The invention relates to the field of aviation. An aircraft comprises a polyhedral body with rotatable cylinders 1 mounted around its periphery. In order to supply air into the aircraft, the main body is provided with an inlet 2 leading to an intake area and a gas supply area located inside the main body, and centrifugal impellers 3 are mounted at the top and bottom of the main body for generating a forced air flow. At the outlet of the intake and gas supply areas, and around the top and bottom of the periphery, there is a flow channel in the form of a unit 4 extending into a tunnel 5 which narrows at the outlet immediately upstream of the cylinder 1. The top flow channel and the bottom flow channel are independent of each other and are not connected to each other. The impeller 3 and the air cylinder 1 move through the engine 6. The claimed operating method is characterized in that the oncoming airflow acts on the region of the cylinder 1, generating lift by using the Magnus effect. The torque of the top impeller is compensated by the torque of the bottom impeller. The invention aims to reduce noise and increase load capacity.
本申请涉及航空领域。一种飞行器,包括具有围绕其周边安装的可旋转气缸1的多面体主体。为了将空气供应到飞行器中,主体设置有进口2,该进口通向位于主体内部的进气区域和气体供应区域,并且在主体的顶部和底部安装有离心叶轮3,用于产生强制气流。在进气区域和气体供应区域的出口处,及围绕在周边的顶部和底部,是以具有延伸到隧道5中的单元4形式的流动通道,该隧道在紧接气缸1上游的出口处变窄。顶部流动通道和底部流动通道彼此独立,并且不相互连接。叶轮3和气缸1通过发动机6进行运动。所要求保护的操作方法在于迎面而来的气流作用于气缸1的区域,通过使用马格努斯效应产生升力。顶部叶轮的扭矩由底部叶轮的扭矩补偿。本发明组旨在降低噪音和提高负载能力。
Magnus effect aircraft and method of operation thereof
马格努斯效应飞行器及其操作方法
2023-06-27
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |