support features

COMPRESSOR FLOWPATH

GAS TURBINE ENGINE WITH HIGH SPEED LOW PRESSURE TURBINE SECTION AND BEARING SUPPORT FEATURES

SYSTEM AND METHOD FOR REDUCING STRESS IN A ROTOR

High pressure compressor

Compressor having purge circuit and method of purging

Impeller

Fan rotor with cooling holes

Vortex generators for generating vortices upstream of a cascade of compressor blades

Rotor for a compressor of a gas turbine

Metallic fan blade platform

Motor with cooled rotor

Axial flow compressor

Efficient, low pressure ratio propulsor for gas turbine engines

Noise reduction in a turbomachine, and a related method thereof

Integrally bladed rotor with slotted outer rim

Vortex reducer

Gas turbine engine rotor construction

Rear hub cooling for high pressure compressor

Propeller hub having a reinforced polygonal ring and turbine engine provided with such a hub

Rotor of a turbomachine compressor, with an optimised inner end wall

Rotating component of a turbine engine

Turbine engine rotating cavity anti-vortex cascade

Fan rotor for air cycle machine

FAN ROTOR RING FOR AN AIR CYCLE MACHINE

Supersonic compressor rotor and methods for assembling same

SUPERSONIC COMPRESSOR AND METHOD OF ASSEMBLING SAME

Hub for a propeller having variable pitch blades

SYSTEM AND METHOD FOR OPERATING A COMPRESSOR

Rotor for a turbo machine

Rotor for a turbo machine

Rotor for a turbo machine

Rotor and method for manufacturing a rotor for a turbo machine

Propeller hub

Gas turbine engine with axial movable fan variable area nozzle

Inner Bleed Structure of 2-Shaft Gas Turbine and a Method to Determine the Stagger Angle of Last Stage Stator of Compressor for 2-Shaft Gas Turbine

Gas turbine engine havinga rotatable off-take passage in a compressor section

ROTOR FOR A TURBOMACHINE

Gas turbine engine and method for cooling the compressor of a gas turbine engine

Rotor assembly disk spacer for a gas turbine engine

Dual blisks in the high-pressure compressor

VORTEX REDUCING DEVICE FOR A GAS TURBINE ENGINE

Lightened axial compressor rotor

Rotor for an axial flow turbomachine

Gas turbine engine and frame

Rear hub cooling for high pressure compressor

Electromagnetic machine with a fiber rotor

Turbine rotor wheel

Reduced monobloc multistage drum of axial compressor

Turbomachine impeller

Integrally bladed rotor with slotted outer rim

Centripetal air bleed from a turbomachine compressor rotor

Turbomachine compressor rotor including centripetal air bleed means

Circulation structure for a turbo compressor

Turbomachine compressor wheel member

Anti-vortex device for a gas turbine engine compressor

Multi-stage pump rotor for a turbomolecular pump

Increased volumetric capacity of axial flow compressors used in turbomolecular vacuum pumps

Turbine engine rotating cavity anti-vortex cascade

Turbine engine rotating cavity anti-vortex cascade

PROCESS FOR PREPARING ROTORS OR STATORS OF A TURBOMOLECULAR PUMP

Split impeller configuration for synchronizing thermal response between turbine wheels

METHOD OF FABRICATING A TURBOMACHINE COMPRESSOR DRUM

Turbomachine rotor wheel having composite material blades

Compressor stator blade and compressor rotor blade

Blade assembly

Air directing assembly and method of assembling the same

Method for improving the flow conditions on the propeller or fan of an aircraft engine and accordingly designed hub cone

Fluid flow machine featuring a groove on a running gap of a blade end

SYSTEM AND METHOD FOR REDUCTION OF UNSTEADY PRESSURES IN TURBOMACHINERY

Combined vortex reducer

Propeller with Flexible Variable Blades

Fluid flow machine with blade row-internal fluid return arrangement

Casing treatment for axial compressors in a hub area

Multistage compressor for a gas turbine, comprising discharge ports and injection ports to stabilize the compressor flow

Wheel for a rotating flow machine

Turbomachinery disc

ROTORS OR STATORS OF A TURBOMOLECULAR PUMP

System and a method for assembling a rotor stack

Mounting tubes for pressurizing an internal enclosure in a turbomachine

Organic matrix composite integrally bladed rotor

Vortex spoiler for delivery of cooling airflow in a turbine engine

Turbo-molecular pump

Turbomachine fan

Balanced turbine rotor fan blade for a tip turbine engine

Anti-stall casing treatment for turbo compressors

Compressor with centripetal air takeoff

Method for machining an integrally bladed rotor

Part span shrouded fan blisk

Turbomachine with reduced leakage penalties in pressure change and efficiency

Method for the repair of a compressor rotor designed in blisk technology

Intake cone in a fiber compound material for a gas turbine engine and method for its manufacture

Woven turbomachine impeller

Rotor for an engine

Axial-flow compressor for a gas turbine engine

Flow structure for a turbocompressor

Methods and systems for turbine rotor balancing

Method of modifying a turbocompressor

Turbomachine rotor including at least one disk reinforced by a composite ring

Axial compressor blading

Methods and apparatus for operating gas turbine engines

Cylindrical rotor with internal blades

Gas turbine engine and a rotor for a gas turbine engine

Fluid Flow Chambers and Bridges in Bladeless Compressors, Turbines and Pumps

Apparatus and method for optimizing vibration of a gas turbine

Rotor with core surrounded by shielding rings

Gas turbine engine

Axial flow supercharger and fluid compression machine

Composite integrally bladed rotor

Turbojet architecture with two fans at the front

Rotor with core surrounded by shielding rings

Tube-type vortex reducer

Cantilevered stator stage

Method for repairing gas turbine compressor rotor blades

Method of manufacturing an article by diffusion bonding and superplastic forming

Connection between bladed discs on the rotor line of a compressor

Screw and nut fastening device

Recirculation structure for a turbocompressor

Power transmission system for turbine or compressor having counter-rotating blades