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    • 4. 发明授权
    • Self-diagnosing differential pressure flow meter
    • 自诊断差压流量计
    • US08820178B2
    • 2014-09-02
    • US13607259
    • 2012-09-07
    • Jared Steven AyersGerald E. DavisClinton Paul HobbsEric Dahl Mikkelsen
    • Jared Steven AyersGerald E. DavisClinton Paul HobbsEric Dahl Mikkelsen
    • G01F1/34
    • G01F1/36G01F1/74G01F1/88G01F15/06
    • An aspect provides a method of metering flow through a fluid conduit having an obstruction therein, including: placing an obstruction body within the conduit; generating at least two differential pressure measurement signals using at least three different pressure ports, said at least three different pressure ports comprising: an upstream pressure port; a downstream pressure port; and an auxiliary pressure port; wherein at least one of the upstream pressure port, the downstream pressure port, and the auxiliary pressure port is positioned at an angle between 0 and 90 degrees with respect to a conduit wall; establishing a baseline relationship between the at least two differential pressure measurement signals; and determining if the baseline relationship between the at least two differential pressure measurement signals differs by a predetermined amount. Other aspects are described and claimed.
    • 一方面提供了一种计量流过其中具有障碍物的流体导管的方法,包括:将阻塞体放置在导管内; 使用至少三个不同的压力端口产生至少两个差压测量信号,所述至少三个不同的压力端口包括:上游压力端口; 下游压力口; 和辅助压力口; 其中所述上游压力端口,所述下游压力端口和所述辅助压力端口中的至少一个相对于导管壁定位在0和90度之间的角度; 建立所述至少两个差压测量信号之间的基线关系; 以及确定所述至少两个差压测量信号之间的基线关系是否相差预定量。 描述和要求保护其他方面。
    • 8. 发明授权
    • Removable interior window unit for aircraft
    • 飞机内置可拆卸机组
    • US4541595A
    • 1985-09-17
    • US479674
    • 1983-03-28
    • Peter E. FialaGerald E. DavisAlan J. TumaJack E. Hart
    • Peter E. FialaGerald E. DavisAlan J. TumaJack E. Hart
    • B64C1/14
    • B64C1/1492Y10T292/0901Y10T292/0902
    • In an aircraft having a pressure window mounted in the hull, an interior window assembly is removably mounted in an interior wall spaced from the hull. The interior window assembly is in register with the pressure window to enable occupants of the aircraft to view the outside. The interior wall has an opening formed therein to accept the interior window assembly and the portions of the wall surrounding the opening are biased toward the interior of the aircraft. The interior window assembly includes a windowpane mounted in a frame. The frame includes a flange that overlies the inboard surface of the portions of the wall surrounding the opening, and the bias of the wall portions is exerted on the flange. A constraint means is affixed to the hull of the aircraft and releasably engages the frame to constrain the frame from inboard movement. The bias force of the wall portions and the constraint means cooperate to hold the window in place. Preferably, the interior wall is comprised of stiffly flexible panel members that are flexed upon placement of the window assembly into the opening and tend to return to their unflexed state, thereby exerting the bias force on the flange.
    • 在具有安装在船体中的压力窗的飞行器中,内部窗组件可移除地安装在与船体间隔开的内壁中。 内部窗组件与压力窗口对准,以使飞机的乘客能够观察外部。 内壁具有形成在其中的开口以接纳内部窗户组件,并且围绕开口的壁的部分朝向飞行器的内部偏置。 内窗组件包括安装在框架中的窗玻璃。 框架包括覆盖围绕开口的壁的部分的内侧表面的凸缘,并且壁部分的偏压施加在凸缘上。 约束装置固定在飞行器的船体上并且可释放地接合框架以将框架从内侧运动限制。 壁部分和约束装置的偏压力协调以将窗口保持在适当的位置。 优选地,内壁由刚性柔性的面板构件组成,其在将窗组件放置在开口中时弯曲,并且倾向于返回到其非折叠状态,从而在凸缘上施加偏压力。
    • 10. 发明申请
    • SELF-DIAGNOSING DIFFERENTIAL PRESSURE FLOW METER
    • 自诊断差压流量计
    • US20140069208A1
    • 2014-03-13
    • US13607259
    • 2012-09-07
    • Jared Steven AyersGerald E. DavisClinton Paul HobbsEric Dahl Mikkelsen
    • Jared Steven AyersGerald E. DavisClinton Paul HobbsEric Dahl Mikkelsen
    • G01F1/34
    • G01F1/36G01F1/74G01F1/88G01F15/06
    • An aspect provides a method of metering flow through a fluid conduit having an obstruction therein, including: placing an obstruction body within the conduit; generating at least two differential pressure measurement signals using at least three different pressure ports, said at least three different pressure ports comprising: an upstream pressure port; a downstream pressure port; and an auxiliary pressure port; wherein at least one of the upstream pressure port, the downstream pressure port, and the auxiliary pressure port is positioned at an angle between 0 and 90 degrees with respect to a conduit wall; establishing a baseline relationship between the at least two differential pressure measurement signals; and determining if the baseline relationship between the at least two differential pressure measurement signals differs by a predetermined amount. Other aspects are described and claimed.
    • 一方面提供了一种计量流过其中具有障碍物的流体导管的方法,包括:将阻塞体放置在导管内; 使用至少三个不同的压力端口产生至少两个差压测量信号,所述至少三个不同的压力端口包括:上游压力端口; 下游压力口; 和辅助压力口; 其中所述上游压力端口,所述下游压力端口和所述辅助压力端口中的至少一个相对于导管壁定位在0和90度之间的角度; 建立所述至少两个差压测量信号之间的基线关系; 以及确定所述至少两个差压测量信号之间的基线关系是否相差预定量。 描述和要求保护其他方面。