Patent Assignment
Reel/Frame 026141/0311
Change of Name
Recorded: 2011-04-18
Pages: 9
Assignor
AIRBUS UK LIMITED
Executed: 2009-06-17
Assignee
AIRBUS OPERATIONS LIMITED
NEW FILTON HOUSE, FILTON, BRISTOL, BS99 7AR, UNITED KINGDOM
Covered Properties
(220)
Wing Root Aerofoil for Forward Swept Wings
Patent:
5,314,142 →
Application:
07/854,016 →
Fusion Bonded Thermoplastic Leading Edge for Aircraft Aerodynamic Surfaces
Patent:
5,362,347 →
Application:
07/932,297 →
Lightning Shield
Patent:
5,499,782 →
Application:
08/095,376 →
Cutting Tools of Composite Construction
Patent:
5,486,072 →
Application:
08/102,901 →
Aircraft Landing Gear Trolley
Patent:
5,460,474 →
Application:
08/149,337 →
Auxiliary Control of Aircraft Landing Gear Movement
Patent:
5,460,340 →
Application:
08/149,339 →
Rigging of Aircraft Wing Flaps
Patent:
5,564,655 →
Application:
08/400,255 →
Testing a Metal Component for Cold Compression of the Metal
Patent:
5,619,327 →
Application:
08/403,441 →
Composite Laminate
Patent:
5,806,796 →
Application:
08/610,230 →
Deployment Mechanisms for Aircraft Auxiliary Airfoils
Patent:
6,149,105 →
Application:
08/703,435 →
Blind Stitching Apparatus and Composite Material Manufacturing Methods
Patent:
5,829,373 →
Application:
08/718,309 →
Joint Assemblies
Patent:
5,944,286 →
Application:
08/840,048 →
Composite Material Construction
Patent:
6,042,916 →
Application:
08/921,479 →
Repair of Composite Laminates
Patent:
6,149,749 →
Application:
08/959,725 →
Manufacture of Composite Laminates
Patent:
6,048,477 →
Application:
08/985,721 →
Method of Forming or Treating an Article or Preform
Patent:
6,270,706 →
Application:
09/065,519 →
Friction Welding Metal Components
Patent:
6,328,261 →
Application:
09/212,569 →
Aircraft Wing Leading Edge High Lift Device with Suction
Patent:
6,135,395 →
Application:
09/349,453 →
Blind Rivet Connector
Patent:
6,161,998 →
Application:
09/397,145 →
Aircraft Undercarriage Locking System
Patent:
6,131,852 →
Application:
09/397,146 →
An Aerofoil Having a Slat with Flexible Data Link
Patent:
6,286,790 →
Application:
09/428,533 →
Collapsible Annular Retaining Assembly
Patent:
6,368,007 →
Application:
09/434,469 →
An Aircraft Fin and Ribber
Patent:
6,202,959 →
Application:
09/434,470 →
Thermographic Wiring Inspection
Patent:
6,995,565 →
Application:
09/437,226 →
Machine for Laying Up Fabric to Produce a Laminate
Patent:
6,343,639 →
Application:
09/448,897 →
Composite Laminate Manufacture with Multiaxial Fabrics
Patent:
6,372,072 →
Application:
09/449,997 →
Forming Reinforcing Components
Patent:
6,355,133 →
Application:
09/465,940 →
A Jig Loading System
Patent:
6,684,601 →
Application:
09/465,941 →
Surface Topology Inspection
Patent:
6,809,803 →
Application:
09/466,899 →
Load measurement
Patent:
6,273,613 →
Application:
09/485,749 →
Aircraft undercarriage lock mechanism
Patent:
6,279,853 →
Application:
09/486,435 →
Method of Constructing Skin for a Member of a Body Such as an Aircraft
Patent:
6,669,806 →
Application:
09/490,954 →
Composite Material Construction
Patent:
6,582,792 →
Application:
09/490,955 →
Roll Forming Machine
Patent:
6,701,990 →
Application:
09/507,927 →
An Aircraft Landing Gear
Patent:
6,345,787 →
Application:
09/529,381 →
Friction Welding Metal Components
Patent:
6,450,394 →
Application:
09/572,571 →
Aircraft Structure Fatigue Alleviation
Patent:
7,073,751 →
Application:
09/582,760 →
A Sheath Protecting a Pin-Tail Locking Bolt
Patent:
6,685,410 →
Application:
09/647,664 →
Fairing Arrangement for an Aircraft
Patent:
6,450,457 →
Application:
09/647,797 →
Aircraft Noise Reduction Apparatus
Patent:
6,619,587 →
Application:
09/655,347 →
Method of Producing a Joint
Patent:
6,558,503 →
Application:
09/673,843 →
Feature Based Assembly
Patent:
6,748,284 →
Application:
09/674,308 →
Aircraft Landing Gear
Patent:
6,811,116 →
Application:
09/674,681 →
Friction Welding Metal Components
Assembling Composite Structures
Material Analysis
Fuel Inerting System
Solid Phase Welding
Aircraft noise reduction apparatus
Application:
10/300,916 →
Publication:
US 2003/0102406
Jig and a Method and Apparatus of Applying a Surface Treatment to a Member on the Jig
Wind Tunnel Testing
Stiffening Means for Structural Components, Method of Manufacturing and Apparatus Therefor
Non-Destructive Testing Apparatus
