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    AUGMENTED REALITY SYSTEM FOR ASSESSING AN AFFECTED AREA OF AN AIRCRAFT
    3.
    发明申请
    AUGMENTED REALITY SYSTEM FOR ASSESSING AN AFFECTED AREA OF AN AIRCRAFT 审中-公开

    公开(公告)号：US20170210492A1

    公开(公告)日：2017-07-27

    申请号：US15479642

    申请日：2017-04-05

    Applicant: The Boeing Company

    Inventor： Samantha A. Schwartz ,  Andre Lutz ,  Rex Byron Douglas ,  Nicolas Boecher

    IPC: B64F5/60 ,  G07C5/00 ,  G07C5/08

    CPC classification number: B64F5/60 ,  G07C5/008 ,  G07C5/0808 ,  G07C5/0825 ,  G07C2205/02

    Abstract: A portable electronic device for assessing an affected area of an aircraft is disclosed. A reference marker having a known size is located on the aircraft. The portable electronic device includes a processor in communication with a structural database, where the structural database includes a template that defines a maximum allowable size of damage to the aircraft. The processor executes instructions for determining an actual size of the affected area based on the known size of the reference marker. The processor also executes instructions for comparing the actual size of the affected area with the maximum allowable size of damage to the aircraft. The processor further executes instructions for determining that the actual size of the affected area exceeds the maximum allowable size of damage to the aircraft.

    DE-ICING COMMUNICATION SYSTEMS AND METHODS FOR AN AIRCRAFT
    4.
    发明申请
    DE-ICING COMMUNICATION SYSTEMS AND METHODS FOR AN AIRCRAFT 有权

    公开(公告)号：US20250066025A1

    公开(公告)日：2025-02-27

    申请号：US18455746

    申请日：2023-08-25

    Applicant: The Boeing Company

    Inventor： Samantha A. Schwartz

    IPC: B64D15/20

    Abstract: A system and a method include a first communication system onboard an aircraft and a control unit having one or more processors that determine that one or more ambient conditions require a de-icing event of the aircraft, determine a location of the aircraft, and a status of one or more systems of the aircraft. The first communication system establishes a bi-directional communication link with a second communication system of a de-icing system. The first communication system receives one or more command messages from the second communication system indicating a status of the de-icing event. The control unit changes one or more operating settings of the aircraft responsive to completion of the de-icing event

    RUNWAY EXITING SYSTEMS AND METHODS FOR AIRCRAFT
    6.
    发明申请
    RUNWAY EXITING SYSTEMS AND METHODS FOR AIRCRAFT 审中-公开

    公开(公告)号：US20180165975A1

    公开(公告)日：2018-06-14

    申请号：US15375230

    申请日：2016-12-12

    Applicant: THE BOEING COMPANY

    Inventor： Samantha A. Schwartz ,  Jason W. Clark ,  Jeffrey L. Williams ,  Katie M. Reid

    IPC: G08G5/06

    CPC classification number: G08G5/065 ,  G08G5/02 ,  G08G5/025

    Abstract: A runway exiting system is configured to determine a suitable exit off of a runway for an aircraft. The runway exiting system includes a housing, and one or more processors within the housing that are configured to determine a current position of the aircraft on the runway, determine a current rate of deceleration of the aircraft on the runway, and determine the suitable exit off of the runway for the aircraft based, at least in part, on the current position of the aircraft on the runway and the current rate of deceleration of the aircraft on the runway.

    Augmented reality system for assessing an affected area of an aircraft
    7.
    发明授权
    Augmented reality system for assessing an affected area of an aircraft 有权

    公开(公告)号：US09646431B2

    公开(公告)日：2017-05-09

    申请号：US14520642

    申请日：2014-10-22

    Applicant: The Boeing Company

    Inventor： Samantha A. Schwartz ,  Andre Lutz ,  Rex Bryon Douglas ,  Nicolas Boecher

    IPC: B64F5/60 ,  G07C5/08 ,  G07C5/00

    CPC classification number: B64F5/60 ,  G07C5/008 ,  G07C5/0808 ,  G07C5/0825 ,  G07C2205/02

    Abstract: A system for assessing an affected area of an aircraft is disclosed. A reference marker having a known size is placed along an exterior of the aircraft. The system includes a portable electronic device including a processor in communication with a structural database. The structural database includes a template that defines a maximum allowable size of damage to the aircraft. The processor executes an instruction for determining an actual size of the affected area based on the known size of the reference marker. The processor executes an instruction for comparing the actual size of the affected area of the aircraft with the maximum allowable size of damage to the aircraft. The processor executes an instruction for determining if the actual size of the affected area exceeds the maximum allowable size of damage to the aircraft. The processor executes an instruction for determining a further action.

