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1.发明申请公开(公告)号：US20110048312A1
公开(公告)日：2011-03-03
申请号：US12549262
申请日：2009-08-27
CPC分类号： G01K11/06 , G01K11/12 , G01K2207/06 , Y10T156/1057
摘要： An apparatus indicates a temperature of an object. The apparatus includes a porous substrate, a mirror image of a first image pattern printed with a first phase-change ink having a first phase change temperature on a first side of the porous substrate, and an adhesive layer applied to the first side of the porous substrate to enable the porous substrate to be affixed to an object.
摘要翻译： 装置表示物体的温度。 该装置包括多孔基材，印刷有在多孔基材的第一面上具有第一相变温度的第一相变油墨的第一图像图案的镜像，以及施加到多孔基材的第一侧的粘合剂层 基板，以使多孔基材能够固定在物体上。
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2.发明授权公开(公告)号：US08091503B2
公开(公告)日：2012-01-10
申请号：US12549262
申请日：2009-08-27
CPC分类号： G01K11/06 , G01K11/12 , G01K2207/06 , Y10T156/1057
摘要： An apparatus indicates a temperature of an object. The apparatus includes a porous substrate, a mirror image of a first image pattern printed with a first phase-change ink having a first phase change temperature on a first side of the porous substrate, and an adhesive layer applied to the first side of the porous substrate to enable the porous substrate to be affixed to an object.
摘要翻译： 装置表示物体的温度。 该装置包括多孔基材，印刷有在多孔基材的第一面上具有第一相变温度的第一相变油墨的第一图像图案的镜像，以及施加到多孔基材的第一侧的粘合剂层 基板，以使多孔基材能够固定在物体上。
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公开(公告)号：US5463863A
公开(公告)日：1995-11-07
申请号：US662970
申请日：1984-09-19
摘要： A fuel control system for a gas turbine aero engine comprises a first metering valve 22 which is controlled by a feed back loop 43 in flow series with a manually operated metering valve 34. A pressure drop regulator 31, 39 regulates the pressure drop across the series connected valves 22, 34. In this way response of the control system is directly influenced by movement of the manual valve 34 and the automatic valve 22 stabilizes the fuel flow rate in response to monitored operating parameters of the engine.
摘要翻译： 用于燃气轮机航空发动机的燃料控制系统包括第一计量阀22，其由与手动操作的计量阀34流动串联的反馈回路43控制。压降调节器31,39调节该系列上的压降 以这种方式，控制系统的响应直接受到手动阀34的运动的影响，并且自动阀22响应于监测的发动机的运行参数来稳定燃料流量。
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公开(公告)号：US08434854B1
公开(公告)日：2013-05-07
申请号：US13276797
申请日：2011-10-19
IPC分类号： B41J2/165
CPC分类号： B41J2/16538 , B41J2/1652 , B41J2/16541
摘要： A printhead cleaning device includes a housing having an opening and an ink receptacle positioned within the opening. A member extends from the ink receptacle and through the opening. The member is configured to contact a faceplate of a printhead to enable liquid ink emitted onto the faceplate to move from across the member into the ink receptacle.
摘要翻译： 打印头清洁装置包括具有开口的壳体和位于开口内的墨容器。 一个构件从墨水容器延伸并穿过开口。 该构件构造成接触打印头的面板以使得排出到面板上的液体墨水能够跨越该构件移动到墨水容器中。
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公开(公告)号：US20130100203A1
公开(公告)日：2013-04-25
申请号：US13276797
申请日：2011-10-19
IPC分类号： B41J2/165
CPC分类号： B41J2/16538 , B41J2/1652 , B41J2/16541
摘要： A printhead cleaning device includes a housing having an opening and an ink receptacle positioned within the opening. A member extends from the ink receptacle and through the opening. The member is configured to contact a faceplate of a printhead to enable liquid ink emitted onto the faceplate to move from across the member into the ink receptacle.
摘要翻译： 打印头清洁装置包括具有开口的壳体和位于开口内的墨容器。 一个构件从墨水容器延伸并穿过开口。 该构件构造成接触打印头的面板以使得排出到面板上的液体墨水能够跨越该构件移动到墨水容器中。
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公开(公告)号：US5513493A
公开(公告)日：1996-05-07
申请号：US887373
申请日：1986-07-11
申请人： Michael J. Severn , Roy L. Taylor
发明人： Michael J. Severn , Roy L. Taylor
CPC分类号： F02C9/38 , F05D2270/051
摘要： Fuel for the combustion equipment of the engine of a vertical take off aircraft is supplied via pumps 50,24 through a metering valve 22, which is under the control of a digital electronic control unit (DECU) 10. A pressure drop regulator 30 and spill valve 32 ensure there is a constant pressure drop across the metering valve 22. To provide a rapid reduction in fuel output when the aircraft pilot slams shut his control lever 16 when he touches down after a vertical landing, and therefore prevent the aircraft from bouncing, the DECU 10 detects the sudden slamming closed of the lever 16, and opens a solenoid valve 60. Fuel now bleeds along line 58, and the input 54 of the regulator 30 sees an increased pressure drop determined by a potentiometer formed by two flow restricting orifices 56,62. The regulator 30 therefore opens the spill valve 32 giving the desired rapid reduction in fuel flow through the metering valve 22.
摘要翻译： 用于垂直起飞飞机的发动机的燃烧设备的燃料通过泵50,24通过在数字电子控制单元（DECU）10的控制下的计量阀22供应。压降调节器30和泄漏 阀32确保在计量阀22上存在恒定的压力降。为了在飞行员飞行员在垂直着陆之后触摸时关闭其控制杆16并且因此防止飞行器弹跳而提供燃料输出的快速减少， DECU 10检测到杆16的突然打开关闭，并打开电磁阀60.燃料现在沿着线58流出，并且调节器30的输入54看到由由两个流动限制孔形成的电位计确定的增加的压降 56,62。 因此，调节器30打开溢流阀32，从而使通过计量阀22的燃料流快速减少。
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