72609 ⎘
Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
Sub-classes:CONDUIT SYSTEMS AND METHODS
#2BIFURCATED EXHAUST DUCT FOR HYBRID AIRCRAFT POWERPLANT
#3FLUIDIC PROPULSIVE SYSTEM
#4OPEN ROTOR PROPULSION SYSTEM WITH EXHAUST MIXER(S)
#5TURBO-COMPOUNDED ENGINE WITH EXHAUST DUCT ACOUSTIC ARRANGEMENT
#6METHOD AND SYSTEM FOR THERMAL MANAGEMENT
#7THERMALLY PROTECTED POLYMER COMPOSITES AND ASSOCIATED METHODS
#8AIRCRAFT TAIL JET ANTI-STALL SYSTEM
#9GAS TURBINE ENGINE EXHAUST NOZZLE
#10Unducted Thrust Producing System
#11COOLING OF GAS FLOWING OVER AIRCRAFT STRUCTURE
#12FLUIDIC PROPULSIVE SYSTEM AND THRUST AND LIFT GENERATOR FOR AERIAL VEHICLES
#13COOLED VARIABLE AREA NOZZLE FOR AN AIRCRAFT ENGINE
#14ENERGY CONVERSION ARRANGEMENT, ENERGY SYSTEM AND AIRCRAFT COMPRISING SAME
#15ENERGY CONVERSION ARRANGEMENT, ENERGY SYSTEM AND AIRCRAFT COMPRISING SAME
#16DESIGN OF A REAR-CONE EXHAUST DUCT FOR ADDITIVE MANUFACTURING
#17CONFIGURATION FOR VERTICAL TAKE-OFF AND LANDING SYSTEM FOR AERIAL VEHICLES
#18CONFIGURATION FOR VERTICAL TAKE-OFF AND LANDING SYSTEM FOR AERIAL VEHICLES
#19MECHANISM FOR CONNECTING HIGH TEMPERATURE AIR DUCTING FOR AIRCRAFT ENGINE
#20PROPULSION ASSEMBLY FOR AN AIRCRAFT
#21PROPULSION ASSEMBLY FOR AN AIRCRAFT
#22AIRCRAFT
#23EXHAUST NOZZLE ASSEMBLY FOR AIRCRAFT PROPULSION SYSTEM
#24EXHAUST NOZZLE ASSEMBLY FOR AIRCRAFT PROPULSION SYSTEM
#25DEFLECTOR EXHAUST NOZZLE FOR AS350/EC130 AND FOR OTHER SINGLE ENGINE HELICOPTERS
#26ELECTRIC FAN AND ELECTRIC AIRCRAFT
#27TURBO-COMPOUNDED ENGINE WITH EXHAUST DUCT ACOUSTIC ARRANGEMENT
#28DRAG RECOVERY SCHEME USING BOUNDARY LAYER INGESTION
#29AIRCRAFT
#30VERTICAL TAKEOFF AND LANDING AIRCRAFT
#31PROPULSION ASSEMBLY COMPRISING A FUEL CONDITIONING SYSTEM POSITIONED BEHIND A DEBRIS EJECTION ZONE, AIRCRAFT COMPRISING AT LEAST ONE SUCH PROPULSION ASSEMBLY
#32POWER UNIT
#33Exhaust mounting mechanism
#34AFT AIR INLET PARTICLE SEPARATOR FOR TURBINE ENGINE
#35FLUIDIC PROPULSIVE SYSTEM
#36Fluidic propulsive system and thrust and lift generator for aerial vehicles
#37EXHAUST DUCT FOR HYBRID AIRCRAFT POWERPLANT
#38AIRCRAFT PROVIDED WITH AN ENGINE AND AN EXHAUST DUCT AROUND AN EXHAUST NOZZLE OF THE ENGINE
#39METHOD AND SYSTEM FOR THERMAL MANAGEMENT
#40EJECTOR AND AIRFOIL CONFIGURATIONS
#41AIRCRAFT ENGINE WITH EXHAUST HAVING REMOVABLE DEFLECTOR
#42CONFIGURATION FOR VERTICAL TAKE-OFF AND LANDING SYSTEM FOR AERIAL VEHICLES
#43Configuration for vertical take-off and landing system for aerial vehicles
#44EXHAUST SYSTEMS HAVING ADJUSTABLE NOZZLES AND RELATED METHODS
#45AIRCRAFT PROVIDED WITH AN ENGINE AND AN EXHAUST DUCT THAT IS DRAINED AROUND AN EXHAUST NOZZLE OF THE ENGINE
#46Exhaust nozzle assembly for an aircraft propulsion system
#47Extracting water vapor from a powerplant exhaust
#48Exhaust nozzle assembly, propulsion system employing the exhaust nozzle assembly, and aircraft employing the propulsion system
#49Aircraft engine, gas turbine intake therefore, and method of guiding exhaust gasses
#50Exhaust duct assembly and aircraft including the same
#51SYSTEMS AND METHODS FOR MULTI-MODULE CONTROL OF A HYDROGEN POWERED HYBRID ELECTRIC POWERTRAIN
#52Combined cycle propulsion system for hypersonic flight
#53MULTILAYER TUBULAR DUCT AND MANUFACTURING METHOD
#54Aircraft having a single fluid inlet aperture
#55Aircraft assembly fitted with at least one hydrogen-powered thrust reverser actuation system
#56Flow aperture method and apparatus
#57Fuselage for an aircraft with fuselage-integrated tailplane
#58Aircraft having a heat engine and device for using the exhaust gases from the heat engine
