Patents by Inventor Vincent PASCAL
Vincent PASCAL has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).
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Wheel with eddy current magnetic braking device and aircraft landing gear provided with such a wheel
Patent number: 12463501Abstract: A wheel including a rim that rotates on a shaft defining a primary rotational axis and a magnetic braking device. The magnetic braking device includes an actuator which includes a first transmission assembly and one second transmission assembly each includes a pinion mounted on the support to pivot about a secondary rotational axis parallel to the primary axis, an operating bar extending about the secondary axis, a first mechanical connecting member connecting the operating bar to the pinion of the transmission assembly and a second mechanical connecting member connecting the operating bar to one of the stators, and the mechanical connecting members are arranged. The rotation of the pinions causes a movement of the stators parallel to the secondary axis in opposite directions, for varying the air gap, one or more of the mechanical connecting members of each transmission assembly being arranged to ensure a screw-nut helical connection.Type: GrantFiled: May 25, 2022Date of Patent: November 4, 2025Assignee: SAFRAN LANDING SYSTEMSInventors: Vincent Pascal, Yannick Senechal, Graeme Klim -
Publication number: 20250022620Abstract: A molten salt nuclear reactor of the fast neutron reactor type may be designed as a cylindrical shell in the reactor vessel free of moderator or at the very least of a moderator enabling a reactor to be qualified as a thermal neutron reactor, which may make it possible to effectively separate the fluid zones between those delimited at its periphery in which the heat exchanger(s) exchanging heat between primary and secondary circuit is (are) arranged and the zone inside the shell of which the bottom defines the reactor core within which the nuclear fission chain reactions occur, and a neutron reflector at the periphery of the core makes it possible to use a plurality of types of fuel liquid.Type: ApplicationFiled: December 18, 2023Publication date: January 16, 2025Applicant: COMMISSARIAT A L'ENERGIE ATOMIQUE ET AUX ENERGIES ALTERNATIVESInventors: Guillaume CAMPIONI, Vincent PASCAL, Antoine GERSCHENFELD, Yannick GORSSE
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Patent number: 12157558Abstract: An uplock for retaining a capture pin of a movable part includes a hook that is movable between a release position and a retaining position, a locking part that interacts with the hook and is movable between a locking position and an unlocking position, and a detector. The detector includes a first sensor for detecting whether the hook is in the retaining position, and a second sensor for detecting a presence of the mobile part in the immediate vicinity of the uplock in the position occupied by the mobile part when the capture pin is in the hook.Type: GrantFiled: October 15, 2020Date of Patent: December 3, 2024Assignee: SAFRAN LANDING SYSTEMSInventors: Ludovic Dufay, Michel Arbentz, Vincent Pascal
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Publication number: 20240371535Abstract: A nuclear reactor with liquid coolant and solid fuel assemblies incorporates a heat removal system using a liquid metal bath for removing nominal heat and phase-change material(s) (PCM) for removing the decay heat in an accident situation. The nuclear reactor uses a liquid metal or molten salt primary coolant that simultaneously ensures passive heat removal, by natural convection in the primary circuit, in normal and accident operating modes during shutdown through the primary vessel of the reactor, that is, beyond the second containment barrier. In the event of an incident or accident, a compact passive decay heat removal system is capable of performing the safety function for a predetermined period, typically three days, without any intervention by an operator, due to the presence of one or more PCM(s) that store(s) the decay heat produced in the core and removed by the primary vessel.Type: ApplicationFiled: March 1, 2024Publication date: November 7, 2024Applicant: COMMISSARIAT A L'ENERGIE ATOMIQUE ET AUX ENERGIES ALTERNATIVESInventors: Alessandro PANTANO, Vincent PASCAL, Philippe AMPHOUX, Pierre ALLEGRE, Christoph DODERLEIN, Pierre SCIORA
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Patent number: 12134464Abstract: An uplock for selectively retaining a capture pin of a movable element including a hook, a locking member, and a detector. The hook is movable between a release position and a retaining position. The locking member is movable between a locked position that immobilizes the hook and an unlocked position in which the hook is free. The detector detects whether the hook is in the retaining position and the capture pin is present in the hook. The detector includes a sensor associated with a single target which is movable between two positions The sensor emits a signal which is modified when the target passes from one of the positions to the other. The target is independently in kinematic interaction with the hook and the capture pin.Type: GrantFiled: October 15, 2020Date of Patent: November 5, 2024Assignee: SAFRAN LANDING SYSTEMSInventors: Vincent Pascal, Ludovic Dufay, Michel Arbentz
