The present invention relates to a method for stabilizing flight during takeoff and landing of a rotary wing aircraft and for efficiently operating the rotary power of a rotor. The purpose of the present invention is to improve adverse effects such as bearing wear and vibration caused by the existing bevel gear connection method of an aircraft which concentrates all the power load on a single point of the gear connection as an eccentric load. In order to efficiently combine the rotating power of an aircraft, the power is divided by 50% at a position corresponding to 180 degrees of the gear connection, and efficiency can be expected to be increased through gear connection without loss by means of a gear device consisting of a bevel gear combination that adopts a bifurcated gear method, which is a technique for operating with force couple that can double the connection capacity.

    La présente invention concerne un procédé de stabilisation de vol pendant le décollage et l'atterrissage d'un aéronef à voilure tournante et d'exploitation efficace de la puissance rotative d'un rotor. L'objet de la présente invention est d'améliorer les effets indésirables tels que l'usure de roulement et les vibrations provoquées par le procédé de liaison d'engrenage conique existant d'un aéronef qui concentre la totalité de la charge de puissance sur un point unique de la liaison d'engrenage sous la forme d'une charge excentrique. Afin de combiner efficacement la puissance de rotation d'un aéronef, la puissance est divisée par 50 % à une position correspondant à 180 degrés de la liaison d'engrenage, et une augmentation de l'efficacité peut être attendue grâce à une liaison d'engrenage sans perte au moyen d'un dispositif d'engrenage constitué d'une combinaison d'engrenages coniques qui adopte un procédé d'engrenage bifurqué, qui est une technique pour fonctionner avec un couple de force qui peut doubler la capacité de liaison.

    본 발명은 회전익 항공기 이착륙 시 비행을 안정하게 하고, 로터의 회전동력을 효율적으로 작동되게 하는 방법에 관한 것이다. 현재 항공기의 베벨기어 접속 방법은 기어접속 하나의 지점에 모든 동력부하가 편하중으로 집중되므로 떨림의 원인이 되고 베어링의 마모 등 악영향을 개선하는 것으로, 항공기 회전 동력 결합이 효율적으로 되기 위하여 기어 접속이 180도 대응하는 위치에서 동력이 50%씩 분할되며, 접속능력이 2배 가능한 짝힘으로 동작하는 기술인 이분기어 방식을 채택한 베벨기어 조합으로 이루어지는 기어 장치로 손실 없는 기어접속으로 효율 증대를 기대할 수 있다.


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    Title :

    AIRCRAFT USING FORCE COUPLE


    Additional title:

    AÉRONEF UTILISANT UN COUPLE DE FORCE
    짝힘동력을 이용한 항공기


    Contributors:

    Publication date :

    2024-09-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16H Getriebe , GEARING



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