Aircraft fuel filter impending and actual bypass indication system
    1.
    发明授权
    Aircraft fuel filter impending and actual bypass indication system 有权
    飞机燃油滤清器即将和实际旁路指示系统

    公开(公告)号:US09441598B2

    公开(公告)日:2016-09-13

    申请号:US14075418

    申请日:2013-11-08

    Abstract: A fuel supply system includes a fuel supply line, a fuel filter, a filter bypass line, a first differential pressure sensor, a second differential pressure sensor, and a filter bypass valve. The fuel filter is disposed in series in the fuel supply line to remove particulate from the fuel. The filter bypass line has a fuel inlet upstream of the fuel filter, and an outlet that is downstream of the fuel filter. The first differential pressure sensor continuously senses differential pressure across the fuel filter, and the second differential pressure sensor selectively senses differential pressure across the fuel filter. The filter bypass valve is movable between a first non-bypassing position and a second bypassing position and controls whether only the first differential pressure sensor or both the first and second differential pressure sensors sense the differential pressure across the fuel filter.

    Abstract translation: 燃料供给系统包括燃料供给管线,燃料过滤器,过滤器旁路管路,第一差压传感器,第二压差传感器和过滤器旁通阀。 燃料过滤器串联设置在燃料供应管线中以从燃料中除去颗粒。 过滤器旁路管路具有在燃料过滤器上游的燃料入口和位于燃料过滤器下游的出口。 第一差压传感器连续地感测燃料过滤器两端的差压,第二差压传感器选择性地感测燃料过滤器两端的差压。 过滤器旁通阀可在第一非旁通位置和第二旁路位置之间移动,并且控制仅第一压差传感器或第一和第二压差传感器是否感测到燃料过滤器两端的压差。

    AIRCRAFT FUEL FILTER IMPENDING AND ACTUAL BYPASS INDICATION SYSTEM
    2.
    发明申请
    AIRCRAFT FUEL FILTER IMPENDING AND ACTUAL BYPASS INDICATION SYSTEM 有权
    飞机燃油滤清器和实际旁路指示系统

    公开(公告)号:US20150128906A1

    公开(公告)日:2015-05-14

    申请号:US14075418

    申请日:2013-11-08

    Abstract: A fuel supply system includes a fuel supply line, a fuel filter, a filter bypass line, a first differential pressure sensor, a second differential pressure sensor, and a filter bypass valve. The fuel filter is disposed in series in the fuel supply line to remove particulate from the fuel. The filter bypass line has a fuel inlet upstream of the fuel filter, and an outlet that is downstream of the fuel filter. The first differential pressure sensor continuously senses differential pressure across the fuel filter, and the second differential pressure sensor selectively senses differential pressure across the fuel filter. The filter bypass valve is movable between a first non-bypassing position and a second bypassing position and controls whether only the first differential pressure sensor or both the first and second differential pressure sensors sense the differential pressure across the fuel filter.

    Abstract translation: 燃料供给系统包括燃料供给管线,燃料过滤器,过滤器旁路管路,第一差压传感器,第二压差传感器和过滤器旁通阀。 燃料过滤器串联设置在燃料供应管线中以从燃料中除去颗粒。 过滤器旁路管路具有在燃料过滤器上游的燃料入口和位于燃料过滤器下游的出口。 第一差压传感器连续地感测燃料过滤器两端的差压,第二差压传感器选择性地感测燃料过滤器两端的差压。 过滤器旁通阀可在第一非旁通位置和第二旁路位置之间移动,并且控制仅第一压差传感器或第一和第二压差传感器是否感测到燃料过滤器两端的压差。

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