Patent application number | Description | Published |
20090230246 | WINDOW PANEL AND METHOD OF MANUFACTURING SUCH A WINDOW, AIRCRAFT COMPRISING A WINDOW PANEL - This invention relates to the design of aircraft ( | 09-17-2009 |
20100294887 | PRESSURISED AIRCRAFT DOOR EQUIPPED WITH A VENT FLAP - The invention relates to a pressurised aircraft door that minimises risk of ingress of precipitation inside the aircraft, while maintaining venting of the aircraft before unlocking the door. | 11-25-2010 |
20100308172 | INTERCONNECTION DEVICE CONNECTING AN AIRCRAFT INTERNAL STRUCTURE COMPONENT TO THE FUSELAGE OF THIS AIRCRAFT - An aircraft including at least one door for passengers to board the aircraft, and at least one interconnection device connecting an aircraft internal structure component and a skin of a fuselage of the aircraft, the interconnection device being positioned near an internal periphery of the door in a region subject to external knocks and including at least one region that is weakened in terms of compression so as to absorb the knocks experienced by an external face of the skin of the fuselage, the device also being configured to withstand tensile forces applies to an internal face of the skin of the fuselage by internal pressure inside the aircraft. | 12-09-2010 |
20110036946 | AIRCRAFT FLOOR MODULE, STRUCTURE AND METHOD FOR ATTACHING SUCH A MODULE AND AIRCRAFT COMPRISING THEM - A method of fitting-out of an aircraft by laying of a floor, particularly in a cockpit of an aircraft, and such a fitted-out aircraft. The aircraft includes a fuselage part defining an interior volume and at least one internal on-board structure, the on-board structure being secured to the fuselage part and configured to accept a floor module. The method then involves introducing the floor module into the volume and attaching the floor module to the on-board structure. | 02-17-2011 |
20110036949 | STRUCTURAL MEMEBER OF AN AIRCRAFT HAVING A HOLLOW PART AND INDICATOR OF ICE FORMATION IN SUCH A HOLLOW PART - A structural element of an aircraft includes a hollow part. An indicator provides a visual indication, for example by moving, if ice forms in a given region of the hollow part. | 02-17-2011 |
20110042517 | DEVICE FOR CLOSING AN AIRCRAFT DOOR, AIRCRAFT COMPRISING SUCH A DEVICE - An aircraft door closing device, and an aircraft incorporating such a device. The door includes a leaf and, connected to the aircraft fuselage, a frame including an opening configured to take the leaf, the leaf adopting a closed position to block the opening and another position to reveal the opening. The device includes a bearing mechanism, some on the leaf and some on the frame, each formed by a crenelated structure, two crenelated structures being arranged such that the teeth of one pass through notches of the other as the leaf moves from one position to the other, and such that the teeth of the leaf structure bear, in the closed position, on the inside face of the corresponding teeth of the frame structure. | 02-24-2011 |
20130181092 | DEVICE AND METHOD FOR ASSEMBLING TWO SECTIONS OF AIRCRAFT FUSELAGE - Device for assembling two aircraft fuselage sections each comprising a skin and longitudinal stiffeners, the device comprising fishplates fishing couples of mutually aligned longitudinal stiffeners belonging respectively to said sections, each fishplate comprising two fishplate pieces each comprising at least one longitudinal sole plate intended to be fixed to a longitudinal stiffener, and a transverse support head, and at least one demountable connecting member able to mutually clamp the respective support heads of said fishplate pieces to allow a transmission of longitudinal forces between these fishplate pieces. | 07-18-2013 |
20140209740 | AIRCRAFT COCKPIT, IN PARTICULAR THE FRONT PORTION OF AN AIRCRAFT COCKPIT - A device for mixing at least two separate streams of components which, when mixed, form a combined fluid stream. The device comprises a conduit with at least two separate passageways leading to exit openings at an end face of the conduit. Each passageway communicates with a separate component stream and is arranged to direct the separate component stream in a downstream direction. The exit openings each have a predetermined cross-sectional flow area. A separate channel is located at a downstream end of each passageway exit opening. The channels are arranged to redirect the flow from each passageway to an axial direction. A single mixing chamber communicates with all of the separate channels, the mixing chamber being arranged to receive each of the component streams at an upstream end thereof and to permit a mixing of the component streams. An outlet is arranged downstream of the mixing chamber through which the combined fluid stream is dispensed. | 07-31-2014 |