Patent Assignment
Reel/Frame 026124/0168
Change of Name
Recorded: 2011-04-14
Received: 2011-04-14
Pages: 19
Assignor
AIRBUS ESPANA, S.L.
Executed: 2009-03-20
Assignee
AIRBUS OPERATIONS S.L.
AVDA. DE JOHN LENNON, S/N IN GETAFE, MADRID, ESX, SPAIN
Covered Properties
(100)
Method of Manufacturing Aircraft Frames in a Composite Material
Application:
12/941,774 →
Pressure Bulkhead Made of Composite Material for an Aircraft
Application:
12/760,678 →
Device for Electrical Bonding of Electrical Cables Shielding on Composite Structures
Application:
11/794,513 →
Aircraft with a Rear Fuselage Protection Shield
Application:
11/794,487 →
Protection Device against Electrical Discharges in Aircraft
Application:
11/794,485 →
Aircraft Having a Lambda-Box Wing Configuration
Application:
12/481,854 →
Integrative Structure for Aircraft Fairing
Application:
12/478,311 →
Part of Composite Material Having a Wedge Between Two Zones
Application:
12/478,251 →
Hybrid Tooling for the Curing of Composite Pieces
Application:
11/794,486 →
Method and System for a Quick Calculation of Aerodynamic Forces on an Aircraft in Transonic Conditions
Application:
12/475,682 →
Computer-Aided Method for a Cost-Optimized Calculation of Variable Distributions Over an Aerodynamic Surface
Application:
12/475,660 →
Joint Arrangement for Composite-Material Structural Members
Application:
12/474,394 →
Fiber Optic Connection Device for Composite Structures
Application:
12/426,340 →
Fitting for Trimming a Horizontal Stabilizer of an Aircraft
Application:
12/424,811 →
Stabilizing and Directional-Control Surface of Aircraft
Application:
12/415,485 →
Aircraft Horizontal Stabilizer Surface
Application:
12/411,506 →
Methods for Estimating the Effect of Variations of Design Variables on the Weight of an Aircraft Component
Application:
12/397,028 →
Fairing System for a Horizontal Stabiliser of an Aircraft and Process for Installing Said System
Application:
12/395,831 →
Protection of Elements in Composite Material
Application:
12/380,130 →
Aircraft Stabilizer Surface Trailing Edge
Application:
12/388,696 →
Structure of the Load Introduction Zone in the Rear End of an Aircraft
Application:
12/388,750 →
Mobile Surfaces for Aircraft with Sealed Slots
Application:
12/372,144 →
Rib-Fitting
Application:
12/372,162 →
Computer-Aided Method for a Cost-Optimized Calculation of Aerodynamic Forces on an Aircraft
Application:
12/348,053 →
Device and Method for the Manufacture of Elements in Composite Material
Application:
12/334,845 →
Methods and Systems for Adapting a Multi-Block Structured Mesh Topology of an Object to a Modification in Its Geometry
Application:
12/263,534 →
Computer Assisted Method for the Advanced Design of Bent Parts of Composite Material
Application:
12/254,021 →
Control Surface of Aircraft
Application:
12/238,577 →
Method for the Manufacture of One or More Pairs of Components in Composite Material
Application:
12/206,873 →
Structure of an Aircraft Aerofoil
Application:
12/201,310 →
Integrated Aircraft Structure in Composite Material
Application:
12/201,362 →
Methods and Systems for Generating Suitable Meshes for Hybrid Rans/Les Modelling
Application:
12/191,395 →
System for Tilting a Power Unit
Application:
12/182,568 →
Non-Destructive Method for Detecting Zones with Non Conductive Materials in a Composite Part
Application:
12/182,373 →
Process and Tooling for Lining Molds of Curved Pieces
Application:
11/794,001 →
Method for Simulating the Behavior of a Bonded Joint of Two Parts
Application:
12/080,087 →
Optimized Aircraft Manhole
Application:
12/072,691 →
Optimized Configuration of Engines for Aircraft
Application:
12/070,911 →
Piece Made of Composite Material with Areas of Different Thickness
Application:
12/070,906 →
Aircraft Control Device
Application:
12/070,910 →
Method and system to optimize surface design
Application:
12/070,903 →
Process for Making Swaged Lighting Holes in Planar Areas of Preimpregnated Composite Parts
Application:
11/794,221 →
Method and System for a Quick Calculation of Aerodynamic Forces on an Aircraft
Application:
12/070,544 →
Jig and out-of-autoclave process for manufacturing composite material structures
Application:
12/070,338 →
Acoustically Attenuated Fuselage for Aircraft
Application:
12/069,917 →
Integrated Protective Device Against Electrical Discharges in Fixing Elements
Application:
12/069,574 →
Impact Resistant Aircraft Fuselage
Application:
12/012,009 →
Protection device against electrical discharges in fixing elements with high charges
Application:
12/008,990 →
Protective Device Against Electrical Discharges in Fixing Elements
Application:
12/008,987 →
Methods and Systems for Assisting in the Design of Mobile Surfaces of Objects
Application:
12/006,259 →
Computer-aided method for predicting particle uptake by a surface of a moving object
Application:
12/006,260 →
