Airbus Operations Gmbh

Zf Friedrichshafen Ag

Airbus Deutschland Gmbh

Stefan Krahn

Michael Klank

Julian Stratmann

Thomas Rupflin

A magnetic field sensor has a magnet (M) that produces a magnetic field with a magnetic field axis (f), has a magnet axis (a) and is held in a component () that can move about at least one axis and has a component axis (b). Also a method for mounting a magnet (M) of a magnetic field sensor. The magnet (M) is held in the component () in such a manner that the magnetic field axis (f) coincides, as closely as possible, with the component axis (b). A deviation of the magnetic field axis (f) from the magnet axis (a) is measured, and the angle of deviation (&#x3b1;) is corrected during the mounting of the magnet (M) in the component ().

Magnetic field sensor and method for mounting a magnet

A holding element for a spring, having a spring fastening area () for fastening the leaf spring () to the holding element () and a wheel carrier fastening area () for fastening a wheel carrier () to the leaf spring (). The holding element () has a deformation zone () through which webs and openings extend for transmission of forces from the spring fastening area () to the wheel carrier fastening area (), such that the webs (S, S, S, S) and the openings (A, A, A) are formed mirror-symmetrically relative to the longitudinal axis (L) of the holding element.

Holding element for a spring

A window element for insertion in a window cutout in an outer skin of an aircraft, with a window frame for accommodating a window package and a press-on frame. The window frame can be attached to the inside of the outer skin in the region of the window cutout and can be riveted to the external skin, wherein for attaching the press-on frame at least one press-on frame fitting is connected to the window frame and to the outer skin, in particular is riveted to the window frame and to the outer skin, and the window frame comprises an essentially L-shaped or rectangular cross-sectional geometric shape.

Window element for insertion in a window cutout in an outer skin of an aircraft

Window element () with a covering tape () and a covering means () and comprising a window assembly () which can be fixed in a hermetically sealed manner to the window frame () by means of a retainer (), the window frame () being enclosed by an encircling seal () which has an encircling recess ().

Growing community of inventors

Osnabrück, Germany

Stefan Krahn