FLUIDIC PROPULSIVE SYSTEM

AERIAL VEHICLE FLUID CONTROL SYSTEM WITH MULTI-WAY FLOW REGULATOR

FLUIDIC PROPULSIVE SYSTEM AND THRUST AND LIFT GENERATOR FOR AERIAL VEHICLES

AIRCRAFT

FLUIDIC PROPULSIVE SYSTEM

Fluidic propulsive system and thrust and lift generator for aerial vehicles

Engine strut flow control

COMBINATION COMPRESSED-FLUID EJECTOR AND PROPELLER PROPULSION SYSTEM

EJECTOR AND AIRFOIL CONFIGURATIONS

Aerial vehicle fluid control system with multi-way flow regulator

Aerial vehicle fluid control system integrated with gas turbine engine

Process and machine for load alleviation

Fluid systems that include a co-flow jet

DRAG REDUCTION SYSTEM FOR AN AIRCRAFT

Systems and methods for active control of surface drag using intermittent or variable actuation

Variable-porosity panel systems and associated methods

Ice protection and boundary layer suction system for an aircraft aerofoil

DISTRIBUTED PNEUMATIC SUPPLY SYSTEM OF AN AIRCRAFT

HIGH-LIFT DEVICE

Performance evaluation system of an aircraft component

FLUIDIC PROPULSIVE SYSTEM AND THRUST AND LIFT GENERATOR FOR AERIAL VEHICLES

Methods and apparatus for accelerating an aircraft fuselage boundary layer via a fan powered by an auxiliary power unit of the aircraft

Ducted fans having fluidic thrust vectoring

Ducted fans having edgewise flow augmentation

Fluidic roll control systems for use in forward flight

Low observable aircraft having trinary lift fans

Low observable aircraft having tandem longitudinal lift fans

Fluidic split flap systems for yaw control in forward flight

Fluidic yaw control systems for use in hover

Fluidic pitch control systems for use in forward flight

Fluid systems that include a co-flow jet

Shock wave suppression device and aircraft

Vertical tail unit for flow control

Method for managing the propulsive power of an aircraft

Process and machine for load alleviation

Nacelle for an aircraft aft fan

Axial flow ducted fan with a movable section

Flow control systems having movable slotted plates

Aerofoil leading edge structures

Forward swept wing aircraft with boundary layer ingestion and distributed electrical propulsion system

System to promote accelerated boundary layer ingestion

Flow guide body for an aircraft

Methods and apparatus for controlling flow fields

Aerodynamic body having perforated skin

Flow body of an aircraft and aircraft

Estimating fluid parameter

Control system

Aerodynamic aircraft wall comprising at least one vortex generator, and aircraft comprising the said aerodynamic wall

Fluid systems that include a co-flow jet

Leading edge structure for a flow control system of an aircraft

Active flow control systems and methods for aircraft

Fluid systems that include a co-flow jet

Fluid systems that include a co-flow jet

Methods and apparatus for controlling flow fields

Fluid systems that include a co-flow jet

Apparatus for laminar flow control

Vertical tail unit for flow control

Vertical tail unit for flow control

Fluidic device

NACELLE ANTI-ICING TROUBLESHOOTING FOR A TWO VALVE SYSTEM

Variable and adaptable diverterless bump inlet

Active flow control for ducted fans and fan-in-wing configurations

Thermally controlled active flow control system

Variable geometry engine inlet for high speed aircraft

Aircraft and flight control mechanisms used on aircraft

Flight control mechanisms and methods of operating aircraft with flight control mechanisms

Variable-geometry boundary layer diverter

Fluid systems that include a co-flow jet

PASSIVE FLOW CONTROL MECHANISM FOR SUPPRESSING TOLLMIEN-SCHLICHTING WAVES, DELAYING TRANSITION TO TURBULENCE AND REDUCING DRAG

Method and apparatus for determining a movement direction of a component of a mechanism

Aircraft bleed system

Vortex generators responsive to ambient conditions

Air distribution system with drag reducing inlet

Method and system for delaying laminar-to-turbulent transition in high-speed boundary layer flow