#59Aircraft propulsion assembly comprising a plate heat exchanger, of hexagonal longitudinal section, positioned in a bifurcation
#60EXHAUSTING OF HOT GASES FROM WITHIN AN AIRCRAFT
#61Aircraft with a combustion engine having an exhaust ahead of its air intake
#62Heat shield assembly for use with an aircraft engine
#63Variable area exhaust nozzle system and method for control thereof
#64PROPULSION ASSEMBLY FOR AN AIRCRAFT
#65Aircraft and direct drive engine under wing installation
#66GAS GENERATOR BIFURCATING EXHAUST DUCT TO FREE TURBINE
#67Means for handling gaseous fuel
#68Encased exhaust
#69AERIAL VEHICLE
#70Aircraft engine comprising a variable area exhaust nozzle
#71Drag recovery scheme using boundary layer ingestion
#72Hybrid air mobility system
#73Aircraft laser contrail reduction apparatus and system
#74EXHAUST WATER VAPOR MANAGEMENT FOR HYDROGEN FUEL CELL-POWERED AIRCRAFT
#75Optimised nozzle geometry
#76Engine comprising a movable aerodynamic component
#77Internal structure for a turbomachine nacelle
#78Tail cone mounted generator input shaft for an aircraft
#79Method for thermal management for an aircraft propulsion system using a flow of compressed fluid extracted from a compressor section
#80Aircraft with an offset nacelle aligned with the wake of the wing
#81Aircraft
#82Systems and methods for multi-module control of a hydrogen powered hybrid electric powertrain
#83Rotorcraft with cooling anti-torque system
#84DEFLECTOR EXHAUST NOZZLE FOR AS350/EC130 AND FOR OTHER SINGLE ENGINE HELICOPTERS
#85Modular Device For Propulsion In A Vehicle
#86Turbofan gas turbine engine
#87Aircraft with a single fluid inlet aperture
#88Aircraft engines with a fuel cell
#89Air cooling
#90Configuration for vertical take-off and landing system for aerial vehicles
#91Nacelle
#92Systems and methods for multi-module control of a hydrogen powered hybrid electric powertrain
#93Propulsion system arrangement for turbofan gas turbine engine
#94Multistage infrared suppression exhaust system
#95FLUIDIC PROPULSIVE SYSTEM AND THRUST AND LIFT GENERATOR FOR AERIAL VEHICLES
#96Drag recovery scheme using boundary layer ingestion
#97Turbine engine secondary ejector system
#98Engine bleed power recovery systems and related methods
#99Vertical takeoff and landing aircraft
#100Rotatable nacelle for centrifugal fan on aircraft
#101Motor-integrated fan, and vertical takeoff and landing craft
#102Solid oxide fuel cell modular hybrid powertrain for small unmanned aircraft system (UAS)
#103Exhaust nozzle assembly, propulsion system employing the exhaust nozzle assembly, and aircraft employing the propulsion system
#104COMMERCIAL SUPERSONIC AIRCRAFT AND ASSOCIATED SYSTEMS AND METHODS
#105COMMERCIAL SUPERSONIC AIRCRAFT AND ASSOCIATED SYSTEMS AND METHODS
#106COMMERCIAL SUPERSONIC AIRCRAFT AND ASSOCIATED SYSTEMS AND METHODS
#107Ducted fans having fluidic thrust vectoring
#108Ducted fans having edgewise flow augmentation
#109Fluidic roll control systems for use in forward flight
#110Low observable aircraft having trinary lift fans
#111Low observable aircraft having tandem longitudinal lift fans
#112Fluidic yaw control systems for use in hover
#113Fluidic pitch control systems for use in forward flight
#114Exhaust cone with flexible fitting
#115Long-fibre-reinforced-joints-composite thrust reverser cascade
#116Gas turbine engine with axial movable fan variable area nozzle
#117Mechanically-distributed propulsion drivetrain and architecture
#118Exhaust nozzle with vane support structure for a gas turbine engine
