Reference electrode and detector using the same for detecting acidity or basicity of oil
    51.
    发明申请
    Reference electrode and detector using the same for detecting acidity or basicity of oil 审中-公开
    参考电极和检测器用于检测油的酸度或碱度

    公开(公告)号:US20070029196A1

    公开(公告)日:2007-02-08

    申请号:US11493537

    申请日:2006-07-27

    IPC分类号: G01N27/26

    CPC分类号: G01N33/2876 G01N27/301

    摘要: A reference electrode is used for detecting acidity or basicity of an oil with a sensitive electrode changed in response to the acidity or basicity of the oil. The reference electrode and the sensitive electrode are used as a pair of electrodes for detecting a difference between an electric potential of the sensitive electrode and an electric potential of the reference electrode. The reference electrode has a substantially constant output potential with respect to a pH which is changed according to the acidity or basicity of the oil. The reference electrode is constructed with an electrode substrate made of a metal, and a metal salt provided on the electrode substrate, such that the metal salt contains the metal and is hardly soluble in water.

    摘要翻译: 参考电极用于检测响应于油的酸度或碱度而改变的敏感电极的油的酸度或碱度。 参考电极和敏感电极用作一对电极,用于检测敏感电极的电位和参考电极的电位之间的差异。 相对于根据油的酸度或碱度而改变的pH,参考电极具有基本恒定的输出电位。 参考电极由金属制成的电极基板和设置在电极基板上的金属盐构成,金属盐含有金属,难以溶于水。

    SMART ALTITUDE CALLOUT FOR HELICOPTERS
    52.
    发明申请
    SMART ALTITUDE CALLOUT FOR HELICOPTERS 有权
    SMART ALTTUDE CALLOUT for HELICOPTERS

    公开(公告)号:US20070013558A1

    公开(公告)日:2007-01-18

    申请号:US11160509

    申请日:2005-06-27

    申请人: Yasuo Ishihara

    发明人: Yasuo Ishihara

    IPC分类号: G08B21/00

    摘要: A method, computer software product, and system to generate altitude callouts according to proximity to a runway at an airport or heliport includes determining whether the helicopter is flying in proximity to the runway and automatically selecting an altitude threshold increment set based upon the determination. The threshold increment set including a plurality of altitude threshold values. A calculated terrain clearance value is calculated for each of the plurality of altitude threshold values. A suitable warning is automatically generated according to the comparison. Selecting an altitude threshold increment set includes selecting one of the group consisting of first altitude threshold increment set including a plurality of higher altitude threshold values and a second altitude increment set including the plurality of higher altitude threshold values and further including a plurality of lower altitude threshold values.

    摘要翻译: 根据机场或直升机场的跑道附近产生高度标注的方法,计算机软件产品和系统包括确定直升机是否在靠近跑道的地方飞行,并且基于该确定自动选择设置的高度阈值增量。 包括多个高度阈值的阈值增量集合。 为多个高度阈值中的每一个计算出计算出的地形距离值。 根据比较自动生成合适的警告。 选择高度阈值增量集合包括选择由包括多个较高海拔阈值的第一高度阈值增量集合和包括多个较高高度阈值的第二高度增量集合组成的组中的一个,并且还包括多个较低高度阈值 价值观。

    Apparatus, method, and computer program product for generating terrain clearance floor envelopes about a selected runway
    55.
    发明授权
    Apparatus, method, and computer program product for generating terrain clearance floor envelopes about a selected runway 有权
    装置,方法和计算机程序产品,用于在所选择的跑道上产生地形清除地面信封

    公开(公告)号:US06707394B2

    公开(公告)日:2004-03-16

    申请号:US09496296

    申请日:2000-02-01

    IPC分类号: G08B2300

    CPC分类号: G05D1/0676 G01C5/005

    摘要: The present invention provides several apparatus, methods, and computer program products for generating a terrain clearance floor envelope for use in a ground proximity warning system. In one embodiment, the present invention includes a processor that defines a terrain clearance floor envelope having at least two boundaries. In this embodiment, the processor defines at least one of the boundaries based on a runway position quality factor, an altitude data quality factor, and an aircraft position quality factor. Using these factors, the processor of the present invention can more precisely define the boundaries of the envelope about the selected runway. Further, the processor of the present invention does not unnecessarily increase the region between the envelope and runway where no ground proximity alarms are generated. In another embodiment, the present invention includes a processor that defines the terrain clearance floor envelope to be asymmetrical, such that respective profiles of the envelope in a radial cross-section are different in at least two radial directions from a center point of the selected runway. Importantly, in one embodiment of the present invention, the processor defines end regions of the terrain clearance floor envelope adjacent to the ends of the selected runway to have a different slope profile than side regions of the terrain clearance floor envelope adjacent to the sides of the selected runway. This, in turn, allows the processor to define the end regions to reflect a landing pattern for an aircraft approaching the end of the selected runway, while also defining the side regions to reflect a flight pattern for an aircraft approaching the side of the selected runway.

