Airbus Operations Gmbh

Airbus Deutschland Gmbh

Thk Gmbh

Claus-Peter Gross

Oliver Thomaschewski

Dirk Humfeldt

Cord Haack

Patrick Rollfink

Lars Schomacker

Johannes Einig

Eiji Hosaka

Diana Siehndel

Sven Jansen

Torsten Berger

Stefan Krafzik

A method of permanently joining composite parts made from thermoplastic material includes providing a first composite part and a second composite part, both made from thermoplastic material, wherein an orifice is provided in at least one of the composite parts, positioning both composite parts such that a portion of the composite part which includes the orifice is adjacent to a portion of the other composite part, injecting melted thermoplastic material through the orifice to contact the first and the second composite part in a contact area, whereby surfaces of the first and the second composite part in that contact area melt together; and solidifying the thermoplastic material in the orifice and in the contact area to permanently join the first composite part to the second composite part.

Method of permanently joining composite parts made from thermoplastic material, arrangement of composite parts, and aircraft

A method for producing a fuselage structural component for a triangle region of an aircraft by: providing an integral board of a former material, wherein the board has an opening; and deforming at least one internal edge of the board that forms the opening to an internal flange; and deforming at least one external edge of the board to an external flange. Adjacent to the opening, the integral and deformed board forms in each case a former portion, a floor beam and a vertical support. Also a fuselage structural component and an aircraft with the fuselage structural component.

Method for producing a fuselage structural component for a triangle region, and integral fuselage structural component

In order to enlarge a tank volume of a hydrogen powered aircraft, an aircraft tank for storing cryogenic His configured as a non-circular dorsal tank. The aircraft tank may be configured as a conformal fuel tank fitted to an outer contour of an aircraft fuselage. Further, an aircraft is provided with such an aircraft tank.

Hydrogen cryogenic non circular dorsal tank

A panel for covering a part of a structure in an interior space of an aircraft is disclosed including a main panel section having an interior side and an exterior side, and at least one attachment device coupled with the exterior side. The main panel section is exclusively made from a single thermoplastic material, and the at least one attachment device is adapted for attaching the panel to the respective interior structure.

Thermoplastic cover panel for a structure in an interior space of an aircraft

A mounting rail arrangement for an aircraft floor, floor structure and aircraft having the same. To allow full floor structural decoupling for monuments and/or cabin attendant seats, a mounting rail arrangement includes two mounting rails having mounting holes distributed along their longitudinal direction. A mounting bolt is inserted into the mounting holes and an attachment bolt for fixing a cabin monument and/or a cabin attendant seat is inserted into the mounting bolt. As a result, the cabin monument and/or cabin attendant seat may be installed on at different locations and/or with different orientations using all kinds of configurations enabled by the mounting holes.

Mounting rail arrangement for an aircraft floor, floor structure and aircraft having the same

An aircraft-floor element comprising a first cladding element configure to be swung from a first position to a second position. In the first position, the first cladding element is arranged parallel to a main plane of the aircraft-floor element and on a side of the aircraft-floor element which is directed towards a passenger cabin. In the second position, the first cladding is arranged at an angle to the main plane of the aircraft-floor element, wherein it forms a cladding for a cargo space. An aircraft zone having an aircraft-floor element and an aircraft having such an aircraft zone are also disclosed.

Aircraft-floor element, aircraft zone and aircraft having an aircraft-floor element

A storage compartment arrangement for a cabin of a vehicle has a storage compartment, housing, storage compartment opening, lower compartment, and upper compartment. The compartments are directly above each other and separated by an intermediate base pivotable at least in sections into the upper compartment. Items of luggage can be placed onto a lower horizontal pivoting edge and pushed into the lower compartment. Adjacent to a lower delimitation of the upper compartment, when the intermediate base is not pivoted, an upper horizontal pivoting edge is formed, onto which items of luggage can be placed and pushed into the upper compartment. The upper compartment has an upper opening edge adjoined by an auxiliary surface extending over the upper compartment, is at an angle in a range of 10° to 50° to the intermediate base and, as the distance from the upper delimitation increases, encloses an increasing distance from the intermediate base.

Storage compartment arrangement for a cabin of a vehicle including a pivotable intermediate base

A storage compartment arrangement for a vehicle cabin having a storage compartment, housing, closable storage compartment opening, lower compartment section in the housing, and upper compartment section in the housing. The storage compartment opening extends over the structural heights of both compartment sections. Items of luggage can be placed onto a lower horizontal pivoting edge and pushed into the lower compartment section. An upper horizontal pivoting edge is provided onto which items of luggage can be placed and can be pushed into the upper compartment section. The storage compartment opening has an upper opening edge facing an upper side of the upper compartment section and is adjoined by an auxiliary surface extending over the upper compartment section, is at an angle in a range of 10&#xb0; to 50&#xb0; to the separating plane, and, as the distance from the upper delimitation increases, encloses an increasing distance from the separating plane.

