An aircraft is provided and includes a fuselage including a top and a tail, a main rotor apparatus disposed at the top of the fuselage, which rotates one or more rotors to generate lift, and an active flow control (AFC) system. The AFC system includes plasma actuators configured to generate plasma at a location adjacent to the main rotor apparatus and/or at the tail of the fuselage.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ACTIVE FLOW CONTROL SYSTEM


    Beteiligte:
    WAKE BRIAN E (Autor:in) / MATALANIS CLAUDE G (Autor:in) / BOWLES PATRICK (Autor:in)

    Erscheinungsdatum :

    2018-10-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    ACTIVE FLOW CONTROL SYSTEM

    WAKE BRIAN E / MATALANIS CLAUDE G / BOWLES PATRICK | Europäisches Patentamt | 2016

    Freier Zugriff

    ACTIVE FLOW CONTROL SYSTEM

    WAKE BRIAN E / MATALANIS CLAUDE G / BOWLES PATRICK | Europäisches Patentamt | 2018

    Freier Zugriff

    Active flow control system

    WAKE BRIAN E / MATALANIS CLAUDE G / BOWLES PATRICK | Europäisches Patentamt | 2020

    Freier Zugriff

    Autonomous active flow control system

    STALEWSKI WIENCZYSLAW / KRZYSIAK ANDRZEJ / SCHÜLLER MARTIN | Europäisches Patentamt | 2015

    Freier Zugriff

    Active Flow Control Maneuvering System

    Dolgopyat, D. / Seifert, A. / Tekhniyon, Makhon tekhnologi le-Yisra'el | British Library Conference Proceedings | 2014