Airbus Deutschland Gmbh

Daimler-benz Aerospace Airbus Gmbh

Airbus Operations Gmbh

Daimlerchrysler Aerospace Airbus Gmbh

Deutsche Aerospace Airbus Gmbh

Airbus (sas)

Daimler Aerospace Airbus Gmbh

Markus Schumacher

Andrew Muin

Andreas Heidtmann

Cord Haack

Thorsten Otto

Michael Lau

Martin Staub

Jens Romca

Jochen Mueller

Bruno Saint-Jalmes

Jason Zaneboni

Ralf Schliwa

Oliver Thomaschewski

Ian Scoley

Hans-Juergen Mueller

Daniel Glaser

Thomas Bock

André Rezag

Peter Theis

Lutz Franke

Alexander Wieser

Christian Majunke

Frank-Heinrich Schoenenberg

Michael Carr

Joachim Claus

Ingrid Kutzner

Ralf Myska

Harry Kwik

Guenter Schwertfeger

Jana Witt

Uwe Schneider

A cabin monument for an aircraft includes a floor panel, which forms a base surface of the cabin monument, and a surrounding sidewall which defines an interior space of the cabin monument. The surrounding sidewall is assembled from a first wall part and a second wall part which is coupled to this. Provision is made on at least one of the wall parts for a fixing section which is overlapped by the floor panel. Also described is an aircraft which features such a cabin monument.

Cabin monument for an aircraft

A cabin monument for an aircraft. The cabin monument has a framework with a base frame and a frame structure connected to the base frame, and side walls fastened to the frame structure. By fastening the side walls to the structural struts of the frame structure, a mechanical load acting on the cabin monument is distributed between the framework and the side walls.

A module for an aircraft having a fuselage structure and a floor element defining a floor plane. The module includes a frame device adapted for mounting a functional element and the frame device is adapted for attachment to the floor element of the aircraft at a first location in the floor plane. The frame device is adapted for attachment to the fuselage structure of the aircraft at a second location, wherein the second location is not in the floor plane.

Module for an aircraft

The idea of the present invention is that an airfreight container according to the invention, which is designed especially for an unpressurized cargo hold of an aircraft, comprises an airtight and pressure-tight container housing with a container interior space for accommodating airfreight goods. This airfreight container furthermore comprises an internal compressed air generating device which is designed for independently generating compressed air for supplying the container interior space with compressed air. The concept according to the invention of an at least partly autonomous airfreight container, which is created as a result, provides that the airfreight container according to the invention, in addition to the pure bundling of goods, now provides, moreover, different supply systems, such as the device for compressed air generation and compressed air provision, corresponding to the specific requirements. The particular advantage of this solution according to the invention is that cargo aircraft now do not have to provide supply systems, or have to provide at least a significantly reduced number of supply systems, in their cargo hold, and all further functions are now fulfilled by the airfreight container itself when required. The invention also refers to such an aircraft.

Airfreight container and aircraft

A floor system for a fuselage section of an aircraft is provided. The floor system has an essentially self-supporting design and is substantially mechanically separate from the fuselage section as primary structure. Consequent to the free or self-supporting design of the floor system in the fuselage cell, the layout of the floor system along an aircraft axis can be matched to customer specifications in a simple manner without reference to structural boundary conditions of the fuselage structure. A floor surface for the floor system is formed from a number of floor elements which can be fitted with functional elements, wherein filling of empty spaces or cavities can be achieved with a number of floor equalization elements. As the floor elements have a relatively large support or fixing surface the loads induced by the functional elements are introduced into the floor system distributed over a large area such that the structural components thereof can be of a structurally lighter and thus weight-saving size.

Floor system for a fuselage airframe of an aircraft

A folding seat for an aircraft has a backrest, a seat area and an armrest. The seat area is pivotable. When the seat area is pivoted, the armrest is pivotable downwards, the seat area and the armrest being coupled by at least one coupling element in the form of a bevel gear.

