Patent application number | Description | Published |
20090050738 | Combined module for an aircraft - A module for an aircraft for accessing an upper region of the aircraft includes both an ascent region and an accommodation region, with the regions being divided from each other by a divider element. The accommodation region may, for example, be designed as an on-board lavatory. In this way it may be possible to do without the provision of an additional lavatory monument. | 02-26-2009 |
20090242147 | CURTAIN SUPPORT ASSEMBLY WITH INTEGRATED STORAGE FACILITY IN A CABIN OF A VEHICLE - The invention relates to a curtain support assembly to receive a curtain rail for a curtain for separating at least two regions in a cabin of a vehicle, comprising two or more header components for covering a space formed between the curtain rail and a ceiling in the cabin. The assembly according to the invention distinguishes itself from the state of the art in that between the header elements, for the purpose of holding objects, a hollow space is formed that is accessible by way of one or several closable openings to the cabin. In a further improvement, a roller is integrated in the hollow space, by way of which roller the curtain may be rolled up or down and may easily be stowed away. | 10-01-2009 |
20090242149 | Partition wall with integrated curtain rail flap - The invention relates to a partition wall for partitioning at least two regions in a cabin of a vehicle. The invention includes a partition comprising a body that may be moved into a first open position and into a second closed position and comprising a curtain rail, wherein the body is designed in the first position to cover an aisle that is adjacent to the partition, at least in some regions, by means of a curtain that has been affixed to the curtain rail. | 10-01-2009 |
20100230536 | CONVEYOR DEVICE FOR AIRPLANES - A conveyor device is provided for airplane for storing and conveying objects in an arc-shaped shaft. The shaft surrounds an area of a payload space of the airplane. An airplane is also provided with such a conveyor device. | 09-16-2010 |
20110062283 | DEVICE FOR DELIMITING A CREW REST COMPARTMENT AND METHOD FOR IMPLEMENTING SUCH A DEVICE - A device for delimiting a crew rest area in an aircraft passenger cabin includes a curtain which is adapted to separate at least one seat disposed in the aircraft passenger cabin from a region of the aircraft passenger cabin surrounding the seat. In addition, the device includes a fastening device for fastening the curtain in the aircraft passenger cabin. At least a first part of the fastening device is fixed to a grip rail intended for installation in the aircraft passenger cabin or formed integral with the grip rail intended for installation in the aircraft passenger cabin. | 03-17-2011 |
20110065344 | Baby cot with life raft function - A baby cot ( | 03-17-2011 |
20110114788 | DISPOSITION ZONE IN AN AIRCRAFT PASSENGER CABIN - The invention pertains to an aircraft with at least one passenger cabin that comprises at least one door entry area for the passengers and for the flight attendants that is visually separated from the passenger cabin and referred to as a space unit. Variable or mobile elements assigned to at least one partition wall/one monument of the space element can be arranged in the space unit that can be used as a disposition zone during the flight phase in order to realize working areas or service and/or comfort facilities for passengers or for the flight attendants. | 05-19-2011 |
20110114789 | UNIT FOR ACCOMMODATION OF MEMBERS OF AN AIRCRAFT CREW - The application relates to a unit for accommodating at least one member of an aircraft crew, wherein the unit is designed in such a manner that it can be arranged in a crew rest compartment of an aircraft, wherein the unit comprises first means, second means and third means for changing the volume of the unit, wherein the unit comprises: a lying-down facility for crew members, wherein the lying-down facility comprises first means for displacing the lying-down facility, a front panel, wherein the front panel comprises second means for displacing the front panel, and a sidewall, wherein the sidewall comprises third means for displacing the sidewall. Furthermore, the application comprises a crew rest compartment for accommodating at least one crew member, wherein the crew rest compartment is designed to be arranged in an aircraft, wherein the crew rest compartment comprises a unit according to the invention. | 05-19-2011 |
20110139930 | ERGONOMIC AND SPACE-SAVING ARRANGEMENT OF STRUCTURES UNDER A REST AREA IN AN AIRCRAFT - The invention relates to a rest compartment arrangement in an aircraft, comprising a rest compartment and at least one monument, wherein the rest compartment is arranged above a cabin floor and comprises a passage that extends from a rest compartment floor in the direction of the cabin floor. When compared to the state of the art, the invention is characterised in that the at least one monument comprises at least one wall which above a seat region situated therein forms a recess to accommodate the passage. As a result of this, monuments can be positioned in a space-saving manner underneath the passage in the cabin without this resulting in reduced comfort, because the recess above the seat region is not perceived to be distracting by the passenger. | 06-16-2011 |
20120112505 | SCREEN FOR A PASSENGER CABIN - The invention relates to a device for creating an individually delimited zone of a passenger cabin in a means of transport for at least one passenger seat. The device comprises a modular cabin element that has been attached in a positionally variable manner to stationary guide rails of the passenger seat by way of quick-release fasteners. Associated with this cabin element is an extendable and affixable privacy screen roller blind that forms a flexible dividing element, which privacy screen roller blind extends from the underside of the hatrack or the PSU panel or the ceiling arrangement, and in the lateral region in addition the sidewall lining of the passenger cabin, to the modular cabin element, and by means of which privacy screen roller blind an individually delimited zone can be implemented. | 05-10-2012 |
