LOW-FREQUENCY ACOUSTIC CENTER BODY

EXHAUST DUCT FOR HYBRID AIRCRAFT POWERPLANT

AIRCRAFT PROPULSION SYSTEM WITH VARIABLE SPEED ROTATING STRUCTURE

Flexible frustoconical input shaft

GAS GENERATOR BIFURCATING EXHAUST DUCT TO FREE TURBINE

ROTOR BLADE FOR A TURBOMACHINE, ASSOCIATED TURBINE MODULE, AND USE THEREOF

NOISE REDUCING DEVICE HAVING AN OBLIQUELY PIERCED HONEYCOMB STRUCTURE

Variable pitch bladed disc

Sealing device and rotary machine

Aircraft heat exchanger panel array interconnection

Compact accessory systems for a gas turbine engine

Turbine nozzle having an angled inner band flange

Flow deflector for a discharge valve system, discharge valve system and turbomachine comprising such a discharge valve system

Centrifugal compressor

Turbine rotor blade with airfoil cooling integrated with impingement platform cooling

Offset cores for gas turbine engines

Guide vane airfoil for the hot gas flow path of a turbomachine

Transition duct, turbine, and gas turbine engine

Non-contact seal with angled land

Variable nozzle mechanism and rotating machine including the same

Liquid propellant rocket engine turbopump drain

Engine component with non-diffusing section

Compact accessory systems for a gas turbine engine

Gas turbine

Turbine nozzle having an angled inner band flange

Engine component with hollow turbulators

Elliptical slot with shielding holes

Seal structure and turbine

Step seal, seal structure, turbo machine, and method for manufacturing step seal

GAS TURBINE ENGINE WITH FILM HOLES

Turbine engine with fan and reduction of speed on the shaft of the power turbine

Airfoil platform cooling channels

Turbine engine with a platform cooling circuit

Brush seal for a turbine engine rotor

Composite piston ring seal for axially and circumferentially translating ducts

Apparatus including heat exchanger and sound attenuator for gas turbine engine

Film cooling hole including offset diffuser portion

Turbine engine exhaust casing with improved lifetime

Twin shafts driving adjacent fans for aircraft propulsion

Gas turbine engine accessories arrangement

Gearbox comprising an improved reduction gear

System and apparatus for diversified gearbox

GAS GENERATOR BIFURCATING EXHAUST DUCT TO FREE TURBINE

Combustor cooling panel, transition piece and combustor including the same, and gas turbine including combustor

Rotor blade for a gas turbine engine

Turbine

Labyrinth seal with lubricant directing projection

Cooling features with three dimensional chevron geometry

Equipment support of a turbo machine comprising a reducer with magnetic gears

Floating support assembly for compensating for axial thermal expansion

Variable pitch bladed disc

Variable pitch bladed disc

Stator heat shield for a gas turbine, gas turbine with such a stator heat shield and method of cooling a stator heat shield

JET ENGINES AND THEIR ARRANGEMENT IN THE REAR SECTION OF AN AIRCRAFT

Fan case for use in a turbofan engine, and method of assembling a turbofan engine

TRANSITION DUCT SYSTEM WITH A ROBUST CONVERGING FLOW JOINT AT AN INTERSECTION BETWEEN ADJACENT TRANSITIONS EXTENDING BETWEEN A COMBUSTOR AND A TURBINE ASSEMBLY IN A GAS TURBINE ENGINE

Compressor

Blade outer air seal

Staggered crossovers for airfoils

Cooling structure for hot-gas path components with methods of fabrication

Centrifugal fan having impeller with blades between annular shroud and main plate

Gas turbine engine airfoil

Rotor device of an aircraft engine with a damping device between turbines blades

Composite piston ring seal for axially and circumferentially translating ducts

Heat shield for mixed flow turbine wheel turbochargers

Sealing structure and rotary machine

Fan cooling hole array

Engine cowling of an aircraft gas turbine

Structural honeycomb panel

Rotating turbine vane bearing cooling

Decoupled translating sleeve

System and apparatus for diversified gearbox

Gas turbine engine component with film cooling hole with accumulator

Cooled airfoil structure

Staggered crossovers for airfoils

Hot gas components with compound angled cooling features and methods of manufacture