Downwards folding seat

A stowage bin arrangement for fastening a stowage bin for an aircraft, includes a stowage bin unit with a first direction of extension. The stowage bin unit may be fastened to an aircraft structure and be designed such that the stowage bin unit is capable of being telescopically extended along the first direction of extension.

Telescopic stowage bin

The present invention relates to a seat device for an aircraft. The seat device comprises a seat installation and a shell structure. In this arrangement the inside of the shell structure comprises an enclosed stowage space, wherein the shell structure is designed to attach the seat installation to a floor structure. In this arrangement the enclosed stowage space is designed to accommodate an item of baggage.

Seat device for an aircraft

A flight passenger seat for an airplane. The flight passenger seat may comprise a back element, a seat element and an arm rest. The seat element, back element, and arm rest may be pivotable. Reset elements for an automatic pivoting may be integrated into the back element and the seat element in such a way that they occupy as little traffic area space as possible. In an advantageous manner, this allows for an enlargement of a traffic area in an airplane and thereby may effectuate a reduction of a 'turn around' time of an airplane.

Flight passenger seat with an integrated spring element

To save space it is often not possible to provide a comfortable seat beside a bed, for example for a second flightdeck crew. Normally, sitting on a bed is not comfortable for extended periods of time. The present invention states a backrest arrangement which can be changed from a foldaway position to a seating position. The backrest arrangement can be hinged to a wall. In foldaway position, the distance between a lower region of the backrest and the essentially vertical surface is shorter than in the seating position. In this way the backrest arrangement can for example be attached to a wall beside a bed; in the seating position the backrest arrangement provides a comfortable and safe seat.

Seat backrest for the crew rest compartment of an aircraft

The present application describes a chassis for an air passenger seat for an aircraft. According to one exemplary embodiment, the chassis has at least two first lateral parts, and a first and a second spar. The second spar is implemented in the foot region of the air passenger seat and, in addition to its supporting function, ensures baggage is secured. The assumption of additional objects by the chassis construction advantageously allows an air passenger seat to be manufactured with minimum material outlay and therefore weight outlay.

Double-spar chassis for aircraft passenger seat

A vehicle seat, more particularly aircraft seat, includes a seat bottom and a seat back disposed in a seat frame. The seat bottom can be folded down from a first near vertical position (I) into a second near horizontal position (II). This results in a comparatively simple, lightweight construction featuring good accessibility to several vehicle seats configured abreast and/or in rows.

Vehicle seat particularly for aircraft

A passenger chair or a group of passenger chairs, particularly in an aircraft cabin, is equipped with a convenience device that includes an open storage bail which can hold only flat articles but not waste material, and a waste container for holding waste material but not flat articles. The storage bail and waste container form either a mounting unit or retrofit kit or are separate components. In both instances the mounting unit and the separate components are secured to a back facing area of a chair or group of chairs. The separate components are preferably so constructed that individual retrofit kits are provided.

Passenger chair with a convenience device

A seating space such as an aircraft passenger cabin has rows of seats along an aisle, identified by a row number and a seat location letter. A seat row indicator is arranged on the side flank of the seat back of each aisle seat, at the corner where the side flank and upper edge of the seat back meet. A seat location indicator is arranged at the middle of the upper edge of the seat back of each seat. The row numbers and seat letters are indicated on or in the indicators by paint, printing, engraving, inserts, illumination or tactile indicia. The indicators are conspicuous and easily visible to a passenger standing or walking in the aisle without bending or leaning over. Boarding of the aircraft is facilitated and expedited. Emergency evacuation is assisted by appropriate illumination of the indicators.

Passenger orientation arrangement in a passenger cabin

A comfort and illumination unit especially for a passenger space in an aircraft is constructed for cooperation with a straight wall panel that can be integrated in or secured to a vertical straight wall and/or a horizontal straight ceiling wall. The unit has a mounting base and a cover with passenger convenience elements mounted to the base under the cover which is provided with cut-outs for access to the convenience elements. Fluorescent bulbs form a frame around the convenience elements.

Growing community of inventors

Buxtehude, Germany

Markus Schumacher