#119Aircraft propulsion assembly having a ventilation system
#120Electrical power generation from turbine engines
#121EXHAUST-GAS TREATMENT DEVICE, AIRCRAFT PROPULSION SYSTEM, AND METHOD FOR TREATING AN EXHAUST-GAS STREAM
#122Outlet of a hot-gas pipe of an aircraft engine passing through an engine wall
#123EDUCTOR HOUSING WITH LOBED PLENUM DIVIDER
#124Flexible aft cowls for aircraft
#125Flight systems
#126COMMERCIAL SUPERSONIC AIRCRAFT AND ASSOCIATED SYSTEMS AND METHODS
#127Variable thrust catapult
#128Nozzle-to-engine mount reinforcement through which mounting fasteners are visible
#129Dual hybrid propulsion system for an aircraft having a cross-connecting clutch
#130Flying vehicle and propulsion device thereof
#131Passive internal compartment exhaust for an aircraft propulsion system
#132Aircraft engine exhaust systems enabling reduced length aft strut fairings
#133Lightweight parallel combustion lift system for vertical takeoff aircraft
#134Electrical generation from turbine engines
#135Vertical take off and landing aircraft
#136AIRSKI EVTOL PAV WITH INTEGRATED DUCTED-FAN FAIRING
#137Reducing contrails during operation of aircraft
#138Nacelle
#139High Speed Aircraft Flight Technologies
#140Integrated electric propulsion assembly
#141Method to re-loft a redesigned jet engine primary exhaust nozzle for an existing airplane to provide clearance to aircraft heat shield structure to prevent contact, fracture, and liberation of portions of the nozzle which might cause hazard to continued safe flight
#142FLUIDIC PROPULSIVE SYSTEM
#143Winglet ejector configurations
#144Configuration for vertical take-off and landing system for aerial vehicles
#145Aircraft nacelle having electric motor and thrust reversing air exhaust flaps
#146Power supply storage and fire management in electrically-driven aircraft
#147Compound helicopters having hybrid propulsion engines
#148Systems and apparatus to generate electrical power from aircraft engine heat
#149Aircraft having embedded engines
#150Temperature control device for tail cone mounted generator
#151Shockwave mitigation system for supersonic aircraft
#152Linkage assembly preventing axial rotation of the link rod for a gas turbine engine
#153OPTIMIZED GAS TURBINE ENGINE FOR AIRCRAFT
#154Aircraft propulsion system including a heat exchanger system
#155Heat shield for signature suppression system
#156Power supply device and flying body
#157Leading-edge slat for an aircraft
#158Slat-thrust reverser clearance
#159Aircraft refrigeration system having a motor-assisted cabin exhaust air turbine
#160Aircraft assembly with a hot-air exhaust outlet and cooperating vortex generator, and method controlling same
#161Blocker door pressure relief systems and methods
#162STRUCTURE, SUSPENSION SYSTEM, ENGINE ASSEMBLY AND AIRCRAFT
#163Mechanically-distributed propulsion drivetrain and architecture
#164Engine Exhaust Suppressor
#165Aircraft with electric propulsor
#166Geared turbofan gas turbine engine mounting arrangement
#167Propulsion system arrangement for turbofan gas turbine engine
#168Jet engine comprising a nacelle equipped with reverser flaps provided with vortex-generating means
#169Nacelle system and methods of operation
#170Supersonic aircraft turbofan
#171Air supply system for an aircraft
#172Anti-ice system exhaust air disruptor
#173HYDROGEN AFTER BURNER
#174Fluidic propulsive system and thrust and lift generator for aerial vehicles
#175Pressure recovery device for an aircraft engine air intake
#176Engine exhaust-stack plug
