TURBINE ENGINE HAVING A VARIABLE ENGINE INTAKE SYSTEM

SYSTEMS, ASSEMBLIES, AND METHODS TO ENHANCE INTAKE AIR FLOW TO A GAS TURBINE ENGINE OF A HYDRAULIC FRACTURING UNIT

VARIABLE AREA INLET FOR TURBINE ENGINE HEAT EXCHANGE SYSTEM

TURBINE ENGINE HAVING A VARIABLE ENGINE INTAKE SYSTEM

TURBOPROP ENGINE WITH CLOSABLE CORE

INLETS FOR GAS TURBINE ENGINE FANS WITH DISTORTION TOLERANCE

VARIABLE AREA TURBINE NOZZLE ASSEMBLY

VARIABLE AREA TURBINE NOZZLE ASSEMBLY

TAILORING AIRCRAFT POWERPLANT FLOW PARAMETERS USING INFLATABLE BLADDER(S)

TAILORING AIRCRAFT POWERPLANT SPLIT LINE PARAMETER WITH INFLATABLE BLADDER

SHAPEABLE INLET MANIFOLD FOR HYPERSONIC SCRAMJET

UNDUCTED PROPELLER GAS TURBINE COMPRISING A COOLING AIR CHANNEL AND A VARIABLE BLEED VALVE EJECTION CHANNEL

PROPULSION ASSEMBLY FOR AN AIRCRAFT, COMPRISING AN INTERMEDIATE COWL OF THE STATIONARY, REMOVABLE TYPE, MOUNTED ON A HINGE SYSTEM

Aircraft engine assembly for controlling engine oil flow during fire conditions and method for using same

AIR INTAKE WITH CHANGING WALL THICKNESS AND ASSOCIATED NACELLE

AIRCRAFT PROPULSION SYSTEM WITH VARIABLE AREA INLET ASSEMBLY

Inlet system for auxiliary power unit

Pressure control for bifurcated flow of a turbine engine

ENGINE HAVING AN OPEN FAN WITH REDUCED BOUNDARY LAYER INDUCED DISTORTION

SYSTEMS AND METHODS FOR HYDRAULIC FRACTURING

ENGINE HAVING AN OPEN FAN WITH REDUCED BOUNDARY LAYER INDUCED DISTORTION

AIR INTAKE PLENUM WITH STRUTS

VARIABLE GEOMETRY INLET FOR TURBOPROPELLER INLET PRESSURE RECOVERY OPTIMIZATION

Variable turbine geometry component wear mitigation in radial turbomachines with divided volutes by aerodynamic force optimization at all vanes or only vane(s) adjacent to volute tongue(s)

AIRCRAFT PROPULSION SYSTEM WITH VARIABLE AREA INLET

Hypersonic large internal contraction ratio air inlet channel having stepless adjustable air release valve and control method

Systems and methods for controlling an intake inlet shape of a propulsion system air intake

SYSTEMS, ASSEMBLIES, AND METHODS FOR TREATMENT/FILTRATION OF INTAKE AIR FLOWS TO A GAS TURBINE ENGINE OF A HYDRAULIC FRACTURING UNIT

AIR INTAKE

Method for controlling operation modes of gas turbine system

AIRCRAFT PROPULSION SYSTEM WITH VARIABLE AREA INLET

Aircraft intake duct with passively movable flow restrictor

PROPULSION UNIT FOR AN AIRCRAFT COMPRISING A SYSTEM FOR SEALING BETWEEN TWO AIR INTAKE PARTS

Active clearance control of fan blade tip closure using a variable sleeve system

NACELLE AIR INTAKE FOR AN AIRCRAFT PROPULSION ASSEMBLY TO PROMOTE A THRUST REVERSAL PHASE

ENGINES

Air inlet of a turbomachine nacelle including a circulation conduit of a hot air flow between a movable upstream part and a fixed downstream part

Scoop for an aircraft turbine engine

Turbofan engine with at least one guide vane including a variable-geometry zone

Gas turbine engine with diverter fences

Assembly for a turbomachine

Assembly for a compressor section of a gas turbine engine

Air intake plenum with struts

MOBILE GAS TURBINE INLET AIR CONDITIONING SYSTEM AND ASSOCIATED METHODS

Combined cycle propulsion system for hypersonic flight

Systems and methods for hydraulic fracturing

Aircraft propulsion system with variable area inlet assembly

Mobile gas turbine inlet air conditioning system and associated methods

Cantilevered airfoils and methods of forming the same

Gas turbine engine with improved VIGV shielding

Turbine engine with a flow splitter having a profile with inclined serrations

Multi-mode propulsion system

INTEGRATED GASIFICATION COMBINED CYCLE AND OPERATION METHOD THEREOF

Unison ring of gas turbine engine

Mobile gas turbine inlet air conditioning system and associated methods

Dual-purpose control moment gyroscope for vehicle control

Variable turbine geometry component wear mitigation in radial turbomachines with divided volutes by aerodynamic force optimization at all vanes or only vane(s) adjacent to volute tongue(s)

