Inventors list |
Assignees list |
Classification tree browser |
Top 100 Inventors |
Top 100 Assignees |
Chaix
Alain Chaix, Mandelieu-La Napoule FR
| Patent application number | Description | Published |
|---|---|---|
| 20120125571 | Heat-Dissipating Device for Space-Based Equipment, Notably for a Satellite - A device for dissipating heat, for a space-based satellite, includes at least one dissipating panel, the dissipating panel having at least one skin formed from a composite structure comprising an organic resin and carbon fibers, wherein the organic resin is filled with carbon nanotubes. The heat-dissipating device may also comprise a network of heat pipes. The heat pipes may be made from an aluminum alloy incorporating elements having low coefficients of thermal expansion. The present invention is notably applicable to fixed dissipating panels or those that may be used in telecommunications, observation or scientific satellites, or else on racks assembled to dissipating panels. | 05-24-2012 |
Carole Chaix, Chaponnay FR
| Patent application number | Description | Published |
|---|---|---|
| 20090053826 | Electropolymerisable monomers that are soluble in aqueous solution and electroactive probes that can be obtained with such monomers - The invention relates to an electropolymerizable monomer, intended to be polymerized in aqueous solution, comprising a single electropolymerizable unit and an electron-donating group, characterized in that it also comprises at least one arm ionizable in aqueous solution. The invention also relates to the polymerization process, to the electroactive probe thus obtained and to the method for the detection of a target ligand in a biological sample. | 02-26-2009 |
Catherine Chaix, Saint-Cloud FR
| Patent application number | Description | Published |
|---|---|---|
| 20120097102 | APPARATUS FOR DEPOSITING A THIN FILM OF MATERIAL ON A SUBSTRATE AND REGENERATION PROCESS FOR SUCH AN APPARATUS - Disclosed is an apparatus for depositing a thin film of material on a substrate and a regeneration process. The apparatus includes a chamber, a cryogenic panel disposed inside the chamber, a sample holder able to support a substrate, a gas injector able to inject a gaseous precursor into the chamber, a first trap connected to the vacuum chamber and able to trap a part of the gaseous precursor released by the cryogenic panel, the first trap having a fixed pumping capacity S | 04-26-2012 |
| 20120097105 | MOLECULAR BEAM EPITAXY APPARATUS FOR PRODUCING WAFERS OF SEMICONDUCTOR MATERIAL - A molecular beam epitaxy apparatus for producing wafers of semiconductor material includes a growth chamber surrounding a process area, a main cryogenic panel having a lateral part covering the inner surface of the lateral wall of the growth chamber, a sample holder, at least one effusion cell able to evaporate a material, a gas injector to inject a gaseous precursor into the growth chamber, a pumping element connected to the growth chamber to provide high vacuum capability. The apparatus includes an insulation enclosure covering at least the inner surfaces of the growth chamber walls, the insulation enclosure including cold parts having a temperature T | 04-26-2012 |
Nicolas Chaix, Saint-Martin D'Uriage FR
| Patent application number | Description | Published |
|---|---|---|
| 20110151607 | METHOD FOR MANUFACTURING A METAL AND DIELECTRIC NANOSTRUCTURES ELECTRODE FOR COLORED FILTERING IN AN OLED AND METHOD FOR MANUFACTURING AN OLED - A method for manufacturing an OLED and an electrode for an OLED, said electrode comprising a surface comprising a first dielectric nanostructuration and a second metal nanostructuration, on a substrate, wherein the following successive steps are carried out: | 06-23-2011 |
Philippe Chaix, Tournefeuille FR
| Patent application number | Description | Published |
|---|---|---|
| 20100076629 | System and Method for Merging Meteorological Data Predicted and Measured on an Aircraft - The invention consists in merging together the predicted and measured meteorological data to supply them to the flight prediction calculation system so as to smooth the discontinuities brought about in the prior art by the simple update which is carried out. This merging is advantageously done by linear weighting of the data, the weighting coefficient depending upon the positioning in vertical and horizontal distances between the predicted point and the aeroplane in relation to chosen thresholds. | 03-25-2010 |
| 20100131125 | METHOD FOR ASSISTING IN THE MANAGEMENT OF THE FLIGHT OF AN AIRCRAFT IN ORDER TO KEEP TO A TIME CONSTRAINT - The invention relates to the field of civil aviation and, more specifically, relates to the flight management systems, more commonly known by the English acronym FMS. The method for assisting in the management of the flight of an aircraft in order to keep to a time constraint according to the present invention allows for a control of the keeping to the time constraint that presents a rapid dynamic, by avoiding as far as possible having the estimated time of arrival (ETA) at a particular point (P) able to drift relative to a required time of arrival (RTA) at said particular point (P), thanks to the use of a manoeuvring margin (M) granted to the guidance module of the aircraft. | 05-27-2010 |
