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Stratospheric airship with front wings and working method thereof

A stratospheric airship and front wing technology, applied in the field of stratospheric airships, to achieve the effect of extending the cruising time

Inactive Publication Date: 2018-10-12
达天飞艇(宁夏)有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Aiming at the deficiencies in the prior art, the present invention provides a stratospheric airship with a front wing and its working method. The front wing is added to increase the ability to control the pitch of the airship, and on the other hand, the pitch attitude of the airship is controlled by adding a movable counterweight. , to assist in changing the angle of attack of the airship to control the height change of the airship caused by the temperature difference of helium, thus solving the problem of buoyant weight balance

Method used

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  • Stratospheric airship with front wings and working method thereof
  • Stratospheric airship with front wings and working method thereof
  • Stratospheric airship with front wings and working method thereof

Examples

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Embodiment 1

[0035] A stratospheric airship with a front wing, comprising a hull 10, a front wing 20, a horizontal empennage 30, a vertical empennage 40, a front wing rudder surface 50, a vertical tail rudder surface 60, a horizontal tail elevator rudder surface 70, and a vector propeller 80 .

[0036] Refer to attached figure 1 As shown, the front wings 20 are symmetrically arranged on both sides of the front of the hull 10, the horizontal empennage 30 is arranged symmetrically on both sides of the rear of the hull 10, and the vector propeller 80 is symmetrically installed on both sides of the hull 10 and the hull 10, and the vector propeller 80 installed on both sides of the hull 10 is located between the front wing 20 and the horizontal stabilizer 30.

[0037] Refer to attached figure 2 And attached image 3 As shown, the hull 10 includes a main bag 11 and a side bag 12, the main bag 11 is arranged in the middle of the two side bags 12, the head of the main bag 11 protrudes from the...

Embodiment 2

[0041] Refer to attached Figure 4 Shown, a kind of stratospheric airship with front wing, comprises hull 10, front wing 20, horizontal tail 30, vertical tail 40, front wing rudder surface 50, vertical tail rudder surface 60, horizontal tail elevator rudder surface 70, vector Propeller 80, slide rope 120, lead bag 130, fixed pulley 140, movable pulley 150, motor 160.

[0042] Both sides of the front of the hull 10 are symmetrically provided with front wings 20, and both sides of the rear of the hull 10 are symmetrically provided with horizontal empennages 30, and the vector propellers 80 are symmetrically installed on both sides of the hull 10 and the rear of the hull 10. portion, and the vector propeller 80 installed on both sides of the hull 10 is located between the front wing 20 and the horizontal stabilizer 30 .

[0043] The hull 10 includes a main bag 11 and a side bag 12. The main bag 11 is arranged in the middle of the two side bags 12. The head of the main bag 11 protr...

Embodiment 3

[0048] Refer to attached Figure 5 Shown, a kind of stratospheric airship with front wing, comprises hull 10, front wing 20, horizontal tail 30, vertical tail 40, front wing rudder surface 50, vertical tail rudder surface 60, horizontal tail elevator rudder surface 70, vector A thruster 80 , a drone 90 , a magnetic contact charging board 100 , and a solar power generation device 110 .

[0049] Both sides of the front of the hull 10 are symmetrically provided with front wings 20, and both sides of the rear of the hull 10 are symmetrically provided with horizontal empennages 30, and the vector propellers 80 are symmetrically installed on both sides of the hull 10 and the rear of the hull 10. portion, and the vector propeller 80 installed on both sides of the hull 10 is located between the front wing 20 and the horizontal stabilizer 30 .

[0050] The hull 10 includes a main bag 11 and a side bag 12. The main bag 11 is arranged in the middle of the two side bags 12. The head of t...

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Abstract

The invention discloses an airship with front wings and a mobile counterweight. The airship includes a hull, the front wings, horizontal tails and vertical tails. The front wings are symmetrically arranged on both sides of the front portion of the hull, and the horizontal tails are symmetrically disposed on both sides of the rear portion of the hull. The hull includes a main capsule and two side capsules, and the main capsule is disposed in the middle of the two side capsules. The head portion of the main capsule protrudes from the head portions of the side capsules on both sides, and the horizontal position of the main capsule is higher than the side capsules on both sides. The vertical tails are arranged on the upper portions of the tail portions of the side capsules, and the front wingsand the horizontal tails are symmetrically disposed on both sides of the horizontal meridians of the side capsules. According to the buoyancy variation of the airship, the rudder yaw-angles of the front wings are controlled, and the buoyant weight balance problem caused by the helium temperature difference of a stratospheric airship is comprehensively and effectively solved by adjusting the pitchangle of the airship, controlling a power device in a vector mode and the like.

Description

technical field [0001] The invention relates to the field of stratospheric airships, in particular to a stratospheric airship with a front wing and a working method thereof. Background technique [0002] At the beginning of the 21st century, stratospheric airships have attracted the attention of major countries, and the fields of forecasting applications include civilian, police, paramilitary, and military applications. At present, stratospheric airships are mostly used in civil and military fields such as marine research, emergency rescue, urban traffic management, and aerial reconnaissance and early warning. The stratospheric airship is a kind of aerostat that sails in the upper stratosphere. It relies on air buoyancy to stay in the air and can suspend in the upper stratosphere for a long time. It is powered by solar energy and powered by vector propellers. An aerostat that can take off and land vertically and hover over any geographic location. [0003] The most difficu...

Claims

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Application Information

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IPC IPC(8): B64B1/20B64B1/38
CPCB64B1/20B64B1/38
Inventor 许顺利许璐
Owner 达天飞艇(宁夏)有限公司
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