MULTI-LAYERED CONTAINMENT STRUCTURE FOR A BLADED ROTOR OF A GAS TURBINE ENGINE

Turbine engine with a flow splitter having a profile with inclined serrations

Evaporative cooling pack with same direction flutes designed to prevent nesting

System with a rotor blade for a gas turbine with a blade root protective plate having a sealing section

Acoustic structure with floating interior skin

Annular component for supporting a turbine engine bearing

Turbomachine comprising a heat exchanger in the secondary path

Method of forming a cure tool and method of forming a textured surface using a cure tool

Turbo-shaft ejector with flow guide ring

High load capacity hybrid foil bearing

CMC aerofoil

Aircraft propulsion system comprising a member covered with a grooved structure

Fan cowl with a serrated trailing edge providing attached flow in reverse thrust mode

Tunable compliant attachment structure

BLADES AND VANES FOR GAS TURBINE ENGINES AND THE MANUFACTURE THEREOF

Seal interface with a deflection control feature

Method for forming a structural panel

Gimballed Augmentation Shroud

Turbine component assembly

CORE COWL AFTER-BODY

Dry Gas Seal And Turbomachine Having A Dry Gas Seal

Reduced drag system for windmills, fans, propellers, airfoils, and hydrofoils

Abrasive tip blade manufacture methods

Contoured evaporative cooling medium

Fibrous media drift eliminator

Gas turbine seals

Vortex generating device

Mixer assembly group for a turbofan engine

INTEGRATED TURBINE EXHAUST STRUTS AND MIXER OF TURBOFAN ENGINE

High load capacity hybrid foil bearing

Turbine vane with coupon having corrugated surface(s)

Blade with internal rib having corrugated surface(s)

Blade with parallel corrugated surfaces on inner and outer surfaces

Blade with corrugated outer surface(s)

Turbine rotor blade with coupon having corrugated surface(s)

Guide vane ring for a turbomachine

System and method for mixing tempering air with flue gas for hot SCR catalyst

Riblets for a flowpath surface of a turbomachine

Gas turbine engine blade casing

Durable riblets for engine environment

Seal assembly for a turbomachine

Liner for a combustor of a gas turbine engine with metallic corrugated member

Gas turbine engine exhaust mixer with lobes cross-over offset

System and method for creating a fluidic barrier with vortices from the upstream splitter

Containment casing

Thermally compliant additively manufactured fuel injector

Nacelle for an airplane turbojet

Integrated TEC/mixer strut axial position

Seal for a gas turbine engine assembly

Seals for a gas turbine engine assembly

Sheet-metal turbine housing

Inertial particle separator flow and particle bounce control

Non-axisymmetric fan flow path

Plated polymer compressor

CMC oxide-oxide mixer design

Leading edge cooling channel for airfoil

Curved plate/fin heater exchanger

Rotor disk blade with friction-held root, rotor disk, turbomachine and associated assembly method

Sheet metal turbine housing with cellular structure reinforcement

Shroud segment retainer

Gas turbine engine ejector

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

Gas turbine engine component external surface micro-channel cooling

Abrasive tip blade manufacture methods

Integrated turbine exhaust struts and mixer of turbofan engine

Heat exchanger for aircraft engine

Compressor variable vane assembly

Rotor blade with bonded cover

Outer vane support ring including a strong back plate in a compressor section of a gas turbine engine

Variable immersion lobe mixer for turbofan jet engine exhaust and method of fabricating the same

Heat exchanger for aircraft engine

Mixing device and turbofan engine having such mixing device

Actuator shaft boot

Bearing device for turbocharger

Self-locking sealing device

LAST STAGE BLADE INCLUDING A PLURALITY OF LEADING EDGE INDENTATIONS

High temperature fuel manifold for gas turbine engines

Turbomachine seal arrangement

Riblet structure on a flow surface and method

Low-ductility turbine shroud

DESIGN AND SHAPE FOR PULSE CARTRIDGES TO ALLOW HYDROPHOBIC MEDIA TO DRAIN AND GENERALLY INCREASE WORKING SURFACE AREA

Rotor blade with bonded cover

Jet flow nozzle and jet engine

Corrugated core cowl for a gas turbine engine

Gas-turbine exhaust cone with three-dimensionally profiled partition wall and plate-type wall element

Blade of a turbomachine

FLOW DISCHARGE DEVICE

ROUGHENED COATINGS FOR GAS TURBINE ENGINE COMPONENTS

Pump housing and drainage pump

Flexible seal for gas turbine engine system

Method of varying a fan duct throat area

Air turbine starter one-piece air exit port baffle

High temperature manifolds for gas turbine engines

Exhaust washed structure and associated composite structure and method of fabrication

Compressors with casing treatments in gas turbine engines

Turbocharger having fastening elements for fastening vane bearing rings of a variable turbine geometry VTG

Gas turbine engine with non-axisymmetric surface contoured rotor blade platform

TURBOFAN GAS TURBINE ENGINE AERODYNAMIC MIXER

Method for increasing the coefficient of adhesion between two parts rotating as one with a rotor

HEAT SHIELD

Internally damped blade

Containment system for a gas turbine engine

Bypass duct of a turbofan engine

METHODS AND APPARATUS INVOLVING COOLING FINS

Radially translating fan nozzle nacelle

Corrugated core cowl for a gas turbine engine

Turbo engine

Exhaust washed structure and associated composite structure and method of fabrication

LABYRINTH SEAL WITH REDUCED LEAKAGE FLOW BY GROOVES AND TEETH SYNERGISTIC ACTION

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

Airfoil and method for protecting airfoil leading edge

Airfoil and method for protecting airfoil leading edge

Roughened coatings for gas turbine engine components

Seal

Turbine blade with an impingement cooling insert

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

Vortex generators on rotor blades to delay an onset of large oscillatory pitching moments and increase maximum lift

Thermal barrier coating system for a turbine airfoil usable in a turbine engine

System for retaining blades in a rotor

Method and device for reducing engine noise

Structural track support of spraybars/tubing

Active clearance control system for gas turbine engines

Aspherical dimples for heat transfer surfaces and method

Rotor assembly retaining apparatus

Method and device for reducing engine noise

Square ultra thrust reverser system

Cold air refrigerating system and turborxpander turbine for this system

Variable turbine cooling flow system

Variable stator vane arrangement for a compressor

Turbo fluid machine

Reverse vortex ring (RVR) for dramatic improvements in rocket engine turbomachinery rotordynamic stability margins