THRUST REVERSER WITH BLOCKER DOOR FOLDING LINKAGE

TURBINE ENGINE HAVING A COMPRESSOR WITH AN INDUCER

Turbine engine having a compressor with an inducer

Aircraft propulsion system exhaust nozzle with ejector passage(s)

Last chance screen for aircraft fuel system

GAS TURBINE ENGINE INLET

Cartridge tip for turbomachine combustor

Segmented augmented turbine assembly

Gas turbine engine with fluid circuit and ejector

Convergent-divergent flap pair for a variable-geometry turbojet engine nozzle comprising cooling air circulation ducts connected through contact surfaces

Convergent-divergent flap pair for a variable-geometry turbojet engine nozzle, the flaps of which each comprise a cooling air circulation duct

De-icing device for an air intake of an aircraft turbojet engine nacelle

High bypass ratio engine bypass duct nozzle with controlled nozzle area

Exhaust nozzle of a gas turbine engine

Gas turbine component with cooling aperture having shaped inlet and method of forming the same

HOT GAS PATH COMPONENT WITH METERING STRUCTURE INCLUDING CONVERGING-DIVERGING PASSAGE PORTIONS

THRUST NOZZLE FOR A TURBOFAN ENGINE ON A SUPERSONIC AIRCRAFT

Turbocharger

Gas turbine component with cooling aperture having shaped inlet and method of forming the same

Convergent-divergent nozzle mechanism

Acoustic liners with oblique cellular structures

Nozzle of a turbomachine provided with chevrons with a non-axisymmetric inner face

Centrifugal compressor with diffuser with throat

Combustor liner panel with a multiple of heat transfer ribs for a gas turbine engine combustor

Supply duct of a compressor of a turbine engine

Turbomachine airfoil

Compressor bleed apparatus for a turbine engine

Generalized jet-effect and fluid-repellent corpus

CONVERGENT-DIVERGENT NOZZLE FOR A TURBOFAN ENGINE OF A SUPERSONIC AIRCRAFT AND METHOD FOR REDUCING THE BASE DRAG BEHIND SUCH NOZZLE

Rainbow flowpath low pressure turbine rotor assembly

Internally cooled engine components

Diffuser for a turbine engine and method of forming same

Turbine assembly

Gas turbine component with cooling aperture having shaped inlet and method of forming the same

Fluid flow machine with high performance

Turbocharger

Impingement insert for a gas turbine engine

Impingement holes for a turbine engine component

Gas turbine engine trailing edge ejection holes

Variable thickness core for gas turbine engine component

Crossover hole configuration for a flowpath component in a gas turbine engine

Convergent-divergent nozzle

Exhaust mixer for wave rotor assembly

Gas turbine engine airfoil component platform seal cooling

Nozzle of a turbomachine provided with chevrons with a non-axisymmetric inner face

Gas turbine engine convergent/divergent nozzle with unitary synchronization ring for roller track nozzle

Gas turbine engine inlet

Methods and apparatus for passive thrust vectoring and plume deflection

System and method for active clearance control

Component for use in releasing a flow of material into an environment subject to periodic fluctuations in pressure

Nozzle endwall film cooling with airfoil cooling holes

Methods and apparatus for passive thrust vectoring and plume deflection

Cooling passages for turbine buckets of a gas turbine engine

Casing cooling duct

Reflex annular vent nozzle

Combustor transition duct assembly with inner liner

Asymmetrically shaped trailing edge cooling holes

TURBINE AIRFOIL TRAILING EDGE BIFURCATED COOLING HOLES

Method for defining the shape of a turbomachine convergent-divergent nozzle, and corresponding convergent-divergent nozzle

System and method for cooling turbine blades

LEADING EDGE AIRFOIL-TO-PLATFORM FILLET COOLING TUBE

Shaft seal with convergent nozzle

Assembly for directing combustion gas

Nozzle plasma flow control utilizing dielectric barrier discharge plasma actuators

Fluid flow machine with blade row group

Cooling hole exits for a turbine bucket tip shroud

Propulsion system with canted multinozzle grid

DIFFUSER ARRANGEMENT

Turbine arrangement and method of cooling a shroud located at the tip of a turbine blade

Floatable unit for evacuation purposes

DLN DUAL FUEL PRIMARY NOZZLE

Modular transvane assembly

Performance improvements for pulse detonation engines

Optimizing an anti-coke film in an injector system for a gas turbine engine

Apparatus and method for active gap monitoring for a continuous flow machine

Turbocharger for a vehicle with a coanda device

Vectorable nozzle with pivotable triangular panels

High efficiency thermal engine

Nozzles with rotatable sections for variable thrust

Gas turbine engine provided with a foreign matter removal passage

Flow redirector for compressor inlet

Microcircuit cooling for blades

Exhaust turbo-supercharger

Missile control system and method

Pulse combustion device

Axial divergent section slot nozzle

Method of achieving jet separation of an un-separated flow in a divergent nozzle body of a rocket engine

Gas turbine with stator shroud in the cavity beneath the chamber

Cooled gas turbine engine vane

Transpiration cooling system

2D variable-area plug nozzle