    Terminal Area Alert System
    8.
    发明申请
    Terminal Area Alert System 审中-公开
    终端区警报系统

    公开(公告)号：US20160335899A1

    公开(公告)日：2016-11-17

    申请号：US14709890

    申请日：2015-05-12

    Applicant: The Boeing Company

    Inventor： Samantha A. Schwartz ,  Andreas Sindlinger

    IPC: G08G5/00 ,  G08G5/04

    CPC classification number: G08G5/0013 ,  G08G5/0026 ,  G08G5/0082 ,  G08G5/025

    Abstract: A method and system for handling a missed approach of an aircraft. A group of signals that indicates a go-around maneuver occurring during an approach of the aircraft to land at an airport is detected on a data bus in the aircraft. An alert to an air traffic control system for the airport when the signal is detected. The alert indicates an occurrence of the go-around maneuver, enabling rerouting of air traffic in a manner that enhances safety.

    Abstract translation: 一种用于处理飞机错过的方法和系统。 在飞机上的数据总线上检测到一组信号，指示飞机在机场降落期间发生的复飞机动。 当检测到信号时，向机场的空中交通管制系统发出警报。 该警报表示复飞机动的发生，使得能够以增强安全性的方式重新路由空中交通。

    Visual Fuel Predictor System
    9.
    发明申请
    Visual Fuel Predictor System 有权
    视觉燃料预测系统

    公开(公告)号：US20150344148A1

    公开(公告)日：2015-12-03

    申请号：US14291279

    申请日：2014-05-30

    Applicant: The Boeing Company

    Inventor： Samantha A. Schwartz ,  Andreas Godehart ,  Nils Kneuper ,  Andre Lutz ,  Mariusz Nawotczynski

    IPC: B64D45/00 ,  B64D37/00 ,  B64D43/00

    CPC classification number: B64D45/00 ,  B64D37/005 ,  B64D43/00 ,  B64D2045/0075 ,  G05D1/00

    Abstract: A method and apparatus for predicting fuel for an aircraft. Remaining amounts of fuel that will be present for types of fuel use for the aircraft at a destination are predicted. Flight times for the types of fuel use are calculated from the remaining amounts of fuel predicted for the types of fuel use for the aircraft at the destination. Graphical indicators are displayed indicating the types of fuel use and the flight times for the types of fuel use.

    Abstract translation: 一种用于预测飞机燃料的方法和装置。 预测将在目的地为飞机燃料使用的剩余燃料量。 燃料使用类型的飞行时间是根据目的地的飞机燃料类型预测的剩余燃料量计算的。 显示图形指示器，指示燃料使用的类型和燃料使用类型的飞行时间。

    SYSTEM AND METHOD FOR REDUCED-ENGINE TAXIING OPERATION
    10.
    发明公开
    SYSTEM AND METHOD FOR REDUCED-ENGINE TAXIING OPERATION 审中-公开

    公开(公告)号：US20240265818A1

    公开(公告)日：2024-08-08

    申请号：US18163677

    申请日：2023-02-02

    Applicant: The Boeing Company

    Inventor： Samantha A. Schwartz ,  Garoe Gonzalez

    IPC: G08G5/06 ,  B64D43/00 ,  G08G5/00

    CPC classification number: G08G5/065 ,  B64D43/00 ,  G08G5/0073

    Abstract: A system and method are provided for an aircraft at an airport surrounded by an environment, the aircraft having a first engine and a second engine wherein the second engine is to be started after the first engine. The system and method are configured for determining a minimum amount of warm-up time needed for starting the second engine to meet predetermined start-up requirements for the second engine, based on one or more of engine-related information relating to the second engine, aircraft-related information relating to the aircraft, airport-related information relating to the airport, and environment-related information relating to the environment, and producing an alert based on the minimum amount of warm-up time needed.

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