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    PHYSIOLOGICAL MONITOR GAUGE PANEL
    1.
    发明申请
    PHYSIOLOGICAL MONITOR GAUGE PANEL 审中-公开

    公开(公告)号：US20180087937A1

    公开(公告)日：2018-03-29

    申请号：US15719218

    申请日：2017-09-28

    Applicant: MASIMO CORPORATION

    Inventor： Ammar Al-Ali ,  Bilal Muhsin ,  Keith Indorf ,  Massi Joe E. Kiani

    IPC: G01D13/06

    CPC classification number: G01D13/06 ,  G01D7/02

    Abstract: A physiological monitor gauge panel defines parameters to display on a physiological monitor via corresponding gauges. Gauge faces depict a range of parameter values for each of the parameters. An indicator designates a position on each gauge face corresponding to the current parameter value within the range of parameter values. The indicated position on each of the gauges is at the mid-point of each of the gauge faces when each of the parameters is at a nominal value.

    POWER SAFETY INSTRUMENT SYSTEM
    4.
    发明申请
    POWER SAFETY INSTRUMENT SYSTEM 有权
    电力安全仪表系统

    公开(公告)号：US20160272342A1

    公开(公告)日：2016-09-22

    申请号：US15168356

    申请日：2016-05-31

    Applicant: TEXTRON INNOVATIONS INC.

    Inventor： James M. McCollough ,  Erik Oltheten ,  Nicholas Lappos

    IPC: B64D45/00 ,  B64C27/04 ,  B64D43/00

    CPC classification number: G01C23/00 ,  B60Q1/00 ,  B64C27/00 ,  B64C27/006 ,  B64C27/04 ,  B64C27/52 ,  B64C29/00 ,  B64C39/024 ,  B64C2201/108 ,  B64C2201/121 ,  B64D43/00 ,  B64D45/00 ,  G01C21/00 ,  G01D7/02 ,  G05D17/02

    Abstract: A power safety system is configured to provide power information in an aircraft. The power safety system includes a power safety instrument having a power required indicator and a power available indicator, each being located on a display. A position of the power required indicator and the power available indicator represent the power available and power required to perform a hover flight maneuver. The power safety system may be operated in a flight planning mode or in a current flight mode. The power safety system uses at least one sensor to measure variables having an effect on the power required and the power available.

    Abstract translation: 电力安全系统被配置为在飞行器中提供电力信息。 电力安全系统包括具有电力需求指示器和功率可用指示器的电力安全仪器，每个都位于显示器上。 所需电源指示灯和电源指示灯的位置表示执行悬停飞行操作所需的电力和功率。 电力安全系统可以在飞行计划模式或当前飞行模式下操作。 电力安全系统使用至少一个传感器来测量对所需功率和可用功率有影响的变量。

    Angle of attack display
    5.
    发明授权
    Angle of attack display 有权
    攻击角度显示

    公开(公告)号：US09193473B2

    公开(公告)日：2015-11-24

    申请号：US14032840

    申请日：2013-09-20

    Applicant: Safe Flight Instrument Corporation

    Inventor： Arthur C. Barth ,  Randall A. Greene ,  Louis Simons ,  Darren Taillie

    IPC: G08B23/00 ,  B64D43/02 ,  G01D1/00

    CPC classification number: B64D43/02 ,  G01D1/00 ,  G01D7/02

    Abstract: An aircraft safety system includes a Stall/Spin Warning & Recovery Computer, an angle of attack sensor, a side slip sensor and an angle of attack display. The Stall/Spin Warning and Recovery Computer detects whether the aircraft is in a safe condition or an unsafe condition. The angle of attack display includes a first configuration that displays information indicative of safe aircraft condition when the orientation detector detects a safe condition and a second configuration that displays information indicative of unsafe aircraft condition when the computer detects an unsafe condition. The display may transition from the first configuration to the second configuration when the orientation detector detects an unsafe condition and then to a third configuration, which may include visual control-input instructions that enable recovery to a safe condition.

    Abstract translation: 飞机安全系统包括失速/旋转警告和恢复计算机，攻角传感器，侧滑传感器和迎角显示。 失速/旋转警告和恢复计算机检测飞机是否处于安全状态或不安全状态。 所述迎角显示包括当所述方向检测器检测到安全状态时显示指示安全飞行器状况的信息的第一配置和当所述计算机检测到不安全状态时显示指示不安全飞行器状况的信息的第二配置。 当定向检测器检测到不安全状况，然后到第三配置时，显示器可以从第一配置转变到第二配置，其中可以包括能够恢复到安全状态的视觉控制输入指令。

    Power safety instrument system
    7.
    发明授权
    Power safety instrument system 有权
    电力安全仪表系统

