TAIL FIN ASSEMBLY FOR AN AIRCRAFT COMPRISING PIPING AT THE FRONT OF THE TAIL FIN

Rotary-Wing Aircraft Provided with at least one Multi-Plane Pitch Stabilizer

CONVERTIBLE AIRCRAFT CAPABLE OF HOVERING

AIRCRAFT VERTICAL STABILIZER WITH MOVEABLE PROPULSION SYSTEM(S)

AIRCRAFT AIRFRAME COMPONENT WITH AIR SYSTEM

AIRCRAFT VERTICAL STABILIZER WITH AIR SYSTEM

Aircraft System for Reduced Observer Visibility

CONFIGURATION FOR VERTICAL TAKE-OFF AND LANDING SYSTEM FOR AERIAL VEHICLES

VERTICAL TAKE-OFF AND LANDING AIRCRAFT

Aircraft System for Reduced Observer Visibility

REMOVABLE HOLLOW DORSAL FIN

CONFIGURATION FOR VERTICAL TAKE-OFF AND LANDING SYSTEM FOR AERIAL VEHICLES

VERTICAL TAKEOFF AND LANDING HYBRID DRONE SUITABLE FOR FLYING IN WINDY CONDITIONS

RECONFIGURABLE UNMANNED VEHICLES

AIRCRAFT STRUCTURE

Aircraft with articulatable tail section

Aircraft with external upper cargo module

Aircraft system for reduced observer visibility

Coaxial rotor systems for VTOL aircraft

Variable-sweep wing aerial vehicle with VTOL capabilites

LIFTING, STABILIZING AND PROPELLING ARRANGEMENT FOR VERTICAL TAKE-OFF AND LANDING AIRCRAFT

Helicopter, helicopter kit and associated reconfiguration method

SYSTEM FOR FIXED-PITCH LIFT CONFIGURED FOR USE IN AN ELECTRIC AIRCRAFT

Penetrating High Wing Structure of Civil Aircraft with Blended-Wing-Body

Integration driving mechanism for fin control assembly for flying equipment, UAVs, aerial observation equipment and the like

Differential thrust vectoring system

Method and Apparatus for Reducing Download and Drag of VTOL Electric Vehicle

Leading edge structure for a flow control system of an aircraft

AIRFRAME LOCALIZED KEEL STRUCTURES

Quiet urban air delivery system

Rotorcraft with cooling anti-torque system

Autonomous multi-purpose heavy-lift VTOL

Modular unmanned aerial vehicle connection system having insertable tabs

Configuration for vertical take-off and landing system for aerial vehicles

Tailstock type vertical take-off and landing unmanned aerial vehicle and control method thereof

Leading edge structure for a flow control system of an aircraft

Method and system for coupling a vertical stabilizer to an aircraft fuselage

Aeronautical composite structure and method and system for monitoring the physical status thereof

LEADING EDGE STRUCTURE FOR A FLOW CONTROL SYSTEM OF AN AIRCRAFT

Aircraft with multi spar box connection to fuselage

Aircraft with multi spar box connection to fuselage

Vertical and short takeoff and landing (VSTOL) aircraft

MODULAR FIXED VTOL WITH LINE REPLACEABLE UNITS

Aeronautical apparatus

Leading edge structure for an aerodynamic surface of an aircraft

Coaxial rotor systems for VTOL aircraft

Aircraft having convertible tailboom and landing gear systems

AIRCRAFT WINGS WITH REDUCED WINGSPAN

TAIL SITTER STOP-FOLD AIRCRAFT

Aircraft having an engine wing assembly

Aircraft floats

Flying toys

Control surface for an aircraft and control structure for an aircraft with anti-flutter balance weight

Passive and active stability systems for ballistically launched multirotors

COLLAPSIBLE STABILIZER ASSEMBLY FOR AN AIRCRAFT

CONVERTIPLANE

Autonomous propeller propulsion system for an aircraft, said autonomous propeller propulsion system comprising a fuel cell

Free propeller assembly structure and aircraft structure having the same

Butterfly folding fairing

Wing and aircraft

Aircraft with foldable tail

T-tail joint assemblies for aircraft

Flying object and flying object position control system

Profiled structure and associated turbomachine

Aircraft with right and left propulsion unit support beams extending between main and aft wings

Hybrid power tri-propeller helicopter apparatus

Aircraft

FINS USED TO INCREASE THE STABILITY OF AIRCRAFT AND SPACECRAFT RELATED VEHICLES OR PROPELLED/PROJECTILE OBJECTS

Methods and assemblies for mounting equipment to an aircraft

Differential thrust vectoring system

Multirotor joined-wing aircraft with VTOL capabilities

AIRFOIL AND MACHINE PROVIDED WITH SAME

Drag reduction systems for aircraft

FRAME ASSEMBLY FOR A REAR SECTION OF AN AIRCRAFT AND REAR SECTION OF AN AIRCRAFT COMPRISING SAID FRAME ASSEMBLY

AIRCRAFT COMPONENT

Systems and methods for countering an unmanned air vehicle

Methods and apparatus for a distributed aircraft actuation system

Wind Energy Kite Tail

Aircraft having an aft engine

Aircraft having articulated horizontal tail units

Vertical stabilizer

Leading edge structure for a flow control system of an aircraft

Aircraft vertical stabilizer illumination light and aircraft comprising the same

Core structures for composite panels of an aircraft, composite panels and aircraft including the core structures, and methods of manufacturing the composite panels

