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A high-altitude dynamic floater with adjustable attitude

A technology of aerostats and attitude, applied in the direction of balloon aircraft, etc., can solve the problem of long-term fixed-point blanking of aerostats, achieve the effects of simple structure, reduced system scale and manufacturing costs, and reduced ground support requirements

Active Publication Date: 2018-12-25
CHINA ELECTRONIC TECH GRP CORP NO 38 RES INST
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The technical problem to be solved by the present invention is to solve the problem of long-term fixed-point blanking of the aerostat, and provide a high-altitude dynamic aerostat with adjustable attitude

Method used

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  • A high-altitude dynamic floater with adjustable attitude
  • A high-altitude dynamic floater with adjustable attitude
  • A high-altitude dynamic floater with adjustable attitude

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Embodiment Construction

[0028] The embodiments of the present invention are described in detail below. This embodiment is implemented on the premise of the technical solution of the present invention, and detailed implementation methods and specific operating procedures are provided, but the protection scope of the present invention is not limited to the following implementation example.

[0029] like figure 1 As shown, a high-altitude power aerostat with adjustable attitude of the present embodiment includes a main capsule body 1, an auxiliary airbag 2, a tailwind mechanism 3, a first guide wire 4, a second guide wire 5, and a third guide wire 6. The fourth guide wire 7, the high-altitude power mechanism 8, the attitude adjustment mechanism 9 and the equipment cabin 10; the auxiliary airbag 2 is independently arranged inside the main capsule body 1, and the main capsule body 1 is filled with light gas, and the Air is filled in the auxiliary air bag 2, and the density of the light gas is less than t...

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Abstract

The invention discloses a high-altitude power floater with adjustable heading, A sub-balloon is independently arrange in that inner part of the main balloon, A main bladder is fil with light gas, thesecondary air bag is filled with air, the density of the light gas is smaller than the density of the air, the head ends of the first guide cable and the fourth guide cable are respectively connectedwith two opposite vertices on the main bladder, the head ends of the second guide cable and the third guide cable are respectively connected to the side edges of two opposite vertices on the main bladder, The ends of the first guide cable, the second guide cable, the third guide cable and the fourth guide cable are respectively connected with the attitude adjusting mechanism, the high-altitude power mechanism and the attitude adjusting mechanism are respectively arranged on the equipment compartment, and the downwind mechanism is bound to the bladder of the main bladder. We can use the traditional way to release the floating ball to reduce the demand of ground support; Adjust the attitude of the sphere in the air, cooperate with the downwind device, have certain active flight control means.

Description

technical field [0001] The invention relates to a high-altitude aerostat, in particular to a high-altitude dynamic aerostat with adjustable attitude. Background technique [0002] Stratospheric aerostat is a kind of soft structure aircraft, mainly in two forms: stratospheric airship and stratospheric floating ball. Among them, the stratospheric airship carries power equipment. Due to the large number of supporting equipment in the system and the large dead weight, the airbag of the airship is relatively large. Large size, high cost, and relatively harsh conditions for ground release. Air-floating balloons include super-pressure balloons and zero-pressure balloons. They do not carry a power system, are small in scale, low in cost, and have a stronger effective carrying capacity than airships, and lower requirements for ground release. Because the floating ball has no external power equipment, the flight trajectory in the air is greatly affected by the environmental wind fiel...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64B1/40
CPCB64B1/40
Inventor 朱增青刘国梁陈利鞠金彪唐逊
Owner CHINA ELECTRONIC TECH GRP CORP NO 38 RES INST
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