Methods and systems for improving meshes used in computational fluid simulations
Application:
12/221,043 →
Arrangement for Mounting an Engine on the Airframe of an Aircraft
Application:
11/998,991 →
Aircraft Tail Assembly
Application:
11/904,628 →
Structural composite material structures with a metal surface add-on to increase their electrical conductivity
Application:
11/904,629 →
Cover for an Aircraft Access Opening
Application:
11/897,007 →
Stifffened multispar torsion box
Application:
11/897,029 →
Process and jig for manufacturing composite material structures
Application:
11/882,000 →
Integrated Multispar Torsion Box of Composite Material
Application:
11/825,123 →
Complex geometries made of composite material and forming process for same
Application:
11/825,122 →
Method for Evaluating the Effect of an Electric Discharge on a Composite Material
Application:
11/807,902 →
Leading Edge for Aircraft Made of Reinforced Composite Material
Application:
11/807,903 →
Jig and method of manufacturing aircraft frames in a composite material
Application:
11/799,324 →
Method for designing a composite material part with a curved surface
Application:
11/796,744 →
Tool and Process for Manufacturing Pieces of Composite Materials Outside an Autoclave
Application:
11/697,562 →
Composite material structure for aircraft fuselage and process for manufacturing it
Application:
11/731,793 →
Computer-Aided Method of Obtaining a Ply Model of a Composite Component
Application:
11/731,794 →
Aircraft Load Frame Made of a Composite Material
Application:
11/729,990 →
Process for Manufacturing Composite Material Structures with Collapsible Tooling
Application:
11/726,362 →
Pressure bulkhead made of composite material for an aircraft
Application:
11/699,743 →
Tool for Aiding Resin Distribution During the Curing of Composite Material Parts
Application:
11/699,742 →
Methods and Systems of Thermal Simulation for Fire Analysis of Objects
Application:
11/699,126 →
Integrated Composite Skin for Aircraft Mid-Box Lifting Surfaces
Application:
11/651,404 →
Process for manufacturing composite material structures with collapsible tooling
Application:
11/651,403 →
Metallic Local Reinforcement for Heavy Loaded Joints of Composite Components
Application:
11/643,749 →
Process for Optimizing the Structural Design of a Stiffened Composite Material Panel
Application:
11/639,368 →
Method and System for Designing Smooth Surfaces for Vehicle Parts
Application:
11/600,287 →
Method for Determining the Thickness of a Coating on a Composite Material
Application:
11/589,677 →
Tubular Components for Aeronautical Fuselages and Processes and Jigs for Its Manufacturing
Application:
11/589,680 →
Process for the manufacturing of parts made of composite materials with two curing cycles
Application:
11/527,745 →
Tool and process for manufacturing long pieces of composite material
Application:
11/516,030 →
System and method for performing a Zonal Safety Analysis in aircraft design
Application:
11/516,029 →
Cleaning Device for a Preimpregnated Carbon Fiber Placement Machine
Application:
11/516,032 →
Current Insulation System for Fluid Systems
Application:
11/516,033 →
Quality Control Process for a Structural Bonded Joint
Application:
11/516,028 →
Process of Manufacturing Composite Structures with Embedded Precured Tools
Application:
11/476,429 →
Composite Structure with Embedded Optical Fiber and a Process for Its Repair
Application:
11/441,272 →
Composite Structure with Optical Fiber Embedded in One of Its Surface Layers and a Process for Its Connection and Repair
Application:
11/441,273 →
Process of Manufacturing Composite Panels with U-Shaped Stiffening Members
Application:
11/364,494 →
Process and Tools for Manufacturing Composite Ring Frames
Application:
11/363,496 →
Current Insulation Device for Fuel Systems
Application:
11/359,774 →
Method to Monitor Structural Damage Occurrence and Progression in Monolithic Composite Structures Using Fibre Bragg Grating Sensors
Application:
11/296,855 →
Method of surface treatment of composite material structures with atmospheric plasma beams
Application:
11/274,750 →
Method of protecting fuel tanks manufactured with composites against electrical discharges
Application:
11/273,636 →
Composite beam with corrugated web
Application:
11/270,803 →
Stringers made of a composite material with a bulb
Application:
11/267,052 →
Preventive Defect Detection and Control Process in Composite Material Parts
Application:
11/206,661 →
Diffusion Nozzle for an Ultrasonic Probe
Application:
11/119,424 →
Process and Tooling for Reducing Thermally Induced Residual Stresses and Shape Distortions in Monolithic Composite Structures
Application:
10/795,800 →
Lightning Strike Protection System for Aircraft Fuel Tanks Made of Low Electrical Conductivity Composite Material
Application:
10/743,279 →