237066 ⎘
Aeronautics or air transport Wing lift efficiency
Sub-classes:FLUIDIC PROPULSIVE SYSTEM
#2FLUIDIC PROPULSIVE SYSTEM AND THRUST AND LIFT GENERATOR FOR AERIAL VEHICLES
#3FLUIDIC PROPULSIVE SYSTEM
#4Fluidic propulsive system and thrust and lift generator for aerial vehicles
#5ASSEMBLIES AND METHODS FOR DEPLOYING A TRAILING EDGE FLAP OF AN AIRCRAFT
#6EJECTOR AND AIRFOIL CONFIGURATIONS
#7MAST DAMPENER FOR A ROTORCRAFT
#8Assemblies and methods for deploying a trailing edge flap of an aircraft
#9Panels for obstructing air flow through apertures in an aircraft wing
#10FLUIDIC PROPULSIVE SYSTEM AND THRUST AND LIFT GENERATOR FOR AERIAL VEHICLES
#11System for reducing vibrations or stresses in a rotor blade system
#12FLUIDIC PROPULSIVE SYSTEM
#13Winglet ejector configurations
#14Wing flap deflection control removal
#15Fluidic propulsive system and thrust and lift generator for aerial vehicles
#16Propelling system with variable aerodynamic controls
#17Aircraft wing assembly
#18Apparatus and methods for actuating a double-slotted flap using a slave screw
#19Assemblies and methods for deploying a trailing edge flap of an aircraft
#20Fluidic propulsive system and thrust and lift generator for aerial vehicles
#21Panels for obstructing air flow through apertures in an aircraft wing
#22System for transmitting and processing data for controlling a rotor blade actuator
#23Fluidic propulsive system and thrust and lift generator for aerial vehicles
#24Fluidic propulsive system and thrust and lift generator for aerial vehicles
#25Active control flow system and method of cooling and providing active flow control
#26Edge morphing arrangement for an airfoil
#27Ejector and airfoil configurations
#28Leading edge high-lift device
#29Morphing control surface
#30Rotor assembly apparatus
#31Adaptive composite structure using shape memory alloys
#32Lifting surface of an aircraft for increasing the generated lift force
#33Rotor blade system
#34System for reducing vibrations or stresses in a rotor blade system
#35Aircraft flap system and associated method
#36Actuation system for an active element in a rotor blade
#37Independent blade control system with hydraulic cyclic control
#38Independent blade control system with rotary blade actuator
#39Independent blade control system with hydraulic pitch link
#40High speed compound rotary wing aircraft
#41Electromechanical rotary actuator and method
#42Shape memory alloy active spars for blade twist
#43Vortex generation
#44Multi-element rotor blade
#45Continuous moldline technology (CMT) elastomeric control surface
#46Enhanced performance rotorcraft rotor blade
#47Mission adaptive rotor blade
#48System and method for minimising buffeting
#49Flap roller arrangement, flap assembly, and method for removing a roller assembly from a flap fitting
#50Rotor blade component cooling
#51Flap support
#52Aircraft flap mechanism having compact large fowler motion providing multiple cruise positions
#53Active twist hollow beam system
#54Reconfigurable rotor blade
#55System for heat dissipation from an internal actuator in a rotor blade
#56Trailing edge split flap with pneumatic actuation
#57System and method for an air vehicle
#58Retractable vortex generator for reducing stall speed
#59High-lift system for an aircraft
#60Twist mechanism for twisting a rotor blade for a rotorcraft, and a blade
#61Method and apparatus for actively manipulating aerodynamic surfaces
#62High-lift system for an aircraft, method for displacing a lift flap, and aircraft having a high-lift system
#63Rotary wing blade, rotor comprising at least two of such blades and method to implement such a rotor
#64Active gurney flap
#65Active gurney flap
#66Multi-element airfoil system
#67Active gurney flap
#68Modular integrated device for rotor blade control
#69Shape memory alloy actuated torsion lock
#70LEADING EDGE DEVICE FOR AN AIRCRAFT
#71Aircraft electrical power transfer assembly
#72Helicopter rotor control system
#73Elastically deformable side-edge link for trailing-edge flap aeroacoustic noise reduction
#74Adjustment of wings for variable camber for optimum take-off and landing
#75Mission-adaptive rotor blade
#76Aircraft attitude control configuration
#77System for increasing controllability for an aircraft
#78Implementation of Kalman filter linear state estimator for actuator equalization
#79Aircraft comprising a device for influencing the directional stability of the aircraft, and a method for influencing the directional stability of the aircraft
#80Hydrogen powered aircraft
#81Autonomous slat-cove-filler device for reduction of aeroacoustic noise associated with aircraft systems
#82Aircraft control surface operating device
#83AIRPLANE WING
#84Rotor blade with integrated passive surface flap
#85Cyclic blade speed control apparatus and method
#86Helicopter rotor control system with individual blade control
#87Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods
#88Aircraft flap actuator assembly
#89Wing of an aircraft and assembly of a wing comprising a device for influencing a flow
#90ROTOR BLADE CAMBER ADJUSTMENT
#91Aircraft wing load alleviation system
#92Fluidic artificial muscle actuation system for trailing-edge flap
#93Low noise wing slat system with deployable wing leading edge elements
#94ROTARY WING BLADE, A ROTARY WING INCLUDING SUCH A BLADE, AND AN AIRCRAFT