Hybrid type rotorcraft having a horizontal stabilizer and two fins arranged on the horizontal stabilizer

Aircraft system for reduced observer visibility

Box structural arrangement for an aircraft and manufacturing method thereof

Skin-panel interface of an aircraft

Low stall or minimum control speed aircraft

Configuration for vertical take-off and landing system for aerial vehicles

Methods and apparatus for a distributed aircraft actuation system

Aircraft vertical stabilizer design

Structural panels for exposed surfaces

Aircraft system for reduced observer visibility

Impact resistant dorsal fin

Fairing for an aircraft

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

Aircraft having an aft engine

Aircraft exhibiting independent elevators

Structural component of aircraft wing body and aircraft including the structural component

Curved wingtip for aircraft

AIRCRAFT AND EMPENNAGE SECTION OF AN AIRCRAFT

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

Reaction control system

Rotorcraft tail boom, and a rotorcraft

Vortex generator arrangement, flow control system and method for controlling a flow on a rudder surface

Gyroscopic orbiter with vertical takeoff and vertical landing capabilities

Aircraft fuselages

Drone launch systems and methods

Control surface for an aircraft

Bonded and tailorable composite assembly

Aircraft rear structure

Compound wing vertical takeoff and landing small unmanned aircraft system

HAND-LAUNCHED, SOLAR-POWERED AIRCRAFT

Airframe-integrated propeller-driven propulsion systems

Method for manufacturing a nacelle strake

Methods and apparatus to control aircraft horizontal stabilizers

Aircraft fuselages

Bonded and tailorable composite assembly

Tail spar spring

Systems and methods countering an unmanned air vehicle

Leading edge nose structure on the vertical stabilizer of an aircraft

Box wing with angled gas turbine engine cores

Clocked thrust reversers

Aircraft with forward sweeping T-tail

Stabilizer with structural box and sacrificial surfaces

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

Surveillance system

Apparatus and methods to operate laminar flow control doors

Aircraft system for reduced observer visibility

Method of inspecting impacts observed in fan casings

Rudder system for an aircraft

Aircraft having an aircraft fuselage and an air sucking fuselage component

Very low-power actuation devices

Method and device for the lateral stabilization of an aircraft

Tail capable of improving anti-bird strike performance of aircraft

Rotorcraft empennage mounting system

REINFORCED AIRCRAFT FUSELAGE

On-board aircraft auxiliary power systems having dual auxiliary power units

Method for improving the aerodynamic efficiency of the vertical tail of an aircraft

Device for boundary layer suction and composite component therefor

Aircraft attitude control configuration

Airplane with a tailcoat tail assembly and rear engine

Aircraft comprising a device for influencing the directional stability of the aircraft, and a method for influencing the directional stability of the aircraft

Use of auxiliary rudders for yaw control at low speed

Active flow control on a vertical stabilizer and rudder

Method for enhancing the aerodynamic efficiency of the vertical tail of an aircraft

Aerospace vehicle yaw generating tail section

Strut system for the stabilization of the shell of an aerodynamic aircraft component for a commercial aircraft

Control surface assemblies with torque tube base

Aircraft with at least two rudder units in a non central arrangement

DYNAMIC FIN COMPRISING COUPLED FIN SECTIONS

Aircraft with a wing movable along the longitudinal axis of the fuselage

Method for producing an aircraft with reduced environmental impact and the aircraft thus obtained

FUSELAGE AND A METHOD FOR REDESIGNING IT

Support structure for a wing

Cover for an aircraft structure

Airplane with flat rear fuselage said queue-de-morue empennage

Framework wing box for a wing

Methods and apparatus for an integrated aerodynamic panel

Aircraft attitude control configuration

Lateral force joint

Continuous fuselage connection

Methods for making composite material components especially useful for aircraft, and composite material components thereof

Aircraft having a reduced acoustic signature

Aircraft tail assembly

Symmetric leading edge device and method to delay flow separation

CONTROL SURFACE ASSEMBLIES WITH TORQUE TUBE BASE

Double-Shell Design Center Box

Low-noise aircraft, particularly at take-off and landing

Multi-engine aircraft

Aircraft attitude control configuration

Structural panels for use in aircraft fuselages and other structures

Control surface assemblies with torque tube base

Tall V/STOL aircraft

Method and apparatus employing eccentric bushing

Aircraft with foldable tail assembly

Helicopter tail rotor pylon

Rudder unit connection to a fuselage without a bolt-fairing structure

Aircraft converts drag to lift

Drag reduction fin deployment mechanism

Versatile multirotor aerial vehicles

Versatile multirotor aerial vehicles

Wind energy kite tail

Vertical takeoff and landing unmanned aerial vehicle

Supplementary control surface structure for airplanes