AIR TURBINE STARTER CONTAINMENT SYSTEM

SHROUD OF GAS TURBINE ENGINE AND METHOD OF MANUFACTURING THEREOF

Phonic wheel for turbine engine

SEALING STRIP ELEMENT AND SEALING ARRANGEMENT COMPRISING SAID SEALING STRIP ELEMENT

Partition damper seal configurations for segmented internal cooling hardware

Switching valve

Partition damper seal configurations for segmented internal cooling hardware

Internal retaining ring for a rotating assembly in a gas turbine engine

Turbine blade tip shroud surface profiles

Cooling device for a turbomachine casing

Curvilinear coupling for aircraft turbomachinery

Moving blade for a wheel of a turbine engine

Air turbine starter containment system

Gas turbine engine dilution chute geometry

Angular sector for turbomachine blading with improved sealing

Free-tipped axial fan assembly

Seal arrangement for turbine engine component

Cooling passages for gas turbine engine component

Gas turbine engine configured for modular assembly/disassembly and method for same

COOLING ARRANGEMENT WITH CRENELLATION FEATURES FOR GAS TURBINE ENGINE COMPONENT

Gas turbine engine airfoil with tip leading edge shelf discourager

Blade tip clearance control apparatus for gas turbine

Air seal attachment

Sliding seal

Modulation of vane end serrations

Heat dissipation fan

Aerofoil with leading edge slits

Anti-rotation assembly

Mistuned compressor rotor with hub scoops

Gas turbine engine inlet

Seal fin, seal structure, and turbo machine

Inlet pre-swirl gas turbine engine

Inlet pre-swirl gas turbine engine

Hybrid thermal barrier coating

Blade tip seal

Variable nozzle mechanism and variable displacement type exhaust turbocharger

Gas turbine with a radial-to-axial intake, variable-angle inlet guide vane therefore, and method of operation

Systems including rotor blade tips and circumferentially grooved shrouds

GAS TURBINE ENGINE COMPONENT HAVING TIP VORTEX CREATION FEATURE

Three dimensional auxetic structure, manufacturing method and tooling

Turbine engine airfoil with a modified leading edge

Flow control structures for turbomachines and methods of designing the same

Airfoil containment structure including a notched and tapered inner shell

Integrated heat exchangers for low fan pressure ratio geared turbofan

Two pieces stator inner shroud

Constant speed 2 piece ring seal arrangement

Turbofan nacelle assembly with flow disruptor

Dual wall airfoil with stiffened trailing edge

Free-tipped axial fan assembly

Circumferentially varying thickness composite fan casing

Axial fan with grooved trailing edge and outdoor unit

Biomimetic airfoil bodies and methods of designing and making same

Seal device for turbine, turbine, and thin plate for seal device

Turbine vane with coupon having corrugated surface(s)

Forming cooling passages in thermal barrier coated, combustion turbine superalloy components

Blade with corrugated outer surface(s)

Turbine rotor blade with coupon having corrugated surface(s)

Turbine shroud with abradable layer having dimpled forward zone

Crack stopper for welds

Damper ring

Axial Turbine Engine Compressor De-Icing Blade

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

Output director vane for an aircraft turbine engine, with an improved lubricant cooling function using a heat conduction matrix housed in an inner duct of the vane

Vane retainer

Intercomponent seal for a gas turbine engine

Aerofoil

Riblets for a flowpath surface of a turbomachine

Cooled CMC wall contouring

Turbine component thermal barrier coating with depth-varying material properties

Turbine abradable layer with inclined angle surface ridge or groove pattern

Turbine component thermal barrier coating with crack isolating engineered groove features

Turbomachine comprising a shaft sleeve and associated sleeve tube

Tapered land thrust bearing device and turbocharger provided with the bearing device

Turbine blade damper system having pin with slots

Seal arrangement for turbine engine component

Turbine bucket cooling

Sliding seal

Tailored thermal control system for gas turbine engine blade outer air seal array

Turbine vane with heat shield

Incident tolerant turbine vane gap flow discouragement

Air-blowing device

Centrifugal fan and air conditioner provided with the same

Seal for a thrust reverser of a turbojet engine nacelle

Gas turbine engine with seal having protrusions

Afterbody for a turbojet engine comprising a nozzle provided with a thrust reverser system that incorporates a crown of noise-reducing chevrons

Multi-stage inter shaft ring seal

Baffle for gas turbine engine vane

Blade

Mini blind stator leakage reduction

Water removal device for steam turbine and method for forming slit

Plated polymer compressor

Bushing for a variable stator vane and method of making same

Gas turbine engine system for modulating flow of fan by-pass air and core engine air