#95DEVICE FOR GENERATING AERODYNAMIC RESISTANCE ON AN AIRCRAFT
#96Deployable aerodynamic devices with reduced actuator loads
#97Actuation system for a lift assisting device and roller bearings used therein
#98Slot seal
#99Mechanical system for high acceleration environments
#100Active rotor blade control effector system for a rotary-wing aircraft
#101High lift system for an aircraft with a high lift flap and method for adjusting the high lift flap
#102Directionally controllable flying vehicle and a propeller mechanism for accomplishing the same
#103Trailing edge flap
#104Aerodynamic Flap and Wing
#105Traversing jet actuator
#106Shape memory alloy actuator
#107Aircraft with vertical stabilizers arranged on a central fuselage body and method, as well as control unit, for compensating a negative pitching moment
#108Directionally controllable flying vehicle and a propeller mechanism for accomplishing the same
#109ROTOR BLADE FOR ROTARY WING AIRCRAFT HAVING DEFORMABLE PROTRUSIONS TO REDUCE BLADE VORTEX INTERACTION NOISE
#110Slat configuration for fixed-wing aircraft
#111Bearing side face electrical isolation
#112Roadable aircraft with collapsible wings and ductless fan
#113Pinned lug joint
#114High stiffness shape memory alloy actuated aerostructure
#115Method of reducing or even eliminating the vibration of a rotorcraft lift and propulsion rotor, and an airfoil assembly and a rotor implementing said method
#116Leading edge flap method
#117Electrical power transfer assembly
#118Actuator arrangement
#119Blade seal
#120Hinge sealing element and an assembly including said element
#121Systems and methods for controlling aircraft flaps and spoilers
#122Controlling the boundary layer of an airfoil
#123AIRCRAFT DRAG MANAGEMENT STRUCTURE
#124Elongated, torsion-deformable aerodynamic element
#125Process and device for automatically optimizing on the ground the aerodynamic configuration of an aircraft
#126High-lift system on the wing of an aircraft, and method for its operation
#127Deployable flap edge fence
#128Device which is subject to fluid flow
#129Automatic control of a high lift system of an aircraft
#130Actuation system for leading edge high-lift device
#131ROTOR BLADE FOR A ROTARY WING AIRCRAFT
#132Method and device for controlling a rotary wing aircraft
#133Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods
#134Wing
#135Dynamic adjustment of wing surfaces for variable camber
#136Swashplateless rotorcraft with fault tolerant linear electric actuator
#137Link mechanisms, including Stephenson II link mechanisms for multi-position flaps and associated systems and methods
#138Rudder of a commercial aircraft
#139Aircraft structure
#140Slat assembly
#141Aircraft
#142Bi-directional flight control surface utilizing a split-track mechanism
#143Drill-elastic and flexurally rigid rod element for the support and guidance of a movable flap relative to a wing of an aircraft
#144Leading edge structure for an aerofoil
#145Strain energy shuttle apparatus and method
#146System and methods for adaptive blade control surface adjustment
#147Aircraft structure
#148HELICOPTER BLADE VORTEX INTERACTION NOISE REDUCING METHOD AND DEVICE
#149Leading edge flap apparatuses and associated methods
#150Wing debris detector
#151Advanced trailing edge control surface on the wing of an aircraft
#152Dual higher harmonic control (HHC) for a counter-rotating, coaxial rotor system
#153Hybrid device for vibration control
#154Devices and methods to improve wing aerodynamics at low airspeeds
#155Procedure and device for improving the maneuverability of an aircraft during the approach to landing and flare-out phases
#156Aircraft wing
#157Compliant structure design of varying surface contours
#158Apparatus and method for use on aircraft with spanwise flow inhibitors
#159Aircraft attitude control configuration
#160Swashplateless helicopter blade actuation system
#161Rotor blade for a rotary wing aircraft
#162Stabilizing and directional-control surface of aircraft
#163Aerodynamic fan control effector
#164Aircraft structure with hinge rib assembly
#165Aircraft systems with shape memory alloy (SMA) actuators, and associated methods
#166Systems and methods for providing differential motion to wing high lift device
#167Highly efficient supersonic laminar flow wing
#168Self locking trim tab
#169Aircraft control device
#170Trailing edge device catchers and associated systems and methods
#171Actuation system for a lift assisting device and roller bearings used therein
#172Deployable aerodynamic devices with reduced actuator loads, and related systems and methods
#173Aircraft wing and flap deployment system
#174Methods and apparatus for a multi-segment flap fence
#175Link mechanisms for gapped rigid krueger flaps, and associated systems and methods
#176Noise-shielding wing configuration
#177Translating flap drive door
#178Contra-bevel driven control surface
#179High lift longitudinal axis control system
#180Actuation system, helicopter using the same, and controlling method therefor
#181Symmetric leading edge device and method to delay flow separation
#182Connection element for power transmission between a flap actuator and a flap mounted on a wing of an aircraft so as to swivel
#183Helicopter rotor control system with individual blade control
#184Airflow control devices based on active materials
#185Deployable flap edge fence
