A novel V-shaped sopiler airship

A technology of tail fin and airship, applied in the field of aviation, can solve problems such as non-function, and achieve the effects of convenient adjustment, significant social and economic benefits

Inactive Publication Date: 2010-07-28
黄刚
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

But the airship of this patent does not have various parameters that can accurately control the flight attitude of the hull, and the function of good maneuverability

Method used

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  • A novel V-shaped sopiler airship
  • A novel V-shaped sopiler airship
  • A novel V-shaped sopiler airship

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Embodiment Construction

[0015] The present invention will be further introduced below in conjunction with the accompanying drawings and specific embodiments, but not as a limitation of the present invention.

[0016] Such as figure 1 , figure 2 and image 3 As shown, the airship includes a hull 1, a car 5 at the bottom of the hull 1, a propeller 2, a small airbag 3, a control system, a landing gear 4 at the bottom of the car, and a horizontal tail 7 and a vertical tail 6. , the hull 1 is an airbag type, and its shape is a spindle airfoil shape. The upper part is a soft shell, and the lower half is a hard shell. The hull 1 is filled with hydrogen or helium. Generates buoyancy of 50% to 95% of the total weight. The hull 1 structure of the airship is made of aluminum alloy or composite material, and the structure and shape of the airship are maintained through the support of the skeleton, ropes and airbags. Shaped shape, it can generate lift after running in the air.

[0017] Such as Figure 4 As...

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Abstract

The invention relates to an airship, in particular to a modified airship which combines with an airship, an airplane with fixed wings and a gyroplane which can fly up and down vertically; the invention provides an economical, fast and safe aircraft which has excellent operating performance and can take off and land in vertical and sliding way; the invention comprises an airship body, a cage, propellers, a operation and control system and a landing gear; the airship body is in spindle-wing shape; at least two propellers are arranged on two sides of the airship body; two small balloons which can be used for adjusting buoyancy and weight are arranged in the airship body; one of the balloon is a hydrogen balloon, the other balloon is an air balloon; a tail wing is arranged at the tail of the airship body. Compared with a general airship, an airplane with fixed wings and a gyroplane which can fly up and down vertically, the invention is a modified airship combined by an airship, an airplane with fixed wings and a gyroplane which can fly up and down vertically; the invention can realize an economical, fast and safe aircraft which has excellent operating performance, and can take off as well as land in vertical and sliding way; with novel structure, convenient operation, high applicability and wide applicable range, the invention has good applicable prospects and significant social as well as economic benefits.

Description

technical field [0001] The invention belongs to the field of aviation, and in particular relates to a V-shaped tail airship. Background technique [0002] Although ordinary airships have the characteristics of economical operation, they have the disadvantages of bulky, difficult to operate, and difficult to lift and park; while fixed-wing aircraft fly fast and are easy to operate, but they have high cost, low safety performance, and cannot take off and land vertically. ; For rotary wing helicopters, although vertical take-off and landing is possible, there are disadvantages of high cost, low benefit and poor safety. [0003] In U.S. Patent US-2331404A, an airship is disclosed, including: a hull, a car and a propeller are arranged at the lower part of the hull, a control system is arranged in the car, and a landing gear is arranged at the lower part of the car, and both sides of the hull are symmetrical. Two propellers are provided, two small airbags are arranged in the hull...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64B1/02B64B1/58
Inventor 黄刚
Owner 黄刚
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