The invention relates to the field of tools related to flight equipment, and provides a double-shaft folding type rotor aircraft which comprises an aircraft body, a cockpit is arranged in the aircraft body, and fixed wings are arranged on the two sides of the aircraft body; a power block is arranged on the fixed wing on each side, an angular kinetic energy disc is arranged at the upper part of each power block, at least four groups of rotor wings are uniformly arranged on the angular kinetic energy disc on each side, and each group of rotor wings comprises a folding wing and a power assembly; the power assembly is connected to a power machine in the power block; a balance empennage is arranged at the tail of the aircraft body, and movable auxiliary wings are arranged on the balance empennage.
本发明涉及飞行设备相关的用具领域,提供了一种双轴折叠式旋翼飞行器,包括飞行器本体,所述飞行器本体的内部设置有驾驶舱,所述飞行器本体的两侧设置有固定机翼;每侧所述固定机翼上均设置有动力块,所述动力块的上部设置有角动能圆盘,每侧的所述角动能圆盘上均匀设置有至少四组旋翼,每组所述旋翼均包括折叠翼和动力组件;所述动力组件连接于所述动力块内的动力机;所述飞行器本体的尾部设置有平衡尾翼,所述平衡尾翼上设置有活动辅助翼。
Double-shaft folding type rotor craft
一种双轴折叠式旋翼飞行器
01.10.2024
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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