Patent application number | Description | Published |
20090014586 | Light rail system for powered introduction of large loads in a structure - A device for securing installed equipment in an airplane, with one or more oblong attachment rails, one or more attachment means for securing the attachment rails to an airframe structure, and one or more bracket units that can be attached to or in the attachment rails, wherein the bracket units can be attached to the built-in apparatuses to be secured. | 01-15-2009 |
20090026318 | Installation system for an airplane - An exemplary embodiment of the present invention indicates an installation system for an airplane for securing interior equipment, which exhibits longitudinal and transverse rails. The transverse rails are designed as peripheral rails, and exhibit perforations to which the interior equipment can be secured. | 01-29-2009 |
20090127392 | PROTECTION DEVICE - A device is provided for protecting a structure, such as an aircraft structure. The device includes, but is not limited to a skin made of a material comprising a multitude of alternating aluminium and glass-fibre reinforced plastic layers (e.g., GLARE), each being a few tenths of a millimetre in thickness. The skin is attachable to the structure so that a space is created between the structure and the skin, into which space the skin deforms when a force acts on it, so as to absorb the force acting on the skin, thereby minimizing and preferably preventing damage to the structure. | 05-21-2009 |
20100243805 | Structural Element of an Aircraft Fuselage - The structural element of an aircraft fuselage, with stringers running in the longitudinal direction of the aircraft fuselage and ribs running transversely to the stringers in the circumferential direction of the fuselage. According to the invention, at least one of the stringers running in the longitudinal direction of the aircraft fuselage is designed as a fastening rail for elements to be installed in the aircraft fuselage. | 09-30-2010 |
20100301165 | Structural Wing-Fuselage Component For Connecting Two Wings To A Fuselage Section Of An Aircraft - A structural wing-fuselage component for connecting two aerofoils to a fuselage section of an aircraft includes: a first wing shell component for the first wing and a second wing shell component for the second wing, with each component being made in a single piece and comprising a shell component on the wing side and a shell component on the fuselage side, where each shell component on the fuselage side comprises coupling parts and recesses in each case situated between the coupling parts, where in the installed state the coupling parts and the recesses of the shell component on the fuselage side for the first wing and of the shell component on the fuselage side for the second wing interlock, and where at least two coupling parts at their ends pointing away from the shell component on the wing side each comprises an extension part, a partially cylindrical fuselage shell component whose supporting rims include recesses which are engaged by the extension parts of the first wing shell components. | 12-02-2010 |
20110284692 | STRUCTURAL COMPONENT OF AN AIRCRAFT OR SPACECRAFT AND A FUSELAGE COMPONENT ARRANGEMENT OF AN AIRCRAFT OR SPACECRAFT - In the case of a structural component of an aircraft or spacecraft comprising a fuselage portion connection region for connecting to an associated fuselage portion and having a thermal expansion coefficient which is approximately matched to the associated fuselage portion; an inner connection region for connecting to an associated installation element and having a thermal expansion coefficient which is approximately matched to the associated installation element; and a separation region for connecting the fuselage portion connection region and the inner connection region, at least one of the regions has a high heat conduction resistance. | 11-24-2011 |
20120233359 | CONTROL DEVICE, INPUT/OUTPUT DEVICE, CONNECTION SWITCH DEVICE AND METHOD FOR AN AIRCRAFT CONTROL SYSTEM - Methods and apparatus are described for an aircraft network that permits an automatic configuring and/or repairing of the network. | 09-13-2012 |
20120233495 | CONTROL DEVICE, INPUT/OUTPUT DEVICE, CONNECTION SWITCH DEVICE AND METHOD FOR AN AIRCRAFT CONTROL SYSTEM - Methods and apparatus are described for an aircraft network that permits an automatic configuring and/or repairing of the network. | 09-13-2012 |