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    System and Method for Displaying an Electronic Checklist
    1.
    发明申请
    System and Method for Displaying an Electronic Checklist 审中-公开

    公开(公告)号：US20180292953A1

    公开(公告)日：2018-10-11

    申请号：US15480249

    申请日：2017-04-05

    Applicant: THE BOEING COMPANY

    Inventor： Vikram H. Pandya ,  Joshua Lee Downs ,  Alex Jay Campise ,  Mark Ivan Nikolic

    IPC: G06F3/0482 ,  B64D37/26 ,  B64D37/28

    Abstract: A system includes display equipment and a processor coupled to the display equipment. The processor is configured to cause the display equipment to display an electronic checklist associated with an aircraft. The processor is configured determine whether the electronic checklist includes a checklist item associated with a particular control page of a plurality of control pages. The processor is configured to, based on determining that the electronic checklist includes the checklist item associated with the particular control page, cause the display equipment to display the particular control page that includes a control element that is selectable to cause a control command to be sent to one or more components.

    System and method for displaying an electronic checklist for an aircraft
    3.
    发明授权
    System and method for displaying an electronic checklist for an aircraft 有权

    公开(公告)号：US10705684B2

    公开(公告)日：2020-07-07

    申请号：US15480249

    申请日：2017-04-05

    Applicant: THE BOEING COMPANY

    Inventor： Vikram H. Pandya ,  Joshua Lee Downs ,  Alex Jay Campise ,  Mark Ivan Nikolic

    IPC: G06F9/48 ,  G06F3/0482 ,  G06F3/0488 ,  G06F3/0484 ,  B64D43/00

    Abstract: A system includes display equipment and a processor coupled to the display equipment. The processor is configured to cause the display equipment to display an electronic checklist associated with an aircraft. The processor is configured determine whether the electronic checklist includes a checklist item associated with a particular control page of a plurality of control pages. The processor is configured to, based on determining that the electronic checklist includes the checklist item associated with the particular control page, cause the display equipment to display the particular control page that includes a control element that is selectable to cause a control command to be sent to one or more components.

    Flight Deck Touch Screen Interface for Interactive Displays
    5.
    发明申请
    Flight Deck Touch Screen Interface for Interactive Displays 有权
    交互式显示器的飞行甲板触摸屏界面

    公开(公告)号：US20150123912A1

    公开(公告)日：2015-05-07

    申请号：US14073288

    申请日：2013-11-06

    Applicant: THE BOEING COMPANY

    Inventor： Mark Ivan Nikolic ,  Brian David Gilbert ,  Jayson Jean Bowen

    IPC: B64D43/00 ,  G06F3/0488 ,  G08G5/00 ,  G06F3/041

    CPC classification number: B64D43/00 ,  G01C23/00 ,  G01C23/005 ,  G06F3/0416 ,  G06F3/0481 ,  G06F3/04883 ,  G06F2203/04803 ,  G08G5/0047

    Abstract: A system and method for controlling a display on an aircraft. An operator interaction with an edge area of a touch screen is identified by a processor unit when a first format of the display is displayed on the touch screen. The edge area extends along an edge of the touch screen. A second format of the display is displayed on the touch screen by the processor unit in response to identifying the operator interaction with the edge area of the touch screen. The second format of the display is different from the first format of the display.

    Abstract translation: 一种用于控制飞机上的显示器的系统和方法。 当触摸屏上显示第一格式的显示器时，由处理器单元识别与触摸屏的边缘区域的操作者交互。 边缘区域沿着触摸屏的边缘延伸。 响应于识别操作者与触摸屏的边缘区域的交互，处理器单元在触摸屏上显示第二格式的显示。 显示器的第二种格式与显示器的第一种格式不同。

    Display-based flight deck autobrake selection
    6.
    发明授权
    Display-based flight deck autobrake selection 有权

    公开(公告)号：US09738378B1

    公开(公告)日：2017-08-22

    申请号：US15094337

    申请日：2016-04-08

    Applicant: The Boeing Company

    Inventor： Mark Ivan Nikolic ,  Joseph A. Sikora ,  William Lawrence Hunt ,  Jean M. Crane ,  Jennifer L. Gertley

    IPC: B64C25/42 ,  B64D43/00

    CPC classification number: B64C25/426 ,  B64D43/00

    Abstract: A system and method for braking an aircraft. A processor unit identifies an operating condition of the aircraft. The processor unit displays available modes indications on a display device on the aircraft. The available modes indications indicate modes of operating an automatic braking system on the aircraft that are available for selection by an operator based on the operating condition of the aircraft. The processor unit receives a mode selection from an operator interface. The mode selection indicates a selected mode of operating the automatic braking system that is selected by the operator from the available modes. The processor unit displays on the display device a selected mode indication indicating the selected mode.