Propulsion system for an aircraft

Mobile gas turbine inlet air conditioning system and associated methods

SYSTEMS, ASSEMBLIES, AND METHODS TO ENHANCE INTAKE AIR FLOW TO A GAS TURBINE ENGINE OF A HYDRAULIC FRACTURING UNIT

Aircraft propulsion system with variable area inlet

Variable supersonic engine inlet

Airflow control system and methods thereof

Mobile gas turbine inlet air conditioning system and associated methods

Internal-parallel inlet with mode conversion combined with variable geometry adjustment

Aircraft propulsion system with variable area inlet

Aircraft propulsion system with variable area inlet

Bypass turbomachine for an aircraft

Aircraft propulsion system inlet structure with variable airflow inlet area

Aircraft propulsion system with variable area inlet assembly

Method for operating an air intake of a turbojet engine nacelle during a thrust phase and during a reverse thrust phase

Air inlet duct for a nacelle of an aircraft propulsion assembly

Air intake of a turbojet engine nacelle comprising guide vanes

Process for using an air input of a turboreactor nacelle comprising an air input lip which comprises a portion which can be moved to promote a thrust inversion phase

Turbojet comprising a nacelle with an air intake for promoting a reverse thrust phase

Active flow control transpirational flow acoustically lined guide vane

Masking bladed disc for reducing the radar signature of a moving compressor moving disc of a jet engine

System and method for modulating airflow into a bore of a rotor to control blade tip clearance

GAS TURBINE ENGINE WITH PARTIAL INLET VANE

Mobile gas turbine inlet air conditioning system and associated methods

Mobile gas turbine inlet air conditioning system and associated methods

Adaptable flow control for engine nacelles

Inertial particle separator for turbine engine

Mobile gas turbine inlet air conditioning system and associated methods

Inlet guide vane draw heat exchanger system

Variable geometry inlet system

Cam mechanism for variable-geometry caret inlet

Inlet cowl for a turbine engine

RADIAL VARIABLE INLET GUIDE VANE FOR AXIAL OR AXI-CENTRIFUGAL COMPRESSORS

Variable seal for an engine nacelle

Mobile gas turbine inlet air conditioning system and associated methods

Airflow control system and methods thereof

AIRCRAFT TURBOPROP ENGINE INLET COMPACT PROFILE CONFIGURATION

Aircraft comprising a gas turbine engine having an axially adjustable intake and a nacelle

Air intake cover

Compressor inlet adjustment mechanism

Mobile gas turbine inlet air conditioning system and associated methods

Rotorcraft engine inlet configuration to optimize performance in both hover and high speed flight

Turbine engine with a flow splitter having a profile with inclined serrations

Variable Engine Inlet Geometry Algorithm

Single track translating inlet

Nacelle with a translatable inlet for an aircraft propulsion system

Inlet particle separator

Translating inlet for adjusting airflow distortion in gas turbine engine

Turbofan comprising a set of rotatable blades for blocking off the bypass flow duct

Compound helicopters having hybrid propulsion engines

Axial compressor

HYPERSONIC SUPERCONDUCTING COMBUSTION RAM ACCELERATED MAGNETOHYDRODYNAMIC-DRIVE

Mixed-compression inlet duct for turbine engines facilitating supersonic flight

Airflow control system and methods thereof

Fan assembly having flow recirculation circuit with rotating airfoils

CORRECTED FUEL-FLOW-RATE-BASED CONTROL FOR VARIABLE GEOMETRY MECHANISMS

Signal processing for variable geometry mechanism control

Method and system for adjusting a variable geometry mechanism

Guide vane assembly with sealing element

Ramjet engine with rotating detonation combustion system and method for operation

Shapeable inlet manifold for hypersonic scramjet

Debris deflector for a jet engine

Adaptive-area inertial particle separators

Inlet diffusers for jet engines, jet engines, jet aircraft, and methods for diffusing incoming air of jet engines

Adaptive-curvature inertial particle separators

Auxetic bi-stable structure

Air-inlet particle separator having a bleed surface

Foldable RAM air inlet filter

Air intake systems and methods of assembly thereof

Pylon of a propulsion unit

Variable geometry inlet system

GAS TURBINE ENGINE VORTEX SUPPRESSOR

Gas turbine engine with partial inlet vane

Dual function air diverter and variable area fan nozzle

Rotorcraft engine inlet configuration to optimize performance in both hover and high speed flight

