A system for monitoring pressure change within at least one compartment of an aircraft is provided. The system in-cludes a primary pressure sensor for providing a signal corresponding to a pressure within a primary compartment of the aircraft, a primary monitoring channel coupled to the primary pressure sensor, and an output driver coupled to the primary monitoring chan-nel. The primary monitoring channel includes a band pass filter for receiving and filtering the primary pressure signal, a pressure change circuit for determining a change in the filtered pressure signal and for providing a pressure change output signal corre-sponding to the change in pressure, and a threshold logic circuit for determining whether the pressure change output signal meets a predetermined threshold and for providing a threshold output signal indicating that a decompression event has occurred if the pressure change output signal meets the predetermined threshold. The output driver receives the primary threshold output signal and outputs a notification signal.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    RAPID DECOMPRESSION DETECTION SYSTEM AND METHOD


    Weitere Titelangaben:

    SYSTEME ET PROCEDE DE DETECTION D'UNE DECOMPRESSION RAPIDE


    Beteiligte:

    Erscheinungsdatum :

    24.05.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Rapid decompression detection system and method

    LEHMANN MICHAEL | Europäisches Patentamt | 2015

    Freier Zugriff

    DECOMPRESSION DETECTION DEVICE, DECOMPRESSION DETECTION METHOD AND DECOMPRESSION DETECTION PROGRAM FOR TIRE

    MORITA NAOKI / MASUDA HIDENAO / MURAKAMI KEIICHI | Europäisches Patentamt | 2024

    Freier Zugriff


    Electrophysiology of chimpanzees during rapid decompression.

    Hartman, J. L. / Koestler, G. / Lewis, O. F. et al. | NTRS | 1967