An altitude control system for an unmanned aerial vehicle includes a compressor assembly defining a plenum therein, a passive valve assembly coupled to a first portion of the compressor assembly and in fluid communication with the plenum, and an active valve assembly coupled to a second portion of the compressor assembly and in fluid communication with the plenum. A method of controlling an altitude of an unmanned aerial vehicle and an unmanned aerial vehicle are also provided.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Centrifugal compressor based altitude control device with active valve system


    Beteiligte:
    ANDERSON KEVIN (Autor:in) / GARTNER KEEGAN (Autor:in)

    Erscheinungsdatum :

    08.10.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64B LIGHTER-THAN-AIR AIRCRAFT , Luftfahrzeuge leichter als Luft / F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS



    CENTRIFUGAL COMPRESSOR BASED ALTITUDE CONTROL DEVICE WITH ACTIVE VALVE SYSTEM

    ANDERSON KEVIN / GARTNER KEEGAN | Europäisches Patentamt | 2020

    Freier Zugriff

    CENTRIFUGAL COMPRESSOR BASED ALTITUDE CONTROL DEVICE WITH ACTIVE VALVE SYSTEM

    ANDERSON KEVIN / GARTNER KEEGAN | Europäisches Patentamt | 2024

    Freier Zugriff

    Centrifugal compressor based altitude control device with active valve system

    ANDERSON KEVIN / GARTNER KEEGAN | Europäisches Patentamt | 2022

    Freier Zugriff


    Analysis of Performance of Small Centrifugal Compressor Measured at Altitude Test Facility

    Berlowitz, E. / Khosid, S. / Levy, Y. et al. | British Library Conference Proceedings | 2011