An aircraft and method of operating an aircraft. The aircraft includes a temperature sensor and a processor. The temperature sensor that obtains an optical signal indicative of a temperature at a selected location of an outer surface of the aircraft. The processor is configured to determine the temperature at the selected location from the optical signal, and operate the aircraft based on the temperature at the selected location.


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    Titel :

    Active infrared prediction utilizing fiber optic network


    Beteiligte:

    Erscheinungsdatum :

    2022-11-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G01D MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE , Anzeigen oder Aufzeichnen in Verbindung mit Messen allgemein / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G01K MEASURING TEMPERATURE , Messen der Temperatur



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    KAYE JORDAN ALEX / WEINTRAUB ALEXANDER QUINN / PARKHURST JEFFREY K | Europäisches Patentamt | 2021

    Freier Zugriff

    Active In-Flight Load Redistribution Utilizing Fiber-Optic Shape Sensing and Multiple Control Surfaces

    Pena, Francisco / Martins, Benjamin L. / Richards, W. Lance | NTRS | 2018


    Fiber-optic-based infrared scene projector

    Dalbey, Robert Z. | SPIE | 1996


    Infrared imaging with fiber optic bundles

    Hilton, Albert R. / McCord, James / Thompson, W. S. et al. | SPIE | 2003


    Aquatic vessel fiber optic network

    JENG JACK ING | Europäisches Patentamt | 2016

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