AXIAL FAN

AXIAL TURBOMACHINE COMPRESSOR WITH CONTROLLED RECIRCULATION BETWEEN THE INNER SHROUD AND THE ROTOR

Control of leakage for gas turbine engine compressor blades

COOLING FAN AND COOLING FAN MODULE

Method for configuring a leading edge of a compressor stator platform and the corresponding stator platform

Fan

Housing for a ventilator and ventilator with a corresponding housing

Cooling fan and cooling fan module

Counter-Rotating Fan Assembly

Seal assembly

Cooling fan module

AXIAL FAN HOUSING CONFIGURED TO REDIRECT THE RECIRCULATING FLOW OF LEAK AIR IN THE MAIN FLOW DIRECTION

Free-tipped axial fan assembly

Abradable Material

Grooved shroud casing treatment for high pressure compressor in a turbine engine

Retention clip for a blade outer air seal

Fan and refrigeration apparatus including fan

Cover for airfoil assembly for a gas turbine engine

Floating, non-contact seal and dimensions thereof

SHROUDED BLADE ASSEMBLIES

GAS TURBINE ENGINE AIRFOIL

Gas turbine engine vane end devices

De-icing shroud for a compressor of turbomachine

Keystoned blade track

Composite fan blades with integral attachment mechanism

Labyrinth seal for fan assembly

Fan assembly and refrigerator including a fan assembly

Rotatable component for turbomachines, including a non-axisymmetric overhanging portion

Rotor hub seal

Fan shroud

Fan module

Fan system with integrated fan-shroud channel for reduced recirculation flow

Sealing system for turbomachine compressor

Blower and air conditioning apparatus having the same

Galvanic corrosion resistant coating composition and methods for forming the same

GAS TURBINE ENGINE COMPONENT HAVING TIP VORTEX CREATION FEATURE

FAN SHROUD AND/OR FAN BLADE ASSEMBLY

FAN SHROUD AND/OR FAN BLADE ASSEMBLY

TURBOMACHINE WITH AN ADAPTIVE SEALING APPLIANCE

Aspirating face seal with non-coiled retraction springs

Engine cooling fan casing shroud with unobstructed outlet

Grooved shroud casing treatment for high pressure compressor in a turbine engine

Multilayer abradable coating

Turbomachine housing element

Gas turbine seal

Fan impeller and radiator fan module

Serial axial flow fan

Cooling system and an axial fan for a cooling system

Gas turbine engine vane end devices

Brush seal assembly and method

Coated turbomachinery component

Blade tip clearance control for an axial compressor with radially outer annulus

Multi-ply seal

Free-tipped axial fan assembly

Blower and refrigerator having the same

Gas turbine engine airfoil

METHOD FOR DESIGNING A FLUID FLOW ENGINE AND FLUID FLOW ENGINE

Rotary machine

Rotary machine

Fan containment case for a gas turbine engine

Fire containment coating system for titanium

Abradable material

Method and apparatus for active clearance control on gas turbine engines

THICKENED RADIALLY OUTER ANNULAR PORTION OF A SEALING FIN

Air injection for an axial compressor with radially outer annulus

Blowing device

Enhanced Blade Tipping For Improved Abradability

Mechanism and method for rapid response clearance control

Abrasive blade tips with additive resistant to clogging by organic matrix abradable

Abrasive blade tips with additive layer resistant to clogging

Abrasive blade tips with additive resistant to clogging by organic matrix abradable

Organic matrix abradable coating resistant to clogging of abrasive blade tips

Contra-flow strips, contra-flow seal segments, and methods for inhibiting leakage

Outer airseal insulated rub strip

Airfoil tip geometry to reduce blade wear in gas turbine engines

Method for clearance control in a gas turbine engine

Floating, non-contact seal and dimensions thereof

Compressor aerofoil

Gas turbine engine blade casing

Rotor hub seal

Propeller fan and blower unit

Method and apparatus for active clearance control for high pressure compressors using fan/booster exhaust air

Guide vane for a turbomachine, guide vane cascade, and method for manufacturing a guide vane or a guide vane cascade

STATOR VANE SUPPORT SYSTEM WITHIN A GAS TURBINE ENGINE

Outer airseal for gas turbine engine

Method for creating and repairing a turbomachine component and associated turbomachine component

Rotor tip clearance

Cooling hole patterned surfaces

Adaptive blade tip seal assembly

Gas turbine compressor with adaptive blade tip seal assembly

Compressor variable vane assembly

Sealing element for a turbo-machine, turbo-machine comprising a sealing element and method for manufacturing a sealing element

