248431 ⎘
Fluid handling Highspeed fluid intake means [e.g., jet engine intake]
Sub-classes:Internal-parallel inlet with mode conversion combined with variable geometry adjustment
#2Fiber-reinforced aircraft component and aircraft comprising same
#3Fiber-reinforced aircraft component and aircraft comprising same
#4Jet engine with deflector
#5Inlet particle separator systems and methods
#6Variable geometry helicopter engine inlet
#7Fluid system
#8Inlet particle separator systems and methods
#9Isentropic compression inlet for supersonic aircraft
#10Air inlet arrangement and method of making the same
#11Energy-deposition systems, equipment and methods for modifying and controlling shock waves and supersonic flow
#12Variable vane and seal arrangement
#13Gas turbine inlet
#14Method for manufacturing a structure with cellular cores for a turbojet nacelle
#15Fluid intake system
#16Aircraft turbofan comprising an intermediate ring with simplified downstream support
#17Engine inlet duct installation
#18Nacelle inlet lip skin with pad-up defining a developable surface having parallel ruling lines
#19Variable geometry helicopter engine inlet
#20Gas turbine engine inlet wall design
#21Jet engine with deflector
#22Dual inlets for a turbofan precooler
#23Angled inlet system for a precooler
#24Engine mounted inlet plenum for a rotorcraft
#25Suprression of shock-induced airflow separation
#26Air inlet structure for a turbojet engine nacelle of laminar type
#27Splitter nose with a sheet that forms a surface to guide the flow and acts as a de-icing duct
#28Rotational annular airscrew with integrated acoustic arrester
#29Passive boundary layer bleed system for nacelle inlet airflow control
#30Air intake guide
#31Airplane including means for taking at least a portion of the boundary layer of the flow of air over a surface
#32Gas turbine engine exhaust fluid passage duct
#33Aircraft nacelle comprising a reinforced connection between an air intake and a powerplant
#34Structural element of an air vehicle air intake composed of an array of passages with a hexagonal cross section
#35Inlet section of an aircraft engine nacelle
#36Nacelle scoop inlet
#37Integrated thermal protection and leakage reduction in a supersonic air intake system
#38Nacelle with longitudinal translating cowling and rotatable sleeves
#39Exhaust pulse energy divider
#40Airfoils for wake desensitization and method for fabricating same
#41Nacelle
#42Isentropic compression inlet for supersonic aircraft
#43Ram air fan inlet housing
#44Air intake with double inlet door
#45Conformal inlet apparatus for a gas turbine engine
#46Low shock strength propulsion system
#47Supersonic aircraft jet engine installation
#48Air inlet arrangement and method of making the same
#49Pressure influencing assembly for an aircraft auxiliary system
#50Cambered aero-engine inlet
#51Flow body, in particular for aircraft
#52Supersonic engine inlet diffuser with deployable vortex generators
#53Reinforcement members for aircraft propulsion system components configured to address delamination of the inner fixed structure
#54Compression ramp boundary layer removal
#55JET ENGINE NACELLE REAR ASSEMBLY
#56Device For Ventilating A Compartment
#57Isentropic compression inlet for supersonic aircraft
#58Air inlet for aircraft propulsion unit having a structure resistant to excess pressure and a process for repairing an air inlet of an aircraft propulsion unit
#59LEADING EDGE STRUCTURE, IN PARTICULAR FOR THE AIR INTAKE OF THE NACELLE OF AN AIRCRAFT ENGINE
#60Turbomachine nozzle cowl having patterns with lateral fins for reducing jet noise
#61Aircraft cover including means for limiting the scoop phenomena of pneumatic type
#62AIRCRAFT COVER INCLUDING MEANS FOR LIMITING THE SCOOP PHENOMENA OF ELECTROMAGNETIC TYPE
#63Isentropic compression inlet for supersonic aircraft
#64Aircraft nacelle including at least one radial partition between two conducts
#65Aircraft nacelle including a rear frame inclined to the rear
#66Acoustic processing panel, more particularly adapted for an air intake in an aircraft nacelle
#67Aircraft nacelle comprising a reinforced outer wall
#68Wrought and cast aluminum alloy with improved resistance to mechanical property degradation
#69Aircraft nacelle including an optimised acoustic processing system
#70Jet engine intake guard
#71Rotating inlet cowl for a turbine engine, comprising an eccentric forward end
#72Aviation engine inlet with tangential blowing for buzz saw noise control
#73COUPLING DEVICE FOR CONNECTING THE TWO HALF-SHELLS OF AN AIRCRAFT ENGINE NACELLE, AND NACELLE EQUIPPED WITH SUCH A DEVICE
#74Turbojet nacelle having a removable air intake structure
#75Nacelle comprising an air entrance in a cap
#76METHOD FOR CLOSING A MOBILE CRADLE ELEMENT
#77METHOD FOR MANUFACTURING A STRUCTURE WITH CELLULAR CORES FOR A TURBOJET NACELLE
