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Course-adjustable stratosphere balloon and method thereof

An adjustable, stratospheric technology, applied in the direction of balloon aircraft, airbag deployment, and services based on specific environments, can solve problems such as difficult attitude control, high energy demand, and low propeller efficiency, and achieve improved maneuverability and high-altitude parking retention capacity, low energy demand, and simple structure

Pending Publication Date: 2022-01-21
EAGLES MEN AERONAUTIC SCI & TECH GRP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Stratospheric balloon is a new type of low-cost, low-energy stratospheric aircraft. However, the propeller method is often used in the traditional stratospheric balloon power system. High and high energy consumption

Method used

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  • Course-adjustable stratosphere balloon and method thereof
  • Course-adjustable stratosphere balloon and method thereof
  • Course-adjustable stratosphere balloon and method thereof

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Embodiment Construction

[0019] In order to describe the technical content, structural features, and achieved effects of the present invention in detail, the following will be described in detail in conjunction with the embodiments and accompanying drawings.

[0020] see Figure 1 to Figure 2 , the present invention provides a course-adjustable stratospheric balloon 100, which includes an upper capsule body 1, an upper sensing mechanism 2, a lower capsule body 3, a lower sensing mechanism 4, a distance adjusting device 5 and a control device 6, and the upper sensing mechanism 2 It is installed on the upper capsule 1 to sense the wind speed and height of the environment where the upper capsule 1 is located. The lower sensing mechanism 4 is located on the lower capsule 3 to sense the wind speed and height of the environment where the lower capsule 3 is located. The upper capsule 1 and the lower capsule 3 both have upward buoyancy after being inflated, the gas filled can be hydrogen and other gases, the ...

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Abstract

The invention discloses a course-adjustable stratosphere balloon. The balloon comprises an upper balloon body, an upper sensing mechanism, a lower balloon body, a lower sensing mechanism, a distance adjusting device and a control device, the upper sensing mechanism is arranged on the upper bag body, and the lower sensing mechanism is arranged on the lower bag body; the distance adjusting device is connected between the upper bag body and the lower bag body; the distance adjusting device is used for adjusting the distance between the upper bag body and the lower bag body, and the control device is electrically connected with the upper sensing mechanism, the lower sensing mechanism and the distance adjusting device. According to the light balloon, the course is adjusted through a wind field, and the light balloon has the advantages of being low in energy consumption and simple in structure. The invention further comprises a navigation method.

Description

technical field [0001] The invention relates to the technical field of stratospheric aircraft, in particular to a course-adjustable stratospheric balloon. Background technique [0002] In recent years, various countries are conducting research on various types of stratospheric aircraft. Stratospheric balloon is a new type of low-cost, low-energy stratospheric aircraft. However, the propeller method is often used in the traditional stratospheric balloon power system. high and high energy consumption. [0003] At present, it is necessary to provide a heading-adjustable stratospheric balloon. Contents of the invention [0004] The object of the present invention is to provide a heading-adjustable stratospheric balloon that uses wind field to adjust heading, which has the advantages of low energy consumption and simple structure. [0005] In order to achieve the above object, the course-adjustable stratospheric balloon provided by the present invention includes an upper cap...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64B1/40B64B1/58H04W4/38
CPCB64B1/40B64B1/58H04W4/38
Inventor 武哲杨永强谢渊谢欣辉
Owner EAGLES MEN AERONAUTIC SCI & TECH GRP
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