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Airbus Operations S l patents

Recent patent applications related to Airbus Operations S l. Airbus Operations S l is listed as an Agent/Assignee. Note: Airbus Operations S l may have other listings under different names/spellings. We're not affiliated with Airbus Operations S l, we're just tracking patents.

ARCHIVE: New 2017 2016 2015 2014 2013 2012 2011 2010 2009 | Company Directory "A" | Airbus Operations S l-related inventors




Date Airbus Operations S l patents (updated weekly) - BOOKMARK this page
07/13/17Leading edge with laminar flow control and manufacturing method thereof
07/06/17Air conditioning system
07/06/17Air conditioning system
07/06/17Air conditioning system
07/06/17Selection of an equivalent 1d element type in a destination fea tool for 1d elements in a source fea tool
06/29/17Door system for an exhaust gas duct of an auxiliary power unit of an aircraft
06/22/17Pressure bulkhead
06/22/17Aircraft with a bleed supply hybrid architecture
06/15/17Suspension system for an aircraft auxiliary power unit
06/15/17Fuel control system for a gas turbine engine of an aircraft
06/08/17Pressure bulkhead
05/25/17Method for manufacturing rowings of composite materials
05/18/17Electric power distribution system for an aircraft
05/11/17Method, forming and injection tool for manufacturing an aperture surrounding frame for an aircraft fuselage, and frame obtained thereof
04/20/17Leading edge for an airfoil
03/30/17Composite rib for a torsion box and manufacturing method thereof
03/09/17Aircraft rear portion comprising a vertical stabilizer having a box-section structure including a lower portion accommodated in the fuselage
03/02/17Deformable structure for absorption of energy from mechanical and/or acoustic impacts
02/02/17Monolithic primary structural part for aircraft and processes for manufacturing it
01/26/17Method for measuring thickness of carbon fiber components using ultrasounds
01/26/17Boundary layer suction system
01/05/17Aircraft external part with inflatable panels
12/15/16Aircraft with a protective shield against an engine blade release
12/15/16Method for operating a landing gear system
12/15/16Aircraft with an auxiliary power unit attached to the aircraft fuselage by means of an attachment system
12/01/16Inspection methods and systems for detecting leaks in vacuum bag assemblies
11/24/16Auxiliary power unit starting system for an aircraft
11/10/16Horizontal tail plane with a multi-rib torsion box
11/03/16Method for manufacturing composite parts
11/03/16Manufacturing composite structures with curing tools arranged outside the vacuum bag
10/27/16Method for assembling an aircraft aft portion
10/13/16Aircraft rear structure
09/22/16Aircraft comprising a heat exchanger
08/25/16Flat kinked rear pressure bulkhead
08/11/16Aircraft tail cone
06/30/16Tail cone of an aircraft
06/30/16Device for a propeller blade
06/30/16Aircraft rear structure
06/23/16Door for closing opening in structure and aircraft
06/23/16Propeller blade for an aircraft engine
06/16/16Method and system for manufacturing of a moulded cfrp part
06/09/16Impact protective multi-layered fabric
06/02/16Aircraft fuselage frame
06/02/16Fire extinction design for an auxiliary power unit compartment of an aircraft
05/12/16Conversion of geometric entities of 1d elements in a fem from a source fea tool format to a destination fea tool format
04/07/16Orthogonal positioning instrument, system, and automatic machines
03/31/16Method for manufacturing a composite material part comprising a web and at least one flange
03/17/16Multi-fan engine with an enhanced power transmission
03/17/16Aircraft hybrid engine
02/18/16Aircraft with a nacelle-housed main landing gear
12/31/15Leading edge for an aircraft lifting surface and manufacturing method thereof
12/10/15Composite structure for an aircraft and manufacturing method thereof
12/03/15Method for manufacturing an aeronautical torsion box, torsion box and tool for manufacturing an aeronautical torsion box
12/03/15Safety system for autoclaves
12/03/15Method for manufacturing carbon fiber panels stiffened with omega stringers
11/19/15Aircraft air conditioning system and operating an aircraft air conditioning system
11/05/15Method and device for manufacturing a composite part of an aircraft
