Liebherr-Aerospace Lindenberg Gmbh

Anton Straub

Joerg Meyer

Jörg Meyer

Peet Vergouwen

Michael Kopf

Rainer Fritschi

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.

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Constance, Germany

Anton Straub