Assignee: MBDA France

Location: Paris, FR
No. of patents: 19

Number	Title	Issue Date
8145461	Method of functional control of an inertial platform of a moving craft A method for verifying an inertial unit for a moving body, the unit being mounted on a movement simulator, and the method includes: theoretical modeling of the inertial unit on the movement simulator, supplying theoretical inertial data representing measurement iner...	03/27/2012
8030228	Cover for camouflage against electromagnetic radiation A cover for camouflage against electromagnetic radiation. According to the invention, the cover includes a random set of puckered features in relief, these being formed by a camouflage net associated with a flexible dielectric mesh. ...	10/04/2011
8022343	Aiming system with integrated deviation meter According to the invention, the system comprises an infrared detector (7) for alternately generating images (5′) of sources of light (5) in the near infrared emitted by a missile flying towards a target and thermal images of the observed scene...	09/20/2011
7913605	Missile launcher This missile launcher is characterized in that the cells do not extend in rows parallel to an elongated chimney, but by surrounding a central chimney, providing a more compact and especially lighter arrangement with identical resistance conditions. ...	03/29/2011
7788680	Method and system for event management The invention relates to managing events in a standard computer system comprising a central unit connected to memory units and peripheral devices by a data bus (50) allowing a multimaster configuration, the method comprising the following steps: ...	08/31/2010
7763834	Flying object for observing the ground A flying object includes a lift and displacement motor which has a combustible propelling charge and direct thrust flight control and can ensure the lift and displacement of the flying object in an observation position for which the flying object is at least approxi...	07/27/2010
7672480	Method for photographing on board of a flying rotating body and system for carrying out said method The invention relates to a method for photographing on board of a flying rotating body and system for carrying out said method. According to said invention, pictures (V0, V90, V180, V270) are taken at predetermined angular...	03/02/2010
7582853	Method and device for producing an optical link using light flashes The invention relates to a method and device for producing an optical link using light flashes. According to the invention, an arrangement (13) comprising a plurality of capacitors (C1 to C5) is provided in order to power a flash lamp (3)...	09/01/2009
7503149	Method for making a double-walled thermostructural composite monolithic component and resulting component A method of producing a double-walled thermo-structural composite monolith may include assembling, by stitching, a sandwich having a core and outer fibrous armors. The stitched sandwich structure is impregnated with a viscous resin. After the resin hardens, the core...	03/17/2009
7474856	Method and device for producing an optical link with laser pulses A method and device produce an optical link with laser pulses between an emitter of the pulses and a receiver of the pulses. The optical link is used by a locating device for locating a body moving at constant speed away from the locating device. The locating device...	01/06/2009
7464534	Pulsed detonation engine A pulsed detonation engine may include a flame tube with a lateral wall and a transverse base defining a combustion chamber and a supply device cyclically feeding said combustion chamber with a combustible charge. The transverse base of the flame tube may be movable...	12/16/2008
7410119	Rotating missile emitting light pulses The invention concerns a rotating missile emitting light pulses. The invention is characterized in that means are provided to interrupt said light pulses (5) when the rotational movement (3) of the missile (2) about its longitudinal axis (L-L) s...	08/12/2008
7053356	Photodetection cell and laser pulse detector having a cascoded inverting amplifier looped back through a slow follower type feedback Photodetection cell and laser pulse detector furnished with such a cell, as well as laser pulse detection device comprising a matrix of such detectors. The photodetection cell (1) is embodied in the form of an integrated circuit and comprises a photose...	05/30/2006
7000398	Ramjet engine combustion chamber and ramjet engine equipped with same The invention concerns a combustion chamber whereof the inner wall (17)is made at least partly of a thermostructural composite material, which is porous to the fuel passing through the double wall (14); and the porosity of said inner wall (17) i...	02/21/2006
6953924	Method for extracting an illuminate zone from a photosensor matrix A method for extracting an illuminated zone from a matrix of photosensors may include: (a) dividing the matrix into a plurality of search zones, (b) searching for the presence of an active photosensor in the search zones, (c) stopping the search as soon as an active...	10/11/2005
6915626	Blanking-plug system for blanking off an orifice of a pipe, particularly for blanking off an orifice of a duct for introducing air into the combustion chamber of a ramjet A blanking-plug system for blanking off an orifice of a pipe, particularly for blanking off an orifice of a duct for introducing air into the combustion chamber of a ramjet. The blanking-plug system (16) comprises at least one blanking plug (15)...	07/12/2005
6915627	Rocket engine The invention concerns a rocket engine wherein the combustion chamber includes at least one first monolithic component made of a thermostructural composite material comprising a porous wall through which the fuel is introduced in the core of the combustion chamber. ...	07/12/2005
6672068	Ramjet for a supersonic and hypersonic aircraft According to the invention, the wall (5) is mounted movably as one so as to be able to slide longitudinally in translation, bringing the joint line (14) closer to the fuel injector (9) so as progressively to modify the geometries of the oxidant inlet (16)...	01/06/2004
6658985	Site head with integrated laser designator for use in aircraft such as a rotorcraft Sight head with integrated laser designator for use in an aircraft such as a rotorcraft. The laser designator (32) is integrated into a zone of a main external assembly of the pod (14) of the sight head (12), enclosed externally in an existing fairing (34...	12/09/2003

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Assignee: MBDA France