Storage compartment arrangement for a cabin of a vehicle

A passenger seat system for a transportation system includes at least one support structure and at least one seat, which includes a seat frame, which is movable and arrestable on the support structure and has an underside that rests on the support structure and an upper side that receives a seating surface. The seat frame has an arresting device on the underside and an operating unit on the upper side coupled with the arresting device. This is movable into an arresting position and a release position and is blockable at least in the arresting position through a lockable blocking device. The arresting device is adapted for arresting the seat frame on the support structure with the operating unit being in the arresting position and to release it with the operating unit being in the release position.

Passenger seat system having movable seats for a transportation means as well as an aircraft cabin having such a passenger seat system

A fastening system for passenger seats in a vehicle cabin has two or more guide rails to be integrated into or onto a cabin floor, and a plurality of slides, to be brought into engagement with the guide rails and having a flange for connection to a passenger seat in order to retain the passenger seat on a guide rail. Each guide rail has a profile cross section, perpendicularly to a main axis of extent, having a base region and a supporting region. Each slide has a cavity of complementary design with the profile cross section. The guide rails have a plurality of transverse openings spaced apart from one another between the base region and the supporting region. At least one slide has a displaceably mounted retaining body which, when the slide is in engagement with the guide rail, can be brought into engagement with one of the transverse openings.

Fastening system for passenger seats in a cabin of a vehicle

A rail covering for a sliding seat rail between two passenger seats in a cabin of a vehicle has a first and a second elongate covering element. The first and second covering elements are formed complementary with respect to each other, allowing the first covering element to telescopically engage with a lower side of the second covering element. The first covering element has, at least in regions on a lower side, a first guide which displaceably holds the first covering element on the sliding seat rail along the main direction of extent thereof. The second covering element has an open end arranged on the end side and, at an end arranged oppositely on the end side on a lower side, has a second guide which displaceably holds the second covering element on the sliding seat rail along the main direction of extent thereof.

Rail covering for a sliding seat rail between two passenger seats in a cabin of a vehicle

A passenger seat system) for a transport means has an elongate carrier structure, to be attached, fixedly with respect to a structure, mutually spaced-apart raster openings on the carrier structure top side, and a seat having a seat frame. The seat frame is displaceable and arrestable on the carrier structure, has a bottom side lying on the carrier structure, a top side holding a seat surface, an arresting device on the bottom side and an operating unit coupled to the arresting device, and movable into an arresting position and an unlocking position. The arresting device has an arresting body, mounted so as to be movable perpendicularly with respect to the carrier structure and pushed by a spring device, by a spring force, into an arresting position, and a locking unit for automatically holding the arresting body in the arresting position when the arresting body reaches the arresting position.

Passenger seat system for a means of transport

A fastening system for passenger seats in a vehicle cabin has two or more guide rails to be integrated into or onto a cabin floor, and a plurality of slides, to be brought into engagement with the guide rails and having a flange for connection to a passenger seat to retain the passenger seat on a guide rail. Each guide rail has a profile cross section, perpendicularly to a main axis of extent (x), having a base region, a supporting region and an undercut situated therebetween. Each slide has a cavity, of complementary design with the profile cross section, and a necked region, to be brought into engagement with the undercut, thus enabling the supporting region to be enclosed by the cavity of the slide. Each slide has a rotatably mounted roller projecting into the necked region and can be brought into surface contact with a guide rail surface.

A rail system for a vehicle includes a floor rail integratable into or onto the floor, first elongate movement rail elements, second elongate movement rail elements, holding devices to hold the movement rail elements on the floor rail, and gliders supportable on the movement rail elements in a gliding manner. The movement rail elements have a rail profile cross-section perpendicular to their main extension axis; the cross-section has an undercut that faces laterally outwards. The movement rail elements each have two opposed end faces, which can be brought into contact with end faces of other movement rail elements, such that at least one continuous movement rail with a constant rail profile cross-section is created. The gliders include a recess corresponding to the rail profile cross-section for gliding support.

Flexible rail system for fastening of objects on a floor in a cabin of a vehicle

For a seat group arrangement for a passenger cabin of an aircraft it is proposed to realize a temporary enlargement of the circulation area by widening the longitudinal aisle of the aircraft for the entry and exit period. For this purpose, a passenger seat group has a supporting frame which is provided with seat legs for fastening to the aircraft floor. At least one first fixedly secured seat having in each case a seat part and in each case a backrest and a further seat which is movable in the transverse direction and has a seat part and a backrest is provided on the supporting frame. The further seat is connected to the supporting frame via a folding device, and the folding device is configured to realize a change in width of the further seat in relation to the seat legs of the supporting frame.

Growing community of inventors

Hamburg, Germany

Claus-Peter Gross