Liebherr-Aerospace Lindenberg Gmbh

Zhafir Plastics Machinery Gmbh

Joerg Meyer

Anton Straub

Peet Vergouwen

Steffen Franz

Andreas Fensterer

Walter Starzacher

Dirk Issel

Rainer Fritschi

Michael Kopf

Michael Huber

Daniel Maier

Urlrich Grabherr

Hans Rabe

Volker Fritzlar

The invention relates to a strut for the landing gear, preferably the nose landing gear, of an aircraft, which strut comprises a structure branched in a Y shape, wherein the Y-shaped structure is produced as a multi-piece structure and comprises at least two bars, wherein a first bar forms the first branch of the structure and a second bar forms the second branch of the structure and wherein both bars are composed partially or completely of a fiber composite material.

Strut for the landing gear of an aircraft

The present disclosure relates to a method and an apparatus for the contactless measurement of the steering angle of an aircraft landing gear, in particular of a nose landing gear. Furthermore, this present disclosure relates to an aircraft landing gear, in particular a nose landing gear, which allows a contactless measurement of the steering angle.

Apparatus and method for steering angle measurement of an aircraft landing gear and aircraft landing gear

Growing community of inventors

Baienfurt, Germany

Joerg Meyer