#78Turbojet engine nacelle
#79Jet engine nacelle intended to equip an aircraft
#80Air intake arrangement for an aircraft
#81Turbojet engine nacelle
#82Air inlet of an aeroengine having unducted pusher propellers
#83Nacelle with an adaptable outlet section
#84Inlet section of an aircraft engine nacelle
#85Tailorable stiffness shape morphing flow-path
#86Turbine engine bypass fan-bleed noise reduction
#87Aircraft engine inlet having zone of deformation
#88Airplane having engines partially encased in the fuselage
#89Air inlet valve for an airplane and manufacturing method for an air inlet valve
#90Assembly of components connected by a device that maintains the integrity of the surface of one of the components
#91Air inlet for an aircraft turbine engine, an aircraft provided with such an air inlet, and a method of optimizing the operation of an aircraft turbine engine with the help of an air inlet
#92Gas turbine engine system providing simulated boundary layer thickness increase
#93Energy-deposition systems, equipment and method for modifying and controlling shock waves and supersonic flow
#94Aircraft engine protection device
#95System and method for gas turbine chilled water storage discharge control and/or gas turbine output control
#96AIRFLOW SEPARATION INITIATOR
#97Cambered aero-engine inlet
#98Gas turbine engine having slim-line nacelle
#99Gas turbine engine having slim-line nacelle
#100Inlet section of an aircraft engine nacelle
#101Intake cone in a fiber compound material for a gas-turbine engine
#102Gas turbine engine inlet with noise reduction features
#103Bird and debris deflector for aircraft jet engines
#104Aircraft engine nacelle with translating inlet cowl
#105Composite fan case with integral containment zone
#106Passive boundary layer bleed system for nacelle inlet airflow control
#107System, method, and apparatus for throat corner scoop offtake for mixed compression inlets on aircraft engines
#108Intake cone for a gas-turbine engine
#109Air inlet for a vehicle
#110Low shock strength propulsion system
#111Gas turbine engine nacelle
#112Gas turbine engine nacelle having a symmetric flowpath
#113Flow control redistribution to mitigate high cycle fatigue
#114Passive boundary layer bleed system for nacelle inlet airflow control
#115Gas turbine engine assembly including accessory components within the nacelle
#116Turbine engine for aircraft
#117Supersonic inlet
#118Fluid line assembly
#119Seal for pulse detonation engine
#120Low shock strength inlet
#121Apparatus and method for processing airflow with flowfield molded hypersonic inlet
#122Variable shape inlet section for a nacelle assembly of a gas turbine engine
#123Tangential anti-swirl air supply
#124Emergency ram air inlet valve of an aircraft
#125Variable geometry nacelle assembly for a gas turbine engine
#126Isentropic compression inlet for supersonic aircraft
#127Variable fluid intake with ramp and inflatable bag
#128Dual flow APU inlet and associated systems and methods
#129Boundary-layer-ingesting inlet flow control system
#130Segmented inertial particle separators and methods of assembling turbine engines
#131Ram air inlets for use with aircraft environmental control systems and other aircraft and non-aircraft systems
#132Gas turbine engine providing simulated boundary layer thickness increase
#133Tandem air inlet apparatus and method for an airborne mobile platform
#134Air inlet and method for a highspeed mobile platform
#135Gas turbine engine having slim-line nacelle
#136Engine arrangement
#137Aircraft engine inlet having zone of deformation
#138Flow control redistribution to mitigate high cycle fatigue
#139Panel assembly including deformable seal
#140Multiple auxiliary power unit system inlet ducts controlled by a single actuator
#141Gas turbine engine inlet with noise reduction features
#142Method for designing flowfield molded hypersonic inlet for integrated turbojet and ram-scramjet applications
#143Ram air channel for the supply of ambient air in an aircraft
#144Fluid line assembly
#145Control of engine intake door
#146Subsonic diffuser
#147Integrated mount duct for use with airborne auxiliary power units and other turbomachines
#148Integrated air inlet system for multi-propulsion aircraft engines
#149Dual flow APU inlet and associated systems and methods
#150Nozzle and filter-type dust collector
#151Multi-spectral air inlet shield and associated inlet structure
#152Nose cone for a turbomachine
#153Gas turbine engine inlet with noise reduction features
#154Air intake structure for aircraft engine
#155Cowl structure for a gas turbine engine
#156Jet engine nacelle for a supersonic aircraft
#157Hybrid inlet
#158Gas turbine inlet flow straightener
#159Apparatus and methods for varying inlet lip geometry of a jet engine inlet