Multipurpose transmission system and construction scheme thereof

A transmission system and multi-purpose technology, applied in the aerospace field, can solve the problems of the airship airbag inflation rate and skin bearing capacity reaching the limit, the pressure difference between the inside and outside of the airship airbag increasing, etc., achieving easy static hovering and solving slow steering action , the effect of improving efficiency

Pending Publication Date: 2020-11-24
申焕渝
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, as the altitude increases, the atmospheric pressure also drops sharply, and the pressure difference between the inside and outside o

Method used

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  • Multipurpose transmission system and construction scheme thereof
  • Multipurpose transmission system and construction scheme thereof
  • Multipurpose transmission system and construction scheme thereof

Examples

Experimental program
Comparison scheme
Effect test

Example Embodiment

[0044] Example 1.

[0045] All components of the day are completed and passed through the test, which will be moved from the manufacturing base to the space emission ground base (if it is excellent in manufacturing base, it can also be directly transformed into aerospace emission ground base). To facilitate air-driven flight, the system will temporarily combine two sets of autonomous floats, and a set is based on the superfloator (1), and a set is in the giant (4). For the main body. First, the functional module, the task cabin, the cable car (8), the tentative transport cable (712), and the lift overload protective cable (73), and the lift overload protection cable (73), and securely mounted, fixed The respective functional regions received on the superflorator (1), the space emission square (21), the control platform (3); the center is an anchor station (61), The triangular wind-resistant armor station (62) is dismantled as the hollow combination unit (63), and then the lower se...

Example Embodiment

[0046] Embodiment 2. The base is assembled.

[0047] After the day transport system is factory-factory, the medium and low-altitude flight arrives at the space emission ground base. The giant motor (4) low-speed motion to a predetermined triangular wind-resistant armor station (62) hold the hover. The spare cable car (8) is mounted to the channel well by a special slide facility after the hollow combination unit (63) of the triangulation of the triangulation of the triangular antibody tensioning station (62) is loaded. )Inside. The strong magnetic clutch (8113) on the cable car traveling device (811) is separated, and the mount rotation surface (8171) is opened, and the traveling device (811) is driven, and the guide wheel device (833) is interpreted. The lower section (711) enters the center position of the cable car by the cable car frame (821) and the steering cylinder (822). Then, the mount rotation surface (8171) is closed, the strong magnetic clutch (8113) closed. The guide ...

Example Embodiment

[0048] Example 3. Space emission.

[0049] When the day transmission system receives the space emission task in the standby state, take the corresponding operation steps depending on the task type. Since the space emission according to the present invention is starting at sea level 30-50km and above, it avoids a thick and heavy surface atmosphere. The thinner atmosphere makes the rockets very small, and the efficiency of the rocket engine is greatly improved. Therefore, the present invention has a rocket housing size required to complete the same load emission mission compared to conventional ground rocket emissions, the engine size, and the amount of fuel is largely reduced, and the rocket using the same specifications can assume a larger emission load.

[0050]When the small and medium orbit satellite launch task is low, the satellite and the launch vehicle (222) by the total weight of less than 100 ton conventional ground-launched reduce to less than 60 tons. For such emission,...

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Abstract

The invention discloses a multipurpose transmission system and a construction scheme thereof, and belongs to the technical field of aerospace. The multipurpose transmission system comprises an ultra-large near space aerostat and a space launch and control platform which are located at the upper part, a large near space aerostat and a top-bottom intersection transfer station platform which are located at the middle part, an anchor station which is located at the lower part, and a cable and a self-driving cable car which are located among the three parts. The multipurpose transmission system andthe construction scheme thereof are characterized in that a sufficient air bag is reserved in each aerostat, so that the dead weight of the aerostat cannot be reduced due to height increasing. The multipurpose transmission system has a main purpose of being taken as an efficient and energy-saving space launch platform system which is arranged in an ultra-high airspace with an altitude of 30-50 kilometers, and has many great purposes additionally. According to the multipurpose transmission system and the construction scheme thereof, human and material resources, aerospace equipment and the like can be conveyed onto the ultra-large aerostat by the large cable car and through the cable, and then the aerospace equipment is launched into the space by the space launch platform; and the multipurpose transmission system has many advantages compared with various traditional, researching and future aerospace manners.

Description

technical field [0001] The invention discloses a construction scheme of an unprecedented multipurpose space-to-ground transmission system. It is a technology belonging to the field of aerospace. Its main purpose is as a high-efficiency and energy-saving ultra-high-altitude space launch platform system set at an altitude of 30 to 50 kilometers above sea level. It is transported by cables to a super-giant near-space aerostat (super-floater) located at a super high altitude, and then the spacecraft is launched into space through the space launch platform and the control platform on it. Therefore the present invention mainly belongs to the technology of aerospace field. The present invention also has multiple important uses. Background technique [0002] The present invention involves a large number of technical fields. In order to clarify that the present invention has a reliable technical foundation and technological breakthrough, the following main background technologies ...

Claims

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Application Information

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IPC IPC(8): B64G1/00
CPCB64G1/005
Inventor 不公告发明人
Owner 申焕渝
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