Blading

Apparatus to apply a variable surface texture on an airfoil

Cross flow fan and air conditioner

Turbine bucket angel wing features for forward cavity flow control and related method

Turbine bucket platform leading edge scalloping for performance and secondary flow and related method

Turbine of a turbomachine

Turbine component including airfoil with contour

Transition nozzle

NON-UNIFORM VARIABLE VANES

TURBOMACHINE COMPONENT HAVING A FLOW CONTOUR FEATURE

HYDROFOIL WITH FEATURES TO GENERATE CAVITATION

Airfoil including trench with contoured surface

Centrifugal compressor with fluid injector diffuser

Inter-turbine ducts with guide vanes

Flow directing member for gas turbine engine

Turbine blade or vane with separate endwall

Supersonic turbine moving blade and axial-flow turbine

Blade of a turbomachine

INNER PERIPHERAL SURFACE SHAPE OF CASING OF AXIAL-FLOW COMPRESSOR

Airflow control device and airflow control method

Method of reducing asymmetric fluid flow effects in a passage

Turbomachine with axial compression or expansion

Oscillatory vorticity generator and applications thereof

Blade channel having an end wall contour and a turbomachine

Fluid-flow machine—blade with hybrid profile configuration

Blade

Ring diffuser for an axial turbomachine

METHOD OF REDUCING THE OBJECT-TRAVELING RESISTANCE

Strut and a gas turbine structure comprising the strut

Turbine bucket shroud tail

AFT LOADED AIRFOIL

SHROUDED TURBINE BLADE WITH CONTOURED PLATFORM AND AXIAL DOVETAIL

Rotor blade

System and method for enhanced turbine wake mixing via fluidic-generated vortices

Rotor blade having passive bleed path

BLADE EXCITATION REDUCTION METHOD AND ARRANGEMENT

Fluid flow control device for an aerofoil

Bypass duct of a turbofan engine

Ring diffuser for an axial turbomachine

Airfoil having built-up surface with embedded cooling passage

Arrangement for controlling fluid jets injected into a fluid stream of a bleed air discharge nozzle

Turbine blade with improved aerodynamic performance

Blade with non-axisymmetric platform: recess and boss on the extrados

Axial turbo engine with low gap losses

Blade for a turbo device with a vortex-generator

Exhaust Gas Diffuser Wall Contouring

Systems and apparatus relating to compressor stator blades and diffusers in turbine engines

Plasma induced flow control of boundary layer at airfoil endwall

Flow passage for gas turbine engine

BLADE WITH 3D PLATFORM COMPRISING AN INTER-BLADE BULB

Boundary layer energiser

Steampath flow separation reduction system

Turbo machine efficiency equalizer system

Turbines and turbine blade winglets

High temperature radially fed axial steam turbine

Turbofan flow path trenches

Arrangement for controlling fluid jets injected into a fluid stream

HIGH-TURNING DIFFUSER STRUT WITH FLOW CROSS-OVER SLOTS

Biformal platform turbine blade

AIRFOIL WITH FLOW DEFLECTOR

Blade with non-axisymmetric platform

Fluid flow machine with blade row group

Shroudless blade

Aerodynamic performance enhancements using discharge plasma actuators

Compressor blade

TURBINE STAGE

TURBINE BLADE CASCADE ENDWALL

Instability mitigation system using rotor plasma actuators

Separation resistant aerodynamic article

Rotor arrangement

Plasma enhanced rapidly expanded gas turbine engine transition duct

Axial-flow turbine with flow extraction means

REDUCED DRAG SYSTEM FOR WINDMILLS, FANS, PROPELLERS, AIRFOILS, AND HYDROFOILS

Wind turbine blade with submerged boundary layer control means

Impulse turbine for use in bi-directional flows

PLASMA ENHANCED COMPRESSOR DUCT

PLASMA ENHANCED BOOSTER AND METHOD OF OPERATION

Methods and apparatus relating to improved turbine blade platform contours

Curved platform turbine blade

Monomolecular carbon-based film for forming lubricious surface on aircraft parts

Fluid flow machine with sidewall boundary layer barrier

Banked platform turbine blade

Air induction control

VANE STRUCTURE FOR VERTICAL AXIS WIND POWER GENERATOR

Aspirated impeller

Laminar flow rotor and related methods and systems

Blade structure of gas turbine

Separation-resistant inlet duct for mid-turbine frames

Diffuser apparatus in a turbomachine

Turbine blade

Gas turbine engine assemblies with recirculated hot gas ingestion

Combined acoustic absorber and heat exchanging outlet guide vanes

Annular flow duct for a turbomachine through which a main flow can flow in the axial direction

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

FIXING METHOD FOR A TIP WINGLET AND REDUCED TIP LEAKAGE BLADE

Blade with a cooling groove for a bladed wheel of a turbomachine

Turbine blade

Gas turbine engine with valve for establishing communication between two enclosures

