APPARATUS FOR INGESTING BOUNDARY LAYER FLOW FOR AN AIRCRAFT

PROPULSION SYSTEM FOR AN AIRCRAFT

BLADE TIP VORTEX CONTROL

AIRCRAFT AIRFRAME COMPONENT WITH AIR SYSTEM

AIRCRAFT VERTICAL STABILIZER WITH AIR SYSTEM

DRAG RECOVERY SCHEME USING BOUNDARY LAYER INGESTION

AIRCRAFT

Apparatus for ingesting boundary layer flow for an aircraft

MAGNUS-EFFECT AIRCRAFT AND OPERATING METHOD THEREOF

METHODS FOR OPTIMIZING BOUNDARY LAYER CONTROL (BLC) SYSTEMS AND RELATED SYSTEMS

Propulsion System for an Aircraft

Flow control mechanism for nacelle of turbofan engine

Leading edge structure for a flow control system of an aircraft

Leading edge structure for a flow control system of an aircraft

Aircraft boundary layer ingestion using multiple fans and associated methods

BLADE TIP VORTEX CONTROL

Deflected Slip Stream Wing System with Coflow Jet Flow Control

BOUNDARY LAYER SUCTION DESIGN BY USING A CORE OF A WINGTIP VORTEX FOR A LIFT-GENERATING BODY

DRAG MODIFICATION SYSTEMS FOR AIRCRAFT AND RELATED METHODS

CROSS FLOW FAN, LIFT GENERATION DEVICE PROVIDED WITH SAME, AND AIRCRAFT PROVIDED WITH SAME

Active drag control system for an aircraft

Propulsion unit with improved boundary layer ingestion

Gas-electric propulsion system for an aircraft

Ice protection and boundary layer suction system for an aircraft aerofoil

Performance evaluation system of an aircraft component

Tiltrotor propulsion system for an aircraft

Leading edge structure for a flow control system of an aircraft

Apparatus and method for heating an aircraft structure

Flush fluid inlet designs for aero-acoustic tone mitigation of aircraft

Flow control techniques for delaying or accelerating laminar-turbulent boundary-layer transition for high-speed flight vehicles

Mechanically-distributed propulsion drivetrain and architecture

Dual door stall correction mechanism

Cooling system for power cables in a gas turbine engine

Method for managing the propulsive power of an aircraft

Nacelle for an aircraft aft fan

Airfoil for flow control including a common inlet/outlet device connected to a porous section

BOUNDARY LAYER SUCTION DESIGN BY USING WINGTIP VORTEX FOR A LIFT-GENERATING BODY

Propulsion engine for an aircraft

Drag recovery scheme for nacelles

Propulsion system for an aircraft

Engine inlet with deployable particle separator

Aircraft structure for flow control

Aerofoil leading edge structures

Meredith Effect Boundary Layer Energisation System

System to promote accelerated boundary layer ingestion

Boundary layer ingestion fan system

Boundary layer ingestion fan system

Boundary layer ingestion fan system

Gas-electric propulsion system for an aircraft

ENGINE ASSEMBLY WITH POROUS SURFACE OF BOUNDARY LAYER SUCTION

Active laminar flow control plenum panel arrangements and installation methods

Active laminar flow control plenum panel arrangement

Active laminar flow control structural plenums fastened

Tiltrotor propulsion system for an aircraft

Mechanically-distributed propulsion drivetrain and architecture

Method for separated flow detection

Aerodynamic body having perforated skin

Flow body of an aircraft and aircraft

TRANSVERSE FAN PROPULSION SYSTEM

Active laminar flow control system with composite panel

Aft engine nacelle shape for an aircraft

APPARATUS AND SYSTEM FOR DRAG REDUCTION

Electric propulsion engine for an aircraft

Leading edge structure for a flow control system of an aircraft

Apparatus and method for heating an aircraft structure

Leading edge structure for a flow control system of an aircraft

Deployable assembly for a propulsor

Wing comprising a leading edge slat and having means for preventing the transition to a turbulent boundary layer

Apparatus for laminar flow control

Active control flow system and method of cooling and providing active flow control

Wing comprising a leading edge having means for preventing the clogging of holes produced in the leading edge

System and method for operating a boundary layer ingestion fan

Dedicated fans for boundary layer ingestion

Propulsion system for an aircraft

Propulsion system for an aircraft

Variable-geometry boundary layer diverter

Electric propulsion system for an aircraft

Electrical machine

AIR INTAKE STRUCTURE AND AIRFLOW CONTROL SYSTEM

Gas-electric propulsion system for an aircraft

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

Propulsor

Aircraft comprising a rear fairing propulsion system with inlet stator comprising a blowing function