| 20100274418 | Method for Determining the Quantity of Fuel Taken On Board an Aircraft Making it Possible to Maintain a Time Requirement of the RTA Type - A method for determining the quantity of fuel in an aircraft and an optimization criterion such as a cost index, notably used in an FMS, making it possible to maintain a time requirement of the RTA type, comprising a first step of computing the optimization criterion CI | 10-28-2010 |
| 20110077859 | METHOD FOR AIDING THE MANAGEMENT OF A FLIGHT WITH A VIEW TO ADHERING TO A TIME CONSTRAINT - A method of flight management of an aircraft aimed at reaching a constrained point on a predetermined lateral trajectory assumed to be followed by the aircraft, at a required time of arrival RTA to within an absolute tolerance. The method including calculating a flight plan to be followed and a homing flight plan and when the estimated time of arrival ETA based on the homing flight plan strays from an absolute tolerance with respect to the calculation required time of arrival RTAc, calculating a new calculation required time of arrival NRTAc dependent on the calculation required time of arrival RTAc and a function f of the difference between the calculation required time of arrival RTAc and the estimated time of arrival ETA, and replacing the calculation required time of arrival RTAc with the new calculation required time of arrival NRTAc, before recalculating a flight plan to be followed. | 03-31-2011 |
| 20110295501 | METHOD OF PLANNING, TRAJECTORY COMPUTATION, PREDICTIONS AND GUIDANCE FOR COMPLIANCE WITH AN AIRCRAFT FLYPAST TIME CONSTRAINT - A method and device establishes trajectory planning, predictions and guidance so as to obtain the satisfaction of a time constraint (RTA). This objective is achieved by undertaking a computation of a trajectory up to the point where the flypast time constraint applies, on the basis of a profile of altitude and speeds, and then by computing the profile of speeds and altitudes making it possible, throughout the computed trajectory, to comply with the RTA. The method is also a method for readapting the trajectory and the vertical profile when during a mission, the data outside the aeroplane have caused the time predictions to drift and the constraint is no longer complied with under the initial speeds and trajectory assumptions. | 12-01-2011 |
| 20120036124 | METHODS OF ACCESSING A NAVIGATION DATABASE - A navigation database comprises a first set of elements comprising airports, beacons and waypoints; a second set of elements comprising procedures; and a third set of elements comprising routes. The method comprises a step of creating a pair of indices comprising an index comprising the elements of the three sets; identifier, a type and a functional identifier; a first list of pointers to the memory address where the elements are stored; a pre-index comprising a list of code, each code corresponding to the first characters of each element, the codes being indexed by a family of attributes of elements; a second list of pointers to the identifier of the first element in the first index. | 02-09-2012 |
Phillippe Chaix, Tournefeuille FR
| Patent application number | Description | Published |
|---|---|---|
| 20110077858 | METHOD FOR ASSISTING IN THE MANAGEMENT OF A FLIGHT IN ORDER TO KEEP TO A TIME CONSTRAINT - Method for assisting in the flight management of an aircraft aiming to reach a constraint point on a predetermined lateral trajectory that is assumed to have to be followed by the aircraft, at a required time of arrival RTA, said aircraft occupying a current position defined by a current altitude with a current horizontal speed. The method including, when it follows a rallying flight plan, calculating a new rallying flight plan following the lateral trajectory to be followed and including a new estimated speed profile different from the estimated speed profile over at least one update area, the new estimated speed profile including, over said update areas, either a value greater than that of the estimated speed profile, if the arrival time difference is positive, or a value less than that of the estimated speed profile, if the arrival time difference is negative. | 03-31-2011 |
Rodolphe Chaix, Cuers FR
| Patent application number | Description | Published |
|---|---|---|
| 20110147532 | Device for Deploying and Aiming Structural Elements in a Space Environment - A device for deploying and aiming structural elements designed to be placed in Earth includes at least one locking/unlocking device making it possible to deactivate the first coupling mode and to activate a second coupling mode allowing a portion of the device to be aimed at a target. The device uses: a plurality of structural elements linked together by articulations, the assembly forming an articulated arm linked to a payload via a root section; the articulations having at least one pivoting connection making it possible to have two consecutive structural elements pivot relative to one another; a motor making it possible to activate at least one pivoting connection of an articulation; and a system for coupling the articulations making it possible to link the pivoting of all of the structural elements comprising a first coupling mode. | 06-23-2011 |