Airbus Operations Gmbh

Airbus Operations (s.a.s.)

Christopher Perkins

Stuart Strachan Alexander

Neil John Lyons

Nicholas Elliott

Martin Rowlands

Alexandre Legardez

Alan Mann

Alexander Büscher

Xavier Matheis

Dominique Chasteau

Guilherme Barsali

Simon Roux

Martin Griffith Rowlands

Nick White

James Barnes

Aline Scotto

Marco Boscolo

Nicholas White

Mark Grufferty

Sébastien Crouzet

Maxime Itasse

Kevin Ip

Robert Mills

A temporary pintle support which can attach between upper prongs of a landing gear, and which is arranged to hold pintle pins prior to installation of the landing gear assembly at an aircraft. The pintle support is attached at the landing gear to align the pintle pins with their respective attachment bearings on each of the prongs. The pintle support may be removed once the pintle pins are fully inserted.

Pintle support and method of installing a landing gear assembly

A retractable fuselage mounted landing gear assembly is disclosed. The landing gear assembly includes a main strut, a drag stay and a landing gear main fitting. A first end of the drag stay is attached to the main strut and a second end of the drag stay is connected to the fuselage. A first end of the landing main fitting is attached to the main strut and a second end of the main fitting is connected to the fuselage. When the landing gear is extended, substantially all the landing gear loads are transferred from the landing gear to the fuselage via one or more of the drag stay and the main fitting.

Landing gear assembly

An aircraft door controllerincluding a receiverconfigured to receive a commandto move an aircraft door between an open position and a closed position relative to a door frame. The aircraft door controlleris configured to not store the commandwhen power to move the aircraft door between the open position and the closed position relative to the door frame is unavailable.

Aircraft door control

A steering device for an aircraft landing gear leg including a main fitting has a steering collar for rotatably mounting on the outside of the main fitting; an actuator having an actuator body; and an actuator arm arranged to move between an extended position and retracted position with respect to the actuator body. The actuator arm is pivoted to the main fitting, and a bracket is pivoted to the main fitting; a second pivot location pivoted to the actuator body; and a third pivot location pivotally connected to one end of a steering arm. The steering arm is pivoted at its other end to the steering collar. Also, an aircraft landing gear with the steering device and aircraft having the landing gear.

Steering device for an aircraft

Growing community of inventors

Bristol, United Kingdom

Christopher Perkins