NACELLE FOR AN AIRCRAFT AFT FAN

AIRCRAFT WITH A VARIABLE FUSELAGE SURFACE FOR BOUNDARY LAYER OPTIMIZATION

System for dual management of anti-icing and boundary layer suction on an aerofoil of an aircraft, including a function of collecting the anti-icing air

Cross flow fan for wide aircraft fuselage

Integral component with an active flow control device

Turboelectric Aircraft with Aft Propulsion

Air distribution system with drag reducing inlet

Motor driven cooled compressor system

Translating nacelle wall for an aircraft tail mounted fan section

Nacelle for an aircraft aft fan

Aircraft having an AFT engine and stabilizer with a varying line of maximum thickness

Aircraft having an aft engine and internal flow passages

Aircraft having an aft engine and stabilizer root fillet

Tiltrotor propulsion system for an aircraft

Tiltrotor propulsion system for an aircraft

AFT engine nacelle shape for an aircraft

Nacelle for an aircraft aft fan

Deployable assembly for a propulsor

Thermal management system for an electric propulsion engine

Propulsion engine for an aircraft

Propulsion engine for an aircraft

Inlet guide vane assembly for reducing airflow swirl distortion of an aircraft aft fan

Inlet assembly for an aircraft aft fan

Inlet assembly for an aircraft aft fan

Aircraft having an airflow duct

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

Apparatus, system and method for drag reduction

Electric propulsion engine for an aircraft

ELECTRIC PROPULSION ENGINE FOR AN AIRCRAFT

Active control flow system and method of cooling and providing active flow control

Method, injection moulding tool for manufacturing a leading edge section with hybrid laminar flow control for an aircraft, and leading edge section with hybrid laminar flow control obtained thereof

Control of hypersonic boundary layer transition

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

Flow body for an aircraft for passive boundary layer suction

Leading edge with laminar flow control and manufacturing method thereof

Aircraft or spacecraft fluidic oscillator device

Aircraft

Aft engine for an aircraft

AFT engine nacelle shape for an aircraft

Non-axis symmetric aft engine

Aft engine for an aircraft

Aft engine for an aircraft

ACTIVE LAMINAR FLOW CONTROL SYSTEM WITH DRAINAGE

Multi-zone active laminar flow control system for an aircraft propulsion system

Heat exchanger for laminar-flow aircraft

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

Combined inlet laminar and thrust reverser cascade efflux flow control system

Gas-electric propulsion system for an aircraft

Laminar flow panel

Aircraft wing rib

Propulsion system for an aerial vehicle

Method of controlling boundary layer flow

Aerodynamic component and method for producing an aerodynamic component

Modular plenum and duct system for controlling boundary layer airflow

Perforated surface for suction-type laminar flow control

Aircraft environmental control system air duct arrangement

Stable Low Aspect Ratio Flying Wing

Leading edge nose structure on the vertical stabilizer of an aircraft

Aircraft environmental control system selectively powered by three bleed ports

Aircraft wing with system establishing a laminar boundary layer flow

Flow body, method for manufacturing a flow body and aircraft having such a flow body

Apparatus and methods to operate laminar flow control doors

Apparatus and methods for extending hybrid laminar flow control

Active bleed for airfoils

Laminar flow panel

Surface element for an aircraft, aircraft and method for improving high-lift generation on a surface element

Profile plate portion for use as an outer wall of a flow body, method for manufacturing a profile plate portion and flow body component comprising a suction-extraction device for fluid

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

Aircraft having an aircraft fuselage and an air sucking fuselage component

High lift system for an aircraft

Air sucking vehicle tail section component or wing section component, method for producing an air sucking vehicle tail section component and a wing section component and a vehicle, especially an aircraft, with an air sucking vehicle tail section component or wing section component

Wing leading edge venting

Flow body, in particular for aircraft

System and method for reducing the noise of pusher type aircraft propellers

Device for boundary layer suction and composite component therefor

Laminar flow panel

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

Aircraft cooling system

Device for reducing the aerodynamic drag of a leading surface of an aircraft

Apparatus, system and method for drag reduction

Boundary layer control system and methods thereof

Reduction of frictional losses in the region of boundary layers on surfaces, around which a fluid flows

Passive removal of suction air for laminar flow control, and associated systems and methods

Apparatus system and method for drag reduction

Boundary layer pumped propulsion system for vehicles

Boundary layer suction arrangement

Method for increasing a blade performance (variants)

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

Simultaneous multiple-location separation control

Perforated skin structure for laminar-flow systems

Arrangement for bleeding the boundary layer from an aircraft engine

Laminar flow nacelle for an aircraft engine

Apparatus for ingesting boundary layer flow for an aircraft

Y-shaped airliner and associated methods

Parasitic drag induced boundary layer reduction system and method