COMBUSTOR NOZZLE, COMBUSTOR, AND GAS TURBINE INCLUDING SAME

Stator blade for a centrifugal compressor

Adaptable flow control for engine nacelles

Powered augmented fluid turbines

Aerofoil assembly and method

Turbine vane comprising a passive system for reducing vortex phenomena in an air flow flowing over said vane

Method and apparatus to enhance laminar flow for gas turbine engine components

Stator vane of fan or compressor

Methods and apparatus for reducing flow distortion at engine fans of nacelles

Case for gas turbine engine

Steam turbine exhaust chamber and steam turbine system

Secondary flow control

Methods and apparatus for reducing flow distortion at engine fans of nacelles

Turbine engine with variable effective throat

Exhaust diffuser having ejection hole and suction hole, and gas turbine having the same

Variable-geometry boundary layer diverter

Turbine blades and gas turbine having the same

Casing with suction arm for axial turbine engine

Compressor rotor airfoil

Method and apparatus to enhance laminar flow for gas turbine engine components

Air inlet duct for an aircraft turbine engine

Gas turbine exhaust diffuser with air injection

Riblets for a flowpath surface of a turbomachine

Centrifugal compressor and turbocharger

Nacelle

Aircraft turbine engine air intake duct

Air guidance device for a turbomachine with grooves to maintain boundary layer

Inlet flow restrictor

Gas turbine stator with winglets

Turbomachine diffuser including flow mixing lobes and method

System and method for improving exhaust energy recovery

Fan nacelle inlet flow control

Combined inlet laminar and thrust reverser cascade efflux flow control system

Air intake arrangement

Method of controlling boundary layer flow

Guide vane

Pre-cooler inlet ducts that utilize active flow-control and systems and methods including the same

Compressor airfoil

Compressor rotor airfoil

Thrust-reverser assemblies that utilize active flow-control and systems and methods including the same

Group of blade rows

Multistage axial flow compressor

Systems and methods for boundary control during steam turbine acceleration

Gas turbine nozzle trailing edge fillet

Assembly for a fluid flow machine

Valve for gas turbine engine

Gas turbine engines having plasma flow-controlled intake systems

Passive boundary layer bleed system for nacelle inlet airflow control

Blade of a row of rotor blades or stator blades for use in a turbomachine

Diffuser assemblies having at least one adjustable flow deflecting member

Method, process, and system for high efficiency gas turbine exhaust duct flow-path

Turbine blade

Impulse turbine for use in bi-directional flows

Self-centring cage nut

Turbomachine flow stability enhancement device control

Integrated thermal protection and leakage reduction in a supersonic air intake system

Method of using an active flow control system for lift enhancement or destruction in a wind turbine blade

Turbine engine heat recuperator system

Turbomachine

Turbomachine

Customer bleed air pressure loss reduction

GEARED TURBOMACHINE ARCHITECTURE HAVING A LOW PROFILE CORE FLOW PATH CONTOUR

Noise-reduced turbomachine

EXHAUST GAS DIFFUSER

Intermediate housing of a gas turbine having an outer bounding wall having a contour that changes in the circumferential direction upstream of a supporting rib to reduce secondary flow losses

Centrifugal compressor with fluid injector diffuser

Movable strut cover for exhaust diffuser

Diffuser with backward facing step having varying step height

Flow directing member for gas turbine engine

Apparatus for controlling a boundary layer in a diffusing flow path of a power generating machine

Airflow control device and airflow control method

Turbomachine with axial compression or expansion

Compression ramp boundary layer removal

Method for improving the stall margin of an axial flow compressor using a casing treatment

Gas turbine engine with ejector

Fluid flow control device for an aerofoil

Blade for a turbo device with a vortex-generator

Hollow steam guide diffuser having increased pressure recovery

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

Wind turbine blades with controllable aerodynamic vortex elements

Flow passage for gas turbine engine

Boundary layer energiser

Steampath flow separation reduction system

Boundary layer energiser

High temperature radially fed axial steam turbine

Cooled aerofoil blade or vane

HIGH-TURNING DIFFUSER STRUT WITH FLOW CROSS-OVER SLOTS

Passive boundary layer control elements

Gas turbine stator/rotor expansion stage having bumps arranged to locally increase static pressure

Separation resistant aerodynamic article

Cooled exhaust hood plates for reduced exhaust loss

Impulse turbine for use in bi-directional flows

PLASMA ENHANCED COMPRESSOR DUCT

PLASMA ENHANCED BOOSTER AND METHOD OF OPERATION

GAS TURBINE ENGINE WITH EJECTOR

Gas turbine engine with ejector

Curved platform turbine blade

VANE STRUCTURE FOR VERTICAL AXIS WIND POWER GENERATOR

Scalloped surface turbine stage with trailing edge ridges

Passive boundary layer bleed system for nacelle inlet airflow control

Combined acoustic absorber and heat exchanging outlet guide vanes

Passive boundary layer bleed system for nacelle inlet airflow control

Fluid flow machine with fluid injector assembly

Casing treatment for axial compressors in a hub area

AXIAL FLOW FLUID DEVICE

Fan nacelle flow control

Gas turbine engine systems involving mechanically alterable vane throat areas

COMPRESSOR TIP GAP FLOW CONTROL USING PLASMA ACTUATORS

Systems and Methods Involving Variable Vanes

Wind turbine blade with anti-noise devices

Nacelle compartment plenum for bleed air flow delivery system

Aerofoil members for a turbomachine

Nacelle assembly having inlet airfoil for a gas turbine engine

Fluid-flow machine and rotor blade thereof

Particle separator using boundary layer control

Airfoil leading edge end wall vortex reducing plasma

Method of modifying the end wall contour in a turbine using laser consolidation and the turbines derived therefrom

Plasma lifted boundary layer gas turbine engine vane

Airfoil and method for moisture removal and steam injection

Wall configuration of axial-flow machine, and gas turbine engine

Gas turbine vane

Acoustic dampers

Coupled parametric design of flow control and duct shape

Methods and apparatus for aerodynamically self-enhancing rotor blades

Turbine

Shockwave-induced boundary layer bleed

Turbomachine with fluid supply

Airfoil surface impedance modification for noise reduction in turbofan engines

Flow separation control device for an airfoil

System to control flow separation over an airfoil