Thorel
Alain Thorel, Saint-Vrain FR
Patent application number | Description | Published |
---|---|---|
20080213639 | High Temperature Fuel Cell With Mixed Anionic and Protonic Conduction - This invention concerns a high temperature fuel cell with mixed anionic and protonic conduction having a protonic conduction reforming membrane directly coupled to a solid oxide fuel cell with conduction by oxygen ions, enabling use of a gradually reforming anode generating carbon deposits to be avoided. The reverse operation of the present invention outside the reforming stage forms a high water temperature electrolyser to produce hydrogen efficiently without having to separate it from water as is the case with current systems. | 09-04-2008 |
20120156573 | FUEL CELL WITH MONOLITHIC ELECTROLYTES MEMBRANE ASSEMBLY - The invention relates to a fuel cell ( | 06-21-2012 |
Alain Thorel, Evry Cedex FR
Patent application number | Description | Published |
---|---|---|
20120022231 | Method for Manufacturing Cubic Diamond Nanocrystals - A method for manufacturing cubic diamond nanocrystals ( | 01-26-2012 |
20150104804 | Method for Manufacturing Cubic Diamond Nanocrystals - A method for manufacturing cubic diamond nanocrystals (10) comprising the following successive steps: | 04-16-2015 |
Chiristophe Thorel, Le Haver FR
Patent application number | Description | Published |
---|---|---|
20110068222 | PROPULSION UNIT FOR AN AIRCRAFT AND AIR INTAKE STRUCTURE FOR SUCH A UNIT - This propulsion unit for an aircraft comprises: a fan ( | 03-24-2011 |
Christophe Thorel, Le Havre FR
Patent application number | Description | Published |
---|---|---|
20090107108 | NACELL FOR BYPASS ENGINE WITH HIGH BYPASS RATIO - This invention relates to a nacelle for bypass engine with a high bypass ratio comprising an interior flow channel for a secondary flow generated by the bypass engine and having an external structure provided with a reverse thrust device capable of alternately shifting from a closed position in which it enables circulation of the direct-jet secondary flow inside the interior channel, to an open position in which it uncovers an opening in the external structure so as to enable reorientation of the secondary flow in an angled flow via activation of the reverse thrust means; in open position, the reverse thrust device partially blocks the interior channel so as to provide a leakage section therein, enabling circulation of a controlled leakage flow, said nacelle being characterized in that, when the thrust reversal device is in open position and has an angled-jet reversal section and a leakage section through the interior channel the sum of which is substantially equal to a direct-jet secondary flow discharge section, when the thrust reversal device is in closed position. | 04-30-2009 |
20100232932 | AIR INLET SHROUD STRUCTURE - The present invention relates to a nacelle for a turbojet, comprising an air inlet structure capable of channelling a flow of air to a turbojet fan and a middle structure ( | 09-16-2010 |
20130315657 | UNIT FOR AN AIRCRAFT THRUSTER - A unit for an aircraft thruster is provided that includes a first ferrule configured to be attached to a second ferrule and a first connection flange configured to be secured to a second corresponding connection flange secured to the second ferrule. The connection flange includes a portion forming a plane extending along a radial direction with respect to the first ferrule. A link between the first ferrule and the corresponding connection flange is offset to a distance from said plane corresponding to a length for damping a shear-generating flexural moment, generated by fluxes of forces passing through the first ferrule. | 11-28-2013 |
20140086678 | ASSEMBLY FOR AN AIRCRAFT NACELLE - An assembly for an aircraft nacelle includes a reinforcing plate and a flange that includes one first portion and one second portion. The first portion of the flange is attached to another flange, and the second portion extends transversely relative to the first portion and is attached onto a panel of the assembly. In particular, the reinforcing plate is attached directly, or optionally indirectly, onto the flange via an intermediate plate attached between the reinforcing plate and the flange. The reinforcing plate has a beveled portion opposite the second portion of the flange. | 03-27-2014 |
Delphine Thorel, Nanterre FR
Patent application number | Description | Published |
---|---|---|
20150369129 | FACILITY WITH A GAS TURBINE AND METHOD FOR REGULATING SAID FACILITY - The invention relates to an installation with a gas turbine, comprising: | 12-24-2015 |
Fabrizio Thorel, Douvaine FR
Patent application number | Description | Published |
---|---|---|
20160067212 | USE OF INSULIN SIGNALING ANTAGONISTS, OPTIONALLY IN COMBINATION OF TRANSFECTION OF NON-BETA CELLS, FOR INDUCING INSULIN PRODUCTION - The invention relates to methods of inducing insulin production in non-beta-cells or converting non-beta-cells into insulin producing cells, as well as methods of preventing and/or treating diabetes and methods of predicting the susceptibility of a diabetic subject to a treatment. | 03-10-2016 |
Jean-Noel Thorel, Paris FR
Patent application number | Description | Published |
---|---|---|
20120121534 | INJECTABLE COMPOSITION COMBINING A FILLING AGENT AND A FIBROBLAST GROWTH MEDIUM - The invention relates to a composition that can be subcutaneously or intradermally injected, comprising: a filling agent; and a fibroblast growth medium. | 05-17-2012 |
Jean-Noël Thorel, Paris FR
Patent application number | Description | Published |
---|---|---|
20120237610 | INJECTABLE COMPOSITIONS FOR INTRA-ARTICULAR USE COMBINING A VISCOSUPPLEMENTATION AGENT AND A FIBROBLAST GROWTH MEDIUM - Provided is an injectable composition for intra-articular administration including at least one viscosupplementation agent selected from hyaluronic acid, chondroitin sulphate, keratin, keratin sulphate, heparin, cellulose and derivatives thereof, for example, chitosan, xanthans, galactomannan, alginates, and one or more salts thereof, and a fibroblast growth medium. The viscosupplementation agent and the fibroblast growth medium can be provided in a single composition for injection or as separate components for simultaneous, separate, or subsequent injection over time. | 09-20-2012 |
Magali Thorel, Paris FR
Patent application number | Description | Published |
---|---|---|
20130024050 | ON-BOARD MAINTENANCE SYSTEM OF AN AIRCRAFT, AND ASSOCIATED AIRCRAFT - An on-board maintenance system for an aircraft, said aircraft comprising pieces of equipment connected together through a first on-board data transmission network for exchanging operational data intended for piloting the aircraft, said maintenance system including a processing unit and being characterized in that it comprises a second data transmission network, distinct from the first network, for exchanging data intended for maintenance of the equipment of the aircraft, said second network connecting at least some of said pieces of equipment to the processing unit; said processing unit are being adapted for receiving in real time, a data provided by the pieces of equipment on the second network and processing them with view to determining the cause of equipment malfunctions according to at least said received data. | 01-24-2013 |