Gas turbine engine and method of assembling the same

Water removal device for steam turbine

Gas turbine engine heat exchanger manifold

Gas turbine electrical machine arrangement

Offset cores for gas turbine engines

Turbine blade cooling structure

Reverse flow single spool core gas turbine engine

Casting optimized to improve suction side cooling shaped hole performance

Decoupled gas turbine engine

Stator segment

Reverse core engine with thrust reverser

Gas turbine engine v-shaped film cooling hole

Turbine engine impeller

Reverse core turbine engine mounted above aircraft wing

Angled core gas turbine engine mounting

Air exhaust tube holder in a turbomachine

Offset core engine architecture

Angled reverse core gas turbine engine with widened nozzle

Interwoven channels for internal cooling of airfoil

Gas turbine engine with twin offset gas generators

Radially coacting ring seal

Flow outlet

Gas turbinen rotor blade

Compressor for supercharger of internal combustion engine

Conjoined reverse core flow engine arrangement

Tapered-land thrust bearing for turbochargers

Mixed-flow turbocharger with variable turbine geometry

Exhaust mixer with offset lobes

Exhaust gas turbocharger with vibration-insulating mounting of a rotor

Cooled turbine blade with double compound angled holes and slots

Continuous ignition systems

Variable cycle intake for reverse core engine

Free stream intake with particle separator for reverse core engine

Reverse core engine thrust reverser for under wing

Rear mounted reverse core engine thrust reverser

Reverse flow gas turbine engine airflow bypass

Compressor housing and exhaust gas turbine supercharger

Gas turbine centripetal annular combustion chamber and method for flow guidance

Turbine engine blade

Gas turbine engine cooling hole with circular exit geometry

REVERSE FLOW GAS TURBINE ENGINE WITH THRUST REVERSER

TURBINE SHROUD FOR A TURBOMACHINE

Nozzle diaphragm inducer

Turbine diaphragm construction

Trailing edge or tip flag antiflow separation

Mid-section of a can-annular gas turbine engine with a cooling system for the transition