11/05/15Method for obtaining a composite laminate
07/16/15Aircraft control surface
07/02/15Aircraft structure made of composite material
07/02/15Highly integrated infused box made of composite material and manufacturing
07/02/15Horizontal tail plane of an aircraft
07/02/15Aircraft with a trimmable horizontal stabilizer having the pivot elements in its forward side
07/02/15Canard aircraft with rear loading
07/02/15Threaded connection for double-walled pipes
Patent Packs
07/02/15Stiffener element and manufacturing method thereof
07/02/15Auxiliary power unit with integrated fire detection system
06/25/15T-shaped stringer with a rounded web end and manufacturing it
06/25/15Leading edge for an aircraft lifting surface
06/18/15Manufacturing partially cured composite components
06/18/15Double-deck airplane
06/04/15Method for managing a manufacturing plant for the production of carbon fiber pieces
05/28/15Method for manufacturing an integrated composite trailing edge and integrated composite trailing edge
04/30/15Device and manufacturing omega stringers
03/05/15Method of detection and removal of auxiliary material suitable for the manufacturing of an aircraft element
03/05/15Laminate for joining parts, and joining parts
02/26/15Method and device for manufacturing composite material parts
02/05/15Rear fuselage section of an aircraft
01/29/15Injection interface device
01/22/15Drainage mast of the compartment of an aircraft subjected to a negative pressure
Patent Packs
12/25/14Method and system for starting up an aircraft turbomachine by real-time regulation of air flow
12/25/14Method and system for starting up an aircraft turbomachine
12/04/14Hybrid tool for curing pieces of composite material
11/20/14Trailing edge of an aircraft aerodynamic surface
06/05/14Highly integrated structure including leading and trailing edge ribs for an aircraft lifting surface
05/22/14Optimized torsion box for an aircraft
05/15/14Highly integrated leading edge of an aircraft lifting surface
02/20/14Highly integrated inner structure of a torsion box of an aircraft lifting surface
01/23/14Measurement of the inertial properties of an aircraft movable control surface
12/19/13Method for optimising the design of manhole openings on an aircraft
12/05/13Aircraft landing gear
11/21/13Outer fuel tank access cover, wing and aircraft description
10/31/13Method for prevention of porosity in composite material parts
10/24/13Bolted joint of the cover of an access opening in an aircraft lifting surface
10/10/13Aircraft frame and obtaining the same
08/22/13Riveting device for aircraft fuselages
08/22/13Aircraft with fuselage-mounted engines and an internal shield
08/01/13Heterogeneous parallel systems for accelerating simulations based on discrete grid numerical methods
08/01/13Drainage mast of the compartment of the auxiliary power unit of an aircraft
07/25/13Composite rod, manufacturing method and tool
07/25/13Protective shield against ice impacts on aircraft
07/18/13Aircraft versatile power system
07/04/13Method for manufacturing pieces of composite material having varied thicknesses
07/04/13Marking and defect recognition procedure in prepreg material
06/20/13Compaction process of a piece of composite materials
06/06/13Highly loaded frame of an aircraft fuselage with a lattice structured web
05/30/13Manufacturing "t" shaped stringers with an angle different from 90º between the web and the foot
05/16/13Protection device for sensitive areas against impact of foreign objects
04/25/13Pressure compensation device in aircraft
04/25/13Impact resistant and damage tolerant aircraft fuselage
Social Network Patent Pack
04/25/13Optimized stringer run-out zones in aircraft components
04/04/13Air intake with double inlet door
03/07/13Aircraft tail surface with a leading edge section of undulated shape
03/07/13Method for predicting the impact on an aircraft of debris shed off from it
03/07/13Process for applying resin on the surface of a moulding base tool, treated with mould-release substances, in order to obtain bodies of composite material
01/31/13Manufacturing procedure of a composite part of a closed compartment with an integrated access assembly
01/03/13Reinforced aircraft fuselage
11/29/12Systems and methods for improving the execution of computational algorithms
11/29/12Laying-up non-planar composite components
