SYSTEM AND METHOD TO AUTO CREATE AIRCRAFT MAINTENANCE RECORDS BY AIRCRAFT DATA

    公开(公告)号:US20190295331A1

    公开(公告)日:2019-09-26

    申请号:US15928650

    申请日:2018-03-22

    Abstract: A processor-implemented method for automatically creating aircraft maintenance records and work logs during aircraft maintenance operations is disclosed. The method comprises retrieving, using a processor, fault data, testing data, maintenance data, and status data regarding line replaceable units (LRUs) on an aircraft via a central maintenance computer (CMC) on the aircraft; automatically collecting from a remote terminal on the aircraft data regarding maintenance operations performed using the remote terminal; automatically recording, by the processor, in a maintenance database the fault data, testing data, maintenance data, status data, and data regarding maintenance operations performed using the remote terminal; and automatically populating, by the processor using data in the maintenance database, information in a plurality of fields in a maintenance work log.

    Systems and methods for enhancing datalink operation

    公开(公告)号:US12051334B2

    公开(公告)日:2024-07-30

    申请号:US17655915

    申请日:2022-03-22

    CPC classification number: G08G5/0021 G08G5/0013

    Abstract: A flight deck system and method in an aircraft for enhancing controller pilot datalink communication (CPDLC) operation is disclosed. The flight deck system includes a controller configured to: receive a CPDLC message having a CPDLC message type from a flight operation center (FOC) having an FOC name; retrieve an expected response time for the CPDLC message from an expected response time database containing expected response times for a plurality of CPDLC message types for FOCs; generate a timer function that causes the display of a timer (e.g., countdown timer) on an aircraft display device that has a set duration based on the expected response time; signal the aircraft display device to display the timer; monitor communications from flight crew for a response to the CPDLC message; and signal the aircraft display device to end the display of the timer when a communication has been detected within the set duration.

    SYSTEM AND METHOD FOR AUTOMATIC GENERATION OF A DIAGNOSTIC MODEL

    公开(公告)号:US20190324837A1

    公开(公告)日:2019-10-24

    申请号:US15955933

    申请日:2018-04-18

    Abstract: A cloud-based computing system for providing a maintenance message associated with a unique maintenance action for fault rectification is disclosed. The system includes a diagnostic module including one or more processors configured by instructions stored in non-transient computer readable media. The diagnostic module is configured to: identify, for each potential CAS message in an aircraft, a set of inputs that are evaluated to trigger the potential CAS message; identify, for each of the potential CAS messages, each unique combination of input conditions for the set of inputs that triggers the potential CAS message; and identify, for each of the potential CAS messages, a unique maintenance message associated with each unique combination of input conditions that triggers the potential CAS message, wherein each unique maintenance message is associated with a unique maintenance action for fault rectification.

    SYSTEM AND METHOD FOR GRAPHICALLY DISPLAYING WEATHER HAZARDS IN A PERSPECTIVE VIEW
    5.
    发明申请
    SYSTEM AND METHOD FOR GRAPHICALLY DISPLAYING WEATHER HAZARDS IN A PERSPECTIVE VIEW 审中-公开
    在视野中图形显示天气危害的系统和方法

    公开(公告)号:US20140331161A1

    公开(公告)日:2014-11-06

    申请号:US13886347

    申请日:2013-05-03

    CPC classification number: G06F3/0484 G01C23/00 G01W1/02 G01W2203/00

    Abstract: A system and method are provided for graphically displaying a weather hazard. The system is comprised of a display system coupled to a processor that is configured to retrieve weather information from a database and determine the severity of weather hazard present within a predetermined distance. The severity of the weather hazard is based on the phase of flight and type of weather hazards present within the weather envelope. The weather symbology that graphically represents the severe weather hazard within a weather envelope is rendered on the display.

    Abstract translation: 提供了用于图形显示天气危害的系统和方法。 该系统包括耦合到处理器的显示系统,其被配置为从数据库检索天气信息并确定在预定距离内存在的天气危害的严重性。 天气危害的严重性是基于航空的阶段和天气信息中存在的天气危害的类型。 以图形方式表示天气信息中恶劣天气危害的气象符号系统显示在显示屏上。

    System and method to auto create aircraft maintenance records by aircraft data

    公开(公告)号:US11030828B2

    公开(公告)日:2021-06-08

    申请号:US15928650

    申请日:2018-03-22

    Abstract: A processor-implemented method for automatically creating aircraft maintenance records and work logs during aircraft maintenance operations is disclosed. The method comprises retrieving, using a processor, fault data, testing data, maintenance data, and status data regarding line replaceable units (LRUs) on an aircraft via a central maintenance computer (CMC) on the aircraft; automatically collecting from a remote terminal on the aircraft data regarding maintenance operations performed using the remote terminal; automatically recording, by the processor, in a maintenance database the fault data, testing data, maintenance data, status data, and data regarding maintenance operations performed using the remote terminal; and automatically populating, by the processor using data in the maintenance database, information in a plurality of fields in a maintenance work log.

    SYSTEM AND METHOD TO DISPLAY DIFFERENTIAL GROUND SPEED ON A COCKPIT DISPLAY

    公开(公告)号:US20240282200A1

    公开(公告)日:2024-08-22

    申请号:US18295083

    申请日:2023-04-03

    CPC classification number: G08G5/0021 B64D43/02 G08G5/0047

    Abstract: Systems and methods are provided for displaying differential ground speed for traffic surrounding an aircraft. The system includes an aircraft control panel in a cockpit of an ownship aircraft and a digital traffic display located on the control panel. The digital traffic display provides cockpit display of traffic information (CDTI) that shows a speed scale with a graphical display of the ground speed of the ownship aircraft and the ground speed of traffic to follow (TTF). The separation scale also shows a graphical display of a separation distance between the ownship aircraft and the TTF. A change in separation distance is calculated based of the difference in ground speed between the ownship aircraft and the TTF. An advisory/warning indicator that shows a color-coded status of the change in separation distance in comparison a pre-determined desired separation distance between the ownship aircraft and the TTF.

Patent Agency Ranking