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1. 发明申请

WO2016133427A4 VERTICAL TAKE-OFF AND LANDING AIRCRAFT (VARIANTS) 审中-公开
标题翻译：垂直起落飞机（变型）
公开(公告)号：WO2016133427A4
公开(公告)日：2017-01-19
申请号：PCT/RU2016000075
申请日：2016-02-15
申请人： NOROYAN GEVORG SEREZHAEVICH
发明人： NOROYAN GEVORG SEREZHAEVICH
IPC分类号： B64C29/00 , B64C15/00 , B64C39/06
CPC分类号： B64C29/0033 , B64C39/001 , F02C7/042
摘要： The invention relates to the field of aviation and cosmonautics, and more particularly to designs for vertical take-off and landing aircraft. The present vertical take-off and landing aircraft comprises jet propulsion units containing compressors, overflow valves, air tanks, and a nuclear power plant. Turbines are provided with hybrid engines capable of running on electricity or liquid fuel. On the outside of the aircraft, each turbine is provided with a corrugated tip, consisting of two parts: a base and an extendable part. The bases of the corrugated tips are pivotally mounted on the turbine for rotation about their own axis and are coupled to a lateral orientation system for altering the pumping direction. The other part of the corrugated tip is coupled to an angle adjusting system, which, when necessary, extends one side of the corrugated part outside the body in order to alter the pumping angle by more than 90 degrees from vertical to horizontal.
摘要翻译：本发明涉及航空和宇宙航空领域，更具体地涉及垂直起降飞机的设计。目前的垂直起降飞机包括含有压缩机，溢流阀，空气罐和核电站的喷气推进装置。涡轮机配有能够运行电力或液体燃料的混合动力发动机。在飞行器的外侧，每个涡轮机设有波纹尖端，由两部分组成：基部和可延伸部分。波纹尖端的基部枢转地安装在涡轮机上以围绕其自身的轴线旋转并且联接到侧向定向系统以改变泵送方向。波纹尖端的另一部分联接到角度调节系统，当需要时，角度调节系统将波纹部分的一侧延伸到身体外部，以便将抽吸角度从垂直方向改变到水平方向超过90度。

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