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    SYSTEMS AND METHODS FOR DISPLAYING A LANDING RUNWAY EXTENSION ON AN AIRCRAFT
    2.
    发明公开
    SYSTEMS AND METHODS FOR DISPLAYING A LANDING RUNWAY EXTENSION ON AN AIRCRAFT 审中-公开

    公开(公告)号：EP4495914A1

    公开(公告)日：2025-01-22

    申请号：EP24188813.0

    申请日：2024-07-16

    Applicant: Honeywell International Inc.

    Inventor： MIYAZAKI, Yasutaka

    IPC: G08G5/00 ,  B64D43/00 ,  B64D45/08 ,  G01C23/00 ,  G08G5/02

    Abstract: Systems and methods are provided for displaying a landing runway extension on an aircraft. A destination airport of the aircraft is identified based on a flight path of the aircraft received from a flight management system (FMS) of the aircraft. A location of the aircraft is determined based on location data received from at least one geospatial sensor of the aircraft. A landing runway at the destination airport is identified. A display is generated for display on an onboard display device system of the aircraft when the location of the aircraft is within a pre-defined distance from the destination airport. The display includes the landing runway and the landing runway extension associated with a desired final approach flight path to the landing runway.

    AIRCRAFT MODULAR DATA COLLECTION PLATFORM
    4.
    发明公开
    AIRCRAFT MODULAR DATA COLLECTION PLATFORM 审中-公开

    公开(公告)号：EP4474291A1

    公开(公告)日：2024-12-11

    申请号：EP24178056.8

    申请日：2024-05-24

    Applicant: The Boeing Company

    Inventor： HILLER, Nathan D. ,  FRITZ-THOMPSON, Claudia E.

    IPC: B64D43/00

    Abstract: An aircraft data collection system comprising a set of removable data collection units and a computer system. The set of removable data collection units is loadable into a compartment in a commercial aircraft. The computer system is configured to control operation of the set of removable data collection units to collect data during a flight of the commercial aircraft on a flight path. A third party can use a smart phone or other electronic device to control the data collection unit during a commercial aircraft flight. The third party is different from the airline operating the commercial aircraft.

    EXOSKELETTARM-HILFE IM LUFTFAHRZEUGCOCKPIT FÜR HOHE BESCHLEUNIGUNGEN
    7.
    发明公开
    EXOSKELETTARM-HILFE IM LUFTFAHRZEUGCOCKPIT FÜR HOHE BESCHLEUNIGUNGEN 审中-实审

    公开(公告)号：EP4410671A1

    公开(公告)日：2024-08-07

    申请号：EP24154200.0

    申请日：2024-01-26

    Applicant: Deutsches Zentrum für Luft- und Raumfahrt e.V.

    Inventor： Wolz, Florian

    IPC: B64D10/00 ,  B64D43/00 ,  B64D47/00

    CPC classification number: B64D43/00 ,  B64D47/00 ,  B64D10/00 ,  B25J9/0006

    Abstract: Die Erfindung betrifft ein System zum Unterstützen eines Insassen eines Luftfahrzeugs (1) bei der Cockpit-Bedienung unter hohen Beschleunigungen, aufweisend eine Recheneinheit (3), eine inertiale Messeinheit (5), und einen Exoskelettarm (7) mit einer Vielzahl von Gelenken und Aktoren und Lagerflächen für das Abstützen eines Arms des Insassen, wobei die inertiale Messeinheit (5) dazu ausgeführt ist, kinematische Daten des Luftfahrzeugs (1) zu erfassen und an die Recheneinheit (3) zu übermitteln, wobei die Recheneinheit (3) dazu ausgeführt ist, aus den erfassten kinematischen Daten der inertialen Messeinheit (5) eine Beschleunigung am Insassensitz zu ermitteln und die Aktoren des Exoskelettarms (7) zum Erzeugen einer der ermittelten Beschleunigung am Insassensitz entgegengerichteten Gegenkraft in einer Höhe anzusteuern, die die Trägheitskräfte des Arms des Insassen aufgrund der ermittelten Beschleunigung am Insassensitz kompensiert.

    SYSTEM AND METHOD FOR CONTROL OF CABIN WITH INTERNET OF THINGS (IOT) CONCEPT
    9.
    发明公开
    SYSTEM AND METHOD FOR CONTROL OF CABIN WITH INTERNET OF THINGS (IOT) CONCEPT 审中-公开

    公开(公告)号：EP4375187A1

    公开(公告)日：2024-05-29

    申请号：EP23210409.1

    申请日：2023-11-16

    Applicant: Rockwell Collins, Inc.

    Inventor： RAJU, Gopal Rudra ,  NATARAJAN, Rathan ,  DHANUJA, H M ,  LAKSHMIKANTH, GR

    IPC: B64D11/00 ,  B64D43/00

    CPC classification number: B64D11/0015 ,  B64D43/00

    Abstract: A cabin management control device is disclosed for automating cabin features (e.g., shades, lights) and/or a GUI based on flight data. The cabin management control device may include a computing device having a touchscreen. The computing device may be in communication with an aircraft network and cabin controller. The computing device may be configured to display a graphical user interface (GUI) configured to control cabin features. The computing device may be configured to: receive flight data; receive camera feed data; determine whether to display the camera feed data based on the flight data; and direct, based on the flight data, an automatic adjustment of the cabin features. The cabin features may include at least one of: a window level of one or more window shades; or a cabin lighting level of one or more lights.

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