HYDRAULIC ACCUMULATOR AS WELL AS A METHOD FOR ASCERTAINING A STATE OF CHARGE OF A HYDRAULIC ACCUMULATOR
    62.
    发明申请
    HYDRAULIC ACCUMULATOR AS WELL AS A METHOD FOR ASCERTAINING A STATE OF CHARGE OF A HYDRAULIC ACCUMULATOR 审中-公开
    液压蓄能器作为增加液压蓄能器充电状态的方法

    公开(公告)号:US20130019746A1

    公开(公告)日:2013-01-24

    申请号:US13574202

    申请日:2011-01-03

    Inventor: Ralph Engelberg

    CPC classification number: F15B1/16 F15B2201/315 F15B2201/51

    Abstract: A hydraulic accumulator includes: a pressure vessel; a hose which is situated within the pressure vessel, for receiving a first medium; a gap, which is formed between the pressure vessel and the hose, for receiving a second medium; and at least one connection for supplying and discharging the first or the second medium under pressure into or out of the hose or the gap, the supply of the first medium resulting in the compression of the second medium.

    Abstract translation: 液压蓄能器包括:压力容器; 软管,其位于压力容器内,用于接收第一介质; 在压力容器和软管之间形成的用于接收第二介质的间隙; 以及用于在压力下将第一或第二介质供给和排出到软管或间隙中的至少一个连接件,第一介质的供应导致第二介质的压缩。

    Process for monitoring the gas volume in an hydropneumatic accumulator
and apparatus for carrying out the process
    63.
    发明授权
    Process for monitoring the gas volume in an hydropneumatic accumulator and apparatus for carrying out the process 失效
    用于监测液压气动蓄能器中的气体体积的过程和用于执行该过程的装置

    公开(公告)号:US4781061A

    公开(公告)日:1988-11-01

    申请号:US26823

    申请日:1987-03-17

    Inventor: Ulrich Baumgartl

    Abstract: In a hydropneumatic accumulator, the gas volume contained therein is monitored by measuring the volume increase in the hydraulic fluid, which takes place during a pressure increase at a given minimum pressure. Moreover, for monitoring purposes, the hydraulic pressure is measured and a signal transmitted at insufficient gas volume as a function of the volume increase and the pressure increase. In order to obtain reliable signals concerning the filling state of the accumulator at all ambient operating temperatures, the temperature of the environment and the gas volume is detected, a standard value for the volume increase proportional to the ratio of the gas temperature to the minimum pressure determined and the volume increase causing the pressure increase compared to this standard value.

    Abstract translation: 在液压气动蓄能器中,通过测量在给定最小压力下的压力增加期间发生的液压流体的体积增加来监测容纳在其中的气体体积。 此外,为了监视目的,测量液压并且以不足的气体体积传递的信号作为体积增加和压力增加的函数。 为了在所有环境工作温度下获得关于蓄能器的填充状态的可靠信号,检测到环境温度和气体体积,体积增加的标准值与气体温度与最小压力的比例成比例 确定并且体积增加导致与该标准值相比的压力增加。

    INDIRECT HYDRAULIC LOAD HIERARCHICAL CONTROL SYSTEM AND METHOD FOR WAVE ENERGY DEVICE

    公开(公告)号:US20240263608A1

    公开(公告)日:2024-08-08

    申请号:US18685233

    申请日:2023-04-28

    CPC classification number: F15B1/04 F15B13/06 F03B13/14 F15B2201/51

    Abstract: An indirect hydraulic load hierarchical control system and method for a wave energy device includes a first hydraulic cylinder group, a second hydraulic cylinder group, a third hydraulic cylinder group, a high-pressure energy accumulator group, a pressure detection control module, a first hydraulic power generator set, a second hydraulic power generator set and a third hydraulic power generator set. A detection end of the pressure detection control module is used for acquiring an internal pressure of the high-pressure energy accumulator group, comparing the internal pressure with a preset pressure level, and respectively controlling the on-off of reversing valves and electromagnetic valves according to a comparison result. The present invention has the beneficial effects that all hydraulic loads can be automatically loaded or automatically unloaded, so that the wave energy device operates in a full load state or in an optimal energy conversion efficiency state.

    REMOTE HYDRAULIC UTILITY SYSTEM FOR AN AIRCRAFT

    公开(公告)号:US20180043998A1

    公开(公告)日:2018-02-15

    申请号:US15232516

    申请日:2016-08-09

    Inventor: William E. Luce

    Abstract: A remote hydraulic system for an aircraft may provide hydraulic fluid to nose landing gear while being isolated from the main landing gear and other main hydraulic systems of the aircraft. A supply pressure accumulator may be configured to supply hydraulic fluid to a hydraulic load of the nose gear. A pressure sensor may be configured to detect a hydraulic pressure in the supply pressure accumulator. A pump may be in fluid communication with the supply pressure accumulator and configured to switch on in response to the hydraulic pressure below a threshold value. A return pressure accumulator may be configured to store the hydraulic fluid returning from the hydraulic load. The pump may drive fluid from the return pressure accumulator to the supply pressure accumulator.

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