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    • 4. 发明授权
    • Adjusting different areas of a payment instrument image independently
    • 独立调整支付工具图像的不同区域
    • US09384392B2
    • 2016-07-05
    • US14256471
    • 2014-04-18
    • Scott WeberRian Maloney
    • Scott WeberRian Maloney
    • G06K9/00G06Q20/04G06Q40/00
    • G06K9/00463G06K9/2081G06Q20/042G06Q20/0425H04N1/44
    • The present disclosure involves systems, software, and computer-implemented methods for allowing independent adjustment for different areas of a payment instrument image. An example method includes receiving an original payment instrument image associated with a tangible payment instrument; creating a clearing payment instrument image based on the original payment instrument image associated with a first contrast value; presenting the clearing payment instrument image in a user interface in response to creating the clearing payment instrument image; in response to presenting the clearing payment instrument image: receiving an indication of an area of the clearing payment instrument image from the user interface; receiving an indication of a second contrast value to which to update the indicated area from the user interface; and updating a contrast value of the indicated area of the clearing payment instrument image to the second contrast value.
    • 本公开涉及用于允许对支付工具图像的不同区域进行独立调整的系统,软件和计算机实现的方法。 示例性方法包括接收与有形支付工具相关联的原始支付工具图像; 基于与第一对比度值相关联的原始支付工具图像来创建清算支付工具图像; 响应于创建清算支付工具图像,在用户界面中呈现清算支付工具图像; 响应于提供清算支付工具图像:从用户界面接收清算支付工具图像的区域的指示; 从所述用户界面接收用于更新所述指示区域的第二对比度值的指示; 以及将清算支付工具图像的指示区域的对比度值更新为第二对比度值。
    • 5. 发明授权
    • Aircraft cabin door pressure vent system
    • 飞机舱门压力排气系统
    • US08403265B2
    • 2013-03-26
    • US12874061
    • 2010-09-01
    • Greg GowingScott WeberElisabeth ArchibaldShad PlanteMatt Wiley
    • Greg GowingScott WeberElisabeth ArchibaldShad PlanteMatt Wiley
    • B64C1/14
    • B64C1/1461B64C1/14B64C1/1407B64C1/143
    • Disclosed is an aircraft door including a handle-activated pressure relief system that avoids potentially dangerous pressure differences between the cabin and the atmosphere outside the aircraft. A flow path is created between the inboard and outboard handles on the door. A pressure vent door is located in the flow path. The vent door being is opened when either of the inboard and outboard handle assemblies are activated. Once either handle is rotated beyond a particular point, a spring in the supporting mechanics becomes over-center. At the same time, the vent door comes under the influence of a magnet, snapping the vent open. After the door has been opened, it can be relatched by operating the handles in the reverse direction. The magnet and spring hold the vent door open until the aircraft door is fully latched, sealed, and secured. Only then does the vent door sealingly close.
    • 公开了一种飞机门,其包括手柄启动的压力释放系统,其避免了机舱和飞机外部的大气之间潜在的危险压力差。 在门上的内侧和外侧手柄之间形成流路。 压力通风门位于流路中。 当内侧和外侧手柄组件中的任一个被启动时,通风门被打开。 一旦任一个手柄旋转超过特定点,支撑力学中的弹簧变得越过中心。 同时,通风门受到磁铁的影响,将通风口打开。 门打开后,可以通过相反方向操作手柄来重新配置。 磁体和弹簧将通风门打开,直到飞机门完全锁定,密封和固定。 只有这样,通风门密封地关闭。