Airbus Deutschland Gmbh

Airbus Operations Gmbh

Jan Schroeder

Dirk Humfeldt

Andreas Wietzke

Werner Granzeier

Michael Harriehausen

Michael Demary

Martin Sperber

Marc Pein

André Boehme

A force level control for an energy absorber is provided for aircraft, and includes an adjustment element and a housing, whereby via the adjustment element, a bending radius of the energy absorber element is continuously adjustable in the housing.

Force level control for an energy absorber for aircraft

The present application describes a quick-change fastening system for demountably mounting an element to a fastening structure. The element comprises an engagement element that is designed to engage a bearing element of the fastening structure, wherein the element is hingeably held around the bearing element between a hooked-in position and a fastened position. The element further comprises a fastening element that can be affixed to a locking element of the fastening structure when the element is in its fastened position. The engagement element and the bearing element are designed such that along a hingeing movement of the element a form-fit connection is established when the element is in its hooked-in position, and that a force-fit connection is established when the element is in its fastened position.

Quick-change fastening system for mounting an element to a fastening structure

A baggage compartment includes a housing that has a baggage accommodation space, a hinged cover, a latching mechanism, an operating element and a covering element. By moving the hinged cover, the baggage accommodation space may be selectively made accessible or inaccessible. The latching mechanism may be partly placed on the hinged cover in such a way that the hinged cover and the housing may be selectively latched or unlatched by utilizing the operating element. The covering element is placed on the hinged cover such that it covers the latching mechanism but leaves the operating element accessible to the user for operation.

Baggage compartment in passenger transport system

A mounting device for aircraft comprises an energy absorber and wherein the mounting device is mounted between a primary structure of the aircraft and the interior equipment. In this way the load acting on an interior equipment connected to the primary structure of the aircraft by way of the mounting device can be limited if a crash impulse occurs. The load acting on the primary structure is also limited, which can result in enhanced passive safety for the passengers and in weight reduction.

Mounting device for interior equipment in aircraft

A passenger seat having a substructure that comprises a hollow space. The hollow space is designed to accommodate an object such as a luggage item. Accommodating an object in the substructure makes it possible to optimize the space requirement in an aircraft.

Passenger seat with luggage compartment

A joint cover in an aircraft has a clamp section and a cover section for covering a joint. The clamp section is used to mount the cover section over the joint. The joint cover conceals the joint and secures the joint from intrusion of foreign objects. One example presents information to passengers, incorporating visual displays or other devices within the cover section. For example, the joint cover may include a cover section and a clamp section of an elastic material that deforms under pressure, concealing the joint even during compression and decompression of the aircraft, which causes movement of the panels defining the joint.

Growing community of inventors

Hamburg, Germany

Jan Schroeder