专利名称：A FLYING APPARATUS
发明人：Shchukin, Anton Alexandrovich 申请号：EP15166221.0
申请日：20150504
公开号：EP3090945B1
公开日：
20180418
专利内容由知识产权出版社提供
摘要：The invention relate to aircraft and ud for civilian purpos, the delivery of people and freights, also for agricultural and fire-fighting purpos, for military tasks, reconnaissance tasks, for the tasks of air defen and air superiority. Summary of the invention consists in equipping the aircraft carriers of the aerodynamic surfaces each of which can be independently rotated around the axis of the attachment to the fulage and each of which has assigned to it the device that creates cravings in plane of the aerodynamic surfaces to achieve high maneuverability and flight ability in any direction at any position of the fulage. The propod aircraft us innovative aerodynamic scheme and contains four or more independently rotatable around the axis of the attachment to the fulage aerodynamic surfaces installed on each device, each of which creates cravings in the plane of the aerodynamic surfaces. In horizontal flight, aerodynamic surfaces create lift aimed vertically, and a traction device creates a force that is aimed horizontally in the direction of flight. This configuration is designed for maximum range as minimum fuel consumption. Aircraft can gain altitude when changing the angle of the front or rear pairs of aerodynamic surfaces, that will make the fulage, also change the angle of attack. When the front and rear surfaces at the same time is reached maneuverability. If necessary, increa altitude without changing the angle of attack of
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the fulage or change by a specified amount can be achieved by changing the angle of attack of bo
周记大全th pairs of surfaces - (for example, under special conditions of transportation of cargo or pasngers or challenges accompany ground or air targets). Similarly, can implement the vertical climb with horizontally locate the fulage, as well as horizontal flight with vertically located the fulage or even flying aft forward. Can ensure the aircraft hangs with arbitrary pitch angle. Can ensure the aircraft hangs with arbitrary pitch angle. The increa in the number of aerodynamic surfaces adds new features: add horizontal surfaces can provide aircraft combined flight mode. Using the power control devices creating reactive thrust could provide rotating in place when moving the fulage in the horizontal plane and vertical plane.
申请人：SHCHUKIN ANTON ALEXANDROVICH
事迹材料怎么写地址：CY
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冰球杆国籍：CY
代理机构：Sloboshanin, Sergej党的四个意识
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