Patent application number | Description | Published |
20080283665 | Aircraft Ventral Fairing Partition Wall and Aircraft Equipped with a Ventral Fairing - The invention concerns a wall ( | 11-20-2008 |
20100276542 | REINFORCED BLOCK MADE FROM COMPOSITE MATERIAL AND METHOD FOR REINFORCING A COMPOSITE BLOCK - A block including at least one glass ply at least partially covering an outer surface of a core made from composite material. A method for reinforcing a block made from a composite material, including a glass ply placed in a mould, such as to cover the base of the mould; the block is positioned in the mould; the edges of the glass ply are folded such that the glass ply is moulded to the outer edge of the block; the mould is closed with a cover; the block housed inside the mould is cured in an oven such as to polymerize the glass ply; and the glass-ply-covered block is recovered. | 11-04-2010 |
20100314495 | DEVICE FOR ATTACHING A PIECE OF FURNITURE TO THE FLOOR OF AN AIRCRAFT - Devices associated with an interface that is advantageous for the customized attachment of pieces of furniture to the floor of an aircraft. The interface includes rails extending longitudinally in the aircraft cabin, able to receive anchoring devices for connecting the furniture elements to these rails. The anchoring devices include axial and radial claw clamping devices which are associated together in pairs and operated together in pairs by a single and same lever ( | 12-16-2010 |
20120126059 | SEALING DEVICE BETWEEN A CROSS MEMBER AND INSULATION BLANKET PROVIDED AT AN AIRCRAFT FUSELAGE - An insulation blanket to be connected at the inside surface ( | 05-24-2012 |
20120140041 | METHOD AND SYSTEM FOR THE REMOTE INSPECTION OF A STRUCTURE - The invention relates to a method for the remote inspection of a structure, comprising the following operations:
| 06-07-2012 |
20120292461 | MOUNTING FOR HOLDING ELONGATE OBJECTS IN POSITION RELATIVE TO A STRUCTURE - The invention relates to a mounting ( | 11-22-2012 |
20130264428 | METHOD OF SEPARABLY COUPLING A PROPULSION MODULE AND A CARRIAGE MODULE OF AN AIRCRAFT, AND MODULAR AIRCRAFT IMPLEMENTING SAME - According to one embodiment, a modular aircraft includes a propulsion module dedicated to flight, combining avionic equipment—wing structures assembly, flight deck, engines, tail unit—and a module dedicated to the carriage of passengers and/or goods. These modules include external cells extending longitudinally along a main axis and having tubular end parts of the same outline in the region of two disconnectable-coupling structures, one axial-coupling structure for keeping an end face of the propulsion module against an end face of the carriage module, and one radial-coupling structure for keeping an end face of the propulsion module against an end face of the carriage module. The wing structures assembly of the propulsion module includes two wing structures having opposite sweeps which are connected at the end and by a longitudinal connecting spar. | 10-10-2013 |