Patent application number | Description | Published |
20090029599 | COMPUTER NETWORK CONNECTOR - A connector includes an insert including contacts having free parts to receive homologous flat contacts of a plug. The insert further includes a rotation axis about which the insert can be rotated and spring means urging the insert toward the position that it assumes when no plug is present. The insert can include, at the sides, long curved contacts and, in a central portion, shorter curved contacts, the points of contact of the contacts of the insert with the flat contacts of a plug being substantially aligned over all the contacts. | 01-29-2009 |
20090111300 | Rapid-Installation Connector for an Armored Cable - The invention concerns a connector for an armoured cable, this connector comprising a socket body and a conductive earthing member, the socket body being designed to receive a multi-conductor plug and comprising a wall element conformed so as to be in contact with this plug, and the earthing member comprising a band gripping the armouring of the cable and an elongate element electrically connecting the band to the socket body. According to the invention, the elongate element is flexible and the band takes the form of an open elastic clamp designed so as to be forcibly fitted on the armouring of the cable. | 04-30-2009 |
20090124109 | Conductor with Simplified Assembly for Multi-Conductor Cable - The invention concerns a connector designed to be fitted to a multi-conductor cable and which comprises at least one socket, a cable grip formed by a portion connected to the socket and a free portion articulated on the connected portion, and assembly means. The assembly means comprise a lever articulated around an articulation axis, held by the socket and distant from the articulation axis of the grip, wherein this lever has a curved end that may exert on the external surface of the free portion of the grip a thrust force which solicits the grip when closing in response to the application, on the lever, of a rotational torque around the articulation axis. | 05-14-2009 |
20090203239 | DEVICE FOR CONNECTING WITH SECURE ACCESS - The invention relates to a device for connecting with secure access, comprising a socket ( | 08-13-2009 |
20100159735 | CONNECTOR WITH SIMPLIFIED MOUNTING FOR A MULTIPLE CONDUCTOR CABLE - The invention relates to a connector to be mounted on a cable (K) with a plurality of insulated connectors (C), and including a comb ( | 06-24-2010 |
20100190372 | QUICK-FIT CONNECTION SOCKET FOR MULTI-CONDUCTOR CABLE - The invention relates to a socket to be mounted on a multi-conductor cable and including a removable comb ( | 07-29-2010 |
20110136382 | INSERT AND METHOD OF ASSEMBLING SUCH AN INSERT - The insert includes at least three contacts having essentially linear parts and at least one three-pole capacitance between three of the contacts. One of the contacts of each three-pole capacitance is connected to a central armature. A first dimension of the central armature, in the direction perpendicular to the substantially linear parts, is greater than a second dimension, in a direction parallel to the substantially linear parts, the second dimension defining the widths of the zones of the central armature. The mean width of the central armature, between the zones where it faces other armatures, connected to the other contacts of the three-pole capacitance, is greater than one third of the mean length of the central armature in these regions. Preferably, in at least one three-pole capacitance, the mean width of the central armature between the regions where it faces the lateral armatures is greater than one third of the distance between the lateral armatures. | 06-09-2011 |
Patent application number | Description | Published |
20090027261 | METHOD FOR THE CORRECTION, UPON RECEPTION IN A MOVING OBJECT, OF FAULTS AFFECTING THE TRANSMISSION OF BINARY OFFSET CARRIER RADIONAVIGATION SIGNALS - A subject of the present invention is a method for the correction, upon reception in a moving object, of faults affecting the transmission of binary offset carrier radionavigation signals, enabling this correction to be carried out in a simple and reliable manner. The method of the invention is characterized in that each component of the signal received by a conventional BPSK demodulation method is demodulated, in that the phase differential of the two signals is compensated for, source by source, and in that a coherent tracking is carried out by summing the complex outputs of the demodulation processing. | 01-29-2009 |