    摘要翻译: 本发明提供了用于产生用于地面接近警告系统中的地形间隙地面信封的几种装置,方法和计算机程序产品。 在一个实施例中,本发明包括限定具有至少两个边界的地形间隙地面包层的处理器。 在该实施例中,处理器基于跑道位置质量因子,高度数据质量因子和飞机位置质量因子来定义至少一个边界。 使用这些因素,本发明的处理器可以更精确地定义关于所选跑道的信封的边界。 此外,本发明的处理器不会不必要地增加不产生接地接近警报的信封和跑道之间的区域。 在另一个实施例中,本发明包括一个处理器,该处理器将地形间隙底面信封定义为不对称的,使得在径向横截面中的包络的相应轮廓在从所选择的跑道的中心点起的至少两个径向方向上是不同的 。 重要的是,在本发明的一个实施例中,处理器限定与所选择的跑道的端部相邻的地形间隙地板信封的端部区域,以具有与邻近所述跑道侧面的地形间隙地板信封的侧部区域不同的斜率分布 选择跑道。 这反过来又允许处理器定义端部区域以反映接近所选跑道端部的飞行器的着陆模式,同时还限定侧面区域以反映接近所选跑道侧面的飞行器的飞行模式 。

    Solid-state image device with resin lens and resin contact layer
    56.
    发明授权
    Solid-state image device with resin lens and resin contact layer 失效
    具有树脂透镜和树脂接触层的固态成像装置

    公开(公告)号:US4667092A

    公开(公告)日:1987-05-19

    申请号:US564403

    申请日:1983-12-22

    申请人: Yasuo Ishihara

    发明人: Yasuo Ishihara

    CPC分类号: H01L31/0232 H01L31/02162

    摘要: In a solid-state image device comprising an image storage block having a block surface, a plurality of storage elements are embeded along the block surface to store an image in the form of electric charge. An overlying layer is deposited to form an array of optical lenses in correspondence to the storage elements. An intermediate layer is laid between the block surface and the overlying layer. Incident light focuses through the lenses and the intermediate layer onto the storage elements. The intermediate layer serves as an adjusting layer for adjusting a focal length.

    摘要翻译: 在包括具有块表面的图像存储块的固态图像装置中,沿着块表面嵌入多个存储元件以以电荷的形式存储图像。 沉积覆盖层以形成对应于存储元件的光学透镜阵列。 中间层铺设在块表面和上覆层之间。 入射光通过透镜和中间层聚焦到存储元件上。 中间层用作调整焦距的调整层。

    Solid-state imaging device having a reduced image lag
    57.
    发明授权
    Solid-state imaging device having a reduced image lag 失效
    具有减小的图像滞后的固态成像装置

    公开(公告)号:US4484210A

    公开(公告)日:1984-11-20

    申请号:US297759

    申请日:1981-08-31

    CPC分类号: H01L27/14831

    摘要: A solid-state imaging device has a semiconductor substrate of one conductive type. A plurality of light-charge converter regions, of the opposite conductivity type, are formed in the semiconductor substrate. A charge-voltage converter region, formed in the semiconductor substrate, converts the electric charge produced by the light-charge converter regions into a voltage. At least one charge transfer section is formed in the semiconductor substrate for transferring the electric charge produced by the light-charge converter regions to the charge-voltage converter region. At least one charge transfer gate section is in the semiconductor substrate and has a gate electrode for controlling the timing of a transfer of the electric charges from the light-charge converter regions to the charge transfer section. Pulses are generated with a predetermined pulse potential and applied to the gate electrode in the charge transfer gate section. The predetermined pulse potential has the relationshipV.sub.B +2.phi..sub.FP