Method and Control System for Generating Machine Tool Control Data
Method of an Apparatus for Assembling an Aircraft Wheel or Brake Component on an Axle of an Undercarriage
Aircraft Flap Extension Mechanism
Turbulent Flow Drag Reduction
Turbulent Flow Drag Reduction
Split-pin drill jig
Application:
10/475,746 →
Publication:
US 2004/0120780
Adding Glass to Composite Bonding Surfaces
Winglet
Creep Forming a Metallic Component
Method of securing composite elements together
Application:
10/484,383 →
Publication:
US 2004/0195453
Aircraft Structural Components
Composite Material Structure
Drill Tool
Method of Landing an Aircraft and Apparatus Therefor
Light Cover
Landing Gear Door Assembly
Wing Skin and Method of Manufacture Thereof
Landing Gear Door Assembly
Aircraft Braking Method and Apparatus
Landing Gear Door Assembly
Landing Gear Noise Reduction
Landing gear
Application:
10/551,939 →
Publication:
US 2007/0108344
Fibre Optic Connector
Apparatus and Method Suitable for Measuring the Global Displacement or Load on an Aircraft Component
Advanced braking system
Jig and a method and apparatus of applying a surface treatment to a member on the jig
Application:
10/832,251 →
Publication:
US 2004/0206713
Wing Tip Device
Method of marking a piece of material
Application:
11/001,226 →
Publication:
US 2005/0117211
Method of Joining Structural Elements in an Aircraft
Method of Sealing a Joint
Sealing Material
Rib for Aircraft Wing and Methods for the Manufacture Thereof
Welding Process for Large Structures
Optical Alignment Device for Machine Tool
Aircraft Mode Suppression
Aircraft and Fuel Venting System Therefor
Aircraft wing
Application:
11/201,739 →
Publication:
US 2007/0023573
Landing Gear Support
Fastener Assembly
Valve System
Landing Gear
Method and Apparatus for Measuring the Structural Integrity of a Safe-Life Aircraft Component
Gas mixing device and methods of use
Application:
11/525,063 →
Publication:
US 2008/0075655
System and Method for Continuous Detection of an Analyte in Bloodstream
Process for Preparing Acrolein or Acrylic Acid or a Mixture Thereof from Propane
Methods of Detecting Cancer with Antibodies to Cytokine Receptor ZCYTOR19
Structure and Methods Using Multi-Systems for Electricity Generation and Water Desalination
High-Lift Device for an Aircraft
Display Method and System for Stimulating the Blinking of the Eyes of a User by Subliminal Modification of Display Parameters
Low Water-Absorption Plastisol Polymers
Aircraft Structure and a Fastener for Use Therewith
Cargo loading apparatus
Application:
11/640,002 →
Publication:
US 2007/0138342
Aircraft Seat Assembly
Fuel Tank for an Aircraft
Fuel Leak Estimator
Aircraft refuelling system
Aircraft Component
Composite Aircraft Component
Cover Panel for an Aircraft Wing and a Method of Forming Thereof
Method of Producing Structural Components Having Improved Toughness
Trussed Structure
Application:
11/792,159 →
Publication:
US 2008/0223986
Aircraft Wing
Apparatus and Method for Measuring Loads Sustained by a Bearing Pin
Aircraft with improved cargo hold
Application:
11/798,825 →
Publication:
US 2007/0267544
Overpressure Valve for an Aircraft
Lockable Fastener Assembly
Friction Stir Welding Tool
Aircraft fuel pipe coupling
Application:
11/890,516 →
Publication:
US 2008/0078880
Method for Forming a Feature in a Piece of Composite Material
Cable Routing Clip
Overpressure Protector
Aircraft fuel pipe coupling
Application:
11/979,677 →
Publication:
US 2008/0122221
Self Curing Injection Nozzle
Method and System for Making Holes in Composite Materials
Landing Load Monitor for Aircraft Landing Gear
Aircraft Fuel Pipe Coupling
A Method and an Apparatus for Performing a Program Controlled Process on a Component
Method, Apparatus or Software for Controlling the Heading of an Aircraft on the Ground
Machining Template Based Computer-Aided Design and Manufacture Of An Aerospace Component
Application:
12/064,879 →
Publication:
US 2008/0201002
Assembly of Aircraft Components
Wing Tip Device
Landing Gear
Standoff support system
Application:
12/076,589 →
Publication:
US 2008/0265112
Method and Apparatus for Deploying an Auxiliary Lift Foil
Unloading and Loading of Aircraft
Aircraft Braking System
Structural Element and Method of Manufacture
Aircraft Cooling Duct
