Massot
Aurelien Rene-Pierre Massot, Vaux Le Penil FR
Patent application number | Description | Published |
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20090129917 | SEALING A ROTOR RING IN A TURBINE STAGE - A turbine stage in a turbomachine, the stage comprising a wheel mounted in a ring carried by a turbine casing, and a nozzle situated upstream from the wheel and including an annular fastener rim for fastening to the turbine casing, sealing being provided between the outer rim of the nozzle and the upstream end of the ring by a radial annular sheet bearing axially at its inner and outer peripheries against a downstream face of the outer rim of the nozzle, with its middle annular portion being axially spaced apart from the outer rim of the nozzle and bearing axially against the upstream end of the ring. | 05-21-2009 |
20090155061 | SECTORIZED NOZZLE FOR A TURBOMACHINE - A sectorized nozzle for a turbomachine, the nozzle being made up of cylindrical sectors and comprising two annular platforms interconnected by substantially radial vanes, together with an annular rail for supporting elements of abradable material, each inner platform having longitudinally-extending edges that are V-shaped, and each rail sector having, on at least one of its sides, means for bearing axially on corresponding means provided on an adjacent nozzle sector. | 06-18-2009 |
20090155071 | SEALING A HUB CAVITY OF AN EXHAUST CASING IN A TURBOMACHINE - The exhaust casing of a turbomachine includes a cylindrical jacket for guiding a flow of exhaust gas and for defining a hub cavity inside the casing, the jacket including at its ends an annular flange and a radial annular portion extending inwards and formed with an annular rim that is designed to be received in an annular groove of the inner wall of the exhaust casing to close the hub cavity in substantially sealed manner. | 06-18-2009 |
20140348637 | INTERFACE DEVICE BETWEEN TWO TURBOMACHINE ELEMENTS - The main purpose of the invention is an interface device ( | 11-27-2014 |
Aurélien René-Pierre Massot, Moissy Cramayel FR
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20160003088 | COOLING DEVICE FOR THE CASING OF AN AIRCRAFT JET ENGINE COMPRISING A SUPPORTING DEVICE - A cooling device for the casing of a jet engine, includes a cooling tube and a supporting device, the supporting device including an attachment plate and an attachment clamp, the attachment clamp including a clamp body surrounding the cooling tube and an attachment element attached to the attachment plate, wherein the attachment plate includes: an opening; and an attachment tab secured to the main wall of the attachment plate and arranged on at one portion of the periphery of the opening, the attachment clamp passing through the opening, and the attachment element of the attachment clamp being attached to the attachment tab. | 01-07-2016 |
Felix Massot, Mauquenchy FR
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20090309339 | CURTAIN AIRBAG UNIT - Curtain air bag unit for a motor vehicle is provided which comprises an air bag extending parallel to the longitudinal axis of the motor vehicle. Further it comprises fixing means for fixing the air bag in the area of the roof bar of the motor vehicle, whereby the fixing means comprise a tension member, that extends from a first fixing element to a second fixing element. It also comprises tensioning means for influencing the tensile stress of the tension member during mounting of the curtain air bag unit into the motor vehicle. A pre-cut tension member can be used whose length is chosen in a way that the mounting in the vehicle can be carried out simply and conveniently. | 12-17-2009 |
Gilles Massot, Voisenon FR
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20130218399 | METHOD AND SYSTEM FOR MONITORING THE LEVEL OF OIL CONTAINED IN A TANK OF AN AIRCRAFT ENGINE - A method of monitoring oil level in a tank of an aircraft engine, including: for at least two predetermined operating stages of the engine, during at least one mission of the aircraft: obtaining a plurality of measurements of an oil level of the tank, each measurement being associated with an oil temperature and with an engine speed of rotation, and selecting measurements representative of oil level variations and associated with oil temperatures that are close to a reference temperature and with engine speeds of rotation that are close to a reference speed of rotation; aggregating the measurements selected over the operating stages and during the at least one mission of the aircraft; and comparing the aggregated measurements with reference data to identify abnormal oil consumption of the engine. | 08-22-2013 |
Gilles Claude Gabriel Massot, Voisenon FR
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20090194485 | DETECTING THE CLOGGING OF A FLUID FILTER - The invention relates to the field of fluid filters. It provides a method of detecting clogging of a fluid filter, which method comprises measuring, at successive sampling instants, the pressure difference ΔP from upstream to downstream across the filter, and then calculating the first time derivative {ΔP}′ of the pressure difference ΔP at different instants, and then sending a clogging signal S | 08-06-2009 |
Lucie Massot, Aix En Provence FR
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20140200790 | MONITOR SYSTEM FOR MONITORING THE STARTING OF A ROTARY WING AIRCRAFT, AN AIRCRAFT, AND A METHOD USING THE SYSTEM - A method of starting a turboshaft engine ( | 07-17-2014 |
20150367951 | MONITOR SYSTEM FOR MONITORING THE STARTING OF A ROTARY WING AIRCRAFT, AN AIRCRAFT, AND A METHOD USING THE SYSTEM - A method of starting a turboshaft engine ( | 12-24-2015 |
Max Massot, Barsac FR
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20150040396 | METHOD OF FABRICATING A COMPOSITE MATERIAL TURBINE ENGINE VANE WITH INCORPORATED PLATFORMS - Multilayer weaving is used to form a fiber blank having a longitudinal direction corresponding to the longitudinal direction of the vane to be made and comprising across its thickness a first woven portion with a plurality of layers of yarns interlinked by weaving, and also a second and third woven portions. The first portion is situated between the second and third portions and interlinked thereto by weaving over only a fraction of its longitudinal dimension. A preform for the vane is formed by folding out, on either side of the first portion, segments of the second and third portions not interlinked with the first portion, by shaping the first portion to form a preform portion for the airfoil of the vane, and by shaping the folded-out segments of the second and third portions to form preform portions for the inner and outer platforms of the vane to be fabricated. | 02-12-2015 |
Oriol Massot, Barcelona ES
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20140187779 | Process for preparing [4,6-bis-dimethylamino-2-[4-(4-trifluoromethylbenzoylamino)benzyl]pyrimid- in-5-yl]acetic acid - The present invention relates to a process for preparing a compound of formula (I). | 07-03-2014 |
Ronan Massot, Vertout FR
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20100175697 | FLUID PRODUCT DISPENSING DEVICE - A fluid dispenser device comprising a body ( | 07-15-2010 |