140342 ⎘
Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto Nozzles having means for adding air to the jet or for augmenting the mixing region between the jet and the ambient air, e.g. for silencing
Sub-classes:ADAPTIVE FLUIDIC PROPULSIVE SYSTEM
#2DISSIMILARLY SHAPED AIRCRAFT NOZZLES WITH TANDEM MIXING DEVICES, AND ASSOCIATED SYSTEMS AND METHODS
#3UNDUCTED THRUST PRODUCING SYSTEM ARCHITECTURE
#4ADAPTIVE FLUIDIC PROPULSIVE SYSTEM
#5Thrust enhancing device
#6Gas turbine engine with third stream
#7Aircraft propulsion system exhaust nozzle with ejector passage(s)
#8TURBOMACHINE EXHAUST CASE
#9PROPULSION SYSTEM FOR A GAS TURBINE ENGINE
#10Dissimilarly shaped aircraft nozzles with tandem mixing devices, and associated systems and methods
#11Inlet for unducted propulsion system
#12METHODS AND SYSTEMS OF MITIGATING HIGH-SPEED JET NOISE
#13ADAPTIVE FLUIDIC PROPULSIVE SYSTEM
#14THREE-STREAM GAS TURBINE ENGINE WITH EMBEDDED ELECTRIC MACHINE
#15LOBED MIXER NOZZLES FOR SUPERSONIC AND SUBSONIC AIRCRAFT, AND ASSOCIATED SYSTEMS AND METHODS
#16Supersonic aircraft and method of reducing sonic booms and jet noise
#17SHEARED EXHAUST NOZZLE
#18Systems and methods for supressing noise from an aircraft engine
#19Exhaust nozzle with centerbody support structure for a gas turbine engine
#20Reducing contrails during operation of aircraft
#21Heating system for convergent-divergent secondary nozzle
#22Unducted thrust producing system architecture
#23Unducted thrust producing system
#24Sheared exhaust nozzle
#25Modified acoustic secondary nozzle
#26Propulsion system for an aircraft, a nozzle for use with the propulsion system, and a method of manufacturing a propulsion system for an aircraft
#27GAS TURBINE ENGINE
#28Exhaust nozzle assembly
#29Vortex generators for turbine engine exhaust
#30Jet noise suppressor
#31TURBOFAN ENGINE
#32Directionally targeted jet noise reduction system and method
#33Nozzle of a turbomachine provided with chevrons with a non-axisymmetric inner face
#34Unducted thrust producing system
#35Fan cowl with a serrated trailing edge providing attached flow in reverse thrust mode
#36Swirling flow eductor system and method
#37STRUCTURAL FRAME INTEGRATED WITH VARIABLE-VECTORING FLOW CONTROL FOR USE IN TURBINE SYSTEMS
#38Convergent-divergent nozzle for a turbofan engine of a supersonic aircraft and method for adjusting the nozzle throat surface in a nozzle of a turbofan engine
#39VENT NOZZLE SHOCKWAVE CANCELLATION
#40Method and apparatus for variable supplemental airflow to cool aircraft components
#41RAMBURNING ENGINE WITH INLET TURBINE
#42Coanda device for a round exhaust nozzle
#43CHEVRON SYSTEM FOR GAS TURBINE ENGINE
#44Exhaust plume cooling using periodic interruption of exhaust gas flow to form ambient air entraining vortices
#45System and method for creating a fluidic barrier with vortices from the upstream splitter
#46Variable exhaust mixer and cooler for a three-stream gas turbine engine
#47Systems and methods for restricting movement in flexible ducts
#48Turbine engine nozzle having confluent streams and including a core cowl with overlapping flaps
#49Nozzle of a turbomachine provided with chevrons with a non-axisymmetric inner face
#50Gas turbine engine system for modulating flow of fan by-pass air and core engine air
#51Variable fan nozzle using shape memory material
#52Jet noise suppressor
#53System and method for improved thrust reverser with increased reverse thrust and reduced noise
#54Air inlet arrangement and method of making the same
#55Heat exchanger arrangement for turbine engine
#56Core cowl for a turbofan engine
#57Structural frame integrated with variable-vectoring flow control for use in turbine systems
#58Vane assembly for an unducted thrust producing system
#59Repair of surface damage at edges of cellular panels
#60Methods and apparatus for passive thrust vectoring and plume deflection
#61System of support thrust from wasted exhaust
#62Unducted thrust producing system architecture
#63Unducted thrust producing system
#64Variable exhaust mixer and cooler for a three-stream gas turbine engine
#65Variable area exhaust mixer for a gas turbine engine
#66Exhaust plume cooling using periodic interruption of exhaust gas flow to form ambient air entraining vortices
#67Flow control device for a three stream turbofan engine
#68Methods and apparatus for passive thrust vectoring and plume deflection
#69Variable immersion lobe mixer for turbofan jet engine exhaust and method of fabricating the same
#70Exhaust nozzle and method for changing exhaust flow path
#71Long-duct, mixed-flow nozzle system for a turbofan engine
#72Tail cone for a microjet rotary turbine engine