#177System including telescoping hidden drag link assembly for actuating blocker door of thrust reverser
#178AIRCRAFT, AND AIRCRAFT MAINTENANCE METHOD
#179Aircraft propulsion system with a low-fan-pressure-ratio engine in a forward over-wing flow installation, and method of installing the same
#180Nacelle
#181Aircraft propulsion system comprising an internal fixed structure with a discharge slot
#182Aircraft system with distributed propulsion
#183Duct support
#184PROPULSION SYSTEM FOR AN AIRCRAFT, A NOZZLE FOR USE WITH THE PROPULSION SYSTEM, AND A METHOD OF MANUFACTURING A PROPULSION SYSTEM FOR AN AIRCRAFT
#185Gas turbine engine exhaust component
#186Heat shield assembly and mounting thereof on aircraft
#187NACELLE EQUIPPED WITH A REVERSER SYSTEM COMPRISING DOORS AND SYSTEMS FOR LOCKING THE DOORS IN THE STOWED POSITION
#188Aircraft propulsion assembly comprising two adjacent engines, of which the outlet nozzles have a straight portion in the vicinity of a median plane of the propulsion assembly
#189Moveable aircraft cowl and bypass section
#190NACELLE FOR AN AIRCRAFT POWER UNIT
#191Electrical power supply device in an aircraft, and a method of cooling the device
#192Turboprop engine assembly with combined engine and cooling exhaust
#193Fluidic propulsive system and thrust and lift generator for aerial vehicles
#194Deployable assembly for a propulsor
#195Internal structure of a primary exhaust duct
#196Floating ducts
#197Devices and methods for exhaust vectoring in tilt rotor aircraft
#198Gas turbine exhaust cooling system
#199Seal system for variable geometry gaps in aircraft systems
#200Fluidic propulsive system and thrust and lift generator for aerial vehicles
#201Fluidic propulsive system and thrust and lift generator for aerial vehicles
#202LIFTING BODY VTOL AIRCRAFT
#203Gas turbine engine with axial movable fan variable area nozzle
#204Automated takeoff system for an aircraft
#205Mounting device with pin actuator
#206Drive device for an aircraft
#207Linkage assembly preventing axial rotation of the link rod
#208Operation of a vertical takeoff and landing aircraft
#209Vertical takeoff and landing aircraft
#210Vertical takeoff and landing aircraft having a diffusion assembly for lift fan(s)
#211Vertical takeoff and landing aircraft
#212Vertical takeoff and landing aircraft
#213Ejector and airfoil configurations
#214Vertical takeoff and landing aircraft
#215Vertical takeoff and landing aircraft
#216Aircraft propulsion unit having thrust reverser flaps connected to an inter-compressor casing located between the engine compressors
#217Heat shield for signature suppression system
#218Nacelle
#219Nacelle
#220SYSTEM FOR PREVENTING EXHAUST GAS IMPINGEMENT ON AIRCRAFT SURFACES AND SURROUNDING AREAS
#221Vertical takeoff and landing aircraft having a forward thrust propulsor
#222VTOL vehicle with fan blades outside of exhaust flowpath
#223Vertical takeoff and landing aircraft
#224Vertical takeoff and landing aircraft
#225Actuator for use in aircraft
#226TURBOFAN ENGINE
#227System and method of operating a ducted fan propulsion system during aircraft taxi
#228Jet engine comprising a nacelle equipped with reverser flaps
#229EXHAUST STUB FOR AN AIRCRAFT ENGINE ASSEMBLY
#230Configuration for vertical take-off and landing system for aerial vehicles
#231ELECTRIC TAXIING SYSTEM OF AIRCRAFT AND METHOD FOR CONTROLLING THE SYSTEM
#232Exhaust arrangement for aircraft having sensor
#233Aft fan counter-rotating turbine engine
#234CORE COWL AFTER-BODY
#235Aircraft and flight control mechanisms used on aircraft
