A shock wave detection system includes a light beam emitter, a light beam receiver and an analysis unit. The light beam emitter emits a light beam oblique to a direction of an air flow through which a shock wave may propagate. The light beam receiver receives the light beam that has passed through the air flow. The analysis unit is configured to detect a presence and a position of the shock wave based on a change in a receiving position of the light beam by the light beam receiver.


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    Titel :

    SHOCK WAVE DETECTION SYSTEM, METHOD OF DETECTING SHOCK WAVE AND AIRCRAFT


    Beteiligte:
    SATO RYOSUKE (Autor:in) / TAKAYA RYOTA (Autor:in)

    Erscheinungsdatum :

    28.03.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G01H MEASUREMENT OF MECHANICAL VIBRATIONS OR ULTRASONIC, SONIC OR INFRASONIC WAVES , Messen von mechanischen Schwingungen oder Ultraschall-, Schall- oder Infraschallwellen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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    Ryhming, I.L. / Yoler, Y.A. / Aoki, Y. | Engineering Index Backfile | 1960


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    NAGASHIKI MAYUKO | Europäisches Patentamt | 2021

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    NAGASHIKI MAYUKO | Europäisches Patentamt | 2021

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    SHOCK WAVE NOISE OF SUPERSONIC AIRCRAFT

    RYHMENG, I. L. / AOKI, Y. / YOLER, Y. A. | SAE Technical Papers | 1960