STATOR PART HAVING A FIN, IN A TURBINE ENGINE

GAS TURBINE ENGINE

GAS TURBINE ENGINE

GAS TURBINE ENGINE

GAS TURBINE ENGINE

NOTCHED TURBINE AIRFOILS FOR WEIGHT REDUCTION IN GAS TURBINE ENGINES

GAS TURBINE ENGINE WITH CLUTCH ASSEMBLY

PROPULSION SYSTEM AND METHOD FOR OPERATION

TANDEM BLADE ROTOR DISK

ROTOR ASSEMBLY FOR A GAS TURBINE ENGINE

Group of stator vanes

Fan for a turbine engine

ADVANCE RATIO FOR SINGLE UNDUCTED ROTOR ENGINE

Tandem blade rotor disk

Axial fan with trailing edge flap

Tandem blade rotor disk

SEGMENT FOR A TURBINE ROTOR STAGE

Layered fuselage shield

VARIABLE-CYCLE COMPRESSOR WITH A SPLITTERED ROTOR

Gas turbine engine with clutch assembly

Gas turbine engine outlet guide vane assembly

Rotor blade pair for rotational equipment

Gas turbine engine

System and method for control for unducted engine

Tandem blade rotor disk

Multi-blade vane for a turbomachine rotor and rotor comprising same

Impeller splitter optimization

TANDEM FAN FOR BOUNDARY LAYER INGESTION SYSTEMS

Guide vane cascade for a turbomachine

FAN BLADES WITH RECESSED SURFACES

Tandem rotor blades

Aerodynamic Regulation of Airscrew-, Fan- and Wind Turbine Blades with Bores and/or Cutting and/or Notching

Aerodynamic Regulation of Airscrew-, Fan- and Wind Turbine Blades with Bores and/or Cutting and/or Notching

Methods of manufacturing a tandem guide vane segment

Heat dissipation fan

Integrated strut-vane

Turbine Engine and Method of Assembling

Turbine wheel for a turbo-machine

Variable inlet guide vane

Turbine module for a turbomachine

Turbofan engine's fan blade and setting method thereof

Aerofoil with leading edge slits

Flowmeter with discontinuous helicoid turbine

Turbine blade, turbine including same turbine blade, and gas turbine including same turbine

Impeller

Mistuned concentric airfoil assembly and method of mistuning same

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

Method and system for leading edge auxiliary vanes

Method and system for compressor vane leading edge auxiliary vanes

Method and system for leading edge auxiliary turbine vanes

Turbocharger having a meridionally divided turbine housing and a variable turbine nozzle

Interdigitated counter rotating turbine system and method of operation

Tip leakage flow directionality control

Turbofan nacelle assembly with flow disruptor

Assembly of turbine engine parts comprising a fan blade having an integrated platform, and corresponding turbine engine

Turbine engine part with non-axisymmetric surface

Double impingement slot cap assembly

Fluid flow machine with high performance

Stationary blades for a steam turbine and method of assembling same

Device for controlling the flow in a turbomachine, turbomachine and method

Methods of manufacturing a tandem guide vane segment

Strut assembly for an aircraft engine

Turbine impeller and variable geometry turbine

Turbine engine and method of assembling

Lifting foil

Tandem tip blade

Turbocharger compressor and method

Mistuned concentric airfoil assembly and method of mistuning same

Method for operating a compressor of a turbomachine comprising providing a plurality of stages in a front compressor area, a rear compressor area, and allowing a swirl in the rear compressor area

Method, compressor and turbomachine

Exhaust gas diffuser with main struts and small struts

Morphing vane

MANUFACTURE OF BLADE CHANNELS OF TURBOMACHINE ROTORS

Floating panel for a gas powered turbine

Designing the geometry of a gas turbine exhaust diffuser on the basis of fluid dynamics information

Gas turbine engine airfoil with auxiliary flow channel

Turbine engine with a turbo-compressor

Axial compressor rotor incorporating splitter blades

Axial compressor rotor incorporating non-axisymmetric hub flowpath and splittered blades

