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    SYSTEM AND METHOD FOR SMART ELECTRIC FLIGHT DISPATCH
    1.
    发明公开
    SYSTEM AND METHOD FOR SMART ELECTRIC FLIGHT DISPATCH 审中-公开

    公开(公告)号：US20240265816A1

    公开(公告)日：2024-08-08

    申请号：US18241620

    申请日：2023-09-01

    申请人： ARINC Incorporated

    发明人： Avinash Arun Kumar ,  Anmol Kumar ,  Sreepriya Payyalore Thekkanath

    IPC分类号： G08G5/00 ,  G06N20/00

    CPC分类号： G08G5/0065 ,  G06N20/00 ,  G08G5/0026

    摘要： A method for e-AC flight dispatch is disclosed, in accordance with one or more embodiments of the present disclosure. The method may include receiving a set of training data. The method may include training a machine learning algorithm of an electric flight dispatch module based on the received set of training data. The method may include receiving one or more sets of real-time data, the one or more sets of real-time data including at least one of airport infrastructure data, airline information data, or battery management data. The method may include generating a set of output data for dispatching an electric aircraft using the trained machine learning algorithm of the electric flight dispatch module.

    Device and method for determining a safe aircraft runway distance
    5.
    发明授权
    Device and method for determining a safe aircraft runway distance 有权

    公开(公告)号：US11842650B2

    公开(公告)日：2023-12-12

    申请号：US17537531

    申请日：2021-11-30

    申请人： Kaunas University of Technology

    发明人： Darijus Pagodinas ,  Vytautas Dumbrava

    IPC分类号： G08G5/00 ,  G08G5/06

    CPC分类号： G08G5/0065 ,  G08G5/0021 ,  G08G5/065 ,  G08G5/0091

    摘要： The following teachings are of a portable autonomous device and method operating independently of aircraft flight control equipment. The device can be easily moved from one aircraft to another. The device measures the acceleration of the aircraft from the instantaneous speed and the runway distance covered from the start of the acceleration. Once the runway length and take-off speed is input, the device calculates the remaining distance to safely reach the take-off speed. If the remaining runway distance is not enough for the safe take-off, the device provides visual or audible information about the situation and signals to the pilot. In other embodiments, the determination and presentation of the remaining runway length may be implemented in the aircraft flight control equipment.

    Lightning threat information-providing apparatus, lightning threat information-providing method, and program
    6.
    发明授权
    Lightning threat information-providing apparatus, lightning threat information-providing method, and program 有权

    公开(公告)号：US11822049B2

    公开(公告)日：2023-11-21

    申请号：US16642323

    申请日：2018-08-09

    申请人： JAPAN AEROSPACE EXPLORATION AGENCY

    发明人： Eiichi Yoshikawa ,  Tomoo Ushio

    IPC分类号： G01W1/16 ,  G06N20/00 ,  G01W1/10 ,  G08G5/00

    CPC分类号： G01W1/16 ,  G01W1/10 ,  G06N20/00 ,  G08G5/0021 ,  G08G5/0065 ,  G08G5/0091

    摘要： [Object] To provide a lightning threat information-providing apparatus, a lightning threat information-providing method, and a program that are capable of providing a user with accurate information regarding a lightning threat.
    [Solving Means] A lightning threat information-providing apparatus 1 includes: an input unit 10 that inputs observation parameters 11 regarding weather observation data, prediction parameters 12 regarding weather prediction data, and case data 13 regarding a case that occurs in association with lightning occurrence; an intermediate parameter calculation unit that calculates, on the basis of the input observation parameters 11 and prediction parameters 12, an intermediate parameter 27 which is a parameter regarding physical quantity associated with the lightning occurrence and cannot be directly obtained from the observation data or the prediction data; and an arithmetic control unit 20 that estimates a lightning threat on the basis of the observation parameters 11, the prediction parameters 12, the case data 13, and the intermediate parameter 27.

    Systems and methods for generating displays for noise abatement departure procedures
    8.
    发明授权
    Systems and methods for generating displays for noise abatement departure procedures 有权

    公开(公告)号：US11733712B2

    公开(公告)日：2023-08-22

    申请号：US16999525

    申请日：2020-08-21

    申请人： HONEYWELL INTERNATIONAL INC.

    发明人： Saravanakumar Gurusamy ,  Kantha Chikkegowda ,  Ivan Wyatt

    IPC分类号： G05D1/06 ,  G08G5/00 ,  G01C23/00 ,  G05D1/10 ,  B64D31/06

    CPC分类号： G05D1/0661 ,  B64D31/06 ,  G01C23/00 ,  G05D1/106 ,  G08G5/0065

    摘要： Methods and systems for generating a vertical situation display for a noise abatement departure procedure (NADP). Other NADP relevant displays are also disclosed including display of NADP parameters on altitude tape and primary flight displays, an NADP bug on an engine display and NADP status annunciations. The methods and systems include receiving NADP parameters entered into a flight management system (FMS) on a user interface of the aircraft system. The NADP parameters include: an initial altitude at which take-off thrust should be reduced to NADP thrust, an acceleration altitude at which the aircraft should begin accelerating to a final take-off speed whilst maintaining the NADP thrust, a climb excitement altitude at which a speed target is changed to the final take-off speed whilst maintaining the NADP thrust, and an end altitude at which the NADP should be exited. The methods and systems include generating a vertical situation display for a display device of the aircraft system indicating the NADP parameters on a flight path indication.