METHOD FOR CONTROLLING THE ROTATION SPEED OF A MOTOR

    公开(公告)号:US20250043805A1

    公开(公告)日:2025-02-06

    申请号:US18779367

    申请日:2024-07-22

    Inventor: MARCO IOTTI

    Abstract: A method for controlling the rotation speed of a motor that includes the steps of preparing a first function which puts in relation the flow rate delivered by a pump with the pump rotation speed, preparing a second function which puts in relation a flow rate delivered by a flow rate control valve with a level of the control signal received, detecting the presence of control signals and the level of each control signal, using the second function, calculating the flow rate delivered by each flow rate control valve as a function of the level of the control signal received, calculating a total required flow rate, as the sum of the flow rates delivered by each flow rate control valve, using the first function, calculating a required rotation speed of the pump and adjusting the speed of rotation of the motor.

    HYDRAULIC SYSTEM
    2.
    发明公开
    HYDRAULIC SYSTEM 审中-公开

    公开(公告)号:US20240352951A1

    公开(公告)日:2024-10-24

    申请号:US18682369

    申请日:2022-08-05

    Inventor: Myeongku YEO

    CPC classification number: F15B13/06 F15B13/025 F15B2211/45

    Abstract: A hydraulic system according to an embodiment of the present invention comprises: a main hydraulic pump for discharging a hydraulic fluid; a plurality of driving apparatuses operating by receiving the hydraulic fluid; a parallel flow path through which the hydraulic fluid discharged by the main hydraulic pump flows; a plurality of control spools respectively connected to the parallel flow path in parallel to control the supply of hydraulic fluid to the plurality of driving apparatuses; and a plurality of electronic proportional decompression valves for adjusting a pilot pressure, applied to the respective control spools to be proportional to a current signal which has been input, wherein, if the plurality of control spools do not operate, the hydraulic fluid discharged by the main hydraulic pump is drained into an oil tank via the parallel flow path without passing through the plurality of control spools.

    TELESCOPIC ARM FOR SELF-PROPELLED OPERATING MACHINES

    公开(公告)号:US20240336466A1

    公开(公告)日:2024-10-10

    申请号:US18621780

    申请日:2024-03-29

    Inventor: MARCO IOTTI

    CPC classification number: B66F9/22 B66F9/0655 B66F9/0755 F15B13/06 F15B15/16

    Abstract: Described is a telescopic lifting arm (1) for self-propelled operating machines (10) comprising three tubular elements (21, 22, 23, 24, 25, 26), with a decreasing cross-section and telescopically connected to each other to define a supporting structure, designed to move between a retracted configuration wherein said tubular elements (21, 22, 23, 24, 25, 26) are inserted one in the other and an elongated configuration wherein two tubular elements are partly extracted. The arm (1) comprises actuator means (5) associated with the tubular elements (21, 22, 23, 24, 25, 26) and configured for actuating two tubular elements (21, 22, 23, 24 25, 26) for pulling them out independently from one other and with different speeds.

    METHOD AND APPARATUS FOR GENERATING HYDRAULIC POWER IN AN AIRCRAFT

    公开(公告)号:US20240328436A1

    公开(公告)日:2024-10-03

    申请号:US18622719

    申请日:2024-03-29

    CPC classification number: F15B11/17 B64D41/00 F15B13/06

    Abstract: An apparatus and method for hydraulically powering at least one consumer of a hydraulic system of an aircraft is disclosed including a first electrical power source and a first electrically driven motor pump (MPU1) electrically powered by the first electrical power source, a second electrical power source and a second electrically driven motor pump (MPU2) electrically powered by the second electrical power source (B), and a hydraulic power generation control which controls a supply of electrical energy from the first and second electrical power sources to the first and second motor pumps (MPU1, MPU2). A method is disclosed for determining the actual available electrical power (APA, APB) of each of the first and second electrical power sources and to set a load factor (UPA, UPB) of each motor pump in order to share a load to generate hydraulic power demanded from the at least one consumer between the first and second motor pumps.

    Pneumatic Drive Apparatus
    5.
    发明公开

    公开(公告)号:US20240309892A1

    公开(公告)日:2024-09-19

    申请号:US18605955

    申请日:2024-03-15

    CPC classification number: F15B1/265 F15B13/06

    Abstract: A pneumatic circuit for a pneumatic drive apparatus is disclosed. The pneumatic circuit includes a reservoir, a pump, and first, second and third valves. The first valve selectively provides a fluid connection between an inlet of the pump and the reservoir. The second valve selectively provides a fluid connection between an outlet of the pump and the reservoir. The third valve selectively provides a fluid connection between the reservoir and an actuation port. The pneumatic circuit is configured such that the first and second valves can selectively pressurise the reservoir, and such that the third valve can selectively communicate pressure from the reservoir to the actuation port.

    THREE SERVOVALVE THRUST REVERSER ACTUATOR SYSTEM

    公开(公告)号:US20240287949A1

    公开(公告)日:2024-08-29

    申请号:US18175120

    申请日:2023-02-27

    Applicant: Woodward, Inc.

    CPC classification number: F02K1/763 F15B1/265 F15B13/027 F15B13/06 F15B15/2815

    Abstract: The subject matter of this specification can be embodied in, among other things, an engine assembly having a nacelle partially surrounding an engine, and a thrust reverser having a first element movable relative to the nacelle between a stowed and deployed position, a first hydraulic actuator configured to move the first element between the stowed and deployed position, the first hydraulic actuator being connected to a fluid source and a return reservoir, and a second element movable between a stowed and deployed position, a second hydraulic actuator configured to move the second element between the stowed and deployed position, the second hydraulic actuator being connected to the fluid source and the return reservoir, and a fluid control system having a servo valve operable to selectively route fluid between the fluid source, the first hydraulic actuator, and the return reservoir, and a controller configured to operate the servo valve.

    IN HYDRAULIC SYSTEMS
    9.
    发明公开

    公开(公告)号:US20240140382A1

    公开(公告)日:2024-05-02

    申请号:US18383181

    申请日:2023-10-24

    CPC classification number: B60T13/12 B64C25/44 F15B13/06

    Abstract: A hydraulic brake system for activating the wheel brakes of an aircraft landing gear assembly includes a hydraulic fluid supply line and an associated return line. There is a valve which separates a source of hydraulic fluid from a portion of the return line and an associated leak path associated with the valve that in use maintains the pressure and/or volume of hydraulic fluid in the portion of the return line above a minimum acceptable level. The leak path may be provided by a hole drilled in a part (e.g. the poppet) of a non-return check valve.

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