The present invention provides third-generation aircraft, ship, train and automobile having angle-variable lift force adjusting wings. The present invention comprises: a fuselage; angle-variable lift force adjusting compound wings which are disposed on both lateral parts of the upper part of the fuselage and of which the angle is adjusted about a wing drive shaft portion so as to provide the fuselage with a lift force or a reversed lift force opposite from the lift force; and a driving unit which is for driving the angle-variable lift force adjusting compound wings so as to adjust same about the wing drive shaft portion in an angle for providing a lift force or an angle for providing a reversed lift force. The present invention enables the adjustment and control of the anti-centrifugal force by means of erecting the wings vertically, and thus enables safe operation even in case of sudden weather changes or unexpected situations and enables stable takeoff and landing in a short taxiing distance.

    La présente invention concerne un aéronef, un navire, un train et une automobile de troisième génération ayant des ailes de réglage de force de levage à angle variable. La présente invention comprend : un fuselage; des ailes composées de réglage de force de levage à angle variable qui sont disposées sur les deux parties latérales de la partie supérieure du fuselage et dont l'angle est réglé autour d'une partie d'arbre d'entraînement d'aile de façon à donner au fuselage une force de levage ou une force de levage inversée opposée à la force de levage; et une unité d'entraînement qui est destinée à entraîner les ailes composées de réglage de force de levage à angle variable de façon à régler celle-ci autour de la partie d'arbre d'entraînement d'aile selon un angle pour fournir une force de levage ou un angle pour fournir une force de levage inversée. La présente invention permet le réglage et la commande de la force anti-centrifuge au moyen du dressage vertical des ailes, et permet ainsi un fonctionnement sûr même en cas de changements climatiques soudains ou de situations inattendues et permet un décollage et un atterrissage stables dans une courte distance de roulement au sol.

    본 발명은 변각형 양력 조절방식의 날개를 장착한 제3세대 항공기와 선박 및 열차 그리고 자동차를 개시한 것으로, 이러한 본 발명은 동체; 상기 동체의 양측부 또는 상부에 배치되며, 상기 동체에 양력 또는 상기 양력과 반대되는 반양력을 제공하도록 날개구동축부를 중심으로 각도가 조절되는 변각형 양력조절방식 융합날개; 및, 상기 변각형 양력조절방식 융합날개를 상기 날개구동축부를 중심으로 양력 을 제공하는 각도 또는 반양력을 제공하는 각도로 조절하도록 구동하는 구동부; 를 포함하여 구성하는 것이다. 이같은 본 발명은 날개를 수직으로 세워 항원심력을 조절 제어하는 것이 또한 가능한 것이므로 갑작스런 일기 변화와 예기치 못한 상황 속에서도 안전운행이 가능하며, 더욱이 짧은 활주거리 만으로도 안정된 이착륙을 가능하게 하는 것이다.


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    Title :

    THIRD-GENERATION AIRCRAFT, SHIP, TRAIN AND AUTOMOBILE HAVING ANGLE-VARIABLE LIFT FORCE ADJUSTING WINGS


    Additional title:

    AÉRONEF, NAVIRE, TRAIN ET AUTOMOBILE DE TROISIÈME GÉNÉRATION AYANT DES AILES DE RÉGLAGE DE FORCE DE LEVAGE À ANGLE VARIABLE
    변각형 양력 조절방식의 날개를 장착한 제 3세대 항공기와 선박 및 열차 그리고 자동차


    Contributors:

    Publication date :

    2019-11-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B61D Einzelheiten oder Arten des Wagenaufbaus von Eisenbahnfahrzeugen , BODY DETAILS OR KINDS OF RAILWAY VEHICLES / B64C AEROPLANES , Flugzeuge / B63B Schiffe oder sonstige Wasserfahrzeuge , SHIPS OR OTHER WATERBORNE VESSELS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B62D MOTOR VEHICLES , Motorfahrzeuge



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    Duncanson, F. | Engineering Index Backfile | 1931




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