Raes
Marc Raes, Brunoy FR
Patent application number | Description | Published |
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20110169640 | TURBO-MACHINE CONTROL INSTALLATION EQUIPPED WITH A PASSIVE RADIOFREQUENCY IDENTIFICATION CHIP UNIT VERIFICATION SYSTEM - This invention relates to a control installation ( | 07-14-2011 |
20140145737 | METHOD FOR CORRECTING THE VOLTAGE MEASURED ACROSS THE TERMINALS OF A SENSOR - A method for correcting measurement of a voltage across output terminals of a sensor, the sensor configured to be assimilated with an assembly including a generator and a series resistance, each of the output terminals being respectively connected to a pull up/down resistor. The method includes: evaluating the series resistance of the sensor, including measuring first and second voltages across the output terminals when first and second bias voltages are applied on each pull up/down resistor; evaluating the series resistance from the first and second voltages; and correcting, from the series resistance, a voltage measured across the output terminals of the sensor to infer therefrom a corresponding voltage generated by the generator. | 05-29-2014 |
Mark Raes, Andover, CT US
Patent application number | Description | Published |
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20100021304 | Blade pitch actuation mechanism - A blade pitch actuation mechanism for a plurality of propeller blades supported in a blade hub comprises a plurality of bearing assemblies, a bearing support plate and a yoke. The plurality of bearing assemblies receives a plurality of actuation trunnion pins from the plurality of propeller blades. The bearing support plate is connected to the plurality of bearing assemblies and unifies the plurality of bearing assemblies in a ring-like configuration. The yoke is connected to the bearing support plate and translates within the hub to adjust the pitch of the plurality of propeller blades. | 01-28-2010 |
20100226776 | Sacrificial blade tip - A propeller blade device used in environments where a propeller system is subjected to blade erosion and wear and may also be subjected to an axial force from water. The propeller blade includes a blade tip mounted on its outer end using a mounting device such as nuts and bolts to form a junction there between. The tip may easily be replaced when worn or damaged without removing the blade. The tip is designed to fracture upon impact with an axial force before transmitting the force radially inward to the propeller blade. | 09-09-2010 |
20110286842 | COUNTER-ROTATING OPEN-ROTOR (CROR) - A method of controlling a Counter-Rotating Open-Rotor (CROR) includes mechanically linking a pitch change system of a first rotor with a pitch change system of a second rotor and commanding a Blade Angle (Beta1 commanded) of the first rotor such that a Blade Angle (Beta2 Actual) of the second rotor is a function of the commanded Blade Angle (Beta1 commanded) to provide a linear relationship between an actual Blade angle (Beta1 Actual) and Beta1 commanded of the first rotor and a non-linear relationship between Beta2 Actual and Beta1 commanded. | 11-24-2011 |
Michel Raes, Mouans Sartoux FR
Patent application number | Description | Published |
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20150145221 | DEVICE FOR AUTOMATICALLY ADJUSTING THE CAMBER ANGLE FOR A SUSPENSION SYSTEM - Disclosed is a device for automatically adjusting a camber angle for a suspension system that includes a shock absorber. The device includes a first member rotationally drivable by a driving element during a displacement of a change of direction of the wheel, and a second member fixable to a vehicle frame. The first and second members cooperate to cause a relative translation of the first member and of the second member during a rotation of the shock absorber. | 05-28-2015 |
Niko Raes, Zwijnaarde BE
Patent application number | Description | Published |
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20120125311 | PREMIX AIR HEATER - A gas-fired heater includes a gas supply line, an air supply line, a valve coupled to the gas supply line and a controller coupled to the valve. The controller is configured to control the valve to control a gas-air mixture. The gas-fired heater also includes a burner configured to receive the gas-air mixture and burn the gas-air mixture, and a heat exchanger coupled to the burner. The heat exchanger is configured to perform a heat exchange process and output heated air. The gas-fired heater further includes a combustion fan located downstream of the heat exchanger, the combustion fan being configured to pull or draw flue gases through the heat exchanger. | 05-24-2012 |