The present invention relates to an airplane structure which applies Bernoulli′s principle to allow an airplane to vertically take off and land. The present invention improves the efficiency of lift generated by streamlined wings and the speed of the airplane, and enables an airplane which is unable to take off and land vertically with the principle of action and reaction to be operated like a conventional airplane taking off and landing vertically by obtaining high-efficiency lift using the upper part of the fuselage instead of wings. The airplane comprises: a fuselage; wings which have air paths; a blower which is arranged on the front top end of the fuselage; air current doors which are opened and closed to guide air currents; drag panels which are arranged in the rear of the wings; nose doors which are arranged in the left and right of the front part of the fuselage; and rear doors which are arranged in the left and right of the rear part of the fuselage.
본 발명은 비행체의 수직 이착륙을 위해 베르누이의 원리를 응용하는 비행체 구조에 관한 것이다. 본 발명은 유선형상의 날개와 비행체의 속도에 의해 발생되는 양력의 효율도 높이는 것은 물론, 날개가 아닌 비행체의 동체의 윗부분을 활용해서도 고효율의 양력을 얻어 작용 반작용 원리로는 수직 이착륙이 불가능했던 비행체도 기존의 수직 이착륙 비행체처럼 작동시킬 수 있다.
AIRPLANE CAPABLE OF TAKING OFF AND LANDING VERTICALLY
수직 이착륙이 가능한 비행체
2016-07-08
Patent
Electronic Resource
Korean
IPC: | B64C AEROPLANES , Flugzeuge |
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