
基本信息:
- 专利标题: A FLYING APPARATUS
- 专利标题(中):飞行装置
- 申请号:EP15166221.0 申请日:2015-05-04
- 公开(公告)号:EP3090945B1 公开(公告)日:2018-04-18
- 发明人: Shchukin, Anton Alexandrovich
- 申请人: Shchukin, Anton Alexandrovich
- 申请人地址: Arch Makariou III, 132 Sagro Building, 4th floor 3021 Limassol CY
- 专利权人: Shchukin, Anton Alexandrovich
- 当前专利权人: Shchukin, Anton Alexandrovich
- 当前专利权人地址: Arch Makariou III, 132 Sagro Building, 4th floor 3021 Limassol CY
- 代理机构: Sloboshanin, Sergej
- 主分类号: B64C29/00
- IPC分类号: B64C29/00 ; B64C39/08 ; B64C3/38
摘要:
The invention relate to aircraft and used for civilian purposes, the delivery of people and freights, also for agricultural and fire-fighting purposes, for military tasks, reconnaissance tasks, for the tasks of air defense 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 fuselage 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 fuselage. The proposed aircraft uses innovative aerodynamic scheme and contains four or more independently rotatable around the axis of the attachment to the fuselage 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 fuselage, also change the angle of attack. When the front and rear surfaces at the same time is reached maneuverability. If necessary, increase altitude without changing the angle of attack of the fuselage or change by a specified amount can be achieved by changing the angle of attack of both pairs of surfaces - (for example, under special conditions of transportation of cargo or passengers or challenges accompany ground or air targets). Similarly, can implement the vertical climb with horizontally locate the fuselage, as well as horizontal flight with vertically located the fuselage or even flying aft forward. Can ensure the aircraft hangs with arbitrary pitch angle. Can ensure the aircraft hangs with arbitrary pitch angle. The increase 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 fuselage in the horizontal plane and vertical plane.
公开/授权文献:
- EP3090945A1 A FLYING APPARATUS 公开/授权日:2016-11-09
IPC结构图谱:
B | 作业;运输 |
--B64 | 飞行器;航空;宇宙航行 |
----B64C | 飞机;直升飞机 |
------B64C29/00 | 能垂直起飞或着陆的飞机 |