140338 ⎘
Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto; Introducing air inside the jet mixing devices in the jet pipe, e.g. for mixing primary and secondary flow
AIRFLOW MIXER ASSEMBLY FOR A GAS TURBINE ENGINE
#2DISSIMILARLY SHAPED AIRCRAFT NOZZLES WITH TANDEM MIXING DEVICES, AND ASSOCIATED SYSTEMS AND METHODS
#3COOLED VARIABLE AREA NOZZLE FOR AN AIRCRAFT ENGINE
#4DESIGN OF A REAR-CONE EXHAUST DUCT FOR ADDITIVE MANUFACTURING
#5GEARBOX ASSEMBLY WITH LUBRICANT EXTRACTION VOLUME RATIO
#6Exhaust mixer with protrusions
#7AIRCRAFT ENGINE EXHAUST MIXER
#8VARIABLE GEOMETRY THRUSTER
#9Turbine engine with a flow splitter having a profile with inclined serrations
#10Dissimilarly shaped aircraft nozzles with tandem mixing devices, and associated systems and methods
#11VARIABLE GEOMETRY THRUSTER
#12VARIABLE MIXING NOZZLE DESIGN FOR JET NOISE REDUCTION
#13Variable geometry thruster
#14Gas turbine system and movable body including the same
#15Turbine engine separate flow mixer with lobes
#16Gas turbine engine exhaust chevrons
#17Exhaust duct of gas turbine engine
#18Multistage infrared suppression exhaust system
#19Variable area nozzle exhaust system with integrated thrust reverser
#20High temperature gradient gas mixer
#21JET TUBE FOR A TURBOMACHINE
#22Turbine engine with a flow splitter having a profile with inclined serrations
#23Heating system for convergent-divergent secondary nozzle
#24TURBINE EXHAUST CASE MIXER
#25Turbo-shaft ejector with flow guide ring
#26Flow mixer stiffener ring segmented springs
#27Supersonic aircraft turbofan
#28Supersonic aircraft turbofan engine
#29CMC OXIDE-OXIDE MIXER DESIGN
#30Encapsulated flow mixer stiffener ring
#31Nozzle of a turbomachine provided with chevrons with a non-axisymmetric inner face
#32Engine assembly with combined engine and cooling exhaust
#33Turboprop engine assembly with combined engine and cooling exhaust
#34Gas turbine exhaust cooling system
#35Exhaust systems and methods for gas turbine engine
#36HEATING SYSTEM FOR CONVERGENT-DIVERGENT SECONDARY NOZZLE
#37Reinforced oxide-oxide ceramic matrix composite (CMC) component and method of making a reinforced oxide-oxide CMC component
#38Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines
#39Exhaust systems and methods for gas turbine engine
#40Ceramic matrix composite turbine exhaust assembly for a gas turbine engine
#41Flow path routing within a gas turbine engine
#42Exhaust stream mixer
#43Assembly comprising an exhaust case and a downstream rotationally symmetrical part
#44Mixer for an engine manufactured from at least one composite material, manufacturing method and manufacturing device
#45High stiffness shape memory alloy actuated aerostructure
#46Mixer assembly group for a turbofan engine
#47INTEGRATED TURBINE EXHAUST STRUTS AND MIXER OF TURBOFAN ENGINE
#48Variable geometry thruster
#49Gas turbine exhaust assembly
#50Flow segregator for infrared exhaust suppressor
#51Exhaust systems and methods for gas turbine engine
#52Gas turbine engine exhaust ejector/mixer
#53Engine assembly with combined engine and cooling exhaust
#54Compression cowl for jet engine exhaust
#55Exhaust plume cooling using periodic interruption of exhaust gas flow to form ambient air entraining vortices
#56Methods of creating fluidic barriers in turbine engines
#57Turboprop engine assembly with combined engine and cooling exhaust
#58Variable exhaust mixer and cooler for a three-stream gas turbine engine
#59Preloaded AFT vent area for low pressure fan ducts
#60Power generation system exhaust cooling
#61Segmented multi-lobe mixer
#62Integrated TEC/mixer strut axial position
#63Turbine engine nozzle having confluent streams and including a core cowl with overlapping flaps
#64AFTERBODY FOR A MIXED-FLOW TURBOJET ENGINE COMPRISING A LOBED MIXER AND CHEVRONS WITH A NON-AXISYMMETRIC INNER SURFACE
#65Turbomachine flow diverting device and method
#66Nozzle of a turbomachine provided with chevrons with a non-axisymmetric inner face
#67CMC oxide-oxide mixer design
#68Gas turbine engine exhaust mixer
#69Gas turbine engine system for modulating flow of fan by-pass air and core engine air
#70Boot for repair of chevron on nacelle
#71Variable fan nozzle using shape memory material
#72Fairing for a mixer of a nozzle of a dual-flow turbomachine
