Petrol-electric hybrid power airship

A hybrid and airship technology, applied in the aviation field, can solve the problems of short battery life, small load, poor controllability, etc., and achieve the effect of long battery life

Inactive Publication Date: 2016-02-03
DONGGUAN SOUTH CHINA DESIGN INNOVATION INST +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, most of the unmanned aerial vehicles in the prior art have the following disadvantages: short endurance time, small load capacity, poor controllability and other shortcomings. The existence of these shortcomings has greatly restricted the wide industrial application of unmanned aerial vehicles.

Method used

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  • Petrol-electric hybrid power airship
  • Petrol-electric hybrid power airship
  • Petrol-electric hybrid power airship

Examples

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Embodiment 1

[0021] An oil-electric hybrid power airship, comprising an airship body 1 and a power unit 2, the power unit 2 is installed under the airship body 1, and a bracket 3 is installed under the airship body 1; Device 2 is an oil-electric hybrid power device, including three propellers 21, 22, 23, of which two propellers 21, 22 are electric propellers, and one propeller 23 is powered by liquid fuel (such as gasoline, kerosene, hydrogen, etc.) Propellers; the three propellers 21, 22, 23 are arranged in an inverted triangle, wherein the electric propellers 21, 22 are horizontally arranged, and the liquid fuel powered propeller 23 is located behind the line connecting the two electric propellers 21, 22 and the The liquid fuel powered propeller 23 is located on the mid-perpendicular line between the two electric propellers 21, 22; the electric propellers 21, 22 each include two sub-propellers 211, 212, and the two sub-propellers 211, 212 are coaxially arranged; The rotating shafts of th...

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Abstract

The invention relates to the field of aviation, in particular to a petrol-electric hybrid power airship. The petrol-electric hybrid power airship comprises an airship body (1) and a power device (2), and the power device (2) is arranged below the airship body (1). The petrol-electric hybrid power airship is characterized in that the power device (2) is a petrol-electric hybrid power device and comprises three propellers (21, 22, 23), wherein two of the propellers (21, 22) are electric propellers, and one propeller (23) is liquid fuel power propeller. According to the petrol-electric hybrid power airship, the liquid fuel power propeller and the electric propellers are organically combined, so that control response of the airship in the aviation process can be rapidly achieved, and the flight posture is rapidly adjusted so that different aviation requirements can be met.

Description

technical field [0001] The invention relates to the field of aviation, and in particular to an oil-electric hybrid airship. Background technique [0002] At present, unmanned aerial vehicles are very popular and widely used due to their high controllability and flexible applications. They are widely used in industrial and agricultural applications such as homeland security, industry, agriculture, fire protection, forestry, and transportation. It has a huge potential application space, and its promotion and application prospects are very broad, and it has become a current research and development hotspot. However, most of the unmanned aerial vehicles in the prior art have the following disadvantages: short endurance, small load capacity, poor controllability and other shortcomings. The existence of these shortcomings has greatly restricted the wide industrial application of unmanned aerial vehicles. Contents of the invention [0003] In order to overcome at least one defec...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64B1/30
Inventor 伍鸿辉苏成悦肖佳栋朱留洲黄日恒许树琦林志聪施振华
Owner DONGGUAN SOUTH CHINA DESIGN INNOVATION INST
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