11/08/12Composite material part with large variation in thickness
Patent Packs
10/04/12Aircraft fuselage with high strength frames
09/20/12Load transfer devices at a stringer run-out
08/02/12Torsion box skin stiffened with non parallel stringers
07/26/12Manhole assembly in the lower skin of an aircraft wing made of a composite material
07/26/12Method for assembling fuselage sections of an aircraft
07/05/12Composite material part with reinforced areas and manufacturing procedure
07/05/12Wind tunnel with a closed section for aeroacoustic measurements with an anechoic coating
07/05/12Adjustable iron fitting for the installation and fitting of aircraft fairing
07/05/12Ball-joint support in thin parts
06/28/12Method for integrating metallic elements into composite materials
06/28/12Aircraft black box
06/21/12Optimization of structures subjected to hot gas streams
06/14/12Lightning and corrosion protection arrangement in an aircraft structural component
06/07/12System for increasing controllability for an aircraft
06/07/12Liquid fuel tank for measuring fuel volume
05/31/12Aircraft lifting surface skin
05/31/12Interface arrangement between two-components of an aircraft structure
05/31/12Tail-cone of an aircraft with movable fairing
05/31/12Interface arrangement between two components of an aircraft structure using a sealing part
05/24/12Peel ply material for use in an automated tape laying machine
05/17/12Computer-assisted optimising surfaces of composite-material structures
05/10/12Process for repairing airplane panels
05/10/12Engine exhaust
05/03/12Manufacturing procedure of a part made out of a composite material introducing a geometric change in one of its faces
05/03/12Inner bent repairment
05/03/12Re-usable retainers for co-bonding uncured stringers
04/19/12Weathertight fitting for aircraft tail vertical stabiliser mounting
04/19/12Lightning strike protection in aircraft
04/12/12Interchangeable joint concept for an aircraft rear fuselage cone
03/29/12Rear fuselage of an aircraft
Patent Packs
03/15/12Directionally strengthened union arrangement of parts made out of composite materials
01/05/12Internal structure of aircraft made of composite material
01/05/12Aircraft fuselage made out with composite material and manufacturing processes
12/15/11Procedure for the manufacture of large parts of composite material controlling the thickness of the edges thereof
12/01/11Attachment system of aircraft components
11/03/11Internal structure for aircraft in composite material
10/20/11Protection device against electrical discharges in aircraft
10/13/11Device for installing conducting components in structures
09/29/11Impact resistant and damage tolerant aircraft fuselage
09/15/11Multiple damage structural design optimization
07/21/11Joining arrangement for the lateral boxes of a horizontal tail stabiliser with a tubular central box and manufacturing said box
07/21/11Aircraft component with panels stiffened with stringers
07/14/11Joining arrangement for two boxes of composite material with an intermediate part and manufacturing said intermediate part
06/30/11Aircraft fuselage frame in composite material with stabilized web
06/30/11Composite material part with stringer on ramp
06/30/11Methods and systems for optimising the design of aerodynamic surfaces
06/30/11Aircraft fuselage frame of composite material with stabilising ribs
06/23/11Pivoting stabilising surface for aircraft
06/02/11Methods and systems for minimizing flow disturbances in aircraft propeller blades caused by upstream pylons
05/26/11Connection of aeronautical structural elements with other thermoplastic elements
Social Network Patent Pack
05/05/11Wind tunnel aircraft model with truncated wing
04/28/11Arrangement of a circumferential joint of structural elements with a coupling element manufactured in composite material
03/31/11Joining of structural aircraft elements
03/17/11Method for locating pressure losses in vacuum bags
12/30/10Design of aircraft frames
11/25/10Device for joining torsion boxes of aircraft
10/21/10Fittings for attaching the vertical tail stabilizer of an aircraft
09/16/10Closed structure of composite material
09/02/10Protection against direct lightning strikes in riveted areas of cfrp panels







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