STRUCTURAL FRAME INTEGRATED WITH VARIABLE-VECTORING FLOW CONTROL FOR USE IN TURBINE SYSTEMS

Centrifugal compressor for a turbocharger, having synergistic ported shroud and inlet-adjustment mechanism

System and method for variable geometry mechanism control

Inlet bleed heat system for use in a turbine engine

Clearance control device

Translating turning vanes for a nacelle inlet

ROTATING DEVICES FOR MITIGATION OF ADVERSE FLOW CONDITIONS IN AN ULTRA-SHORT NACELLE INLET

High tip speed gas turbine engine

Variable and adaptable diverterless bump inlet

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

LOW NOISE AEROENGINE INLET SYSTEM

Variable stator blade operating device

System and Method for Regulating Flow in Turbomachines

Variable pitch fan blade system

Air intake unit for an aircraft engine and provided with an air filter and with an air filter bypass duct

Nacelle for a turbofan engine

Systems and methods for closed loop control of OBB valve for power generation systems

Systems and methods for controlling overboard bleed heat of a turbine inlet filter

System and method for controlling a position of an auxiliary power unit inlet door

Aircraft comprising a rear fairing propulsion system with inlet stator comprising a blowing function

Fuel control device and control method for a combustor of a gas turbine

Signal processing for auto-tuning a gas turbine engine

RADIAL VARIABLE INLET GUIDE VANE FOR AXIAL OR AXI-CENTRIFUGAL COMPRESSORS

Gas turbine control device and method, non-transitory storage medium, and gas turbine

LOW NOISE AEROENGINE INLET SYSTEM

LOW NOISE AEROENGINE INLET SYSTEM

Power Generation System and Method for Operating Same

GAS TURBINE ENGINE BLEED CONFIGURATION

System and method for turbomachinery rotor and blade prognostics and diagnostics

Systems and methods of reducing distortions of the inlet airflow to a turbomachine

Guide vane assembly with compensation device

Propulsion assembly comprising a duct for feeding the gas generator in an inter-duct casing

Low partial load emission control for gas turbine system

Engine for hypersonic aircrafts with supersonic combustor

Variable geometry helicopter engine inlet

Inlet cowl for a turbine engine

Device and method for gas turbine unlocking

System and method for dynamically controlling the operation of an aircraft

Inlet guide vane control for aircraft single engine operation

Inlet guide vane assembly for reducing airflow swirl distortion of an aircraft aft fan

Device of high-temperature solar turbine power generation with thermal energy storage

Inlet assembly for an aircraft aft fan

Method of extended thermodynamic turbine mapping via compressor inlet throttling

GAS TURBINE ENGINE COMPRISING AN ADJUSTABLE SPINNER

Method for improving turbine compressor performance

VARIABLE STATOR VANE MECHANISM

Jet engine

Method and system for cooling down a gas turbine

Translating inlet for adjusting airflow distortion in gas turbine engine

System and method for actuating gas turbine engine components using integrated jamming devices

Air intake for turboprop engine

Air intake with scroll portion and strutted portion for gas turbine engine

Adjusting Airflow Distortion in Gas Turbine Engine

Gas turbine engine having instrumented airflow path components

Radial turbocharger comprising a swirl generator

Inlet turbine for high-mach engines

Gas turbine inlet guide vane control device, system and control method

Auxiliary power unit inlet apparatus and methods

Mobile multi-mode power generation system with mode based adjustable drag configuration

Gas Turbine Combined Electric Power Generation Apparatus

Methods and apparatus to vary an air intake of aircraft engines

Turbine engine flow path

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

Combined cycle plant, control method of same, and control device of same

Variable vane device maintenance method and variable vane device

Propulsion system

Actuator control

AUXILLARY POWER UNIT ASSEMBLY AND A METHOD OF USING THE SAME

Cooled cooling air system for a turbofan engine

Inlet flow restrictor

Method for operating a gas turbine installation and a gas turbine installation for carrying out the method

Supersonic caret inlet system leading edge slat for improved inlet performance at off-design flight conditions

Jet engine, flying object, and method of operating jet engine

Pitch change mechanism for shrouded fan with low fan pressure ratio

OPERATION OF A GAS TURBINE SYSTEM IN PART LOAD OPERATION

Operation of a gas turbine plant having a compressor and a turbine

TURBINE ENGINE HAVING VARIABLE PITCH OUTLET GUIDE VANES

METHOD FOR CONTROLLING THE TEMPERATURE OF A GAS TURBINE DURING A SHUTDOWN

Variable-capture supersonic inlet

Variable inlet guide vane scheduling

Aircraft power outtake management

Partial-load operation of a gas turbine with an adjustable bypass flow channel

Supersonic caret inlet system

Isentropic compression inlet for supersonic aircraft

METHOD FOR CONTROLLING THE OPERATION OF A GAS TURBINE WITH SEQUENTIAL COMBUSTION

Compound engine assembly with modulated flow

Self-latching piezocomposite actuator

Variable geometry gas turbine engine for use in inclement weather

Articulated diffuser and door for submerged ram air turbine power and cooling control