Perforated drum of a compressor of an axial turbine engine

Gas turbine rapid response clearance control system with annular piston

Fan blade tip as a cutting tool

Fire containment coating system for titanium

Gas turbine engine rapid response clearance control system

Blower

Blade and shroud with socket for a compressor of an axial turbomachine

Rotary blade manufacturing method

Blower

Composite keystoned blade track

Blade outer air seal mount

Retention clip for a blade outer air seal

Max phase reinforced polymer matrix composite abradables with enhanced thermal conductivity

Meter plate for blade outer air seal

Keystoned blade track

ENGINE FAN

Blade outer air seal with secondary air sealing

Cooling fan module and system

Active clearance control for axial rotor systems

Fan comprising an impeller with blades

Optimized circumferential groove casing treatment for axial compressors

Stator vane with platform having sloped face

Rotor with axial arm having protruding ramp

Gas turbine engine component providing prioritized cooling

BOAS with radial load feature

Flowpath boundary and rotor assemblies in gas turbines

Gas turbine engine with rotor blade tip clearance flow control

Blade of a ventilator wheel, ventilator wheel and axial ventilator

Tuned rotor disk

Fan shroud assembly

Sealing device

Turbine bearing and seal assembly for a turbocharger

Turbomachine blade tip shroud

Shroud wear ring for a work vehicle

Rotors with stall margin and efficiency optimization and methods for improving gas turbine engine performance therewith

Gas turbine rotors

Ring seal for blade outer air seal gas turbine engine rapid response clearance control system

Gas turbine engine rapid response clearance control system with air seal segment interface

Compressor case snap assembly

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

Pretrenched rotor for gas turbine engine

Gas turbine engine component having tip vortex creation feature

Fan coil unit with shrouded fan

Shrouded axial fan with casing treatment

Mould for an abradable track beneath the inner shroud of an axial-flow turbomachine compressor

Blade retaining ring for an internal shroud of an axial-flow turbomachine compressor

Filament-Wound Tip-Shrouded Axial Compressor or Fan Rotor System

Compressor variable vane assembly

Ventilation device and vehicle with a ventilation device

Rotor tip clearance

Sealing arrangement for fuel cell compressor

Turbine engine casing and rotor wheel

Low profile fan platform attachment

Tip treatment bars in a gas turbine engine

Double bell mouth shroud

Compressor casing comprising cavities with optimised setting

Compressor casing comprising cavities having an optimised upstream shape

Motor vehicle fan of reduced axial size

Angular stator sector for a turbomachine compressor comprising a brush seal

Fan and impeller thereof

Gas turbine engine vane end devices

Blower device

Duct blocker seal assembly for a gas turbine engine

LIGHTWEIGHT SHROUDED FAN

Cooling fan module

Segmented composite inner ferrule and segment of diffuser of axial compressor

FAN BLADE BRUSH TIP

Blade for a continuous-flow machine and a continuous-flow machine

Aerodynamic seals for rotary machine

Blade outer air seal for a gas turbine engine

Segmented seal with ship lap ends

Compressor tip clearance management for a gas turbine engine

Stall margin enhancement of axial fan with rotating shroud

Ring-type fan and impeller structure thereof

Gas turbine engine compressor stator seal

Cooling fan

Airfoils including tip profile for noise reduction and method for fabricating same

Compressor airfoil tip clearance optimization system

Honeycomb seal and method

Method for Reducing Stress on Blade Tips

Axial turbomachine compressor outer casing

Frame assembly of ring-type fan with pressure-releasing function

Anti-relief fan frame body structure

Rotating vane seal with cooling air passages

Turbomachine rotor having patterned coating

ABRADABLE PANEL AND METHOD OF FORMING THE SAME

Turbo-Machinery With Flow Deflector System

Mixed-flow ducted fan

Fan assembly for vehicles

Guide vane with a winglet for an energy converting machine and machine for converting energy comprising the guide vane