    公开(公告)号：US09035802B2

    公开(公告)日：2015-05-19

    申请号：US13641325

    申请日：2010-12-22

    Applicant: James M. McCollough ,  Erik Oltheten ,  Nicholas Lappos

    Inventor： James M. McCollough ,  Erik Oltheten ,  Nicholas Lappos

    IPC: G08B21/00 ,  B60Q1/00 ,  B64C27/04 ,  B64D43/00

    CPC classification number: G01C23/00 ,  B60Q1/00 ,  B64C27/00 ,  B64C27/006 ,  B64C27/04 ,  B64C27/52 ,  B64C29/00 ,  B64C39/024 ,  B64C2201/108 ,  B64C2201/121 ,  B64D43/00 ,  B64D45/00 ,  G01C21/00 ,  G01D7/02 ,  G05D17/02

    Abstract: A power safety system is configured to provide power information in an aircraft. The power safety system includes a power safety instrument having a power required indicator and a power available indicator, each being located on a display. A position of the power required indicator and the power available indicator represent the power available and power required to perform a hover flight maneuver. The power safety system may be operated in a flight planning mode or in a current flight mode. The power safety system uses at least one sensor to measure variables having an effect on the power required and the power available.

    Abstract translation: 电力安全系统被配置为在飞行器中提供电力信息。 电力安全系统包括具有电力需求指示器和功率可用指示器的电力安全仪器，每个指示器位于显示器上。 所需电源指示灯和电源指示灯的位置表示执行悬停飞行操作所需的电力和功率。 电力安全系统可以在飞行计划模式或当前飞行模式下操作。 电力安全系统使用至少一个传感器来测量对所需功率和可用功率有影响的变量。

    METHOD OF DISPLAYING A PARAMETER
    8.
    发明申请
    METHOD OF DISPLAYING A PARAMETER 审中-公开
    显示参数的方法

    公开(公告)号：US20150084963A1

    公开(公告)日：2015-03-26

    申请号：US14265625

    申请日：2014-04-30

    Applicant: GE Aviation Systems Limited

    Inventor： Donna Louise Green ,  Brian David Larder ,  Andrew James Smith ,  Peter Robin Knight

    IPC: G01D7/02 ,  G06T11/20

    CPC classification number: G01D7/02 ,  G06T11/206

    Abstract: A method of displaying a parameter that can be modeled by an algorithm having multiple variables on a display to provide an understanding of an impact of the variables on the parameter, the method includes displaying on a first portion of the display a plot of the parameter for a first period and simultaneously with the display of the plot of the parameter, displaying on a second portion of the display, different from the first portion, a plot related to the parameter.

    Abstract translation: 一种显示可以通过在显示器上具有多个变量的算法来建模的参数以提供对变量对参数的影响的理解的方法，所述方法包括在显示器的第一部分上显示参数的图， 第一时段，同时显示参数图，在与第一部分不同的显示器的第二部分上显示与该参数有关的曲线。

    ANGLE OF ATTACK DISPLAY
    9.
    发明申请
    ANGLE OF ATTACK DISPLAY 有权
    攻击角度

    公开(公告)号：US20150084792A1

    公开(公告)日：2015-03-26

    申请号：US14032840

    申请日：2013-09-20

    Applicant: Safe Flight Instrument Corporation

    Inventor： Arthur C. BARTH ,  Randall A. GREENE ,  Louis SIMONS ,  Darren TAILLIE

    IPC: B64D43/02

    CPC classification number: B64D43/02 ,  G01D1/00 ,  G01D7/02

    Abstract: An aircraft safety system includes a Stall/Spin Warning & Recovery Computer, an angle of attack sensor, a side slip sensor and an angle of attack display. The Stall/Spin Warning and Recovery Computer detects whether the aircraft is in a safe condition or an unsafe condition. The angle of attack display includes a first configuration that displays information indicative of safe aircraft condition when the orientation detector detects a safe condition and a second configuration that displays information indicative of unsafe aircraft condition when the computer detects an unsafe condition. The display may transition from the first configuration to the second configuration when the orientation detector detects an unsafe condition and then to a third configuration, which may include visual control-input instructions that enable recovery to a safe condition.

    Abstract translation: 飞机安全系统包括失速/旋转警告和恢复计算机，攻角传感器，侧滑传感器和迎角显示。 失速/旋转警告和恢复计算机检测飞机是否处于安全状态或不安全状态。 所述迎角显示包括当所述方向检测器检测到安全状态时显示指示安全飞行器状况的信息的第一配置和当所述计算机检测到不安全状态时显示指示不安全飞行器状况的信息的第二配置。 当定向检测器检测到不安全状况，然后到第三配置时，显示器可以从第一配置转变到第二配置，其中可以包括能够恢复到安全状态的视觉控制输入指令。

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