首页> 外国专利> METHOD FOR MOVING PAYLOADS IN THE ATMOSPHERE OF A PLANET AT VELOCITIES GREATER THAN ORBITAL VELOCITY AND HYPERSONIC AIRCRAFT FOR THE IMPLEMENTATION THEREOF

METHOD FOR MOVING PAYLOADS IN THE ATMOSPHERE OF A PLANET AT VELOCITIES GREATER THAN ORBITAL VELOCITY AND HYPERSONIC AIRCRAFT FOR THE IMPLEMENTATION THEREOF

机译:移动速度大于轨道速度和超音速飞机的行星大气中的有效载荷的方法

摘要

The group of inventions relates to aerospace engineering, and more particularly to hypersonic aircraft and methods for flying in the upper atmosphere at hypersonic velocities. For travel in the atmosphere (or close to the boundary thereof), the hypersonic aircraft is accelerated with the aid of rocket engines to a velocity greater than orbital velocity. The hypersonic aircraft is maintained in a near-circular orbit by means of aerodynamic downforce or the thrust of the rocket engines. The necessary energy (to heat the working fluid of the rocket engines) is supplied with the aid of directed-energy power stations. These power stations are located in space above the flight path of the hypersonic aircraft and provide, in sequence, energy (UHF or laser) to the aircraft, it being possible also for the beams from a plurality of power stations to be focused on the aircraft. The heating of the working fluid to generate thrust and the simultaneous cooling of the structure of the hypersonic aircraft is provided by means of the proposed variants for the aerodynamic design thereof and by means of the thermal protection (active and passive) of the hypersonic aircraft. The result is an increase in the velocities of near-space cargo and passenger flights with a reduction in the environmental impact thereof.
机译:本发明组涉及航空航天工程,并且更具体地涉及高超音速飞机和用于以高超音速在高层大气中飞行的方法。为了在大气中(或其边界附近)行驶,借助火箭发动机将高超音速飞机加速到大于轨道速度的速度。高超音速飞机通过空气动力下压力或火箭发动机的推力保持在接近圆形的轨道上。在定向能量发电站的帮助下,提供了必要的能量(用于加热火箭发动机的工作流体)。这些发电站位于高超音速飞机的飞行路径上方的空间中,并依次向飞机提供能量(UHF或激光),来自多个发电站的光束也可能会聚焦在飞机上。通过所提出的用于其空气动力学设计的变型以及通过高超声速飞机的(主动和被动)热保护,提供工作流体的加热以产生推力并且同时冷却高超声速飞机的结构。结果是增加了近空货运和客运航班的速度,并减少了其对环境的影响。

著录项

  • 公开/公告号WO2014021742A3

    专利类型

  • 公开/公告日2014-06-12

    原文格式PDF

  • 申请/专利权人 ALEKSANDROV OLEG ALEKSANDROVICH;

    申请/专利号WO2013RU00659

  • 发明设计人 ALEKSANDROV OLEG ALEKSANDROVICH;

    申请日2013-07-31

  • 分类号B64C30;B64C9;B64D27/16;

  • 国家 WO

  • 入库时间 2022-08-21 15:51:52

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