Safety valve and method for controlling a hydraulic circuit

    公开(公告)号:US10935052B2

    公开(公告)日:2021-03-02

    申请号:US16621158

    申请日:2018-06-28

    Abstract: Described herein is a safety valve for a hydraulic circuit comprising a pump designed to supply a hydraulic fluid at a first pressure value to a pressure line, comprising: a chamber, which can be fluidically connected to the pressure line and is filled with the hydraulic fluid at a pressure value and a temperature value; and a casing with an opening, which can be connected to a reservoir of the hydraulic circuit; a shutter, which delimits the first chamber and can be displaced between a first position, in which it occludes the first opening, and a second position, in which it leaves the opening at least in part free; the valve comprises a thermally expandable element, which can be displaced, as a result of the temperature of the hydraulic fluid, between a first configuration that it assumes when the temperature of the hydraulic fluid is below the threshold value and a second configuration that it assumes when the temperature of the hydraulic fluid is above the temperature threshold value and in which it holds or displaces the first shutter in or towards the second position so as to reduce the pressure in the first chamber.

    HIGH EFFICIENCY ELECTROCHEMICAL POWER SUPPLY SOURCE FOR AN UNDERWATER VEHICLE

    公开(公告)号:US20200295342A1

    公开(公告)日:2020-09-17

    申请号:US16818307

    申请日:2020-03-13

    Inventor: Yuri GASSANI

    Abstract: An electrochemical-type power supply source for use in marine environment, is provided with: an electrochemical stack, which generates electric power in the presence, internally, of an electrolytic fluid; a first tank, designed to contain electrolytic fluid at a first temperature; a second tank, designed to contain electrolytic fluid at a second temperature, lower than the first temperature; a thermostatic valve, that mixes electrolytic fluid at a lower temperature with electrolytic fluid at a higher temperature, for generating a mixed electrolytic fluid to be introduced into the electrochemical stack at a controlled temperature for generating a desired electric power. The electrochemical power supply is further provided with an auxiliary tank, adapted to contain electrolytic fluid at a third temperature, higher than the first temperature; and the thermostatic valve is connected to the auxiliary tank and receives, at an input, the electrolytic fluid at the third temperature, as a higher-temperature electrolytic fluid, for generating the mixed electrolytic fluid, in a given operating condition.

    CENTRIFUGAL SEPARATOR OF GAS - LIQUID FOR ELECTROCHEMICAL BATTERY

    公开(公告)号:US20200282409A1

    公开(公告)日:2020-09-10

    申请号:US16808976

    申请日:2020-03-04

    Inventor: Dino BARTOLI

    Abstract: A centrifugal gas-liquid separator wherein a tubular casing houses a central tubular duct, which is provided with a first free end and with a second end that communicates with a gas-outlet duct and carries a transversal annulus-shaped plate having a perimetral edge that faces the inner wall of the tubular body to define an annular gap. The plate divides the space inside the tubular casing into a first chamber and into a second chamber that communicate with each other through the annular gap. A liquid-outlet duct communicates with the second chamber and a liquid-phase/gas-phase inlet duct extends tangentially from the tubular casing and discharges into the first chamber through an inlet nozzle. A regulation device is provided, which is designed to modify the section of the inlet nozzle in order to modify the rate of entry of the liquid phase and gas phase into the first chamber and to adapt the operation of the centrifugal gas-liquid separator following variations of flow rate.

    STABILITY AND COMMAND AUGMENTATION SYSTEM FOR AN AIRCRAFT, AND STABILIZATION AND CONTROL METHOD OF AN AIRCRAFT

    公开(公告)号:US20200278698A1

    公开(公告)日:2020-09-03

    申请号:US16649745

    申请日:2018-10-05

    Abstract: A stability and command augmentation system for controlling an aircraft, comprising: a first member moveable by a pilot input device to a first position defining a first input; a second member moveable to a second position associated with a second input; and an adder device configured to add the first and second inputs and supply an output signal defining a command for an element to be controlled of the aircraft; the stability and command augmentation system comprises: a casing, a first and a second piston integrally movable with one another inside the casing and operatively connected to the second member; and control means configured to exert a first force on the first piston and a second force on the second piston; the second force is independent of the first force.

    VIBRATION DAMPING DEVICE AND DAMPING METHOD FOR A ROTOR OF AN AIRCRAFT CAPABLE OF HOVERING

    公开(公告)号:US20190047690A1

    公开(公告)日:2019-02-14

    申请号:US16076557

    申请日:2017-02-22

    Abstract: A damping device is described that is designed to counter the transmission of vibrations to a further element and comprises: a beam element, which extends mainly parallel to an axis, is constrained to the further element and is designed to flexurally oscillate, in use, in a plane parallel to the axis to counter the transmission of vibrations to the further element; an actuator, which comprises a transmission element operatively connected to the beam element and extending mainly along the axis; the actuator being controllable to apply a direct tensile or compressive load along the axis on the transmission element that is variable according to the frequency of the vibrations to be dampened.

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