Patent application number | Description | Published |
20100046235 | WINDOW, IN PARTICULAR A WINDOW FOR AN AIRCRAFT CABIN - Such a window is intended to be assembled over an opening ( | 02-25-2010 |
20100108808 | SYSTEM FOR FIXING - This system makes it possible to join a substantially flat base of an element to be fixed to a top plate ( | 05-06-2010 |
20100163676 | AIRCRAFT WITH WINDSHIELD GLASS PLATES INTERCHANGEABLE BETWEEN DIFFERENT TYPES - An aircraft in which it is possible to replace windshield panes of the mineral type with windshield panes of the organic type and vice versa, without the frame of the aircraft structure having to be modified. The pane is held in place on the frame by a window pane retainer specific to the pane. The frame has no through-holes opening to the outside of the aircraft for fastening the pane. The window pane retainer specific to a pane of the organic type has pins passing through the acrylic panes. The disclosed embodiments also relate to a method of replacing a pane of a first type with a pane of a second type. | 07-01-2010 |
20120006940 | METHOD FOR REALIZATION OF AN AIRCRAFT STRUCTURE AND RESULTING STRUCTURE - An aircraft structure includes a skin ( | 01-12-2012 |
20120102719 | ATTACHMENT INTERFACE DEVICE FOR ATTACHING MOBILE EQUIPMENT TO AN AIRCRAFT STRUCTURE - An interface device for attaching mobile equipment ( | 05-03-2012 |
20130146710 | AIRCRAFT NOSE STRUCTURE WITH LANDING GEAR COMPARTMENT - An aircraft nose structure includes a fuselage and a pressuretight bulkhead fixed at its periphery to the fuselage and transversely dividing the fuselage into a pressurized upper zone and an unpressurized lower zone for accommodating retractable nose landing gear. The pressuretight bulkhead includes a floor of the pressurized upper zone, and a substantially flat rear panel extending between a rear edge of the floor and the fuselage. The floor and the rear panel are fixed laterally to the fuselage. The fuselage includes an exterior wall and reinforcing transverse frames to which the exterior wall is fixed. In line with the pressuretight bulkhead, at least some of the transverse reinforcing frames extend along the outline of the pressurized upper zone and constitute members that reinforce the pressuretight bulkhead. | 06-13-2013 |
20130306795 | AIRCRAFT FUSELAGE FRAME ELEMENT - The subject of the invention is an aircraft fuselage frame element ( | 11-21-2013 |
20140069984 | SYSTEM FOR FRICTION STIR WELDING INCLUDING A MOBILE COUNTER-BEARING - System for friction stir welding of two parts which includes a welding unit which includes at least one welding head fitted with a rotating pin and a counter-bearing unit which has a support surface to support the parts against a pressure exerted by the welding head, and wherein each welding head can be moved relative to the support surface in a first direction parallel to an axis of rotation of the rotating pin and in a second direction orthogonal to the axis of rotation, and wherein the support surface can be moved in the second direction and is formed of two coaxial clamp rollers which are set apart from each other. | 03-13-2014 |
20140069987 | PROCESS AND SYSTEM FOR FRICTION STIR WELDING OF A STIFFENER ON AN AIRCRAFT PANEL - Process for linear transparency friction stir welding of a flange of a stiffener onto at least one panel for an aircraft, wherein a weld bead is made along the flange of the stiffener and wherein the weld bead extends in cross-section from a first lateral edge to an opposite second lateral edge of the stiffener flange. System for the implementation of the above welding process, which includes three welding heads arranged as a triangle, each of which includes a rotating pin as well as a shoulder extending at the base of said rotating pin. | 03-13-2014 |
20140159949 | AIRCRAFT COMPRISING AN ONBOARD WEATHER RADAR ANTENNA PROVIDED WITH INCLINED PANELS - An aircraft comprising a fuselage and a radome fixed to the fuselage. The radome defines a housing and the fuselage comprises a sealed bulkhead closing the housing. A weather radar antenna comprises a main panel. A plurality of peripheral panels are arranged around the main panel, inclined from a planar surface of the main panel and located on the same side of the planar surface. The housing contains the antenna which is mounted on the fuselage through a mechanical support fixed to the fuselage and to the weather radar antenna on the same side of the planar surface as the peripheral panels. A bird strike shield is located between the antenna and the sealed bulkhead. The shield comprises a dome with a top and a base, the base being fixed to the aircraft fuselage. An opening is formed at the top of the dome through which the mechanical support passes. | 06-12-2014 |
Patent application number | Description | Published |
20090198188 | ADAPTOR FOR AN INTRODUCER VALVE IN A HUMAN OR ANIMAL BODY - An adaptor ( | 08-06-2009 |
20100224802 | VALVE FOR A SURGICAL OR MEDICAL INSTRUMENT - A valve for surgical or medical instruments including: a passage that can be at least partially sealed by twisting a flexible section ( | 09-09-2010 |
20130066416 | BIFURCATED ENDOLUMINAL PROSTHESIS - An endoluminal stent that can include, in various embodiments, perpendicular hoop members, each hoop member being formed of wire in a sinuous configuration, at least some of juxtaposed apices in neighboring hoops being secured to one another, such stents also being formed with axially aligned segments in straight stents, and segments of bifurcated stents. Certain embodiments of such stents also can include barbs, fabric covering, and radiopaque markers. | 03-14-2013 |
20130123904 | BIFURCATED ENDOLUMINAL PROSTHESIS - The present disclosure provides a bifurcated stent for use in juxtaposition with an angiological bifurcation. The disclosure provides a bifurcated stent that includes a proximal portion adapted to be disposed within a blood vessel in juxtaposition with a bifurcation, a first distal stent portion adapted to extend across the bifurcation into one of the branched blood vessels, and a second distal stent portion adapted to allow blood to flow from the proximal portion into the other branch blood vessel. The disclosure also provides a bifurcated prosthesis including such a bifurcated stent and a tubular graft layer formed from a biocompatible fabric in juxtaposition with the stent. The disclosure also provides a stent joining means for joining two stents one to the other to define a continuous lumen through the two stents. | 05-16-2013 |