中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

19 records (took 0.017 seconds)

    TOUCH SCREEN CONTROLLER WITH DATA EXCHANGE AND MINING SERVICE
    11.
    发明申请
    TOUCH SCREEN CONTROLLER WITH DATA EXCHANGE AND MINING SERVICE 审中-公开

    公开(公告)号：US20190243504A1

    公开(公告)日：2019-08-08

    申请号：US15888810

    申请日：2018-02-05

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Raghu Shamasundar ,  Mahesh Sivaratri ,  Mark Pearson ,  Kalimulla Khan ,  Todd Wisner

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

    CPC classification number: G06F9/5038

    Abstract: A touch screen controller for an aircraft and a method for operating the same are provided. The method, for example, may include, but is not limited to, receiving, by a core interface in a first core of a touch screen controller, a data or service request for a flight management system from a second core of a touch screen controller, validating, by the core interface, the received data or service request for the flight management system, wherein the data or service request is validated when the applications executing on the first core are idle, a flight phase of the aircraft matches a flight phase associated with the application executing on the second core, and the data or service request is within aircraft performance limits and operational limits.

    FLIGHT DECK MULTIFUNCTION CONTROL DISPLAY UNIT
    14.
    发明申请
    FLIGHT DECK MULTIFUNCTION CONTROL DISPLAY UNIT 有权
    飞行机组多功能控制显示单元

    公开(公告)号：US20160034250A1

    公开(公告)日：2016-02-04

    申请号：US14552757

    申请日：2014-11-25

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Sue McCullough ,  Mark Pearson ,  Phillip Toews ,  Charles Dairman ,  Shane Lai ,  Hariharan Saptharishi ,  Venkat Ramana Mummadi

    IPC: G06F3/16 ,  G06F3/041 ,  G06F3/01

    CPC classification number: G06F3/167 ,  B64D43/00 ,  G06F3/017 ,  G06F3/0416 ,  G10L15/22 ,  G10L15/26

    Abstract: Systems and methods for controlling a flight deck multifunction control display unit are disclosed. In various embodiments, the systems may comprise a flight management system or other MCDU driven devices, a command database that stores a plurality of voice commands and a plurality of multifunction control display unit commands. In various embodiments, each voice command is associated with one of the plurality of multifunction control display unit commands. The systems may further comprise a pilot voice interface configured to receive a voice command from a pilot and transmit the voice command to the multifunction control display unit. The multifunction control display unit can receive the voice command from the pilot voice interface and, in response, access the command database to identify a multifunction control display unit command in the command database that is associated with the voice command.

    Abstract translation: 公开了用于控制驾驶舱多功能控制显示单元的系统和方法。 在各种实施例中，系统可以包括飞行管理系统或其他MCDU驱动设备，存储多个语音命令的命令数据库和多个多功能控制显示单元命令。 在各种实施例中，每个语音命令与多个多功能控制显示单元命令之一相关联。 系统还可以包括导频语音接口，其被配置为从导频接收语音命令，并将语音命令发送到多功能控制显示单元。 多功能控制显示单元可以从导频语音接口接收语音命令，作为响应，访问命令数据库以识别与语音命令相关联的命令数据库中的多功能控制显示单元命令。

    Custom search queries for flight data
    15.
    发明授权
    Custom search queries for flight data 有权

    公开(公告)号：US11328610B2

    公开(公告)日：2022-05-10

    申请号：US16043854

    申请日：2018-07-24

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Sripathi Ramachandra ,  Mark Pearson ,  Greg Carlucci ,  Richard Snyder

    IPC: G08G5/00 ,  G06F16/9537 ,  B64D43/00

    Abstract: Systems and methods of searching stored flight plan information using a custom search query including at least one aircraft parameter condition or environmental parameter condition. The systems and method include receiving, using a user interface module, a custom search query comprising an aircraft parameter condition or an environmental condition; searching, using a processor module, stored flight plan information for instances in the stored flight plan information that satisfy the aircraft parameter condition or environmental condition; and displaying, using a display module, the instances in the stored flight plan information that satisfy the aircraft parameter condition or environmental condition.

    MULTIPLE FLIGHT DATA REFERENCE FOR A SPECIFIC SELECTION ON A VERTICAL AND LATERAL DISPLAY
    17.
    发明申请
    MULTIPLE FLIGHT DATA REFERENCE FOR A SPECIFIC SELECTION ON A VERTICAL AND LATERAL DISPLAY 审中-公开

    公开(公告)号：US20190279514A1

    公开(公告)日：2019-09-12

    申请号：US15912942

    申请日：2018-03-06

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Sripathi Ramachandra ,  Mark Pearson ,  Greg Carlucci ,  Richard Snyder ,  Balaji Srinivasan

    IPC: G08G5/00 ,  G01C23/00

    Abstract: Methods and systems for a flight display system are provided. The method includes: commanding a vertical situation display (VSD) and a lateral navigation display (ND) to render, concurrently, a viewing segment of a flight plan. The method includes receiving a user input selecting a section of the viewing segment, the user input being received on only one of the VSD and the ND. The method continues by commanding, concurrently, the VSD and the ND to visually distinguish the section, and to demark the section on the VSD with starting points and ending points. The method identifies a flight parameter, and for the flight parameter, includes (a) determining which display, among the VSD and the ND, is appropriate for the rendering of flight parameter information; (b) generating flight parameter information based on (a); and (c) overlaying the flight parameter information on the appropriate display.

    EXTENSIBLE FLIGHT MANAGEMENT SYSTEMS AND METHODS
    18.
    发明申请
    EXTENSIBLE FLIGHT MANAGEMENT SYSTEMS AND METHODS 审中-公开

    公开(公告)号：US20190012921A1

    公开(公告)日：2019-01-10

    申请号：US15644501

    申请日：2017-07-07

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Mark Pearson ,  Susan McCullough ,  Phillip Toews ,  Todd Wisner ,  Charles Dairman

    IPC: G08G5/00

    Abstract: Aircraft systems and related methods are provided for extensible flight management capabilities. One exemplary system includes a multifunction computing module including a user interface, a first processing system, and a first communications interface supporting a first data characteristic, and a flight management computing module. The flight management computing module includes at least one avionics interface to receive operational data from an avionics system onboard an aircraft and having a second data characteristic different from the first data characteristic, a second communications interface communicatively coupled to the first communications interface to the multifunction computing module, and a second processing system coupled to the avionics interface and the second communications interface to convert the operational data to input data having the first data characteristic and provide the input data to the multifunction computing module.

Patent Agency Ranking