#186Dynamic adjustment of wing surfaces for variable camber
#187Hydrogen powered aircraft
#188Helicopter blade vortex interaction noise reducing method and device
#189Yaw control system and method
#190Hydrogen powered aircraft
#191Support structure for a retractable and extendable flap, and use of said structure
#192Hybrid actuator for helicopter rotor blade control flaps
#193On-blade actuator for helicopter rotor blade control flaps
#194Self-lubricated actuator for on-blade rotor control
#195Rotor system with pitch flap coupling
#196Brushless direct current (BLDC) motor based linear or rotary actuator for helicopter rotor control
#197Elastomeric bearing with heatable shims
#198Fluid-driven artificial muscles as mechanisms for controlled actuation
#199Cellular support structures used for controlled actuation of fluid contact surfaces
#200Aerospace vehicle fairing systems and associated methods
#201Composite structural member having an integrated electrical circuit
#202MOBILE AIRFOIL DEVICE FOR AN AIRCRAFT WING
#203Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance
#204Seal assemblies for use with drooped spoilers and other control surfaces on aircraft
#205High-lift device for an aircraft
#206Miniature trailing edge effector for aerodynamic control
#207Sandwich-structure flat actuator and application to structural torsion
#208Actuation device positioning systems and associated methods, including aircraft spoiler droop systems
#209Rotorcraft control system and method of using
#210Aircraft having variable incidence wing and air cushion landing system
#211Rotorcraft blade provided with a tiltable flap
#212Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods
#213Servo mounting system for direct drive of an aircraft control surface
#214Aircraft attitude control configuration
#215Rotorcraft blade provided with a tiltable flap and a fastener tongue
#216Rotorcraft blade provided with a flap that is tiltable with the help of at least one main ball joint having a first shaft that is secured to said flap
#217Rotary flap
#218Procedure and device for improving the maneuverability of an aircraft during the approach to landing and flare-out phases
#219Lift augmentation system and associated method
#220Aerospace vehicle flow body systems and associated methods
#221System for aerodynamic flows and associated method
#222Movable nose cap and control strut assembly for supersonic aircraft
#223Electrostrictive compound actuator
#224Aerospace vehicle yaw generating systems and associated methods
#225Compact co-axial rotor system for a rotary wing aircraft and a control system therefor
#226Airflow control devices based on active materials
#227Aerospace vehicle fairing systems and associated methods
#228Canard position and dihedral for boom reduction and pitch/directional control
#229Airflow control devices with planar surfaces
#230Deformable aerodynamic profile
#231Airflow control devices using current
#232Adaptive compliant wing and rotor system
#233Wing of aircraft
#234Systems and methods for controlling aircraft flaps and spoilers
#235High lift longitudinal axis control system
#236Leading edge flap apparatuses and associated methods
#237Aircraft with forward opening inlay spoilers for yaw control
#238Aircraft wing systems for providing differential motion to deployable lift devices
#239Fluid dynamically effective surface for minimizing induced resistance
#240Apparatus and methods for structurally-integrated conductive conduits for rotor blades
#241Active control of airfoils
#242Forward pivoted full flying control tail boom
#243Aircraft leading edge apparatuses and corresponding methods
#244Horizontal augmented thrust system and method for creating augmented thrust
#245Methods and apparatuses for controlling airflow proximate to engine/airfoil systems
#246Method of manufacturing a composite structural member having an integrated electrical circuit
#247Lifters, methods of flight control and maneuver load alleviation
#248Compact co-axial rotor system for a rotary wing aircraft and a control system thereof
#249Airflow control devices based on active materials
#250Forward pivoted full flying control tail boom
#251Lifting surface provided with at least one rotary flap
#252Lift and twist control using trailing edge control surfaces on supersonic laminar flow wings
#253Rotor blade pitch control assembly
#254Airflow control devices based on active materials
#255Airflow control devices based on active materials
#256Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance
#257Supersonic aircraft with channel relief control
#258Rotorcraft having coaxial counter-rotating rotors which produce both vertical and horizontal thrust and method of controlled flight in all six degrees of freedom
#259Wing gull integration nacelle clearance, compact landing gear stowage, and sonic boom reduction
#260Aircraft thickness/camber control device for low sonic boom
#261Canard position and dihedral for boom reduction and pitch/directional control
#262Aircraft lift device for low sonic boom
#263Active control of multi-element rotor blade airfoils
#264Strain energy shuttle apparatus and method
#265Slotted aircraft wing
#266Multi-function trailing edge devices and associated methods
#267Main rotor shaft mounted hydraulic pressure system
#268Rotary flap
#269Variable trailing edge geometry and spanload control