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Solar unmanned aerial vehicle

A solar-powered unmanned aerial vehicle and solar energy technology, applied in the field of unmanned aerial vehicles, can solve the problems of increased weight of unmanned aerial vehicles

Inactive Publication Date: 2014-08-20
宁波市科技园区绿牌软包装技术贸易有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, as the area that absorbs sunlight increases, the weight of the UAV will also increase, which is an unavoidable solution

Method used

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Embodiment Construction

[0026] The present invention will be described in detail below in conjunction with the accompanying drawings.

[0027] attached figure 1 The marking names are: short-range radar (01), equipment compartment (02), airframe (03), long-range radar (04), tracking solar system (05), transparent delta wing (06), empennage (07) and propeller (08).

[0028] attached figure 2 The mark names are: slider and chute (1), pneumatic valve A (2), "L" frame A (3), rotary joint (4), bearing housing (5), double-connected pneumatic valve B (6 ), push rod A (7), upper pillar (8), helical gear (9), push rod B (10), "L" frame B (11), bearing (12), mounting ring seat (13), push Bar C (14), cross bracket (15), connecting bolt (16), daylighting plate (17), lower pillar (18), pillar seat bolt (19), pillar seat (20).

[0029] attached Figure 7 The marking names are: lower valve body (21), liquid nozzle in the rear chamber (22), mounting screw hole (23), sealing ring A (24), square guide post (25), ...

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Abstract

The invention belongs to the field of an unmanned aerial vehicle and especially relates to a solar unmanned aerial vehicle suitable for early warning of an aircraft carrier. The solar unmanned aerial vehicle comprises a short-range radar (01), an equipment cabin (02), a vehicle body (03), a long-range radar (04), a tracking type solar energy system (05), a transparent delta wing (06), an empennage (07) and a propeller (08), wherein a power system, an early warning system, a communication system and a built-in weapon system are arranged in the equipment cabin (02); the arrangement of the transparent delta wing is adopted by the solar unmanned aerial vehicle, so that a daylighting area as big as possible is obtained; the tracking type solar energy system comprises a pneumatic valve (2), a duplex pneumatic valve B (6) and a daylighting panel (17); the daylighting panel (17) is driven by the pneumatic valve A (2) and the duplex pneumatic valve B (6) and a central axis of the daylighting panel (17) is adjusted to be parallel to a sunlight axis in real time; and the daylighting panel (17) is mounted in the transparent delta wing (06) in decentralized and rotary mode, so that the sunlight axis is tracked in real time and the solar energy conversion rate above 50% is obtained.

Description

technical field [0001] The invention belongs to the field of unmanned aerial vehicles, and is especially suitable for solar-powered unmanned aerial vehicles for early warning of aircraft carriers. Background technique [0002] Solar aircraft is an aircraft that uses solar radiation as the propulsion energy. Solar-powered aircraft came out in the 1970s, when there were only miniature models. In 1980, the United States developed the "Sun Challenger" single-seat solar-powered aircraft. This aircraft successfully flew from Paris to the UK in July 1981, with an average speed of 54 kilometers per hour. meters, with a range of 290 kilometers; until 2007, the solar-powered drone named "Zephyr-6" (zephyr-6) developed by the United Kingdom set the first night flight record by staying in the air for more than 3 days. In 2002, a Chinese solar-powered unmanned aircraft exploration and development program called "Green Pioneer" was officially launched, marking a new breakthrough in the d...

Claims

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Application Information

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IPC IPC(8): B64D27/24
Inventor 李万红李正
Owner 宁波市科技园区绿牌软包装技术贸易有限公司
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