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Helfrich, Hamburg

Felix Helfrich, Hamburg DE

Patent application numberDescriptionPublished
20080302911Habitation and sleeping module for accommodating at least one member of a flight crew - A habitation and sleeping module, in an aircraft, for accommodating at least one member of a flight crew, with the module having a first sleeping area. Furthermore, an ascent region is provided for ascending from a lower level into the module, wherein the ascent region includes an ascent device that is laterally arranged on the module.12-11-2008
20100019087MODULE FOR ACCOMMODATION OF CREW MEMBERS HAVING A STOWAGE BIN USABLE FROM INSIDE THE MODULE - A module for an aircraft is provided for the accommodation of crew members. The module includes, but is not limited to a trough-shaped floor region having an external contour that corresponds to the contour of further stowage bins installed in the aircraft. The storage space created in this way in the interior of the module is accessible from the interior of the module. In this way the stability of the module may be enhanced and the installation expenditure may be reduced. Furthermore, comfort may be enhanced, in particular as a result of more space being available for the crew.01-28-2010
20100044509MOVABLE STORAGE UNIT FOR AN ACCOMMODATION MODULE OF AN AIRCRAFT - According to an exemplary embodiment of the invention, a storage module is stated that is positioned in a region between two frame elements of an aircraft and that can be moved to a folded-out state. The storage unit forms part of a crew rest compartment in an aircraft.02-25-2010
20100140400Compartment For Accommodating At Least One Flight Crewmember - An exemplary embodiment of the present invention provides a compartment for accommodating at least one flight crewmember, comprising a first module and a stowage area, wherein the first module comprises a first rest facility, wherein the first rest facility is arranged substantially perpendicular to the longitudinal axis of the aircraft, as well as substantially parallel to the traverse axis of the aircraft, and wherein the stowage area is substantially arranged under the first rest facility.06-10-2010
20100140402RESIDENCE AND SLEEPING MODULE WITH A CONNECTABLE PARTIAL MODULE FOR ACCOMOPATING AT LEAST ONE MEMBER OF AND AIRCRAFT CREW HAVING A DOCKABLE PARTIAL MODULE - The invention relates to a residence and sleeping module in an aircraft, for accommodating at least one member of an aircraft crew, wherein the module comprises a first partial module for docking a second partial module to it. In this arrangement, the first partial module or the second partial module comprises a connecting element, and the first partial module is designed to be arranged at a vertical height of an aircraft, which vertical height differs from that of the second partial module. In this arrangement, the connecting element is designed such that the second partial module can be docked to the first partial module by means of the connecting element.06-10-2010
20100187354INFORMATION SYSTEM FOR MESSAGES FROM PASSENGERS TO THE CABIN CREW - An embodiment of the invention relates to an information system for an aircraft, comprising an operating unit with input elements, by means of which operating unit a message from a passenger to the cabin crew can be input; and comprising a display unit, which is associated with a passenger and is arranged in the region of passenger accommodation, for displaying the message, wherein the operating unit makes it possible to input a message from several selection options. Furthermore, the invention relates to the use of such an information system.07-29-2010
20100288881SECURED COCKPIT HAVING AN INTEGRATED ACCOMMODATION AREA AND LAVATORY FACILITIES - The invention relates to a work and accommodation module for providing a cockpit and for accommodating at least one pilot of an aircraft. To this end, the work and accommodation modules have a work area and a accommodation area, wherein the work area contains all equipment for controlling and piloting the airplane. The accommodating area contains at least one element, selected from the group consisting of a rest area and lavatory facilities. In addition, the module is separated from a passenger area by at least one security partition.11-18-2010
20110139930ERGONOMIC 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

Patent applications by Felix Helfrich, Hamburg DE

Felix Caspar Helfrich, Hamburg DE

Patent application numberDescriptionPublished
20090050738Combined 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
20090140098COMPONENT WITH CARBON NANOTUBES - The present invention relates to a component, in particular in the field of aviation and spaceflight, having a resin matrix in which carbon nanotubes are embedded for high conductivity of the component.06-04-2009
20100243152DEVICE AND METHOD FOR PROCESSING A FIBRE COMPOUND STRUCTURE - The present invention provides a connecting device for connecting an unhardened fibre layer which is arranged on a surface section of a fibre compound structure to the fibre compound structure. The connecting device comprises pressure cushion comprising a pressure cap for being arranged above the surface section and a pressure tight cap mat which is pressure tightly connected to a circumferential border of the pressure cap, thereby forming a pressure area which is limited by the pressure cap and by the cap mat. The connecting device further comprises a pressure inducing means for inducing an overpressure which presses the cap mat against the fibre layer into the pressure area. According to a further aspect the invention provides a processing method for processing a fibre compound structure. In a first step at least one unhardened fibre layer is arranged on a surface section of the fibre compound structure.09-30-2010