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self-positioning solar vehicle

A solar energy and aircraft technology, applied in the field of aircraft, can solve the problems of increasing the overall weight of the aircraft, increasing the volume of the aircraft, etc., to save energy components, facilitate long distances, and ensure flexibility.

Active Publication Date: 2018-05-11
广东众恒科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] With the development of science and technology, the aircraft has been greatly improved; unmanned aerial vehicles have been promoted in many fields such as monitoring, exploration, entertainment, etc., and the aircraft must have good stability, light weight and sufficient power; Long-distance power transmission, therefore, the aircraft needs to carry enough energy during the flight. At present, the energy supply device of the aircraft occupies a large proportion of the overall weight of the aircraft; this not only increases the volume of the aircraft, but also improves the performance of the aircraft. overall weight; therefore, a light-weight, long-distance flying aircraft urgently needs to be promoted

Method used

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Embodiment

[0015] exist figure 1 , figure 2 In the illustrated embodiment, the self-positioning solar-powered aircraft includes a body 1, and propellers 11 are respectively arranged at the front end and the tail end of the body 1;

[0016] A rotating shaft 12 is fixed at the fuselage position of the body 1, and the rotating shaft 12 is installed at the center of gravity of the body 1; A group of connecting rings 21 are arranged parallel to the inner ring surface. On the rotating shaft 12, a connecting brush 121 is arranged at a position facing the connecting ring 21; the connecting ring 21 is electrically connected with the connecting brush 121;

[0017] A strut is installed in the radial direction of the energy supply ring 2, and a buoyancy disc 3 is fixed at the end of the strut; an auxiliary thrust fan 31 is also installed on the lower surface of the buoyancy disc 3, and the auxiliary thrust fan 31 is electrically Connected in the drive circuit; on the upper surface of the buoyancy...

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Abstract

The present invention relates to a self-positioning solar aircraft, comprising a body; a rotary shaft is fixed to a main part of the body and is sleeved with a power ring, a junction ring set is parallelly disposed in the inner annulus of the power ring, and a junction brush is disposed at the part of the rotary shaft right facing the junction rings; the power ring is radially fitted with a support rod, and a buoyant disc is fixed to an end of the support rod; the upper surface of the buoyant disc is symmetrically and rotationally fitted with photosensors and telescopic rods; each photosensor set is electrically connected into a drive circuit of the corresponding telescopic rod; the photosensors are also electrically connected to a control chip; the telescopic rods jointly support a solar absorbing panel; the solar absorbing panel is electrically connected with the junction rings; The aircraft is simple in structure, the whole weight of the aircraft is effectively reduced, and it is possible to provide consistent power for the aircraft and greatly improve the properties of the aircraft.

Description

technical field [0001] The invention relates to an aircraft, especially a solar-powered aircraft. Background technique [0002] With the development of science and technology, the aircraft has been greatly improved; unmanned aerial vehicles have been promoted in many fields such as monitoring, exploration, entertainment, etc., and the aircraft must have good stability, light weight and sufficient power; Long-distance power transmission, therefore, the aircraft needs to carry enough energy during the flight. At present, the energy supply device of the aircraft occupies a large proportion of the overall weight of the aircraft; this not only increases the volume of the aircraft, but also improves the performance of the aircraft. overall weight; therefore a light-weight, long-distance flying aircraft needs to be promoted urgently. Contents of the invention [0003] In view of the above problems, the present invention provides a self-positioning solar-powered aircraft, which h...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D27/24H02S10/40H02S20/32
CPCB64D27/24H02S10/40H02S20/32Y02E10/50Y02T50/40Y02T50/60
Inventor 屈金城胡波戴高山
Owner 广东众恒科技有限公司