VANE STRUCTURE FOR AXIAL FLOW TURBOMACHINE AND GAS TURBINE ENGINE

Guide vane

Multi-piece turbine airfoil

Tandem rotor blades

Blading with branches on the shroud of an axial-flow turbomachine compressor

Axial turbomachine compressor blade with branches at the base and at the head of the blade

Blade with branches for an axial-flow turbomachine compressor

Variable span splitter blade

Monobloc blade preform and module for a turbo machine intermediate casing

Rotor for a gas turbine engine

Compressor wheel of a radial compressor of an exhaust-gas turbocharger

Group of blade rows

Group of blade rows

Group of blade rows

Group of blade rows

Group of blade rows

Group of blade rows

Group of blade rows

Compressor wheel of the compressor of an exhaust-gas turbocharger

Turbine hub with surface discontinuity and turbocharger incorporating the same

Turbocharger shroud with cross-wise grooves and turbocharger incorporating the same

Variable geometry turbo system

Gas turbine diffuser strut including coanda flow injection

Airfoil with leading edge reinforcement

Turbomachine airfoil positioning

Axial compressor, gas turbine with axial compressor, and its remodeling method

Variable geometry nozzle and associated method of operation

Blade cascade and continuous-flow machine

Axial turbomachine stator with ailerons at the blade roots

Dual rotor blades having a metal leading airfoil and a trailing airfoil of a composite material for gas turbine engines

Integrated strut-vane

Turbomachine bucket having flow interrupter and related turbomachine

Stator vane row

Gas turbine engine variable geometry flow component

Lifting Foil

Tip leakage flow directionality control

Staggered double row, slotted airfoil design for gas turbine exhaust frame

Exhaust diffuser and method for manufacturing an exhaust diffuser

Process for producing a TiAl guide vane ring for a gas turbine and a corresponding guide vane ring

Continuous-flow machine with at least one guide vane ring

Tip leakage flow directionality control

Axial compressor

Blade group arrangement as well as turbomachine

Turbomachine

Turbomachine

Turbomachine

Turbine Diffuser

Method for chemical milling an apparatus with a flow passage

Aerodynamic coupling between two annular rows of stationary vanes in a turbine engine

TRANSITION CHANNEL OF A TURBINE UNIT

Movable strut cover for exhaust diffuser

Noise reduction in a turbomachine, and a related method thereof

TANDEM FAN-TURBINE ROTOR FOR A TIP TURBINE ENGINE

CENTRIFUGAL COMPRESSOR ASSEMBLY WITH STATOR VANE ROW

Fluid-flow machine—blade with hybrid profile configuration

Integrated variable geometry flow restrictor and heat exchanger

Tandem blade design

Multiple airfoil vanes

Turbine blade

Compressor performance adjustment system

Fluid flow machine with blade row group

Anti-Erosion shield for rotor blades

Fluid dynamic body having escapelet openings for reducing induced and interference drag, and energizing stagnant flow

Fluid flow machine with a blade row group featuring a meridional edge distance

Deflector for a gas turbine strut and vane assembly

Spanwise split variable guide vane and related method

Inlet guide vanes and gas turbine engine systems involving such vanes

VANE ASSEMBLY CONFIGURED FOR TURNING A FLOW IN A GAS TURBINE ENGINE, A STATOR COMPONENT COMPRISING THE VANE ASSEMBLY, A GAS TURBINE AND AN AIRCRAFT JET ENGINE

VARIABLE GEOMETRY TURBOCHARGER

Multi-vane variable stator unit of a fluid flow machine

SYSTEM AND METHOD FOR REDUCTION OF UNSTEADY PRESSURES IN TURBOMACHINERY

Twin-airfoil blade with spacer strips

Fan blade

Systems and Methods Involving Variable Vanes

Vane assembly with metal trailing edge segment

Variable-shape variable-stagger inlet guide vane flap

Gas turbine with a guide vane

GAS TURBINE GUIDE VANES WITH TANDEM AIRFOILS AND FUEL INJECTION AND METHOD OF USE

Fan platform fin

Vane assembly with metal trailing edge segment

Turbine

High pressure tandem turbine

Rotary apparatus for a gas turbine engine

Bifurcated outlet guide vanes

De-icing device for turbojet inlet guide wheel vane, vane provided with such a de-icing device, and aircraft engine equipped with such vanes