Airfoil for an aircraft having reduced noise generation

Active flow control systems and methods for aircraft

Fluid systems that include a co-flow jet

Fluid systems that include a co-flow jet

Distributed compressor for improved integration and performance of an active fluid flow control system

Synchronization of fluidic actuators

Thermally controlled active flow control system

System for the dual management of anti-icing and boundary-layer suction on an aerofoil of an aircraft

Propulsion assembly for an aircraft having a turbojet with a non-ducted fan and an attachment pylon

Cooperative actuator system for active flow control

ACTIVE LAMINAR FLOW CONTROL SYSTEM WITH DRAINAGE

Variable geometry flush boundary diverter

Cancelling damping induced by drag in synthetic jets using performance enhancements

System and method for enhancing the high-lift performance of an aircraft

Optimized nacelle profile and plenum shape for boundary layer ingestion active laminar flow control

SYSTEM AND METHOD FOR MULTIPLE DIRECTION CONTROL OF FLOW

Recessed lift spoiler assembly for airfoils

Vortex generators responsive to ambient conditions

Positionable ejector member for ejector enhanced boundary layer alleviation

System and method for distributed active fluidic bleed control

Flow control actuator with an adjustable frequency

Frequency response and health tracker for a synthetic jet generator

Strain amplification structure and synthetic jet actuator

Apparatus and methods to operate laminar flow control doors

Synchronization of fluidic actuators

Externally driven flow control actuator

Flow control actuator with an adjustable frequency

Systems and methods for attenuation of noise and wakes produced by aircraft

Strain amplification structure and synthetic jet actuator

High speed compound rotary wing aircraft

Fluid actuator for influencing the flow along a flow surface, as well as blow-out device and flow body comprising a like fluid actuator

Method of using an active flow control system for lift enhancement or destruction in a wind turbine blade

Flow body having a leading edge, a surface and an active flow control system and vehicle comprising at least one such flow body and an air source

High lift system for an aircraft

Aircraft with wings and a system for minimizing the influence of unsteady flow states

Flow body and method for taking in and/or blowing out fluid through a plurality of openings in a flow surface section of a flow body

Systems and methods for attenuation of noise and wakes produced by aircraft

System for global flow field management using distributed, surface-embedded, nano-scale boundary layer actuation

Base drag reduction for road vehicles and ‘airdrop’ cargo aircraft

Active aircraft pylon noise control system

High-lift flap, arrangement of a high-lift flap together with a device for influencing the flow on the same and aircraft comprising said arrangement

Wing of an aircraft and assembly of a wing comprising a device for influencing a flow

Boundary layer energiser

Boundary layer energiser

Aerodynamic body and high-lift system comprising such an aerodynamic body

Controlling the boundary layer of an airfoil

Method and system for global flow field management using distributed, surface-embedded, nano-scale boundary layer actuation

High-lift system for an aircraft with a main wing and an adjustable slat

DEVICE FOR DELAYING BOUNDARY LAYER SEPARATION

High performance airfoil with co-flow jet flow control

Aircraft component exposed to streaming surrounding air

Method of Reducing Drag and Increasing Lift Due to Flow of a Fluid Over Solid Objects

Controlling aircraft aerial movements, defeating icing on aircraft surfaces, aiding decontamination, and damping turbulence effects on aircraft by the method of micro-perforated airfoil coordinated precision flow management

Element for generating a fluid dynamic force

Method of improving lift of an aircraft wing

Aircraft component exposed to streaming surrounding air

Oscillating vane actuator apparatus and method for active flow control

Lift augmentation system and associated method

System for aerodynamic flows and associated method

Flow surface for a three-dimensional boundary-layer flow, especially on a swept wing, a swept tail plane or a rotor

Cross-flow fan propulsion system

Aerospace vehicle leading edge slat devices and corresponding methods

Simultaneous multiple-location separation control

Perforated skin structure for laminar-flow systems

Wide fuselage aircraft with increased boundary layer ingestion