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Publication number: 20240304344Abstract: A nuclear reactor with forced-convection liquid coolant and solid fuel assemblies incorporates a heat removal system using a liquid metal bath for removing the nominal heat and phase-change material(s) (PCM) for removing the decay heat in an accident situation. The solid-fuel nuclear reactor with liquid metal or molten salt primary coolant simultaneously ensures heat removal by forced convection in the primary circuit, in normal and accident operating modes, during shutdown through the primary vessel of the reactor, that is, beyond the second containment barrier. In the event of an incident or accident, a compact passive decay heat removal system is capable of performing the safety function for a predetermined period, typically three days, without any intervention by an operator, due to the presence of one or more PCM(s) that store(s) the decay heat produced in the core and removed by the primary vessel.Type: ApplicationFiled: March 1, 2024Publication date: September 12, 2024Applicant: COMMISSARIAT A L'ENERGIE ATOMIQUE ET AUX ENERGIES ALTERNATIVESInventors: Alessandro PANTANO, Vincent PASCAL, Philippe AMPHOUX, Pierre ALLEGRE, Christoph DODERLEIN, Pierre SCIORA
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WHEEL WITH EDDY CURRENT MAGNETIC BRAKING DEVICE AND AIRCRAFT LANDING GEAR PROVIDED WITH SUCH A WHEEL
Publication number: 20240262212Abstract: A wheel including a rim that rotates on a shaft defining a primary rotational axis and a magnetic braking device. The magnetic braking device includes an actuator which includes a first transmission assembly and one second transmission assembly each includes a pinion mounted on the support to pivot about a secondary rotational axis parallel to the primary axis, an operating bar extending about the secondary axis, a first mechanical connecting member connecting the operating bar to the pinion of the transmission assembly and a second mechanical connecting member connecting the operating bar to one of the stators, and the mechanical connecting members are arranged. The rotation of the pinions causes a movement of the stators parallel to the secondary axis in opposite directions, for varying the air gap, one or more of the mechanical connecting members of each transmission assembly being arranged to ensure a screw-nut helical connection.Type: ApplicationFiled: May 25, 2022Publication date: August 8, 2024Applicant: SAFRAN LANDING SYSTEMSInventors: Vincent PASCAL, Yannick SENECHAL, Graeme KLIM -
Publication number: 20240228024Abstract: An uplock for retaining a capture pin of a movable part includes a hook that is movable between a release position and a retaining position, a locking part that interacts with the hook and is movable between a locking position and an unlocking position, and a detector. The detector includes a first sensor for detecting whether the hook is in the retaining position, and a second sensor for detecting a presence of the mobile part in the immediate vicinity of the uplock in the position occupied by the mobile part when the capture pin is in the hook.Type: ApplicationFiled: October 15, 2020Publication date: July 11, 2024Applicant: SAFRAN LANDING SYSTEMSInventors: Ludovic DUFAY, Michel ARBENTZ, Vincent PASCAL
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Patent number: 12030619Abstract: An uplock for the selective retention of a capture pin of a movable element includes a hook, a locking member, and a detector. The hook is movable between a release position and a retaining position for retaining the capture pin. The locking member moves between a locked position, and an unlocked position. The detector detects whether the hook is in the retaining position and the capture pin is in the hook. The detector includes a sensor movable relative to a target. The target or the sensor is carried by the locking member and the other by an indicator lever which is movable between a first position indicating absence of the capture pin in the hook and a second position indicating presence. The target and the sensor are only in the proximate position if the locking member is in the locked position and the indicator lever is in the second position.Type: GrantFiled: October 15, 2020Date of Patent: July 9, 2024Assignee: SAFRAN LANDING SYSTEMSInventors: Vincent Pascal, Ludovic Dufay
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Publication number: 20240203613Abstract: A molten salt nuclear reactor of the fast neutron reactor type may be designed as a reactor vessel free of moderator or at the very least of a moderator enabling a reactor to be qualified as a thermal neutron reactor, having a shape exhibiting symmetry of revolution surrounded by another vessel at the periphery of the reactor vessel thereby delimiting a guard gap filled with an inert liquid salt which acts as a coolant for removing the decay heat from the reactor by conduction through the reactor vessel.Type: ApplicationFiled: December 18, 2023Publication date: June 20, 2024Applicant: COMMISSARIAT A L'ENERGIE ATOMIQUE ET AUX ENERGIES ALTERNATIVESInventors: Guillaume CAMPIONI, Antoine GERSCHENFELD, Vincent PASCAL, Yannick GORSSE