Systems and methods involving variable throat area vanes

Gas turbine engine systems involving mechanically alterable vane throat areas

Blade

INLET FILM COOLING OF TURBINE END WALL OF A GAS TURBINE ENGINE

Axial flow turbine and stage structure thereof

Component to be arranged in the flow channel of a turbomachine and spraying method for producing the coating

Shape of gas passage in axial-flow gas turbine engine

Arrangement for controlling fluid jets injected into a fluid stream

Systems and methods involving aerodynamic struts

Steam turbine rotating blade

Steam turbine rotating blade

Systems and Methods Involving Variable Vanes

Blade with tangential jet generation on the profile

Nacelle compartment plenum for bleed air flow delivery system

Aerofoil members for a turbomachine

Arrangement for controlling fluid jets injected into a fluid stream

Non-axisymmetric end wall contouring for a turbomachine blade row

Fluid-flow machine and rotor blade thereof

Anti-stall casing treatment for turbo compressors

Axial flow turbine

Air intake circuit arrangement for high pressure compressor of a turbine engine

Gas turbine engines including multi-curve stator vanes and methods of assembling the same

Gas turbine engines including lean stator vanes and methods of assembling the same

SYSTEM AND METHOD FOR REDUCING WAKE

Turbine assembly for a gas turbine engine and method of manufacturing the same

Plasma induced virtual turbine airfoil trailing edge extension

Airfoil leading edge end wall vortex reducing plasma

Bullnose seal turbine stage

Transition duct for a gas turbine engine

Method of modifying the end wall contour in a turbine using laser consolidation and the turbines derived therefrom

Turbine blade for a gas turbine

Blades

Plasma lifted boundary layer gas turbine engine vane

Fan platform fin

Turbine airfoil with submerged endwall cooling channel

Transition channel between two turbine stages

AXIAL TURBINE

Turbine airfoil with endwall horseshoe cooling slot

Counter tip baffle airfoil

Airfoil and method for moisture removal and steam injection

Boundary layer suction arrangement

Airfoil array with an endwall protrusion and components of the array

Airfoil array with an endwall depression and components of the array

Blade or vane with a laterally enlarged base

Inlet distortion and recovery control system

Offset blade tip chord sealing system and method for rotary machines

Blade row for a rotary machine and method of fabricating same

Gas turbine vane

Vane comprising a transition zone

Cooled turbine blade

Method for the production of secondary fluid ducts

Methods and apparatus for assembling turbine engines

Turbine nozzle with purge cavity blend

Active multistable twisting device

Multi-slot inter-turbine duct assembly for use in a turbine engine

Axial flow turbine

Turbine cascade structure

Blade of a turbomachine with block-wise defined profile skeleton line

Noise reduction of aircraft flap

Arrangement for controlling fluid jets injected into a fluid stream

Turbine blade

Method for air circulation in a turbomachine compressor, compressor arrangement using this method, compression stage and compressor incorporating such a arrangement, and aircraft engine equipped with such a compressor

Turbine blade

Linear propulsor with radial motion

Funnel fillet turbine stage

Turbomachine exerting dynamic influence on the flow

Scalloped surface turbine stage

Turbine engine guide vane and arrays thereof

Bullnose step turbine nozzle

Method and apparatus for modulating flow separation

Impingement cooling of large fillet of an airfoil

Coupled parametric design of flow control and duct shape

Methods and apparatus for aerodynamically self-enhancing rotor blades

Flow structure for a gas turbine

Turbine

Boundary layer control arrangement

Inlet film cooling of turbine end wall of a gas turbine engine

High area-ratio inter-turbine duct with inlet blowing

Compressor blade with reduced aerodynamic blade excitation

Shockwave-induced boundary layer bleed

Turbomachine with fluid removal

Compressor for an aircraft engine

Cooling system for an airfoil vane

Mitigation of unsteady peak fan blade and disc stresses in turbofan engines through the use of flow control devices to stabilize boundary layer characteristics

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

Turbomachine with fluid supply

Vorticity control in a gas turbine engine

Blade structure in a gas turbine

Arrangement for bleeding the boundary layer from an aircraft engine

Turbine blades

Casing, a compressor, a turbine, and a combustion turbine engine including such a casing

Method and device for altering the separation characteristics of air-flow over an aerodynamic surface via intermittent suction

Axial flow turbine

Recirculation structure for a turbocompressor

Blade structure in a gas turbine

Suction side micro-riblet patches for a turbine airfoil

Blade having a rib for an engine and method of directing ingestion material using the same

Offtake scoops for bleed pressure recovery in gas turbine engines

Internal core profile for a turbine nozzle airfoil

Efficient gas turbine engine installation and operation

Method to control flow separation over an airfoil