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 (19 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
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 ...


4
Paul Anthony Cooper: Joint for use in aircraft construction. Airbus Operations, Lowe Hauptman Ham & Berner, March 22, 2011: US07909290 (14 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 ...


5
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 ...


6
Michael Stuart Yates, Philip Gregory Keen: Landing load monitor for aircraft landing gear. Airbus Operations, Nixon & Vanderhye P C, November 8, 2011: US08055396 (13 worldwide citation)

A landing gear monitor for aircraft landing gear including a plurality of pairs of wheels on a bogie, in which the main strut oil pressure serves to indicate landing load and is monitored in relation to, respectively, the two-wheel mode and the four-wheel mode, the two-wheel mode being the condition ...


7
Gilles Joannis, Kathrin Voelkner, Yannick Chourreau, Martin Geldien, Dejan Golubovic: Rest module with a first partial module with direct access to a possible second partial module. Airbus Operations, Airbus Operations SAS, Lerner David Littenberg Krumholz & Mentlik, April 24, 2012: US08162258 (13 worldwide citation)

The invention relates to a rest module for accommodating a least one crew member of an aircraft, wherein the module comprises a first partial module. Further on the first partial module comprises a first section and a second section; wherein the first section and the second section are spatially div ...


8
Jack Blanchard, Anthony Bryant: Aircraft cable routing harness. AIRBUS OPERATIONS, Lowe Hauptman & Ham, May 26, 2015: US09040821 (13 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.


9
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 (13 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 ...


10
Nicholas Elliott, Arnaud Didey: Jam-tollerant actuator. Airbus Operations, Lowe Hauptman Ham & Berner, September 18, 2012: US08267350 (12 worldwide citation)

An actuator, comprises a housing, a first prime mover for producing rotary motion, a first gearbox arranged to convert in use the rotary motion from the first prime mover into rotary motion having higher torque and lower speed. The first gearbox comprises a casing mounted for rotation relative to th ...



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