TIP SHROUDED BLADE

Gas turbine annular diffusor

Gas turbine engine with separate core and propulsion unit

Gas turbine engine with modular cores and propulsion unit

Compressor and a turbine engine with optimized efficiency

Cooled turbine blade for gas turbine engine

Gas turbine combustion chamber arrangement of axial type of construction

AERO-DERIVATIVE GAS TURBINE ENGINE WITH AN ADVANCED TRANSITION DUCT COMBUSTION ASSEMBLY

Blade outer air seal assembly leading edge core configuration

LOW PRESSURE STEAM TURBINE INCLUDING PIVOTABLE NOZZLE

Gas turbine

Torque frame and asymmetric journal bearing for fan drive gear system

ANGLED TRENCH DIFFUSER

Gas turbine engine with angled and radial supports

Gas turbine and repairing method of gas turbine

Load member for transition duct in turbine system

Curved Passages for a Turbine Component

Method of reducing asymmetric fluid flow effects in a passage

MULTIPLE CORE VARIABLE CYCLE GAS TURBINE ENGINE AND METHOD OF OPERATION

Turbine blade fastening for a turbomachine

Leaf seal device

Reverse thrust device

Turbine and turbine rotor blade

ROTATING SEAL RING WITH TARGETED SPLIT SURFACE ORIENTATION

Method for manufacturing an integrally bladed rotor

Axial turbomachine having an axially displaceable guide-blade carrier

Turbine stage shroud segment

LABYRINTH SEAL

Turbine blade system

Axially angled annular seals

Gas turbine engine and a gas turbine engine component

Gas turbine engine sealing structure

Turbocharger

Turbomachine

Method and apparatus for labyrinth seal packing rings

Rotating blade system for a row of rotating blades of a turbomachine

Thrust bearing, especially for a turbocharger

Turbine engine components

GAS TURBINE, DISK, AND METHOD FOR FORMING RADIAL PASSAGE OF DISK

Leaf seal device

Deswirling exhaust mixer

Stator vane assembly

Rotor arrangement

Turbocharger diffuser

Bleed structure for a bleed passage in a gas turbine engine

Turbomachine

Device for inhibiting the flow of oil along a rotating shaft

Seal structure

Turbine engine having two off-axis spools with valving-enabled modulation between high and low power modes

VARIABLE TURBINE GEOMETRY TURBOCHARGER

Blade for a rotor

Integrated guide vane assembly

Stator ring configuration

Steam turbine rotating blade for a low pressure section of a steam turbine engine

Turbocharger

Canted outlet for transition in a gas turbine engine

Gas turbine

Shroud segment cooling configuration

Device for injecting mono-propellant at a flow rate that can be modulated with an injection speed that is stable

Device for injecting a mono-propellant with a large amount of flow rate modulation

Aircraft engine thrust reverser

Damper

Casing treatment for axial compressors in a hub area

Turbine blade with multiple impingement cooled passages

System and method of continuous detonation in a gas turbine engine

Aircraft Propulsion System

Compact bearing support

Blade Mounting

Cooling structure

Steam turbine with two steam chambers

Supercharger

Turbine airfoil concave cooling passage using dual-swirl flow mechanism and method

Rolling Bearing and Supercharger Using Same

Turbine vane securing mechanism

Angled tripped airfoil peanut cavity

Turbine wheel with backswept inducer

Propulsion unit for aircraft with heat exchanger having front inlet faces for cooling air flow and hot air flow

Damper for turbomachine vanes

Angled on-board injector

Turbine component

Out-flow margin protection for a gas turbine engine

Turbomachine having an axially displaceable rotor

Turbine blade trip strip orientation

Methods and apparatus for fabricating a rotor assembly

Method and system to facilitate cooling turbine engines

Rotary machine components and methods of fabricating such components

Bleed structure for a bleed passage in a gas turbine engine

Turbocharger having inclined volutes

Gas turbine airfoil with leading edge cooling

Method and apparatus for fabricating a nozzle segment for use with turbine engines

Turbo machine

Leaned high pressure compressor inlet guide vane

Ball bearing turbocharger balancer

Aeroengine bleed valve

Compact compound engine package

Integral cooling system for rotary engine

Turbine airfoil with weight reduction plenum

Tilted turbine vane with impingement cooling

Method and apparatus for cooling gas turbine rotor blades

Cooled turbine blade

Damper cooled turbine blade

Retention arrangement

Cooling arrangement

Methods and apparatus for injecting fluids into a turbine engine

Bleed valve outlet flow deflector

Cooled airfoil trailing edge tip exit

Aerodynamically enhanced bearing housing pocket geometry

Turbofan arrangement

Industrial gas turbine blade assembly

BLEED STRUCTURE FOR A BLEED PASSAGE IN A GAS TURBINE ENGINE

Forward tilted turbine nozzle

Coverplate deflectors for redirecting a fluid flow

Steam turbine blade, steam turbine rotor, steam turbine with those blades and rotors, and power plant with the turbines

Cooling system for a gas turbine engine

Compact mixer with trimmable open centerbody

Fluid vectoring nozzle

Turbofan arrangement

Turbine rotor blade and turbine

Wave rotor apparatus

Twisted mixer with open center body

Heat transfer arrangement

Gas turbine airfoil film cooling hole

Turbomachine nozzle cover for reducing jet noise

Turbine blade

Cooling system for a showerhead of a turbine blade

Cooled rotor blade

Method and apparatus for fabricating gas turbine engines

Turbulated hole configurations for turbine blades

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

Exhaust diffuser assembly with tunable velocity profile

Rotating pulse detonation system for a gas turbine engine