20090219201 | GNSS RECEIVER WITH ENHANCED ACCURACY USING TWO SIGNAL CARRIERS - A satellite positioning receiver is disclosed having at least one receive channel. Each receive channel is intended to perform a combined processing of a first S | 09-03-2009 |
20120188126 | Synthetic Aperture Antenna Device for Transmitting Signals of a Satellite Navigation System Comprising a Carrier and Means for Determining its Trajectory - A synthetic aperture antenna device for transmitting signals of a system includes a carrier and means for determining its trajectory, and, for each signal respectively associated with a spatial direction, processing means suitable for generating a stationary phase signal over a time window corresponding to the distance traveled by the device throughout the period of coherent integration, before modulation of the received signal, the processing means comprising correction means suitable for correcting the carrier phase of the signal. | 07-26-2012 |
20120212369 | METHOD AND SYSTEM FOR DETERMINING NAVIGATION PARAMETERS OF AN AIRCRAFT - Method for determining navigation parameters of an aircraft, characterized in that it consists at least in determining the geographic speed {right arrow over (V)}, expressed in a given local fixed coordinate system {{right arrow over (i)}, {right arrow over (j)}, {right arrow over (k)}}, based on the measurements m, of carrier phase increments Δφ | 08-23-2012 |
20120226395 | METHOD AND SYSTEM FOR DETERMINING THE ATTITUDE OF AN AIRCRAFT BY MULTI-AXIS ACCELEROMETRIC MEASUREMENTS - An inertial system measures the attitude of an aircraft consisting at least in determining the angle of pitch and/or the angle of heading and/or the angle of roll of the aircraft, each of the said angles of attitude being determined by successive double integration of their second derivative. A pair of accelerometers to determine the angle of pitch being are disposed on either side of the centre of gravity along an axis substantially merged with the longitudinal axis of the aircraft. A pair of accelerometers to determine the angle of heading are disposed on either side of the centre of gravity along an axis substantially merged with the transverse axis of the aircraft. A pair of accelerometers to determine the angle of roll are disposed on either side of the centre of gravity along a vertical axis perpendicular to the plane formed by the other axes. | 09-06-2012 |
20120314821 | AUTOMATIC GAIN CONTROL DEVICE FOR SATELLITE POSITIONING RECEIVERS - Automatic gain control device for satellite positioning receivers characterized in that it comprises means for estimating the temporal occupancy rate of the pulses within the useful band, closed-loop control of the automatic gain control being applied in an optimal manner as a function of the said temporal occupancy rate, in such a manner as to reduce the influence of the pulsed interference within the band and out-of-band; notably, an AGC decision module ( | 12-13-2012 |
20130093620 | DUAL FREQUENCY RECEIVER FOR SATELLITE BASED POSITIONING AND ASSOCIATED METHOD OF RECEPTION - Dual-frequency (L | 04-18-2013 |
20130120183 | DUAL FREQUENCY RECEIVER FOR SATELLITE-BASED POSITIONING AND ASSOCIATED METHOD OF RECEPTION - The present invention relates to a method for locating an aircraft (A | 05-16-2013 |
20140146929 | DEVICE FOR ELIMINATING LOCAL PERTURBATIONS FOR REFERENCE RECEIVER OF GNSS GROUND STATIONS - The present invention relates to a device for eliminating the perturbation signals received by a reference GNSS station. | 05-29-2014 |
20140368380 | SATELLITE RADIO NAVIGATION SYSTEM WITH REMOTE ARCHITECTURE - Station for receiving satellite radio navigation signals having first wideband transmission means that are suited to receiving a specific signal transmitted by a transmitter/receiver and extracting therefrom at least one user radio navigation signal, first centralized signal processing means that are suited to determining a measurement of pseudo distance and centralized calculation means for calculating navigation information (PVT), the reception station having a first reference channel for receiving radio navigation signals having a directional antenna for forming a channel, second means for processing the radio navigation signal received by said directional antenna for forming a channel and a calculation unit that is suited to performing an improvement in reliability, an integrity check and authentication of said navigation information (PVT). | 12-18-2014 |