Nose tower structure of captive balloon anchoring facility
A technology for mooring balloons and facilities, applied in the direction of balloon aircraft, lighter-than-air aircraft, aircraft, etc., can solve the problems of inability to adjust the height, not having wide applicability, and the anchoring facilities cannot be transported normally, and achieve wide applicability Effect
Inactive Publication Date: 2021-08-17
AEROSPACE INFORMATION RES INST CAS
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Problems solved by technology
At present, due to the high nose tower structure, the mooring facilities cannot be transported normally; and each type of tethered balloon needs to correspond to a nose tower structure of a certain height, that is, the same nose tower structure can only be used for the same spherical shape. Since the height cannot be adjusted, Therefore, it is not widely applicable
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[0026] In order to make the purpose, technical solutions and advantages of the present invention clearer, the technical solutions in the present invention will be clearly and completely described below in conjunction with the accompanying drawings in the present invention. Obviously, the described embodiments are part of the embodiments of the present invention , but not all examples. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.
[0027] In the description of the embodiments of the present invention, it should be noted that the terms "upper", "lower", "left", "right", "vertical", "horizontal", "top", "bottom", "inner ", "outside" and other indicated orientations or positional relationships are based on the orientations or positional relationships shown in the drawings, which are only for the convenience of describing t...
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The invention relates to the technical field of aerostats, and provides a nose tower structure of a captive balloon anchoring facility. The nose tower structure comprises a base, a first main body, a first driving device, a second main body and a nose tower end part, wherein the base is used for being arranged on the anchoring facility; the inner side of the first end of the first main body is rotatably connected with the top end of the base; the first driving device is used for being hinged to the anchoring facility, the driving end of the first driving device is hinged to the outer side of the first end of the first main body, and the first driving device is used for driving the first main body to be switched between a folded state and an unfolded upright state; the first end of the second main body is telescopically connected with the second end of the first main body; and the nose tower end part is arranged at the second end of the second main body. The nose tower structure can be stretched, retracted and folded, is convenient to anchor and transport, meets captive balloons of different sizes and shapes, and has wide applicability.
Description
technical field [0001] The invention relates to the technical field of aerostats, in particular to a nose tower structure of a tethered balloon mooring facility. Background technique [0002] A tethered balloon is a lighter-than-air, unpowered aerostat having a bladder filled with a lighter-than-air gas and thus exerting upward buoyancy. [0003] The tethered balloon system includes tethered balloons, tether components, mooring facilities, and ground comprehensive support facilities. The tethered balloon is suspended in the air by buoyancy. The tethered balloon is connected to the ground mooring facility through the tethered cable assembly. The height of the tethered balloon can be adjusted by adjusting the length of the tethered cable, thereby providing a quasi-static aerial platform for other equipment. Wherein, the mooring cable assembly includes a main cable, a nose lanyard and a side lanyard, etc. When the tethered balloon is in the air, the height of the tethered bal...
Claims
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IPC IPC(8): B64B1/50B64B1/66
CPCB64B1/50B64B1/66
Inventor 栗颖思龚文韬秦玉梅乔涛张远平
Owner AEROSPACE INFORMATION RES INST CAS