GAS TURBINE ENGINE INLET

METHOD FOR OPERATING A GAS TURBINE

Gas turbine engine and method of assembling the same

Variable supersonic engine inlet

Adjustable-trim centrifugal compressor, and turbocharger having same

Aircraft turbine engine comprising an air intake housing with a variable aerodynamic profile

Gas turbine engine with partial inlet vane

Device for the extraction of bleed air and aircraft engine with at least one device for the extraction of bleed air

Turbomachine comprising a plurality of fixed radial blades mounted upstream of the fan

Variable geometry inlet for a ducted fan and method of assembling same

Low NOturbine exhaust fuel burner assembly

Structural frame integrated with variable-vectoring flow control for use in turbine systems

Low noise aeroengine inlet system

Low noise aeroengine inlet system

Low noise aeroengine inlet system

Variable geometry inlet system

Adjustable size inlet system

Ventilation inlet

Airflow modulation system and method

Gas turbine engine with fan-tied inducer section

Flow guiding system, turbo engine with a flow guiding system and method for manufacturing a flow guiding system

Dual function air diverter and variable area fan nozzle

Variable geometry helicopter engine inlet

Gas turbine engine inlet assembly and method of making same

Intake arrangement in gas turbine power plant

Gas turbine engine combustor with fluidic control of swirlers

Systems and methods for controlling exhaust gas flow in exhaust gas recirculation gas turbine systems

Gas turbine power plant with exhaust gas recirculation

Gas turbine engine actuation systems including high temperature actuators and methods for the manufacture thereof

HIGH-SPEED-LAUNCH RAMJET BOOSTER

Air intake guide

Variable cycle intake for reverse core engine

ADJUSTABLE SUPERSONIC AIR INLET

Gas-turbine engine with telescope-type air inlet of the engine cowling (nacelle)

Aircraft airflow modulation system and method

Low shock strength inlet

Isentropic compression inlet for supersonic aircraft

Propulsive unit for an aircraft

INLET FLUID FLOW AND IMPINGEMENT ANGLE CONTROL

Low shock strength propulsion system

Laval nozzle

Supersonic aircraft jet engine installation

Cambered aero-engine inlet

Mass flow increase at takeoff in supersonic airliner

Isentropic compression inlet for supersonic aircraft

Isentropic compression inlet for supersonic aircraft

Aviation engine inlet with tangential blowing for buzz saw noise control

Air inlet of an aeroengine having unducted pusher propellers

Double-ducted fan

Tailorable stiffness shape morphing flow-path

TURBINE INLET FLOW MODULATOR

CONVERTIBLE FAN SYSTEM

ADAPTIVE ENGINE

CONVERTIBLE FAN ENGINE

METHOD OF OPERATING A CONVERTIBLE FAN ENGINE

Airflow modulation for dual mode combined cycle propulsion systems

LOCKING SYSTEM FOR AIR INTAKE STRUCTURE FOR TURBOJET ENGINE NACELLE

Inlet Guide Vane for a Gas Compressor

Cambered aero-engine inlet

System for inertial particles separation

Aircraft fluid diversion inlet louver

Gas turbine engine inlet with noise reduction features

Relating to air-breathing flight vehicles

Low shock strength propulsion system

Hypersonic inlet systems and methods

Ventilating air intake arrangement

Fan nacelle flow control

Rotating auxiliary power unit air inlet door

Low shock strength inlet

Systems and methods for altering inlet airflow of gas turbine engines

Systems and Methods for Extending Gas Turbine Emissions Compliance

Device for determining the angular position of a rotatable compressor stator blade

Variable contour nacelle assembly for a gas turbine engine

VARIABLE GEOMETRY GAS TURBINE ENGINE NACELLE ASSEMBLY WITH NANOELECTROMECHANICAL SYSTEM

NACELLE WITH ARTICULATING LEADING EDGE SLATES

Nacelle compartment plenum for bleed air flow delivery system

Variable geometry nacelle assembly for a gas turbine engine

Variable contraction ratio nacelle assembly for a gas turbine engine

Isentropic compression inlet for supersonic aircraft

Nacelle assembly having inlet airfoil for a gas turbine engine