Water removal device for steam turbine

Tapered cooling channel for airfoil

Leading edge cooling channel for airfoil

Multi-stage-type compressor and gas turbine equipped therewith

Sealing device

Gas turbine engine inlet

Core cowl for a turbofan engine

Compressor casing

Castellated latch mechanism for a gas turbine engine

Aircraft turbomachine comprising a deflector

Seal assembly including a notched seal element for arranging between a stator and a rotor

Edge treatment for gas turbine engine component

Debris removal system

Gas turbine engine configured for modular assembly/disassembly and method for same

Gas turbine engine component having tip vortex creation feature

Gas turbine engine coupling stack

Acoustic treatment to mitigate fan noise

Integrated heat exchangers for low fan pressure ratio geared turbofan

Bladed rotor

Turbine abradable layer with zig zag groove pattern

Transition duct assembly with modified trailing edge in turbine system

Noise attenuation in rotating blades

Turbomachine stage and method for detecting a sealing gap of such a turbomachine stage

Turbine split ring retention and anti-rotation method

Gas turbine shroud assemblies

Coating interface

Fan containment system

Cooling hole with crenellation features

Turbine

Nozzle with guiding devices

Cooling structures for turbine rotor blade tips

Vortex generators for improved film effectiveness

Turbine rotor cover plate lock

Rotational debris discourager for gas turbine engine bearing

Gas turbine engine components with film cooling holes having cylindrical to multi-lobe configurations

Cooling hole with crenellation features

Turbine engine shaft coupling

Machine with Abradable Ridges and Method

Airflow assembly having improved acoustical performance

STATOR-ROTOR ASSEMBLIES WITH FEATURES FOR ENHANCED CONTAINMENT OF GAS FLOW, AND RELATED PROCESSES

Seals in steam turbine

Prestressing device having circumferential activity

Endwall component for a turbine stage of a gas turbine engine

Component with inspection-facilitating features

SEAL TEETH FOR SEAL ASSEMBLY

Turbojet engine with an element of the nacelle attached to the intermediate casing

Flow discouraging systems and gas turbine engines

Seal assembly for use with turbine nozzles

IMPELLER FOR TURBINE

Method of forming a seal element

Airfoil cooling hole flag region

Blade for a turbo device with a vortex-generator

Method and apparatus for labyrinth seal packing rings

TURBOCHARGER

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

ARTICLE HAVING DIFFUSER HOLES AND METHOD OF MAKING SAME

High efficiency turbine system

Internally damped blade

DUAL-FLOW TURBINE ENGINE FOR AIRCRAFT WITH LOW NOISE EMISSION

Blade outer seal assembly and method

Shroudless blade

Fastening arrangement of a pipe on a circumferential surface

Airfoil attachment

WALL OF A ROCKET ENGINE

Method for the manufacture of an ejector nozzle tube

Blade outer seal assembly

SIDE CHANNEL COMPRESSOR

Variable nozzle mechanism

Method for improving the sealing on rotor arrangements

Turbomachinery

Turbine with at least one rotor which comprises rotor disks and a tie-bolt

Crenelated turbine nozzle

Turbine blade assembly

Diffuser for decelerating a compressed fluid

Nozzle with guiding elements

ARTICLE HAVING A PROTECTIVE COATING AND METHODS

Acoustic liners

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

Seals in steam turbine

Blade outer air seal with improved thermomechanical fatigue life

Inspection tool for measuring bucket Z notch position

Airfoil and method for protecting airfoil leading edge

Airfoil and method for protecting airfoil leading edge

Blade angle setting for a turbomachine

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

System for ventilating a combustion chamber wall

Heat shield with stress relieving feature

Turbo machine

Methods and apparatus to facilitate sealing in a turbine

Geothermal turbine

Radially-compact assembly between a turbine shaft and a stub axle of a turbomachine compressor shaft

Method and apparatus for assembling turbine nozzle assembly

High pressure turbine disk hub with reduced axial stress and method

Turbine airfoil with counter-flow serpentine channels

Annular wiper for a sealing labyrinth, and its method of manufacture

Fastening arrangement of a pipe on a circumferential surface

Device for damping vibration of a ring for axially retaining turbomachine fan blades

Nozzle blade for steam turbine, nozzle diaphragm and steam turbine employing the same, and method of fabricating the same

Device for rotationally locking a clamping nut for a component on a shaft, clamping nut and shaft comprising it, and aircraft engine equipped therewith

Moisture removal grooves on steam turbine buckets and covers and methods of manufacture

Sealing arrangement, in particular for the blade segments of gas turbines

Blade outer seal assembly

Sealing arrangement, in particular for the blade segments of gas turbines

Article having diffuser holes and method of making same

Turbine case reinforcement in a gas turbine jet engine

Airfoil insert with castellated end

Cold air refrigerating system and turborxpander turbine for this system

Seal element for sealing a gap and combustion turbine having a seal element

Geothermal turbine