Emeric
Emeric Baracat-Nasr, Croissy-Sur-Seine FR
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20160030301 | Method for Manufacturing a Cosmetic Article Having a Decorative Embossed and/or Debossed Surface - The invention relates to a method of manufacturing a cosmetic article having a decorative embossed and/or debossed surface, based on at least one cosmetic product hot-poured into a container, this method making use of: a receptacle forming said container and having a peripheral wall and a bottom, said receptacle having at least one filling area, each filling area extending from the bottom of said receptacle and having a filling hole and at least one vent hole, and a closure member that cooperates with the receptacle to define an enclosed filling cavity with the at least one filling area, and having an embossed and/or debossed surface adapted to give the cosmetic product poured into said cavity an embossed and/or debossed surface, said method comprising at least the following steps: a) positioning the receptacle on the closure member so that the embossed and/or debossed surface extends into the filling area; b) hot-injecting the cosmetic product into the filling cavity by means of a filling head inserted in the filling hole; c) separating the receptacle from the closure member. | 02-04-2016 |
Emeric Chancerelle, Toulouse FR
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20100087132 | Air Intake Arrangement for a Vehicle, in Particular an Aircraft - The arrangement of the invention includes mobile means for blocking an air passage channel (10) which are controlled by an aerodynamic surface (20) provided in said air passage channel (10) and capable of generating a lift force (P) under the action of the external air flow (F) flowing through said air passage channel (10). | 04-08-2010 |
20110253843 | Air Intake Arrangement For An Aircraft - The invention relates to an arrangement ( | 10-20-2011 |
20130032669 | FASTENING DEVICE PARTICULARLY SUITABLE FOR THE FASTENING BETWEEN AN AIR INTAKE AND AN ENGINE OF AN AIRCRAFT NACELLE - An aircraft nacelle with a connecting device between a first conduit of an air intake and a second conduit of a motor, both conduits being arranged end-to-end, the connecting device including an annular flange connected to the air intake, an annular flange connected to the motor pressed against annular flange of the air intake, the flanges extending in a plane perpendicular to the longitudinal axis of the nacelle; bolt holes formed in annular flanges and disposed plumb to one another; and connecting elements located in bolt holes, for connecting the annular flanges, wherein at least one flange includes at least one opening interposed between a bolt hole and junction zone of the flange and/or between a bolt hole and outer edge of the flange. | 02-07-2013 |
Emeric Daniau, St. Florent Sur Cher FR
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20100186370 | PULSE DETONATION ENGINE OPERATING WITH AN AIR-FUEL MIXTURE - The invention relates to a pulse detonation engine operating with an air-fuel mixture. According to the invention, the engine ( | 07-29-2010 |
20110030340 | PULSE DETONATION ENGINE - According to the invention, the said engine (I), which comprises at least one flame tube ( | 02-10-2011 |
20110088370 | PULSED DETONATION ENGINE - According to the invention, the engine (I) includes a means for supplying fuel to the combustion chamber ( | 04-21-2011 |
Emeric De Foucauld, Seyssinet FR
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20090066440 | METHOD FOR AUTOMATIC IMPEDANCE MATCHING FOR A RADIOFREQUENCY CIRCUIT AND TRANSMISSION OR RECEPTION SYSTEM WITH AUTOMATIC MATCHING - The invention relates to a method for automatically matching the antenna impedance for a radiofrequency transmission circuit having an amplifier. An impedance matching network is inserted between the amplifier and the antenna. The output current i and voltage V from the amplifier and their phase shift are measured, and from this the complex impedance, defined by V/i, is deduced. The antenna impedance is calculated as a function of this complex impedance and as a function of the known present values of the adjustable impedances of the matching network. New values are calculated, from the calculated value of the antenna impedance, for the adjustable impedances of the matching network that allow an overall load impedance of the amplifier to be obtained which is as close as possible to the nominal load impedance Z | 03-12-2009 |
20120256689 | Radiofrequency Emission or Reception Chain with Automatic Impedance Adaptation, and Corresponding Method - As relates to automatic matching of antenna impedance for a radiofrequency transmit or receive circuit, an impedance matching network is inserted between an amplifier and antenna. The current i and output (resp. input) voltage V of the amplifier and their phase shift are measured, the complex impedance defined by V/i is deduced; the impedance of the antenna is calculated as a function of this complex impedance and the known existing values of the adjustable impedances of the matching network. New adjustable values of impedances of the matching network to obtain a desired overall load impedance for the amplifier are calculated on the basis of the calculated antenna impedance value, and the matching network is controlled to adjust the adjustable impedances to these new values. The measurement is made at a measurement frequency different from the working frequency to allow automatic matching without interrupting normal operation of the chain. | 10-11-2012 |
