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Results 1-10 of 79,818 for Criteria: Office(s):all Language:EN Stemming: true maximize
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TitleCtrPubDate
Int.ClassAppl.NoApplicantInventor
1. WO/2016/113473 O-QUINONE COMPOUNDS AS AGENTS NEUTRALISING NITRIC OXIDEWO21.07.2016
A61K 31/122
PCT/FR2015/050064INSTITUT DES SUBSTANCES VÉGÉTALESJEAN, Daniel
The invention relates to O-quinone compounds of general formula (I) as agents neutralising nitric oxide, and to the therapeutic or cosmetic use thereof.

2. WO/2016/113506 METHOD FOR DETERMINING A FILTER FOR AN OPHTHALMIC LENS AND OPHTHALMIC LENS COMPRISING SUCH A FILTERWO21.07.2016
G02C 7/02
PCT/FR2016/050065ESSILOR INTERNATIONAL (COMPAGNIE GÉNÉRALE D'OPTIQUE)SCHERLEN, Anne-Catherine
The invention relates to a method for determining a filter for an ophthalmic lens to be placed in front of the eye of the wearer, said filter being able to improve or maintain the visual comfort and/or the visual performances of said wearer. According to the invention, the determination method comprises: a step of measuring a variable representative of sensitivity of the eye or both eyes of the wearer to a characteristic light flow, and a step of determining at least one optical characteristic of said filter according to the representative variable measured.

3. WO/2016/113507 SYSTEM FOR CONNECTING A DECENTRALIZED, SINGLE-PHASE GENERATOR TO A THREE-PHASE GRIDWO21.07.2016
H02J 3/26
PCT/FR2016/050066INSTITUT POLYTECHNIQUE DE GRENOBLEMERCIER, Aurélien
The invention relates to a system for connecting a decentralized, single-phase generator to one phase or another of a three-phase grid. Said system includes: - an analyzer, providing the values VØ1, VØ2, and VØ3 of the voltages of the three phases and the value of the current I flowing towards one of the three phases; - a processor capable of making the following relations comply: (VØi + θØi*Ι)β < VØi+1 or i+2, VØi < VØi+1 or i+2' I > n Imax, wherein i = 1, 2 or 3, modulo 3, αØi is a sensitivity coefficient, β is a weighting coefficient greater than 0.5, n is a coefficient less than 0.5, and Imax is the maximum current that the generator can provide; - a switch for switching the output of the single-phase generator from the phase i+1 or i+2 to the phase i if the three relations above are satisfied; and - a memory for storing, upon each instance of switching, the value αØi of the sensitivity of the phase i.

4. WO/2016/113510 DRUM FOR PRODUCING A TYRE BLANKWO21.07.2016
B29D 30/24
PCT/FR2016/050071COMPAGNIE GENERALE DES ETABLISSEMENTS MICHELINMONBRUN, Florent
The invention relates to a drum (2) for producing a tyre casing blank, comprising sections (8) forming a circumferential face of the drum, expansion means (40, 36, 28, 30, 32) that can move the sections in the radial direction such that all of the sections extend at the same distance from the shaft at any given moment, and regulating means (12, 22) different from the expansion means and able to move the sections in the radial direction such that all of the sections extend at the same distance from the shaft at any given moment. The expansion means can be used in any position of the sections under the effect of the regulating means.

5. WO/2016/113511 METHOD FOR CORRECTING THE CALCULATION OF A FLIGHT CHARACTERISTIC OF AN AEROPLANE BY TAKING VERTICAL WIND INTO ACCOUNT, METHOD FOR CALCULATING THE DRAG COEFFICIENTWO21.07.2016
G01P 13/02
PCT/FR2016/050072BERDOULAT, LaurentBERDOULAT, Laurent
The invention relates to a method for correcting at least one result of calculating at least one flight characteristic of an aeroplane, in particular a drag coefficient Cx of the aeroplane, said calculation being based on in-flight measurements and on values calculated using said measurements, the in-flight measurements being taken under at least one predetermined flight condition defining a predetermined flight point, each flight condition being defined by specific flight parameter values, said measurements and values being, in particular: θmesure the measured attitude of the aeroplane and αmodèle the angle of attack of the aeroplane calculated by solving a lift equation and an aerodynamic model linking the angle of attack α of the aeroplane to at least one flight parameter which is the lift coefficient Cz of the aeroplane. The attitude measurements θmesure are corrected by a term for correcting the attitude Δθο which is a specific constant for each flight and the calculated angles of attack αmodèle are corrected by a term for correcting the angle of attack Aa(Cz...). The terms for correcting the attitude Δθο and the angle of attack Δα(Cz...) are calculated under the constraint that the vertical wind WZ is practically zero on average.