#73Nozzle, structural element, and method of producing a nozzle
#74Mixing device and turbofan engine having such mixing device
#75Gas turbine exhaust noise reduction
#76GAS TURBINE ENGINE EXHAUST MIXER WITH AERODYNAMIC STRUTS
#77Primary cowl of a turbofan comprising a rotating ring having micro-jets
#78Nozzle with guiding devices
#79Nozzle with guiding devices
#80Infrared suppressing exhaust system
#81Panel for the acoustic treatment comprising hot air ducts and at least one stabilization chamber
#82Exhaust nozzle of a gas turbine engine
#83Turbojet engine nacelle with variable ventilation outlet cross section
#84Jet noise reduction using eduction effect
#85Noise-reducing engine nozzle system
#86Method for defining the shape of a turbomachine convergent-divergent nozzle, and corresponding convergent-divergent nozzle
#87Nozzle arrangement and method of making the same
#88Jet flow nozzle and jet engine
#89Turbojet engine outlet lobe mixer with guiding protrusions, and method of mixing airflows
#90Device for reducing the noise emitted by the jet of an aircraft propulsion engine
#91Air inlet arrangement and method of making the same
#92Gas turbine engine exhaust nozzle including a plurality of flaps movable over a flow control surface
#93Eductor exhaust silencer assembly with bypass gasflow
#94FLOW EVACUATION SYSTEM FOR AN AIRCRAFT ENGINE
#95POROUS CORE COWLING FOR A TURBOJET ENGINE
#96Noise reduction system
#97Fluid-cooling device for a turbine engine propulsive unit
#98Noise reduction system with chamber
#99Aircraft jet engine comprising a system for reducing the noise generated by the ejection of the gases
#100Jet nozzle mixer
#101Arrangement for controlling fluid jets injected into a fluid stream of a bleed air discharge nozzle
#102Inlet bleed heat system with ejector/mixer nozzles for noise reduction
#103Arrangement for controlling fluid jets injected into a fluid stream
#104Nozzle plasma flow control utilizing dielectric barrier discharge plasma actuators
#105Device for reducing noise generated by an aircraft jet engine with curve ducts
#106Device with secondary jets reducing the noise generated by an aircraft jet engine
#107Systems and methods for reducing noise from jet engine exhaust
#108Noise reducing device and jet propulsion system
#109Trailing edge for an aircraft engine, of the type with moving chevrons
#110Aircraft jet engine provided with a device for reducing propulsion jet noise
#111Dual flow turboshaft engine and improved hot flow nozzle
#112Engine noise
#113Method and apparatus for affecting a recirculation zone in a cross flow
#114Device with plane jets for reducing the noise generated by an aircraft engine
#115Gas turbine engine with variable area fan nozzle
#116Variable fan nozzle using shape memory material
#117Turbojet Nacelle Equipped With Means For Reducing The Noise Produced By Said Turbojet
#118Systems and methods for reducing noise from jet engine exhaust
#119System, method and apparatus for fluidic effectors for enhanced fluid flow mixing
#120Variable area nozzle assisted noise control of a gas turbine engine
#121Gas discharge device for a vehicle engine
#122Heat exchanger arrangement for turbine engine
#123Fan nozzle of adjustable section
#124Bypass turbomachine with reduction of jet noise
#125Arrangement for controlling fluid jets injected into a fluid stream
#126Modular chevron exhaust nozzle
#127Integrated support and mixer for turbo machinery
#128Jet engine nozzle exit configurations, including projections oriented relative to pylons, and associated systems and methods
#129Turbojet engine with attenuated jet noise
#130Arrangement for controlling fluid jets injected into a fluid stream
#131Stator for a jet engine, a jet engine comprising such a stator, and an aircraft comprising the jet engine
#132Localized arc filament plasma actuators for noise mitigation and mixing enhancement
#133Wet active chevron nozzle for controllable jet noise reduction
#134Adjustment assembly
#135Serrated nozzle trailing edge for exhaust noise suppression
#136Jet nozzle mixer
#137Arrangement for controlling fluid jets injected into a fluid stream
#138Jet nozzle mixer
#139Turbomachine nozzle cover for reducing jet noise
#140Localized arc filament plasma actuators for noise mitigation and mixing enhancement
#141Jet nozzle mixer
#142Jet nozzle mixer
#143Gas turbine engine exhaust nozzle
#144Axial divergent section slot nozzle
#145Method and apparatus for operating gas turbine engines
#146Confluent exhaust nozzle
#147Gas turbine engine exhaust nozzle having a noise attenuation device driven by shape memory material actuators
#148Aircraft turbine engine and an air ejection assembly for use therewith