Fluid-flow machine

Abradable liner

Impeller wheel for a ventilator

Turbomachine comprising an annular casing and a bladed rotor

Fan and impeller thereof

Compressor tip clearance control and gas turbine engine

Compressor blade with flexible tip elements and process therefor

Shroud leakage cover

Air conditioner with outdoor unit

Ventilator

Rotor blade

Compressor rectifier architecture

AXIAL TURBO COMPRESSOR FOR A GAS TURBINE HAVING LOW RADIAL GAP LOSSES AND DIFFUSER LOSSES

Compressors with casing treatments in gas turbine engines

AXIAL FAN APPARATUS, HOUSING, AND ELECTRONIC APPARATUS

Fan and shroud assembly

Skewed axial fan assembly

Free-tipped axial fan assembly

PANELLED ASSEMBLY

Method and system for a leakage controlled fan housing

Blower and heat pump apparatus using the same

Heat dissipation fan and rotor thereof

Two-Part Shroud or Shroud Section for a Stator Stage with Vanes of an Axial Compressor

Axial-centrifugal compressor having system for controlling play

Partial ring cooling fan

Casing for a moving-blade wheel of turbomachine

COOLING FAN WITH INTERNALLY TAPERED HOUSING

Open-blade engine-cooling fan shroud guide vanes

Compressor blade and production and use of a compressor blade

BLOWER AND HEATPUMP USING THE SAME

Actuatable seal for aerofoil blade tip

Circulation structure for a turbo compressor

Shroudless blade

Rotor casing treatment with recessed baffles

Abradable seals

Propeller fan

Gas turbine engine casing assembly

Axial flow fan, in particular for a motor vehicle

Buried casing treatment strip for a gas turbine engine

Cooling apparatus for a motor vehicle

Cooling device and construction machine or working machine equipped with the same

Cooling device and construction machine or working machine equipped with the same

Cooling device and construction machine or working machine equipped with the same

Cooling device and construction machine or working machine equipped with the same

Axial compressor

Closed-loop control for a gas turbine with actively stabilized compressor

Turbomachine rotor wheel having composite material blades

Turbomachine rotor having blades of composite material provided with metal labyrinth teeth

Segmented composite inner ferrule and segment of diffuser of axial compressor

Compressor stator blade and compressor rotor blade

Ring fan and shroud air guide system

Fluid flow machine with running gap retraction

Axial flow fan

Reduced tip clearance losses in axial flow fans

AXIAL FAN CASING DESIGN WITH CIRCUMFERENTIALLY SPACED WEDGES

Axial fan for conveying cooling air for a cooling device of a motor vehicle

Gas turbine having a peripheral ring segment including a recirculation channel

Multistage turbomachine compressor

FAN BLADE

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

Compressor stator with partial shroud

ABRADABLE MATERIAL COMPOSITION, A THERMOMECHANICAL PART OR CASING INCLUDING A COATING, AND A METHOD OF FABRICATING OR REPAIRING A COATING PRESENTING SAID COMPOSITION

Sealing assembly for a turbine engine

Wheel for a rotating flow machine

Gas turbine with a compressor with self-healing abradable coating

FAN MODULE

Apparatus for eliminating compressor stator vibration induced by TIP leakage vortex bursting

Sealing system for a turbomachine

COMPRESSOR TIP GAP FLOW CONTROL USING PLASMA ACTUATORS

Blade shroud with fluid barrier jet generation

Seal assembly

Axial fan apparatus, housing, and electronic apparatus

Turbomachine having an axially displaceable rotor

Abradable component for a gas turbine engine

Liquid Cooling System Fan Assembly

Turbomachine casing with treatment, a compressor, and a turbomachine including such a casing

Fan with spiral supercharging device

Fan rub strip in situ machining system and method

Engine cooling fan assembly

Rotor disc assembly with abrasive insert

Turbomachine with reduced leakage penalties in pressure change and efficiency

Leakage flow control and seal wear minimization system for a turbine engine

Split knife edge seals

Axial fan assembly

Axial fan assembly

Variable clearance positive pressure packing ring and carrier arrangement with coil type spring

Fan assembly

Compressor casing

Cooling device

METHOD AND APPARATUS FOR REDUCING AXIAL COMPRESSOR BLADE TIP FLOW

Blade

Abradable material composition, a thermomechanical part or casing including a coating, and a method of fabricating or repairing a coating presenting said composition

Vane for a gas turbine engine

Fan and shroud assembly

Fan

Apparatus for eliminating compressor stator vibration induced by tip leakage vortex bursting

High efficiency air conditioner condenser fan with performance enhancements

Fan

Compressor bleed air manifold for blade clearance control

Axial fan assembly

Cellular materials

Spacing arrangement

Cowl structure for a gas turbine engine

Cellular materials

Compliant brush shroud assembly for gas turbine engine compressors

Compressor airfoils with movable tips

Cantilevered stator stage

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

Sheet metal turbine or compressor static shroud

Recirculation structure for a turbocompressor