    Pilot Health and Alertness Monitoring, Communication and Safeguarding
    8.
    发明申请
    Pilot Health and Alertness Monitoring, Communication and Safeguarding 有权

    公开(公告)号：US20210034053A1

    公开(公告)日：2021-02-04

    申请号：US16526850

    申请日：2019-07-30

    Applicant: The Boeing Company

    Inventor： Mark Ivan Nikolic ,  Lisa C. Thomas

    IPC: G05D1/00 ,  G08G5/00 ,  B64D25/00 ,  A61B5/18

    Abstract: Systems and methods for monitoring, communicating and safeguarding the health and alertness of a pilot during operation of an aircraft. The state of the pilot is monitored using biometric sensors. A pilot state data processor of an onboard computer system determines whether the value of any health/alertness parameter has exceeded a specified threshold or not.
    The onboard computer system further includes an automatic control processor that automatically transfers control authority from the pilot to the autopilot and then issues an unfit pilot alert. Then a real-time audio/video/data connection is established between the pilot onboard the aircraft and a remote medical professional. The remote medical professional evaluates the medical fitness of the pilot and determines whether the pilot automated mitigations should be continued (pilot unfit for duty) or removed (pilot fit for duty).

    Flight deck touch-sensitive hardware controls
    9.
    发明授权
    Flight deck touch-sensitive hardware controls 有权
    飞行甲板触摸屏硬件控制

    公开(公告)号：US09471176B2

    公开(公告)日：2016-10-18

    申请号：US14509063

    申请日：2014-10-08

    Applicant: The Boeing Company

    Inventor： Mark Ivan Nikolic ,  Stephen Minarsch

    IPC: G01C23/00 ,  G05D1/00 ,  G05D3/00 ,  G06F7/00 ,  G06F17/00 ,  G06F7/70 ,  G06F19/00 ,  G06G7/00 ,  G06G7/76 ,  G06F3/041 ,  G06F3/00 ,  G06F3/0488

    CPC classification number: G06F3/0416 ,  G01C23/00 ,  G01C23/005 ,  G05D1/00 ,  G06F3/00 ,  G06F3/0488

    Abstract: Touch or proximity sensors are integrated into control devices such as knobs, dials or wheels incorporated in a user control panel. A control output processor detects whether any of the sensors are outputting signals indicating that a control device is being touched (or nearly touched) by a user. The control output processor causes an associated display area to be highlighted or otherwise modified on a display screen to indicate to the user which control device is being touched. This feature allows for “no-look” interaction with control panels, and keeps the user's eyes focused on the relevant displays where the control devices produce effects. This allows users to preview and verify that the correct control device is being manipulated prior to taking any (potentially erroneous) control actions.

    Abstract translation: 触摸或接近传感器集成到控制设备中，例如嵌入用户控制面板中的旋钮，刻度盘或轮。 控制输出处理器检测是否有任何传感器正在输出指示控制设备被用户触摸（或几乎被触摸）的信号。 控制输出处理器使相关联的显示区域在显示屏幕上被突出显示或以其他方式修改，以向用户指示正在触摸哪个控制装置。 该功能允许与控制面板进行“无外观”交互，并将用户的眼睛保持在控制设备产生效果的相关显示器上。 这允许用户在采取任何（潜在的错误）控制动作之前，预览和验证正在操纵正确的控制设备。

    Flight deck touch screen interface for interactive displays
    10.
    发明授权
    Flight deck touch screen interface for interactive displays 有权
    飞行甲板触摸屏界面，用于交互式显示

    公开(公告)号：US09352848B2

    公开(公告)日：2016-05-31

    申请号：US14073288

    申请日：2013-11-06

    Applicant: The Boeing Company

    Inventor： Mark Ivan Nikolic ,  Brian David Gilbert ,  Jayson Jean Bowen

    IPC: G06F3/041 ,  B64D43/00 ,  G06F3/0488 ,  G08G5/00 ,  G01C23/00 ,  G06F3/0481

    CPC classification number: B64D43/00 ,  G01C23/00 ,  G01C23/005 ,  G06F3/0416 ,  G06F3/0481 ,  G06F3/04883 ,  G06F2203/04803 ,  G08G5/0047

    Abstract: A system and method for controlling a display on an aircraft. An operator interaction with an edge area of a touch screen is identified by a processor unit when a first format of the display is displayed on the touch screen. The edge area extends along an edge of the touch screen. A second format of the display is displayed on the touch screen by the processor unit in response to identifying the operator interaction with the edge area of the touch screen. The second format of the display is different from the first format of the display.

    Abstract translation: 一种用于控制飞机上的显示器的系统和方法。 当触摸屏上显示第一格式的显示器时，由处理器单元识别与触摸屏的边缘区域的操作者交互。 边缘区域沿着触摸屏的边缘延伸。 响应于识别操作者与触摸屏的边缘区域的交互，处理器单元在触摸屏上显示第二格式的显示。 显示器的第二种格式与显示器的第一种格式不同。

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