Stratospheric airship with full-motion front wings and mobile counterweight

A technology for stratospheric airships and front wings, applied in the field of stratospheric airships, can solve the problems of bulky flight or turning, poor maneuverability, poor adjustment ability, etc., to increase pitch performance, increase maneuverability and controllability, and increase attitude The effect of the change

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] Stratospheric airships generally have fixed flying wings on both sides, with poor adjustment ability, cumbersome when flying or turning, slow response, and poor maneuverability

Method used

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  • Stratospheric airship with full-motion front wings and mobile counterweight
  • Stratospheric airship with full-motion front wings and mobile counterweight
  • Stratospheric airship with full-motion front wings and mobile counterweight

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0041] A stratospheric airship with a front wing comprises a hull 10, a front wing 20, a horizontal tail 30, a vertical tail 40, a vertical tail rudder surface 60, a horizontal tail elevator rudder surface 70, and a vector propeller 80.

[0042] Refer to attached figure 1As shown, front wings 20 are arranged symmetrically on both sides of the front of the hull 10, and the front wings 20 can rotate relative to the hull as a whole. Rotate to set the angle, the angle between the front wing 20 and the horizontal plane is ±45°. Specifically, the center shaft can be selected to be arranged in the front wing 20, and the driving device drives the center shaft to rotate. Alternatively, both sides of the front wing 20 are provided with adjusting rods, and both ends are adjusted simultaneously to make the front wing 20 rotate.

[0043] Both sides of hull 10 rear portion are symmetrically provided with horizontal empennage 30, and vector propeller 80 is installed symmetrically on the bo...

Embodiment 2

[0048] Refer to attached Figure 4 Shown, a kind of stratospheric airship with front wing, comprises hull 10, front wing 20, horizontal empennage 30, vertical empennage 40, vertical empennage rudder surface 60, horizontal empennage elevator rudder surface 70, vector thruster 80, slide cable 120, lead bag 130, fixed pulley 140, movable pulley 150, motor 160.

[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 the main bag 11 protrudes fro...

Embodiment 3

[0056] Refer to attached Figure 5 Shown, a kind of stratospheric airship with front wing, comprises hull 10, front wing 20, horizontal empennage 30, vertical empennage 40, vertical empennage rudder surface 60, horizontal empennage elevator rudder surface 70, vector propeller 80, unmanned Machine 90, magnetic suction type contact charging board 100, solar power generation device 110.

[0057] Front wings 20 are symmetrically arranged on both sides of the front of the hull 10, and the front wings 20 can rotate relative to the hull as a whole. Angle, the angle between the front wing 20 and the horizontal plane is ±45°. Specifically, the center shaft can be selected to be arranged in the front wing 20, and the driving device drives the center shaft to rotate. Alternatively, both sides of the front wing 20 are provided with adjusting rods, and both ends are adjusted simultaneously to make the front wing 20 rotate.

[0058] Both sides of hull 10 rear portion are symmetrically pr...

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Abstract

The invention discloses a stratospheric airship with full-motion front wings and a mobile counterweight. The front wings are symmetrically arranged on both sides of the front portion of a hull, and the front wings can be rotated relative to the hull. 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. Vertical tails are arranged on the upper portions of the tail portions of the side capsules, and the front wings and the horizontal tails are symmetrically disposed on both sides of the longest weft of the side capsules. The full-motion front wings have more remarkable adjustment effect on the airship, and the buoyant weightbalance problem caused by the helium temperature difference of the stratospheric airship is comprehensively and effectively solved by adjusting the pitch angle 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 full-motion front wing and a movable counterweight. 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 m...

Claims

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Application Information

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IPC IPC(8): B64B1/38B64B1/58B64B1/20
CPCB64B1/20B64B1/38B64B1/58
Inventor 许顺利许璐
Owner 达天飞艇(宁夏)有限公司
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