Assembly of Aircraft Components
Fastener Assembly
Fastener Assembly
Application:
12/095,363 →
Publication:
US 2008/0292427
Fuel Tank Valve
Aircraft Fuel Tank Assembly
Aerofoil with Leading Edge Projection
Method and Apparatus for Monitoring Gas Concentration in a Fluid
Overpressure Protection for an Aircraft Fuel Tank System
Fibre Placement Tool
Method and Apparatus for Testing Composite Materials
Aircraft Noise Reduction Apparatus
Aircraft Auxiliary Fuel Tank System and Method
Ultrasonic Fluid Measurement Method
Aircraft Landing Gear Assembly
Landing Gear
Shim for Arrangement Against a Structural Component and a Method of Making a Shim
Panel with Impact Protection Membrane
Method for Forming Composite Components and Tool for Use Therein
Aircraft Landing Gear Load Sensor
Aircraft Wing Spoiler Arrangement
Aircraft Component
Apparatus for and Method of Inhibiting Delamination
Method and Apparatus for Providing Power in an Aircraft to One or More Aircraft Systems
Method and Apparatus for Operating an Aircraft Landing System
Aircraft wing with slotted high lift system
Method of monitoring the performance of a pressure intensifier
Application:
12/232,223 →
Publication:
US 2009/0091052
Aircraft Landing Gear and Door Assembly
Method and Apparatus for Manufacturing an Article and Generating a Report
Aileron Actuator Bracket
Slat Support Funk Plate
Landing Gear
Control Surface Failsafe Drop Link
Aircraft Wing
Testing Strut Assembly
Aircraft Steering Angle Warning System
Aircraft Fuselage Interior
Aircraft Wing and Flap Deployment System
Bearing Failure Indicator
Stringer for an Aircraft Wing and a Method of Forming Thereof
Wing Cover Panel Assembly and Wing Cover Panel for an Aircraft Wing and a Method of Forming Thereof
Method of Manufacturing Composite Part
Application:
12/303,422 →
Publication:
US 2009/0197050
Stringer for an Aircraft Wing and a Method of Forming Thereof
Aircraft Wing Box and Manufacture Thereof
Composite Manufacturing Method
Platform
Moulding Tool and Method of Manufacturing a Part
Application:
12/310,138 →
Publication:
US 2010/0000667
Fitting
Actuator
A Door for Opening and Closing a Door Aperture in an Aircraft
Method and Apparatus for Controlling the Geometry of a Composite Component
Aerodynamic Sealing Member for Aircraft
Blade Seal
Fitting for Pivotally Connecting Aerodynamic Control Element to Aircraft Structure
Hinge Rib
Trailing Edge Aircraft Structure with Overhanging Cover
Aircraft Structure with Hinge Rib Assembly
Jam-Tollerant Actuator
Method of Manufacturing Composite Material
Clamped friction joint
Application:
12/379,211 →
Publication:
US 2009/0208284
Aircraft Structure
Flight Surface Seal
Method of Manufacturing Composite Material
Method and Apparatus for Monitoring a Structure
Cutting Tool and Method
Application:
12/415,101 →
Publication:
US 2009/0269152
Method of Manufacturing Composite Material
Application:
12/439,267 →
Publication:
US 2010/0004388
Water Scavenging System
Leading Edge Structure for an Aerofoil
Fitting, Crane Hook, and Crane Hook Assembly
Aircraft Wing
Method of Designing an Airfoil Assembly
Method of Designing a Composite Panel
Apparatus for Providing Variable Thermal Insulation for an Aircraft
Aircraft Wing Assembly
Water Scavenging System
Method for Manufacturing Composite Components
Composite Structure
Aircraft Landing Gear Monitoring Apparatus
Method of Sealing a Joint
Application:
12/752,667 →
Publication:
US 2010/0253014
Slat Deployment Mechanism
Related Assignments
(6)
Other recorded transfers of the patents in this record — the chain of ownership.
Assignment of Assignor's Interest
Mar 6, 2002
From: BRITISH AEROSPACE PLC
To: BAE SYSTEMS PLC
Reel/Frame 012621/0679 →
Assignment of Assignor's Interest
May 14, 2002
From: BAE SYSTEMS, PLC
To: AIRBUS UK LIMITED
Reel/Frame 012936/0314 →
Assignment of Assignor's Interest
Sep 10, 2002
From: BAE SYSTEMS PLC
To: AIRBUS UK LIMITED
Reel/Frame 013269/0690 →
Assignment of Assignor's Interest
May 11, 2005
From: BAE SYSTEMS PLC
To: AIRBUS UK LIMITED
Reel/Frame 016547/0416 →
Assignment of Assignor's Interest
Jun 21, 2005
From: BAE SYSTEMS PLC
To: AIRBUS UK LIMITED
Reel/Frame 016700/0460 →
Assignment of Assignor's Interest
Mar 21, 2006
From: BAE SYSTEMS PLC
To: AIRBUS UK LIMITED
Reel/Frame 017649/0571 →