#73Jet noise suppressor
#74Gas turbine engine ejector
#75Gas turbine engine exhaust ejector/mixer
#76Flow path routing within a gas turbine engine
#77Turbofan engine with variable exhaust cooling
#78Integrated turbine exhaust struts and mixer of turbofan engine
#79Variable exhaust mixer and cooler for a three-stream gas turbine engine
#80High durability turbine exhaust case
#81Flow outlet
#82Exhaust stream mixer
#83Exhaust plume cooling using periodic interruption of exhaust gas flow to form ambient air entraining vortices
#84High durability turbine exhaust case
#85Variable immersion lobe mixer for turbofan jet engine exhaust and method of fabricating the same
#86High durability turbine exhaust case
#87INTEGRATED TURBINE EXHAUST STRUTS AND MIXER OF TURBOFAN ENGINE
#88Long-duct, mixed-flow nozzle system for a turbofan engine
#89Exhaust mixer with offset lobes
#90Nozzle, structural element, and method of producing a nozzle
#91Mixing device and turbofan engine having such mixing device
#92Primary cowl of a turbofan comprising a rotating ring having micro-jets
#93Reduced noise gas turbine engine system and supersonic exhaust nozzle system using elector to entrain ambient air
#94Method of mixing between a primary flow and a secondary flow in a turbine engine, corresponding device and turbine engine
#95Gas turbine engine exhaust mixer
#96Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines
#97Nozzle with guiding devices
#98Nozzle with guiding devices
#99Method for assembling a nozzle and an exhaust case of a turbomachine
#100Pre-turbine engine case variable area mixing plane
#101Gas turbine engine variable area exhaust nozzle
#102Noise-reducing engine nozzle system
#103Method for defining the shape of a turbomachine convergent-divergent nozzle, and corresponding convergent-divergent nozzle
#104Article including ceramic structure
#105Gas turbine engine exhaust diffuser including circumferential vane
#106Turbofan engine mixer assembly
#107Jet flow nozzle and jet engine
#108Turbojet engine outlet lobe mixer with guiding protrusions, and method of mixing airflows
#109Gas turbine engine exhaust nozzle including a plurality of flaps movable over a flow control surface
#110Apparatus and methods for linear actuation of flow altering components of jet engine nozzle
#111FLOW EVACUATION SYSTEM FOR AN AIRCRAFT ENGINE
#112Device for mixing fuel and air of a jet engine
#113POROUS CORE COWLING FOR A TURBOJET ENGINE
#114Morphing structure and method
#115Methods and apparatus for assembling a low noise ejector motive nozzle
#116Turbomachine nozzle cowl having patterns with lateral fins for reducing jet noise
#117Gas turbine engine with variable area fan nozzle
#118Bloom mixer for a turbofan engine
#119SHAPE MEMORY MATERIAL ACTUATION
#120GAS TURBINE ENGINE HAVING CORE AUXILIARY DUCT PASSAGE
#121Gas turbine engine exhaust mixer including circumferentially spaced-apart radial rows of tabs extending downstream on the radial walls, crests and troughs
#122Jet engine exhaust nozzle flow effector
#123Noise control chevron for a nozzle, and nozzle and turboshaft engine provided with such a chevron
#124Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines
#125Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines
#126Inlet bleed heat system with ejector/mixer nozzles for noise reduction
#127Exhaust for a gas turbine engine
#128Noise reduction device for turbojet nacelle with mobile chevrons, and associated nacelle
#129TURBOFAN GAS TURBINE ENGINE AERODYNAMIC MIXER
#130Systems and methods for passively directing aircraft engine nozzle flows
#131Nozzle plasma flow control utilizing dielectric barrier discharge plasma actuators
#132DUAL-FLOW TURBINE ENGINE FOR AIRCRAFT WITH LOW NOISE EMISSION
#133Turbine section architecture for gas turbine engine
#134Gas turbine engine exhaust mixer
#135High stiffness shape memory alloy actuated aerostructure
#136Valve system for a gas turbine engine
#137Gas turbine engine nozzle configurations
#138Deswirling exhaust mixer
#139Turbofan engine noise suppression using fan flow deflector
#140Core reflex nozzle for turbofan engine
#141TURBINE ENGINE EXHAUST GAS TUBE MIXER
#142THERMALLY BALANCED AERO STRUCTURES
