The invention relates to the technical field of aircraft lifting force devices, in particular to a novel aircraft lifting force device which structurally comprises an aircraft body, a front vertical frame, a lifting force device body and a rear vertical frame, and the front vertical frame and the rear vertical frame are both installed at the upper end of the aircraft body. When the helicopter moves upwards, the main rotating shaft drives the secondary rotating shafts to enable the wings on the two sides of the outer side to horizontally lie and move downwards, only lift force is generated, air resistance is hardly generated, when the helicopter moves upwards, the main rotating shaft drives the secondary rotating shafts to enable the wings on the inner side to vertically move upwards, and therefore the generated air resistance is small. When a traditional helicopter flies, the larger the area of a rotor wing is, the larger the generated air resistance is, the lift device cannot generate the problem, the area of a wing is not positively correlated with the air resistance, that is, the air resistance cannot be increased when the area of the wing is increased, and therefore the larger area of the wing can be used; more downwash airflow can be generated by a larger wing area, and more lift force is generated, so that the flight efficiency is improved.
本发明涉及飞行器升力装置技术领域,尤其涉及了一种新型飞行器升力装置,其结构包括:飞行器本体、前立架、升力装置、后立架,前立架与后立架均安装在飞行器本体上端,该飞行器在向上运动和向前运动时,主旋转轴会驱使次旋转轴让外侧两边的机翼横躺着向下运动,只产生升力,几乎不会产生空气阻力,同样直升机向上运动时,主旋转轴会驱使次旋转轴让内侧的机翼为竖直向上运动,由此产生的空气阻力也很小,与传统直升机旋翼相比较,传统直升机飞行时,旋翼面积越大,产生的空气阻力越大,而此升力装置却不会产生这个问题,机翼面积与空气阻力并非正相关,即增大机翼面积并不会导致空气阻力变大,因此可以使用更大的机翼面积,更大的机翼面积就能产生更多的下洗气流,产生更多的升力,从而实现飞行效率的提高。
Novel aircraft lift device
一种新型飞行器升力装置
2023-03-10
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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