A landing arrangement for reducing a distance error of a landing aircraft having a high lift-to-drag ratio is disclosed. The landing arrangement comprises a longitudinal landing device (200, 230) having a surface adapted to allow gliding or rolling of the aircraft thereon, and a sloping device (240, 250) configured to set an angle of the longitudinal landing device (200, 230) with respect to a horizontal plane.


    Access

    Download


    Export, share and cite



    Title :

    LANDING ARRANGEMENT FOR REDUCING A DISTANCE ERROR OF A LANDING AIRCRAFT HAVING A HIGH LIFT-TO-DRAG RATIO


    Additional title:

    LANDUNGSANORDNUNG ZUR REDUZIERUNG EINES DISTANZFEHLERS EINES LANDENDEN FLUGZEUGS MIT HOHER GLEITZAHL
    AGENCEMENT DE PALIER POUR RÉDUIRE UNE ERREUR DE DISTANCE D'UN AÉRONEF ATTERRISSANT AYANT UN RAPPORT SUSTENTATION-SUR-TRAÎNÉE ÉLEVÉ


    Contributors:

    Publication date :

    2017-03-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    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




    MINIMUM LIFT-DRAG RATIO REQUIRED FOR GLOBAL LANDING COVERAGE

    GRAY, W. A. / WALLACE, R. A. | AIAA | 1963



    Landing gear assembly for reducing drag on an aircraft

    SKROSKI TYLER | European Patent Office | 2022

    Free access

    Aircraft landing gear arrangement

    WILSON FRASER | European Patent Office | 2015

    Free access