20120326758 | FREQUENCY SYNTHESIS DEVICE WITH FEEDBACK LOOP - A frequency synthesis device with a feedback loop includes: a phase-comparison control circuit; a frequency conversion unit voltage controlled by the control circuit; a feedback loop for supplying at least one signal issuing from the frequency conversion unit to the control circuit; at least one other control circuit for voltage control of the frequency conversion unit; and at least one other feedback loop for supplying at least one other signal issuing from the frequency conversion unit to the other control circuit. | 12-27-2012 |
Emeric De Foucauld, Voiron FR
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20120169566 | IMPEDANCE MATCHING METHOD FOR A MULTIBAND ANTENNA, AND TRANSMISSION OR RECEIVER CHANNEL HAVING AUTOMATIC MATCHING - An automatic antenna impedance matching method for a radiofrequency transmission circuit. An impedance matching network is inserted between an amplifier and an antenna. The output current and voltage of the amplifier and their phase difference are measured by a variable measurement impedance, and the complex load impedance of the amplifier is deduced from this; the impedance of the antenna is calculated as a function of this complex impedance and as a function of the known current values of the impedances of the matching network. Starting from the value found for the impedance of the antenna, new values of the matching network are calculated that allow the load to be matched to the nominal impedance of the amplifier. The measurement impedance has a value controllable by the calculation processor according to the application and notably as a function of the operating frequency and of the nominal impedance of the amplifier. | 07-05-2012 |
20120256698 | Automatic Impedance Matching Method for Radiofrequency Circuit and Modular Emission or Reception Chain - As relates to the automatic impedance matching of a radiofrequency system, a system comprises three modules. In a matching phase a matching computation module is connected in a detachable manner between an amplification module and an antenna module containing an antenna, a matching impedances network, and memory means for storing control data of the network; then a matching computation is carried out; the computation module supplies control data of the network to the memory device. In a phase of using the system, the second module is removed and the antenna module is connected in a detachable manner directly to the amplification module, the matching network being controlled by the stored control data, which correspond to the desired impedance matching. | 10-11-2012 |
Emeric D'Herbigny, Paris FR
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20150047356 | TURBINE ENGINE, SUCH AS A TURBOJET OR A TURBOPROP ENGINE - A turbine engine, a turbojet, or a turboprop engine, including an annular combustion chamber defined by an inner shell and an outer shell, a turbine distributor arranged downstream of the combustion chamber, with a downstream end of the outer shell and/or of the inner shell of the chamber including a radial rim arranged opposite a radial rim of an upstream end of the distributor, a sealing mechanism including at least one strip extending between the rims to provide a seal between the combustion chamber and the distributor. The sealing strip extends axially and circumferentially between the rims and bears sealingly against free ends of the rims. | 02-19-2015 |
Emeric Frejafon, Villiers Sous Saint Leu FR
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20150241357 | METHOD AND SYSTEM FOR ANALYSING PARTICLES IN COLD PLASMA - The invention relates to a method of analyzing particles, in particular particles of diameter less than 1 μm, the method comprising the following steps: | 08-27-2015 |
Emeric Malefant, Worcester, MA US
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20150184694 | COMPOSITE BEARINGS HAVING A POLYIMIDE MATRIX - The present disclosure relates to bearing and seal assemblies comprising a composite structure which includes a substrate and a layer disposed on the substrate. The layer disposed on the substrate includes a polyimide matrix and a filler dispersed within the polyimide matrix. The filler can be a thermoplastic polymer, such as PTFE, and/or an organic filler. The bearing assembly can exhibit a synergistic improvement in wear resistance and coefficient of friction. | 07-02-2015 |
Emeric Reynaud, Muttenz CH
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20100233259 | DOSAGE FORM OF ROPINIROLE - The present invention relates to a dosage form of Ropinirole. The dosage formulation of the invention is intended to control the release rate of one or more therapeutically active agents. | 09-16-2010 |