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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 of the airship airbag continues to increase, so that the expansion rate and skin bearing capacity of the airship airbag quickly reach the limit

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

Embodiment 1

[0044] Embodiment one. Leave the factory.

[0045] After all components of the space-to-ground transmission system are manufactured and passed the test, the manufacturing base will be moved to the space launch ground base (if the manufacturing base has good conditions in all aspects, it can also be directly transformed into a space launch ground base). In order to facilitate air maneuvering flight, the system will be temporarily combined into two sets of autonomous maneuvering aerostats, one set is based on the super-floater (1), and the other is based on the giant aerostat (4). as the subject. First, temporarily install and fix components such as the functional module, the mission cabin, the cable car (8), the mooring transmission cable upper section (712) and the lift overload protection cable (73) that are planned to be carried in sequence. , the functional areas, the space launch plaza (21), and the control platform (3) that are stored on the superfloater (1); mooring the...

Embodiment 2

[0046] Embodiment 2. The base is assembled and lifted off.

[0047] After the space-to-ground transmission system leaves the factory, it flies to the space above the space launch ground base through low-to-medium altitude flight. The giant floater (4) maneuvers at a low speed to directly above the predetermined installation position of the triangular wind-resistant and tension-resistant anchor station (62) and keeps hovering. After the spare cable car (8) is loaded with the hollow combination unit (63) of the triangular wind-resistant and tension-resistant anchor station (62) in the transfer cabin, it moves to the passage shaft (43) through a special slideway facility. )Inside. The strong magnetic clutch (8113) on the traveling device (811) of the cable car is separated, the rotating surface (8171) of the hanger is opened, and the traveling device (811) is driven to deflect, and the guide wheel device (833) is opened similarly. The mooring cable lower section (711) enters th...

Embodiment 3

[0048] Embodiment three. Space launch.

[0049] After the space-ground transmission system receives a space launch mission in the standby state, it will take corresponding operation steps depending on the mission type. Since the space launch involved in the present invention starts at an altitude of 30--50km and above the adjacent space, the thick and heavy surface atmosphere is avoided. The thin atmosphere makes the rocket suffer from little resistance, and at the same time greatly improves the efficiency of the rocket engine. Therefore, compared with the traditional ground rocket launching, the present invention can greatly reduce the size of the rocket shell, the size of the engine, and the amount of fuel needed to complete the same load launch task, and the rocket with the same specification can bear a larger launch load.

[0050]When the launch task is a small and medium-sized satellite in low and medium orbits, the total weight of the satellite and the launch vehicle (2...

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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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