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Near space airship using inflatable wings and tiltable propellers

A technology of tilting propellers and adjacent space, applied in rigid airships and other directions, can solve the problems of reducing airship load and increasing weight, and achieve the effects of reducing self-weight, reducing volume and saving materials

Active Publication Date: 2012-10-10
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Today's airships generally use water recovery, but the water recovery system will add extra weight and reduce the load of the airship

Method used

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  • Near space airship using inflatable wings and tiltable propellers
  • Near space airship using inflatable wings and tiltable propellers

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Embodiment Construction

[0032] The present invention will be further described below in conjunction with accompanying drawing and embodiment, but present embodiment is not intended to limit the present invention, and every similar method of the present invention and similar changes thereof should be included in the protection scope of the present invention.

[0033] See figure 1 , figure 2 , the present invention is an airship in adjacent space that adopts an inflatable wing and a tiltable propeller. The load compartment 7, the battery 8 and the control system 9 are composed; the position connection relationship between them is: the solar cell 2 is covered on the upper surface of the hull 1, and two tiltable propellers 3 are installed along the longitudinal axis on the upper part of the hull 1, The empennage 5 is fixed on the tail of the hull 1, the inflatable wing 4 is located on the left and right sides of the front part of the hull 1, the landing gear 6 is installed on the lower part of the hull...

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Abstract

A near space airship using inflatable wings and tiltable propellers consists of an airship body, solar batteries, the tiltable propellers, the inflatable wings, tail wings, undercarriages, a loading cabin, storage batteries and a control system. The solar batteries cover the upper surface of the airship body; the tiltable propellers are longitudinally arranged on the upper part of the airship body; the tail wings are fixed at the tail of the airship body; the inflatable wings are positioned on the left side and the right side of the middle front part of the airship body; the undercarriages are arranged on the lower part of the airship body and can be folded into the airship body when the airship flies; and the loading cabin, the storage batteries and the control system are placed in the belly of the airship body. The near space airship is small in size, high in effective load and quite convenient to take off and land, and has a good development prospect in the field of near space aircrafts.

Description

technical field [0001] The invention relates to an airship in adjacent space using an inflatable wing and a tiltable propeller. It adopts a combination scheme of the airship, an inflatable wing and a tiltable propeller, and can fly and hover stably in an adjacent space. Proximity to space vehicle field. Background technique [0002] Near space refers to the airspace 20-100 kilometers above the ground, which has attracted widespread attention in the world due to its important development and application value. Stratospheric airship is a kind of aircraft that can work in adjacent space. Stratospheric airships have the advantages of long stagnation time (compared with aircraft and missiles) and high resolution (compared with satellite platforms), and can provide rare air carriers for military purposes such as air early warning, reconnaissance, communication, and surveillance. Therefore, it has attracted extensive attention and research from all over the world. [0003] Howev...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64B1/06B64B1/20B64B1/24B64B1/30
Inventor 王晓慧王新升李人杰
Owner BEIHANG UNIV
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