A rear end section for an aircraft, having a fuselage, a v-tail, and a thruster assembly including at least one propulsion device installed to ingest and consume air forming a fuselage boundary layer, a control surface attached at the rearmost section of the rear end, and a casing covering at least part of the propulsion device such that an air inlet and an air outlet are defined between the casing and the propulsion device. The air inlet is configured to permit passage of the fuselage boundary layer towards the propulsion device. The air outlet is configured to direct the airflow exhausted from the propulsion device into the control surface, to divert the airflow and provide vectoring thrust for the aircraft.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    REAR END SECTION FOR AN AIRCRAFT


    Beteiligte:

    Erscheinungsdatum :

    04.11.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Frame assembly for rear section of aircraft and rear section of aircraft

    CRUZ-DOMINGUEZ FRANCISCO JOSE / COLMENAREJO MATELLANO NURIA / VAZQUEZ CASTRO JESUS JAVIER et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    METHOD FOR MANUFACTURING A REAR SECTION OF AN AIRCRAFT AND AIRCRAFT REAR SECTION

    MARTINO-GONZALEZ ESTEBAN / ARANA HIDALGO ALBERTO / SANCHEZ PEREZ MELANIA et al. | Europäisches Patentamt | 2019

    Freier Zugriff

    Method for manufacturing a rear section of an aircraft and aircraft rear section

    MARTINO-GONZALEZ ESTEBAN / ARANA HIDALGO ALBERTO / SANCHEZ PEREZ MELANIA et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    REAR FUSELAGE SECTION OF AN AIRCRAFT

    GONZALEZ GOZALBO ALFONSO / LLAMAS SANDIN RAUL CARLOS | Europäisches Patentamt | 2021

    Freier Zugriff

    Rear fuselage section of an aircraft

    GONZALEZ GOZALBO ALFONSO / LLAMAS SANDIN RAUL CARLOS | Europäisches Patentamt | 2016

    Freier Zugriff