6. WO/2016/113512 WEAR ADJUSTMENT MECHANISM FOR A CLUTCH DEVICE, PARTICULARLY FOR A MOTOR VEHICLEWO21.07.2016
F16D 13/75
PCT/FR2016/050074VALEO EMBRAYAGESLEBAS, Gilles
The invention relates to a wear adjustment mechanism for a clutch device comprising: - a wear adjustment member (12) including a first ramp (14) for engaging with a counter-ramp; and - a wear detection member (16) including a second ramp (18) for engaging with the counter-ramp. At least one resilient member (20) is mounted between the wear adjustment member (12) and the wear detection member (16) and comprises at least two arms (21) that are connected to each other by resilient means (22) that tension the two arms (21) to separate same from each other. Each arm (21) is capable of engaging with the wear adjustment member (12) and/or the wear detection member (16) so as to move the wear adjustment member (12) relative to the wear detection member (16).

7. WO/2016/113479 STORAGE BATTERY SYSTEM WITH LOW CONSUMPTION VOLTAGE MEASUREMENTWO21.07.2016
H01M 10/48
PCT/FR2015/053556RENAULT S.A.SPALMIERI, Michaël
The invention relates to a storage battery system (1), comprising: - first and second accumulator stages (41, 42); - a first control device (31) supplied with power by the first stage (41); - a second control device (32) supplied with power by the second stage (42), configured to apply, on an output interface, a numerical sequence coding a measured potential difference; - a communication circuit (6) via which the output interface (322) communicates with an input interface (311); - a power supply circuit (313), a control interface (314) of the switch (315) being connected so that the maintaining of at least one logic level on said output interface (322) involves the application of said power supply on said first control device (31); - a control circuit (317) for selectively ordering the cutting off of the power supply from said first control device (31).

8. WO/2016/113482 ATTACHMENT DEVICE OF A MOTOR VEHICLE POWER TRAIN HAVING A BATTERY SUPPORTWO21.07.2016
H01M 2/10
PCT/FR2015/053615PEUGEOT CITROEN AUTOMOBILES SACHALVET, Manuel
The invention relates to an attachment device (10) of a motor vehicle power train, comprising: a body (14) intended to be fixed to a longitudinal structural profile section of the vehicle; an arm (16) intended to be fixed to the power train of the vehicle, said arm (16) being fixed to the body (14) in a flexible manner; a battery support (18) forming an integral part of the body (14). The body (14) comprises a lateral face (22) intended to be in contact with the structural profile section, the battery support (18) forming an upper face (24) extending transversely, preferably perpendicular, to the lateral face (22). The invention also relates to a vehicle comprising such an attachment device (10).

9. WO/2016/113474 MOTOR VEHICLE PROVIDED WITH AN AUTOMATIC STARTING/STOPPING SYSTEM AND A SYSTEM FOR DETECTING BELT SLIPPAGEWO21.07.2016
F02N 11/08
PCT/FR2015/053356PEUGEOT CITROEN AUTOMOBILES SAMALOT, Alex
The invention relates to a motor vehicle comprising a combustion engine (1), a starter or starter-alternator (2), a belt (4) for driving the combustion engine (1) by means of the starter or starter-alternator (2), a module (6) for detecting the risk of the belt (4) slipping, and a module for estimating a distance (8) between the vehicle and a preceding vehicle in such a way that the module (6) for detecting the risk of the belt (4) slipping is designed to detect a risk of the belt (4) slipping by taking account of a distance estimated by the estimation module (8).

10. WO/2016/113489 DEVICE AND METHOD FOR CONTROLLING AN AUXILIARY ENGINE SUITABLE FOR SUPPLYING THRUST POWER TO THE ROTOR OF A HELICOPTERWO21.07.2016
B64C 27/04
PCT/FR2016/050038TURBOMECAMARIN, Jean Philippe, Jacques
The invention relates to a device for controlling an auxiliary engine (8) including a gas generator and a free turbine suitable for being connected mechanically to the rotor (12) of a helicopter in order to supply same with thrust power, characterised in that said control device includes a proportional-plus-integral controller (30) having proportional gain (Kp) and integral gain (Ki), which are functions of the speed of rotation of said gas generator, said controller (30) being configured to receive an error signal representing a speed error of said free turbine, and to generate a signal (Sc) for correcting the drive speed of said gas generator obtained by adding a signal which is proportional to said error signal according to said proportional gain (Kp), and an integrated signal (Si), resulting from adding a signal which is proportional to said error signal according to said integral gain (Ki) and a memory signal (Sm), provided by a feedback loop (31) of said integrated signal (Si), said memory signal (Sm) being dependent on a measurement that represents the speed of rotation of said free turbine.


Results 1-10 of 79,818 for Criteria: Office(s):all Language:EN Stemming: true
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