20130082141 | ACTUATION DEVICE FOR OPENING AN EMERGENCY EXIT FLAP OF A COCKPIT DOOR - An actuation device for opening an emergency exit flap of a cockpit door is provided. The actuation device comprises a support structure, at least two securing elements, an actuation element and a deflection mechanism. The support structure is configured so as to be fastened to the emergency exit flap. The securing elements are integrated into the support structure and are configured so as to fasten the actuation device, and thus the emergency exit flap, to the cockpit door. The actuation element is connected to the support structure. Therein, the deflection mechanism connects the securing elements to the actuation element in such a way that a force which is exerted on the actuation element is diverted in such a way that the securing elements are released from the cockpit door. | 04-04-2013 |
20130269258 | DOOR ASSEMBLY WITH TWO DOOR LEAVES - A door assembly for a vehicle with two door leaves is stated. In each case the door leaves can be opened in such a manner that the maximum angle of opening between them can be limited. After a door leaf has been opened, the door leaves can thus only be pivoted together so that opening the first door leaf results in closing the second door leaf. As a result of this, access to a space in a vehicle may be controlled. | 10-17-2013 |
20140115966 | Security door and security area - A security door comprises a frame structure, having a lateral surface in which a plurality of doorways are constructed. A first doorway has a first width along an inner circumference of the frame structure, and lateral surface portions delimiting the first doorway in a first direction and a second direction, opposing the first direction, along the inner circumference of the frame structure have a second width. A lock element is received in the frame structure and comprises a first segment, movable along the frame structure inner circumference relative to the frame structure, and a second segment, movable independently of the first segment along the inner circumference relative to the frame structure. The first segment is dimensioned so that, in a position in which it closes the first doorway, it also closes a second doorway adjacent to the first doorway in the first direction along the frame structure inner circumference. | 05-01-2014 |
20140332640 | SYSTEM AND METHOD FOR MOUNTING AIRCRAFT SYSTEM COMPONENTS IN THE CROWN AREA OF AN AIRCRAFT - A system for mounting aircraft system components in the crown area of an aircraft comprising a first longitudinal carrier element, a second longitudinal carrier element and a bridging element which connects the first longitudinal carrier element to the second longitudinal carrier element. The system is mountable in the crown area of an aircraft in such a way that the first and the second longitudinal carrier elements extend substantially parallel to the longitudinal axis of the aircraft. A plurality of cable ducts for accommodating electrical lines is provided on the first and/or the second longitudinal carrier elements. | 11-13-2014 |
20140339360 | Modifiable aircraft monument - An aircraft monument for installation in an aircraft cabin comprising a first functional module, a second functional module and a side wall for delimiting the first module from at least one of a region of the aircraft cabin adjacent to the first module and a region of the aircraft monument adjacent to the first module. The side wall is movable between a first and a second operational position and comprises a first side-wall region separating the first and second functional modules and in the second operational position, the side wall is displaced in the direction of the second module relative to its position in the first operational position, so that a movement of the side wall from its first operational position into its second operational position results in an enlargement of a base area of the first module and a corresponding diminution of a base area of the second module. | 11-20-2014 |
20140339361 | Aircraft area - An aircraft area comprises at least one main aisle which extends along a longitudinal axis of an aircraft cabin, a door aisle which extends, substantially perpendicularly to the at least one main aisle, along a transverse axis of the aircraft cabin between a first and a second aircraft door, and an aircraft monument which is arranged substantially centrally in the door aisle. | 11-20-2014 |
20140339362 | Multifunctional aircraft monument and aircraft area - An aircraft monument for installation in an aircraft cabin comprising a sanitary module. The sanitary module comprises a toilet which is adapted to be used as a sanitary facility for passengers when an aircraft equipped with the aircraft monument is in cruising flight. The toilet is further adapted to be used as a flight attendant seat if necessary. The aircraft monument also comprises a door opening which is adapted, when the aircraft monument is installed in an aircraft, to give a person sitting on the toilet which is being used as a flight attendant seat an unimpeded view of an area of the aircraft cabin which is arranged in front of the aircraft monument in the direction of viewing of the person sitting on the toilet which is being used as a flight attendant seat. | 11-20-2014 |
20140339363 | EXPANDABLE AIRCRAFT MONUMENT - An aircraft monument for installation in an aircraft cabin including a first functional module, the first functional module including a side wall for delimiting the first functional module from a region of the aircraft cabin adjacent to the first functional module and/or from a region of the aircraft monument adjacent to the first functional module. The side wall is movable between a first and a second operational position and comprises a side-wall region which merely in the second operational position of the side wall serves for delimiting the first functional module from a region of the aircraft cabin adjacent to the first functional module, so that a movement of the side wall out of its first operational position into its second operational position results in an enlargement of a base area of the first functional module. | 11-20-2014 |