A mission configurable aircraft operable to transition between thrust-borne lift in a VTOL orientation and wing-borne lift in a biplane orientation. The aircraft includes an airframe having first and second wings with first and second pylons extending therebetween. A two-dimensional distributed thrust array is attached to the airframe. The thrust array including a plurality of inboard propulsion assemblies coupled to first and second inboard nacelle stations of the first and second wings. The thrust array also includes a plurality of outboard propulsion assemblies coupled to first and second outboard nacelle stations of the first and second wings. A flight control system is operable to independently control each of the propulsion assemblies. A payload is coupled to the airframe. The inboard propulsion assemblies have a thrust type that is different from the thrust type of the outboard propulsion assemblies.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Mission Configurable Aircraft having VTOL and Biplane Orientations


    Beteiligte:

    Erscheinungsdatum :

    31.01.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Mission configurable aircraft having VTOL and biplane orientations

    MCCULLOUGH JOHN RICHARD / OLDROYD PAUL K | Europäisches Patentamt | 2020

    Freier Zugriff

    M-wing aircraft having VTOL and biplane orientations

    MCCULLOUGH JOHN RICHARD / OLDROYD PAUL K | Europäisches Patentamt | 2022

    Freier Zugriff

    M-Wing Aircraft having VTOL and Biplane Orientations

    MCCULLOUGH JOHN RICHARD / OLDROYD PAUL K | Europäisches Patentamt | 2019

    Freier Zugriff

    RE-CONFIGURABLE VTOL AIRCRAFT

    GIBBONEY JEFF / SINHA PRANAY / FORRETTE CHRISTOPHER | Europäisches Patentamt | 2025

    Freier Zugriff

    BIPLANE TILTROTOR AIRCRAFT

    GRONINGA KIRK L / STAMPS FRANK B / ROBERTSON DANIEL B et al. | Europäisches Patentamt | 2020

    Freier Zugriff