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Publication number: 20240203611Abstract: A molten salt nuclear reactor of the fast neutron reactor type may be designed as a reactor vessel free of moderator or at the very least of a moderator enabling a reactor to be qualified as a thermal neutron reactor, having a shape exhibiting symmetry of revolution surrounded by another vessel at the periphery of the reactor vessel thereby delimiting a guard gap filled with an inert liquid salt which acts as a coolant for removing the decay heat from the reactor by conduction through the reactor vessel.Type: ApplicationFiled: December 18, 2023Publication date: June 20, 2024Applicant: COMMISSARIAT A L'ENERGIE ATOMIQUE ET AUX ENERGIES ALTERNATIVESInventors: Guillaume CAMPIONI, Vincent PASCAL, Antoine GERSCHENFELD, Yannick GORSSE
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Publication number: 20240132204Abstract: An uplock for retaining a capture pin of a movable part includes a hook that is movable between a release position and a retaining position, a locking part that interacts with the hook and is movable between a locking position and an unlocking position, and a detector. The detector includes a first sensor for detecting whether the hook is in the retaining position, and a second sensor for detecting a presence of the mobile part in the immediate vicinity of the uplock in the position occupied by the mobile part when the capture pin is in the hook.Type: ApplicationFiled: October 14, 2020Publication date: April 25, 2024Applicant: SAFRAN LANDING SYSTEMSInventors: Ludovic DUFAY, Michel ARBENTZ, Vincent PASCAL
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Publication number: 20240124132Abstract: An uplock for the selective retention of a capture pin of a movable element includes a hook, a locking member, and a detector. The hook is movable between a release position and a retaining position for retaining the capture pin. The locking member moves between a locked position, and an unlocked position. The detector detects whether the hook is in the retaining position and the capture pin is in the hook. The detector includes a sensor movable relative to a target. The target or the sensor is carried by the locking member and the other by an indicator lever which is movable between a first position indicating absence of the capture pin in the hook and a second position indicating presence. The target and the sensor are only in the proximate position if the locking member is in the locked position and the indicator lever is in the second position.Type: ApplicationFiled: October 15, 2020Publication date: April 18, 2024Applicant: SAFRAN LANDING SYSTEMSInventors: Vincent PASCAL, Ludovic DUFAY
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Publication number: 20240101249Abstract: An uplock for selectively retaining a capture pin of a movable element including a hook, a locking member, and a detector. The hook is movable between a release position and a retaining position. The locking member is movable between a locked position that immobilizes the hook and an unlocked position in which the hook is free. The detector detects whether the hook is in the retaining position and the capture pin is present in the hook. The detector includes a sensor associated with a single target which is movable between two positions The sensor emits a signal which is modified when the target passes from one of the positions to the other. The target is independently in kinematic interaction with the hook and the capture pin.Type: ApplicationFiled: October 15, 2020Publication date: March 28, 2024Applicant: SAFRAN LANDING SYSTEMSInventors: Vincent PASCAL, Ludovic DUFAY, Michel ARBENTZ
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Patent number: 11548624Abstract: A method of moving a door of a well for an aircraft undercarriage during sequences of deploying or retracting the undercarriage includes: using a temporary mechanical connection between the door and the undercarriage that is effective when the undercarriage is close to its retracted position, causing the door to be opened by the undercarriage while the undercarriage is being deployed and causing the door to be closed by the undercarriage while the undercarriage is being retracted, but releasing the door from the undercarriage when the undercarriage is close to its deployed position, and using a door actuator acting on the door to close and open the door when the undercarriage is in its deployed position and the temporary mechanical connection is interrupted.Type: GrantFiled: June 18, 2019Date of Patent: January 10, 2023Assignee: SAFRAN LANDING SYSTEMSInventors: Yannick Senechal, Vincent Pascal, Thierry Blanpain, Aurélien Doux