#236Flight control mechanisms and methods of operating aircraft with flight control mechanisms
#237Engine exhaust duct mounting assembly
#238Aircraft and direct drive engine under wing installation
#239Multi-layer thermal insulator apparatus and methods
#240EJECTOR AND AIRFOIL CONFIGURATIONS
#241Nacelle
#242Configuration for vertical take-off and landing system for aerial vehicles
#243Mechanically attached thermal protection system
#244DEVICE FOR ALTERING INFRARED SIGNATURE OF AN EXHAUST DUCT AND METHOD OF ALTERING AN INFRARED SIGNATURE OF AN EXHAUST DUCT
#245Hydraulic control system for a thrust reverser comprising a data concentrator module
#246Aircraft with multiple fan propulsion assembly fixed under the wing
#247Above-bed goose neck towing apparatus
#248Convergent-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
#249Load distribution panel assembly, system and method
#250System for reducing the installation noise of an aeroplane wing
#251Thrust reverser actuating
#252Aircraft comprising a propulsion assembly including a fan on the rear of the fuselage
#253SUPPLY DEVICE FOR AN ELECTRIC ACTUATOR SYSTEM
#254Exhaust stream mixer
#255Composite fan cowl having core with varying thickness
#256LOW INFRARED SIGNATURE EXHAUST THROUGH ACTIVE FILM COOLING ACTIVE MIXING AND ACITVE VANE ROTATION
#257Airplane with angled-mounted turboprop engine
#258Commercial supersonic aircraft and associated systems and methods
#259Fan nacelle trailing edge
#260SYSTEM AND METHOD FOR REDUCTION OF TURBINE EXHAUST GAS IMPINGEMENT ON ADJACENT AIRCRAFT STRUCTURE
#261Thrust reverser for a nacelle of an aircraft turbojet engine
#262Rotating proprotor arrangement for a tiltrotor aircraft
#263Unmanned aerial vehicle
#264Deployable assembly for a propulsor
#265Heat shield flange sliding joint
#266GAS GENERATOR BIFURCATING EXHAUST DUCT TO FREE TURBINE
#267Gas turbine engine with axial movable fan variable area nozzle
#268Exhaust duct for turbine forward of fan
#269Direct drive aft fan engine
#270Propulsion system arrangement for turbofan gas turbine engine
#271Gas turbine engine with axial movable fan variable area nozzle
#272Sliding joint kits, systems containing the same, and related methods
#273Nacelle
#274Method for producing an ablative resin
#275Integrated aircraft cooling system
#276Gas turbine engine with axial movable fan variable area nozzle
#277Method for producing an ablative resin
#278Laser Projected Engine Hazard Zone Systems And Methods
#279Shockwave mitigation system for supersonic aircraft
#280Short rejected takeoff system and method
#281Aircraft turbojet engine nacelle
#282Tiltwing aircraft
#283WINGLET EJECTOR CONFIGURATIONS
#284Thrust recovery outflow valves for use with aircraft
#285Directional control system and method of providing directional control
#286Structure for anti-adhesion of high-temperature air to airframe, and aircraft
#287Configuration for vertical take-off and landing system for aerial vehicles
#288Tandem thrust reverser with sliding rails
#289Actuated outlet door for aircraft high-temperature exhaust
#290Thrust reverser actuating
#291Thrust reverser compression rod with spring biased engagement
#292EMERGENCY RUNWAY
#293Thrust reverser cascade systems and methods
#294THRUST REVERSER
#295Aircraft with a hot air exhaust that comprises two pivotally mounted exhaust sections
#296Thrust reverser system with translating elements
#297Method and system for optimized production of non-propulsive energy
#298EXHAUST NOZZLE FOR GAS TURBINE ENGINE
#299Variable-geometry ducted fan
#300Hybrid exhaust nozzle