A pair of spaced slots, disposed on each side of an aircraft centerline and spaced well inboard of the wing leading edges, are provided in the wing upper surfaces and directed tangentially spanwise toward thin sharp leading wing edges of a highly swept, delta wing aircraft. The slots are individually connected through separate plenum chambers to separate compressed air tanks and serve, collectively, as a system for providing aircraft lift augmentation. A compressed air supply is tapped from the aircraft turbojet power plant. Suitable valves, under the control of the aircraft pilot, serve to selective provide jet blowing from the individual slots to provide spanwise sheets of jet air closely adjacent to the upper surfaces and across the aircraft wing span to thereby create artificial vortices whose suction generate additional lift on the aircraft. When desired, or found necessary, unequal or one-side wing blowing is employed to generate rolling moments for augmented lateral control. Trailing flaps are provided that may be deflected differentially, individually, or in unison, as needed for assistance in take-off or landing of the aircraft.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Lift augmentation for highly swept wing aircraft


    Beteiligte:

    Erscheinungsdatum :

    26.10.1993


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    FORWARD SWEPT WING VTOL AIRCRAFT WITH EMBEDDED LIFT PROPULSORS

    WINSTON NEIL CLARK / WINSTON ROBERT ALLEN / FULLER CLARK WILLIAM et al. | Europäisches Patentamt | 2025

    Freier Zugriff

    Vortex lift augmentation by suction on a 60 deg swept Gothic wing

    TAYLOR, A. / JACKSON, L. / HUFFMAN, J. | AIAA | 1982


    Active lift-augmentation tandem wing type ground effect aircraft

    LIU XIANGQIANG / YUAN JIA | Europäisches Patentamt | 2025

    Freier Zugriff


    Maximum lift for landing of swept wing aeroplanes

    Palme, H.O. | Engineering Index Backfile | 1953