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Patent number: 11192640Abstract: An emergency extension system for extending at least one aircraft undercarriage, the emergency extension system comprising both electromechanical actuators, each electromechanical actuator having an identification component arranged to allocate an identifier to said electromechanical actuator, which identifier depends in particular on a function performed by said electromechanical actuator, and also an electrical card having a delay component arranged to delay actuation of a the electromechanical actuator by an actuation delay that depends on the identifier allocated to the electromechanical actuator, the electromechanical actuators of the emergency extension system thus being arranged to be actuated in succession in an actuation sequence that is defined by the actuation delays.Type: GrantFiled: February 22, 2018Date of Patent: December 7, 2021Inventors: Raphaël Pierra, Mathieu Rousselet, Vincent Pascal, Jean-Luc Belleval
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Patent number: 10982720Abstract: A device (1) for connecting an end of a first shaft to an end of a second shaft, the end of the first shaft having a radial groove. The device includes a body (2) having a bore (21) into which the end of the first shaft can be introduced, a locking pin (3) movable with respect to the body (2) between a locked position, in which the pin (3) projects into the bore (21) such that, when the end of the first shaft is received inside the bore (21), the locking pin (3) is engaged in the radial groove in the end of the first shaft, and an unlocked position. In the unlocked position, the locking pin (3) is disengaged from the radial groove in the end of the first shaft, and an elastic return member (4) urges the locking pin (3) into the locked position.Type: GrantFiled: March 13, 2018Date of Patent: April 20, 2021Assignee: SAFRAN ELECTRONICS & DEFENSEInventors: Julien Hautecoeur, Mathieu Rousselet, Vincent Pascal
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Publication number: 20200378447Abstract: The invention relates to a device (1) for connecting an end of a first shaft to an end of a second shaft, the end of the first shaft having a radial groove, the device comprising:—a body (2) having a bore (21) into which the end of the first shaft can be introduced,—a locking pin (3) mounted so as to be movable with respect to the body (2) between a locked position, in which the pin (3) projects into the bore (21) such that, when the end of the first shaft is received inside the bore (21), the locking pin (3) is engaged in the radial groove in the end of the first shaft in order to prevent the end of the first shaft from being removed from the bore (21), and an unlocked position, in which the locking pin (3) is disengaged from the radial groove in the end of the first shaft so as to allow the end of the first shaft to be introduced into the bore (21) or to allow the end of the first shaft to be removed from the bore (21), and—an elastic return member (4) for urging the locking pin (3) into the locked positionType: ApplicationFiled: March 13, 2018Publication date: December 3, 2020Inventors: Julien HAUTECOEUR, Mathieu ROUSSELET, Vincent PASCAL
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Publication number: 20190382102Abstract: A method of moving a door of a well for an aircraft undercarriage during sequences of deploying or retracting the undercarriage includes: using a temporary mechanical connection between the door and the undercarriage that is effective when the undercarriage is close to its retracted position, causing the door to be opened by the undercarriage while the undercarriage is being deployed and causing the door to be closed by the undercarriage while the undercarriage is being retracted, but releasing the door from the undercarriage when the undercarriage is close to its deployed position, and using a door actuator acting on the door to close and open the door when the undercarriage is in its deployed position and the temporary mechanical connection is interrupted.Type: ApplicationFiled: June 18, 2019Publication date: December 19, 2019Applicant: SAFRAN LANDING SYSTEMSInventors: Yannick Senechal, Vincent Pascal, Thierry Blanpain, Aurélien Doux
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Publication number: 20180244374Abstract: An emergency extension system for extending at least one aircraft undercarriage, the emergency extension system comprising both electromechanical actuators, each electromechanical actuator having an identification component arranged to allocate an identifier to said electromechanical actuator, which identifier depends in particular on a function performed by said electromechanical actuator, and also an electrical card having a delay component arranged to delay actuation of a the electromechanical actuator by an actuation delay that depends on the identifier allocated to the electromechanical actuator, the electromechanical actuators of the emergency extension system thus being arranged to be actuated in succession in an actuation sequence that is defined by the actuation delays.Type: ApplicationFiled: February 22, 2018Publication date: August 30, 2018Applicant: SAFRAN LANDING SYSTEMSInventors: Raphaël Pierra, Mathieu Rousselet, Vincent Pascal, Jean-Luc Belleval