Techniques for using a sound spectrum to generate models, which identify unmanned aerial vehicle (UAV) configurations, are described herein. The models may be based on components associated with a UAV, and instructions for manufacture of a UAV may be provided. For example, a sound spectrum may be obtained by a computer system which is used to generate one or more models. The one or more models are based in part on components of a UAV and identify UAV configurations that will generate an expected sound within the identified sound spectrum. The UAV configurations identified by the models are used to instruct manufacture of a UAV.


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    Titel :

    Static inverse desymmetrized propellers


    Beteiligte:
    BECKMAN BRIAN C (Autor:in) / KIMCHI GUR (Autor:in)

    Erscheinungsdatum :

    16.07.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL



    Static Testing of Micro Propellers

    Deters, Robert / Selig, Michael | AIAA | 2008


    Static thrust of airplane propellers

    Diehl, Walter S | NTRS | 1934


    Static thrust of airplane propellers

    Diehl, W.S. | Engineering Index Backfile | 1932


    Static Testing of Micro Propellers

    Deters, R. / Selig, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2008


    Static thrust of airplane propellers

    Diehl, Walter S. | TIBKAT | 1932