An airflow modifying device (206, fig.2) for use in an engine duct (204) comprising: a flow inlet; a flow outlet; and a flow passage extending from the flow inlet to the flow outlet; wherein the device is arranged to receive an incident air flow; and wherein the device is configured to at least partially modulate the air flow in the flow passage to improve flow ordering of the incident airflow, the airflow modifying device further comprising: at least one pitot sensor 502 integral with the device located at the flow inlet; and a pressure line 534 comprising a first end and a second end, the first end connected to the pitot sensor and the second end configured to be connected to a transducer 536; wherein the pressure line is completely enclosed within the device.


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    Titel :

    Airflow modifying device


    Beteiligte:

    Erscheinungsdatum :

    06.11.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G01P MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION OR SHOCK , Messen der Linear- oder Winkelgeschwindigkeit, der Beschleunigung, der Verzögerung oder des Stoßes / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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