Method for producing a component for connecting structures and device

Aircraft wing box joint

Fuselage and method for reducing drag

Rotorcraft empennage mounting system

Structure for joining torsion boxes in an aircraft using a triform fitting made from non-metallic composite materials

Bracket

REINFORCED AIRCRAFT FUSELAGE

Flight vehicle fairing having vibration-damping blankets

Digitally designed shims for joining parts of an assembly

Boron fiber reinforced structural components

Aircraft with a pivotable rear portion

Dismountable helicopter

Composite Aircraft Joint

Connection of a fuselage to an aircraft wing

Center fuselage bellows

Joint sealing system

Connector for stiffening frames between an aircraft fuselage and a wing box

Removable horizontal stabilizer for helicopter

Mid-wing airplane

Cooler for an aircraft cooling system, aircraft cooling system and method for operating an aircraft cooling system

Multi-piece fastener with self-indexing nut

Oblique panel at the rear of a central box of an aircraft fuselage

Aircraft provided with a tail plane including means for combating flutter

Airplane with a tailcoat tail assembly and rear engine

Aircraft

Hydrogen powered aircraft

Weathertight fitting for aircraft tail vertical stabiliser mounting

Composite aircraft joint

Multi-spar port box joint

Wing-to-body fairing with spray-on foam and noise reduction method

Aircraft structural assembly and associated assembling method

PROCEDURE FOR THE MANUFACTURE OF LARGE PARTS OF COMPOSITE MATERIAL CONTROLLING THE THICKNESS OF THE EDGES THEREOF

Composite structural member with progressive rigidity

Composite stringer end trim

Structural assembly for an aircraft

Wing/fuselage connection of an aircraft

WING SPAR SPLICE JOINT

Method for manufacturing and attachment of wing fairings

Connection of a wing to a fuselage of an airplane

Control surface assemblies with torque tube base

Fairing of aircraft elevator

Joining arrangement for the lateral boxes of a horizontal tail stabiliser with a tubular central box and manufacturing method for said box

Method of constructing a fixed-wing aircraft

Flying vehicle

Device for providing electrical continuity between aeronautical components with relative movement

Tail structure for an aircraft or spacecraft

Aircraft joint

Method of designing a composite panel

Method of manufacturing a structure

Structural wing-fuselage component for connecting two wings to a fuselage section of an aircraft

Sealing system for the gap existing between the fuselage and the elevator of the orientable horizontal stabiliser of an aircraft, extended with an aerodynamic fairing for sealing of the opening existing between the fuselage and the orientable horizontal stabiliser

Fittings for attaching the vertical tail stabilizer of an aircraft

Attachable wing

Integrative structure for aircraft fairing

Device for attaching a lift member to the fuselage of an aircraft

Support structure for a wing

Central section of aircraft with ventral or belly fairing capable of movement

Aircraft structural element located at the interface between a wing and the fuselage

Fairing system for a horizontal stabiliser of an aircraft and process for installing said system

Structure of the load introduction zone in the rear end of an aircraft

Aircraft horizontal stabilizer surface

Aircraft fuselage section

Assembly between a front fitting and the traction coupling of the two lateral boxes of the horizontal stabilizer of an aircraft

Fitting for trimming a horizontal stabilizer of an aircraft

Aircraft with its fuselage suspended under the wing

Apparatuses and methods for joining composite members and other structural members in aircraft wing boxes and other structures

STRUCTURE OF AN AIRCRAFT AEROFOIL

Aircraft tail cone

Aircraft wing including a plurality of dismountable members

Aircraft floor and fuselage supplied with said floor

Fitting

Lateral force joint

Particle-filled wing-to-body fairing and method for reducing fairing vibrations

Vibration damping for wing-to-body aircraft fairing

Trapezoidal panel pin joint allowing free deflection between fuselage and wing

Methods and systems for attaching aircraft wings to fuselages

Multi-piece fastener with self-indexing nut

Method of locally reinforcing a composite element and reinforced aircraft wing structure central box section

Continuous fuselage connection

Composite wing-body joint

Method for manufacturing and attachment of wing fairings

WING-TO-BODY FAIRING

Device and method for non-symmetrical mixed carbon-metal assembly

Elastic pre-deformed fairings for aircrafts

CONTROL SURFACE ASSEMBLIES WITH TORQUE TUBE BASE

Method and apparatus for attaching a wing to a body

Aircraft ventral fairing partition wall and aircraft equipped with a ventral fairing

Modular aircraft with removable spar

Hydrogen powered aircraft

Double-Shell Design Center Box

Hydrogen powered aircraft

Arrangement for coupling a coupling pivot for a trimmable horizontal stabiliser to the tail fuselage of an aircraft

Composite internal beam for reinforcing the structure of an aircraft

Apparatuses and methods for joining composite members and other structural members in aircraft wing boxes and other structures

Ventral fairing for an aircraft

Fitting with torsion box, of plastic material reinforced with carbon fibre, for coupling a drive motor / spindle unit for trimming of a horizontal stabiliser of an aircraft

Pivoting coupling system for a large dihedral empennage to the tail fuselage of an aircraft

Apparatuses and methods for joining structural members, such as composite structural members

MULTI-PIECE FASTENER FOR LIMITED CLEARANCE APPLICATIONS

Methods for manufacturing composite aircraft, parts and a family of composite aircraft

Control surface assemblies with torque tube base

Unmanned biplane for airborne reconnaissance and surveillance having staggered and gapped wings

Device for joining composite structure elements with metallic structure elements

Method and apparatus for rotatably supporting movable components, including canards

Fuselage spar for aircraft and central sparbox provided with such a spar

Method for making a laminated structure and aircraft provided with such a structure

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

Wing-fuselage joint

Contra-rotating electric helicopter

Attachment apparatus for an aerial vehicle

Methods and apparatus to prevent failures of fiber-reinforced composite materials under compressive stresses caused by fluids and gases invading microfractures in the materials

Highly efficient supersonic laminar flow wing structure