1
Daniel Ferro, Machiel Van Boven: Navigation system for an aircraft and associated command process. Airbus Operations, Oblon Spivak McClelland Maier & Neustadt L, September 27, 2011: US08027758 (20 worldwide citation)

A navigation system for an aircraft, including a calculator of an estimated flight path for the aircraft; a device for determining an estimated value of a flight parameter that corresponds to an estimated speed for the extension of at least a portion of the high-lift devices of the aircraft; and a d ...


2
Alan Mann: Wing tip device. Airbus Operations, Lowe Hauptman Ham & Berner, August 2, 2011: US07988100 (19 worldwide citation)

An aircraft includes a wing having a positive dihedral, the wing having a tip and a wing tip device mounted in the region of the tip. The wing tip device is generally downwardly extending and has a region inclined at a cant of more than 180 degrees. The region is arranged to generate lift during fli ...


3
HUMMEL Gerhard, RAPP Philipp, KROLL Lothar, SCHUBERT Frank, Martin Kausch: [fr] PROCÉDÉ DE FABRICATION DUN COMPOSANT DACHEMINEMENT DE FLUIDE PAR UNE CONSTRUCTION COUCHE PAR COUCHE, [en] METHOD FOR MANUFACTURING A FLUID ROUTING COMPONENT BY LAYER-WISE BUILDUP. AIRBUS OPERATIONS, LIEBHERR AEROSPACE LINDENBERG, HUMMEL Gerhard, RAPP Philipp, KROLL Lothar, SCHUBERT Frank, Martin Kausch, MAIWALD PATENTANWALTS, October 31, 2013: WO/2013/160188 (17 worldwide citation)

[en] A method for manufacturing a fluid-leading component comprises the positioning of a base element (2) machined by means of a material-removing method with a planar upper face (8) in a mounting support and the multiple carrying out of process steps for the layer-wise buildup of the component, whe ...


4
John William Griffin: Landing gear. Airbus Operations, Lowe Hauptman Ham & Berner, June 8, 2010: US07731124 (16 worldwide citation)

In an aircraft having an aircraft landing gear, the aircraft landing gear includes an arm, a leg and a bogie at the lower end of the leg. The bogie is moveable in a direction along the length of the leg and pivotable between a trimmed deployed position and a stowable position. The arm is mounted on ...


5
Paul Anthony Cooper: Joint for use in aircraft construction. Airbus Operations, Lowe Hauptman Ham & Berner, March 22, 2011: US07909290 (15 worldwide citation)

A joint for use in aircraft construction, for example a wing, comprises: a cover skin having an interior surface, an exterior surface and a distal portion, said distal portion having an exterior-facing surface; and a butt-strap having a first portion for connection to the skin, said first portion ha ...


6
Jack Blanchard, Anthony Bryant: Aircraft cable routing harness. AIRBUS OPERATIONS, Lowe Hauptman & Ham, May 26, 2015: US09040821 (15 worldwide citation)

A harness is provided comprising a body having a series of electrical conductors embedded therein and substantially running along the length thereof. The body may be part of a structural component such as stringer.


7
Tobias Dahms, Franz Angerer, Arne Anhalt, Stephan Beier, Martin Dobler, Ulf Glaser, Juergen Hairbucher, Fabian Knaul, Ralf Graefe: System and method for stockkeeping in an aircraft galley. Airbus Operations, Wood Herron & Evans, February 19, 2013: US08378825 (14 worldwide citation)

A system for stockkeeping in an aircraft galley includes a plurality of receiving devices which are provided for reception in a base body of the aircraft galley and are each provided with a transponder which is configured to emit an identification signal characteristic of the content of the correspo ...


8
Helene Cazeneuve, Bruno Cacciaguerra: Splicing of omega-shaped stiffeners at a circumferential joint in an aircraft fuselage. Airbus Operations SAS, Perman & Green, November 6, 2012: US08302909 (14 worldwide citation)

An aircraft fuselage produced by assembling, at a circumferential joint, at least two sections, each section including a coating and at least one element of at least one stiffener, the aforementioned two elements having a closed cross section and being assembled by a splicing piece. The elements of ...


9
TIZAC LAURENT: Dispositif dinterface débrayable entre un système de motorisation de roue de train datterrissage davion et une roue, Auskuppelbare Antriebsvorrichtung für ein Rad eines Flugzeugfahrwerks, Disengageable interface device of a drive system between an aircraft landing gear wheel and a wheel. AIRBUS OPERATIONS SAS, November 28, 2012: EP2527249-A1 (14 worldwide citation)

L'invention vise un dispositif de motorisation d'une roue de train d'atterrissage d'avion comportant : - un pignon d'entrée (301) entraîné par un moteur / réducteur (103), - un élément pendulaire (302), portant deux pignons intermédiaires (303, 304) entrainés en rotation par celui-ci, les pignons in ...


10
LAM JOSEPH K W: Coalescing filter. AIRBUS OPERATIONS, Butler Daniel, September 29, 2011: WO/2011/117609 (14 worldwide citation)

A fuel system comprising a liquid fuel tank, an engine, and a coalescing filter adapted to separate water from fuel, the filter having an inlet fluidically connected to the fuel tank, a first outlet fluidically connected to a fuel feed system for the engine, and a second outlet fluidically connected ...



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