AIR MOVING DEVICE WITH BYPASS INTAKE

CENTRIFUGAL COMPRESSOR WITH LIQUID INJECTION

WATER ACTUATED TIP CLEARANCE CONTROL SYSTEM FOR TURBINE ENGINE

SHORT IMPELLER FOR A TURBOMACHINE

Engine strut flow control

Radial compressor with leading edge air injection

Air moving device with bypass intake

Air moving device with bypass intake

Blower system

Interstage capacity control valve with side stream flow distribution and flow regulation for multi-stage centrifugal compressors

Centrifugal compressor with liquid injection

Vacuum pump

Interstage capacity control valve with side stream flow distribution and flow regulation for multi-stage centrifugal compressors

Apparatus and method for diagnosing and controlling aerodynamic stability of compressor

Air moving device with bypass intake

Diffuser for a radial compressor

Reflux device blade compressor

Integrated structure of refluxer and pressure diffuser, and centrifugal compressor

Diaphragm for a centrifugal compressor

Passageway between a shroud and a rotor platform in a turbine engine

Technique for controlling rotating stall in compressor for a gas turbine engine

Active surge control in centrifugal compressors using microjet injection

Inlet pre-swirl gas turbine engine

Inlet pre-swirl gas turbine engine

Exhaust diffuser having ejection hole and suction hole, and gas turbine having the same

Aircraft comprising a rear fairing propulsion system with inlet stator comprising a blowing function

Short impeller for a turbomachine

Aircraft including a ducted rear thruster with an input stator having movable flaps

Vane diffuser and method for controlling a compressor having same

Casing with suction arm for axial turbine engine

Compressor of a turbocharger having an air recirculation valve and turbocharger and motor vehicle having such a compressor

Assembly and method for influencing flow through a fan of a gas turbine engine

Turbofan engine and method of reducing air flow separation therein

Axial flow compressor, gas turbine including the same, and stator blade of axial flow compressor

Compressor tip injector

Systems and methods for axial compressor with secondary flow

Gas turbine engine airfoil with auxiliary flow channel

Method for manufacturing a propeller blade

Guide vane

Internal combustion engine with exhaust-gas turbocharging and exhaust-gas recirculation

Centrifugal compressor diffuser and method for controlling same

Synthetic jets in compressors

Removal of liquid from airfoil of equipment having gas-liquid flows

Turbomachine, circulation structure and method

METHOD AND DEVICE FOR STABILIZING A COMPRESSOR CURRENT

Gas turbine engines having plasma flow-controlled intake systems

Gas turbine diffuser blowing method and corresponding diffuser

Axial compressor and control method thereof to stabilize fluid

Duct having flow conducting surfaces

System for injecting a fluid, compressor and turbomachine

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

Centrifugal compressor with fluid injector diffuser

Blade of a turbomachine

Turbine engine compressor having air injections

Compressor of exhaust gas turbocharger

Rotor blade

Reversible system for injecting and extracting gas for fluid rotary machines

Compressor

FAN ASSEMBLY

Gas turbine compressor

Housing for a compressor of a gas turbine, compressor, and method for producing a housing segment of a compressor housing

Turbomachine compressor with an air injection system

Gas turbine engine system providing simulated boundary layer thickness increase

Injecting air into the flow path of a turbomachine compressor

FLUIDFOIL TIP VORTEX DISRUPTION

Axial-flow compressor, more particularly one for an aircraft gas-turbine engine

Axial compressor vane

Shroudless blade

Separation resistant aerodynamic article

GAS TURBINE ENGINE WITH EJECTOR

FAN BLADES

Fluid flow machine with sidewall boundary layer barrier

Fluid flow machine with peripheral energization near the suction side

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

Gas turbine having a peripheral ring segment including a recirculation channel

Blade shroud with aperture

Fluid flow machine with blade row-internal fluid return arrangement

Fluid flow machine with fluid injector assembly

Fluid injector nozzle for a main flow path of a fluid flow machine

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

Axial flow fluid apparatus and blade

Flow control arrangement

Blade with tangential jet generation on the profile

Air reinjection compressor

Gas turbine engine providing simulated boundary layer thickness increase

Spiral air induction

Gas turbine engine fan assembly and method for assembling to same

Method for reducing the noise of turbo engines

Self-aspirated flow control system for centrifugal compressors

Flow passage structure for refrigerant compressor

Ported shroud with filtered external ventilation

METHOD AND APPARATUS FOR REDUCING AXIAL COMPRESSOR BLADE TIP FLOW

Turbomachine exerting dynamic influence on the flow

Centrifugal compressor

Turbomachine with means for the creation of a peripheral jet on the stator

Methods and apparatus for aerodynamically self-enhancing rotor blades

Centrifugal blower having auxiliary radial inlet

Flow control arrangement

Method of improving the flow conditions in an axial-flow compressor, and axial-flow compressor for carrying out the method

Turbomachine with fluid supply

Flow separation control device for an airfoil

Method to control flow separation over an airfoil

System to control flow separation over an airfoil