    摘要翻译: 固态成像装置具有一种导电类型的半导体衬底。 在半导体衬底中形成有相反导电类型的多个光电荷转换器区域。 形成在半导体基板中的电荷 - 电压转换器区域将由光电荷转换器区域产生的电荷转换为电压。 在半导体衬底中形成至少一个电荷转移部分,用于将由光电荷转换器区域产生的电荷转移到电荷 - 电压转换器区域。 至少一个电荷转移栅极部分在半导体衬底中并且具有用于控制电荷从光电荷转换器区域转移到电荷转移部分的定时的栅电极。 产生具有预定脉冲电位的脉冲并施加到电荷转移栅极部分中的栅电极。 预定脉冲电位具有关系VB + 2 phi FP

    Two-dimensional charge-coupled device for high-resolution image pickup
and the like
    58.
    发明授权
    Two-dimensional charge-coupled device for high-resolution image pickup and the like 失效
    用于高分辨率图像拾取的二维电荷耦合器件等

    公开(公告)号:US4127877A

    公开(公告)日:1978-11-28

    申请号:US618416

    申请日:1975-10-01

    CPC分类号: H04N3/1575

    摘要: A two-dimensional charge-coupled device for relatively high resolution image pick up includes an imaging area, a storage area, and plural output registers for developing plural video signals delayed by predetermined intervals, e.g., integral multiples of one horizontal line trace period. The several register output signals are combined to provide a composite video signal characterized by a greater resolution vis-a-vis the direct CCD output.

    摘要翻译: 用于相对高分辨率图像拾取的二维电荷耦合器件包括成像区域,存储区域和用于显影以预定间隔延迟的多个视频信号的多个输出寄存器,例如一个水平线迹线周期的整数倍。 多个寄存器输出信号被组合以提供特征在于相对于直接CCD输出更大分辨率的复合视频信号。

    Systems and methods for adjusting target approach speed
    59.
    发明授权
    Systems and methods for adjusting target approach speed 有权
    调整目标进近速度的系统和方法

    公开(公告)号:US08996204B2

    公开(公告)日:2015-03-31

    申请号:US12821445

    申请日:2010-06-23

    IPC分类号: G05D1/00 G05D1/06

    摘要: Systems and methods for adjusting target approach speed for use in a “Too Fast” approach to landing condition. An exemplary system stores predefined maximum wind setting and a predefined reference speed and a pilot set bug speed value. A processing device sets a target speed equal to the bug speed, if the bug speed is less than the reference speed plus a value associated with a predefined maximum wind setting, and sets the target speed equal to the reference speed plus the max wind added value, if the manual bug speed is not less than the reference speed plus the max wind added value. An output device outputs an alert if the received aircraft speed is greater than the set target speed plus a predefined error value when the received aircraft location is within a threshold value of a touchdown point.

    摘要翻译: 调整目标进近速度的系统和方法用于“太快”的着陆条件。 示例性系统存储预定义的最大风力设定和预定的参考速度和飞行员设置的错误速度值。 如果错误速度小于参考速度加上与预定义的最大风力设定相关联的值,则处理设备将目标速度设置为等于故障速度,并将目标速度设置为等于参考速度加上最大风力附加值 ,如果手动的错误速度不低于参考速度加上最大风量附加值。 如果所接收的飞行器位置在接地点的阈值内,则所接收到的飞行器速度大于设定的目标速度加上预定义的误差值,则输出设备输出报警。

    SYSTEMS AND METHODS FOR PERFORMING EXCESSIVE NEGATIVE PITCH ALERT AND BIASING SINK RATE ALERT
    60.
    发明申请
    SYSTEMS AND METHODS FOR PERFORMING EXCESSIVE NEGATIVE PITCH ALERT AND BIASING SINK RATE ALERT 有权
    用于执行过大的负面提示警报和偏移波长提醒的系统和方法

    公开(公告)号:US20110276200A1

    公开(公告)日:2011-11-10

    申请号:US12821591

    申请日:2010-06-23

    IPC分类号: G05D1/08

    CPC分类号: G05D1/0858 G01C23/00

    摘要: Systems and methods that alert the pilot of the unusual negative pitch attitude. Additionally, the system can bias a “sink rate” envelope toward a more sensitive direction, such that the pilot can be alerted while (or before) a large sink rate is built up during an unusual negative pitch attitude condition.

    摘要翻译: 系统和方法提醒飞行员异常负俯仰姿态。 此外,系统可以将“下沉速率”信号偏向更敏感的方向,使得可以在(或之前)在异常负俯仰姿态条件期间建立大的下沉速率时警告飞行员。