#143SYSTEM FOR MIXING GAS FLOWS IN A GAS TURBINE ENGINE, GAS TURBINE ENGINE AND AN AIRCRAFT ENGINE
#144Gas turbine engine variable area exhaust nozzle
#145CMC mixer with structural outer cowling
#146Methods and apparatus for mixing fluid in turbine engines
#147Variable fan nozzle using shape memory material
#148Turbojet Nacelle Equipped With Means For Reducing The Noise Produced By Said Turbojet
#149Nozzle with guiding elements
#150GAS TURBINE COMPRISING A GUIDE RING AND A MIXER
#151Jet flow discharge nozzle and jet engine
#152Morphing structure and method
#153Method of manufacturing a CMC flow mixer lobed structure for a gas turbine aeroengine
#154Systems and methods for reducing noise from jet engine exhaust
#155Duplex tab exhaust nozzle
#156AIRCRAFT PROPULSION UNIT THAT COMPRISES AN EXHAUST PIPE WITH A SCALLOPED TRAILING EDGE
#157Valve system for a gas turbine engine
#158Valve system for a gas turbine engine
#159Sliding ramp nozzle system for a gas turbine engine
#160Gas turbine engine having core auxiliary duct passage
#161TURBOMACHINE NOZZLE COWL HAVING JET NOISE REDUCTION PATTERNS
#162Fluted chevron exhaust nozzle
#163Apparatus and method for reduction of jet noise from single jets
#164Valve assembly for a gas turbine engine
#165Nozzle arrangement for a gas turbine engine
#166Modular chevron exhaust nozzle
#167Integrated support and mixer for turbo machinery
#168Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines
#169Turbofan engine for stol aircraft
#170Jet engine exhaust nozzle flow effector
#171Jet engine nozzle exit configurations, including projections oriented relative to pylons, and associated systems and methods
#172Method for attenuating the noise of a turbofan
#173Fluid mixer with an integral fluid capture ducts forming auxiliary secondary chutes at the discharge end of said ducts
#174Bypass turbomachine with artificial variation of its throat section
#175Systems and methods for passively directing aircraft engine nozzle flows
#176Morphing structure
#177Turbofan engine cowl assembly and method of operating the same
#178Cowling arrangement
#179Turbofan engine nozzle assembly and method for operating the same
#180Rotary motion mixer for a converging-stream nozzle of a turbomachine
#181CURVED LOBE MIXER FOR A CONVERGING-STREAM NOZZLE FOR A TURBOMACHINE
#182Asymmetric serrated nozzle for exhaust noise reduction
#183Turbomachine nozzle cover provided with triangular patterns having pairs of vertices for reducing jet noise
#184Turbomachine nozzle cover provided with triangular patterns having a point of inflexion for reducing jet noise
#185Gas exhaust nozzle for a bypass turbomachine having an exhaust or throat section that can be varied by moving the secondary cowl
#186Methods and apparatus for assembling a low noise ejector motive nozzle
#187Valve assembly for a gas turbine engine
#188Exhaust dust flow splitter system
#189Eductor swirl buster
#190Serrated nozzle trailing edge for exhaust noise suppression
#191Infrared suppressor apparatus and method
#192Quiet airplane configuration
#193Jet nozzle mixer
#194Gas turbine engine and method of operating same
#195Turbofan core thrust spoiler
#196Turbine exhaust case and method of making
#197Jet nozzle mixer
#198Compact mixer with trimmable open centerbody
#199Shape changing structure
#200Twisted mixer with open center body
#201Morphing structure
#202Reduced noise jet engine
#203Quiet chevron/tab exhaust eductor system
#204Split shroud exhaust nozzle
#205Turbomachine nozzle cover for reducing jet noise
#206Turbine exhaust case and method of making
#207Shape memory material actuation
#208Ventilation channels in an afterburner chamber confluence sheet
#209Method of improving the ignition performance of an after-burner device for a bypass turbojet, and an after-burner device of improved ignition performance
#210Apparatus and method for reduction jet noise from single jets
#211Thrust, with or without the ejection of propellant
#212Methods and apparatus for operating gas turbine engines
#213Jet exhaust noise reduction system and method
#214Sinuous chevron exhaust nozzle
#215Device for reducing the jet noise of a turbomachine
#216Aft FLADE engine
#217Selectable inlet for aircraft propulsion system heat exchanger
#218Rotatably driven exhaust mixer