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Airship pod, airship and recovery method of airship pod

A technology of airships and pods, which is applied to the recovery of airships and airship pods, and in the field of airship pods. It can solve the problems of large atmospheric environment impact and uncontrollable landing site, so as to improve recovery efficiency and reduce the search and rescue process.

Inactive Publication Date: 2018-06-15
北京天恒长鹰科技股份有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the above-mentioned method still has great defects
The parachute on the pod is greatly affected by the atmospheric environment during the landing process, and the landing site is uncontrollable

Method used

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  • Airship pod, airship and recovery method of airship pod
  • Airship pod, airship and recovery method of airship pod

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Embodiment Construction

[0024] Exemplary embodiments of the present disclosure will be described in more detail below with reference to the accompanying drawings. Although exemplary embodiments of the present disclosure are shown in the drawings, it should be understood that the present disclosure may be embodied in various forms and should not be limited by the embodiments set forth herein. Rather, these embodiments are provided for more thorough understanding of the present disclosure and to fully convey the scope of the present disclosure to those skilled in the art.

[0025] figure 1 It is a schematic diagram of the overall structure of the airship in the embodiment of the present invention. The airship in this embodiment includes an airship airbag 20 and an airship pod 10 . The airship pod 10 is connected to the bottom of the airship airbag 20 through a polyethylene rope, and a cutter is provided on the polyethylene rope, and the cutter can cut the polyethylene rope according to the control of...

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Abstract

The invention belongs to the technical field of aircrafts, in particular to an airship pod, an airship and a recovery method of the airship pod. The airship pod comprises an airship body, wings arranged on the two sides of the airship body, and a tail wing arranged at the tail of the airship body. A power supply and a control unit which are used for driving the airship pod are arranged in the airship body; ailerons capable of rotating are arranged on the wings; included angles between the ailerons and the wings can be adjusted by rotating the ailerons; a rudder capable of rotating is arrangedon the tail wing; and an included angle between the rudder and the tail wing can be adjusted by rotating the rudder. By using the airship pod, the airship and the recovery method of the airship pod, the gliding path of the airship pod is controlled in the recovery process of the airship pod, the airship pod is effectively made to fall back according to the specified position, the search and rescueprocesses of the airship pod after falling back are reduced, and the recovery efficiency of the airship pod is improved.

Description

technical field [0001] The invention belongs to the technical field of aircraft, and in particular relates to an airship pod, an airship and a recovery method for the airship pod. Background technique [0002] The stratospheric airship relies on the helium inside its capsule to generate enough buoyancy to achieve the purpose of launching and cruising. Its residence altitude is generally 20 kilometers from the earth's surface. When the airship completes its flight mission and is ready to return to landing, its exhaust valve can be controlled to open to release helium. During the release of helium, the buoyancy force on the airship gradually decreases, and the flight altitude gradually drops until it lands. This way of landing makes the airship and pod hit the ground at a very high speed, causing damage to the structure of the pod and its internal equipment, loads, etc. [0003] A feasible solution to this problem in the prior art is to use a parachute. The airship pod is c...

Claims

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Application Information

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IPC IPC(8): B64B1/22B64B1/20B64B1/06
CPCB64B1/22B64B1/06B64B1/20
Inventor 高大亮
Owner 北京天恒长鹰科技股份有限公司