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platform aerostat

A technology of aerostats and platforms, applied in the directions of machines/engines, greenhouse gas reduction, transportation and packaging, etc., can solve problems such as constraints on rising power sources, material constraints, and communication conditions, and achieve low Reynolds number and delay shedding , the effect of small absolute size

Active Publication Date: 2018-09-18
CHINA UNIV OF GEOSCIENCES (WUHAN)
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Problems solved by technology

[0003] However, the flight altitude of most of the current scientific research aircraft cannot reach the height of the stratosphere, or is restricted by the source of ascent power, or is restricted by communication conditions, or is restricted by materials.

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Embodiment Construction

[0034] The present invention will be further described below in conjunction with drawings and embodiments.

[0035] The invention provides a platform aerostat, referring to figure 1 , figure 2 with image 3, provides a platform aerostat, including a main body cabin and a flight wing, the main body cabin is composed of more than three packing boxes distributed according to a regular polygon, and each packing box is located at the apex of the regular polygon. All the boxes are identical, and are composed of the instrument cabin 8 and the hydrogen package cabin 9 in the figure, which ensure the stability of the entire platform aerostat. Each bag box is provided with a windmill 10 in a vertical direction and a flying wing driven by the windmill 10. The plane where the windmill 10 is located is coplanar with the radius of the regular polygon. The center of the support 13 is coaxial with the shaft center of the windmill 10, and the flying wing is composed of two rigid movable sh...

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Abstract

The invention provides a near space platform aerostat. The platform aerostat comprises a main body cabinet and fly wings. Insect-imitating flapping wings are adopted as the fly wings. Blind-window-shaped wind sails are arranged above the main body cabinet, wherein power of each blind-window-shaped wind sail is provided by a wind wheel storage battery, so that each blind-window-shaped wind sail performs opening and closing motion. A transverse wind wheel connected with the corresponding wind wheel storage battery is arranged above each wind sail. An umbrella-shaped flow guiding hood is arranged above each wind wheel. The upper surface of each umbrella-shaped flow guiding hood is a smooth curved face or a convex face which is formed by a set of triangular unit pieces. An inner chamber of each umbrella-shaped flow guiding hood is provided with a parachute package and a control cabinet. Each control cabinet is internally provided with a control module. Each instrument cabinet is internally provided with a 5G communication module which is used for conducting communication with other near space platforms and / or the ground. According to the near space platform aerostat, buoyancy force of hydrogen packages and lift force generated by vertical quivering of the insect-imitating flapping wings are used as power for continuous ascending; and meanwhile, wind force generated from terrestrial space to the stratosphere is utilized, the near space platform aerostat can enter the stratosphere and operate stably, and a good platform basis is provided for future quantum repeater experiments.

Description

technical field [0001] The invention relates to a platform aerostat, which belongs to the technical field of near space vehicles. Background technique [0002] At present, research on qubits is ongoing, especially the application of quantum repeaters is still in the experimental stage. The adjacent space is an important and primary choice for conducting quantum repeater experiments. If a space platform base station were built in the stratosphere, it could provide an airborne transmission path for the upcoming quantum repeater. Since the space from the satellite to the stratosphere is unimpeded, it can effectively improve the scientific research efficiency of quantum communication satellites. [0003] However, the flight altitude of most of the current scientific research aircraft cannot reach the height of the stratosphere, or it is restricted by the source of ascent power, or it is restricted by communication conditions, or it is restricted by materials. Therefore, how t...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64B1/20B64B1/62B64C1/38B64D27/24B64D47/00F03D9/11F03D9/32
CPCB64B1/20B64B1/62B64C1/38B64D27/24B64D47/00F03D9/00F05B2220/706Y02E10/72Y02E70/30
Inventor 韦成
Owner CHINA UNIV OF GEOSCIENCES (WUHAN)
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