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Daytime climbing flight method for reducing weight and size of solar unmanned aerial vehicle

A solar unmanned aerial vehicle, solar energy technology, applied in unmanned aerial vehicles, solar panel accessories, weight reduction and other directions, can solve the limitation of the expansion of the load capacity of the solar unmanned aerial vehicle, the flight performance, and the energy density consumption of the secondary power supply The problems of large manpower, financial resources and time, and low energy density of the secondary power system have achieved the effect of improving the wind resistance and structural strength, making it difficult to realize and difficult to manufacture.

Active Publication Date: 2017-02-15
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At the current level of technology, the energy density of the secondary power supply system is low, and the secondary power supply that meets the needs of night flight is relatively heavy, accounting for more than 35% of the weight of the whole aircraft, which seriously limits the load capacity of solar-powered UAVs. Expansion and improvement of flight performance
The improvement of the energy density of the secondary power supply requires a lot of manpower, financial resources and time, and it is difficult to achieve a major breakthrough in the short term.

Method used

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  • Daytime climbing flight method for reducing weight and size of solar unmanned aerial vehicle
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  • Daytime climbing flight method for reducing weight and size of solar unmanned aerial vehicle

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Embodiment

[0020] Design requirements: the flight time is between the vernal equinox and the autumnal equinox, the flight latitude is 35°north latitude, the minimum cruising altitude is 18km, the mission load power is 2kw, the load weight is 100kg, and the cruise lift-to-drag ratio is 30.

[0021] For a solar-powered UAV cruising at a fixed altitude of 18km, in order to meet the above design requirements, it needs a wing area of ​​344㎡, a length of 101.6m, and a total weight of 2030kg, of which the weight of the secondary power supply is 854kg. Under the same design input, the higher the fixed altitude cruising altitude, the larger the size and weight of the UAV required. Taking the 19km fixed altitude cruising as an example, the solar drone needs a wing area of ​​474㎡ and a length of 119.2 m, with a total weight of 2711kg, of which the weight of the secondary power supply is 1176kg.

[0022] And adopt the flight strategy of climbing and descending again before sunset described in the pr...

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Abstract

The invention discloses a daytime climbing flight method for reducing the weight and size of a solar unmanned aerial vehicle, and belongs to the field of design of air vehicles. The daytime climbing flight method for reducing the weight and size of the solar unmanned aerial vehicle comprises the steps that with 24 hours as a cycle, the solar unmanned aerial vehicle cruises at a normal cruising altitude from the sunrise moment t1 to the time when a secondary power supply is fully charged; from the moment when the secondary power supply is fully charged, residual solar energy is fully used by the unmanned aerial vehicle for climbing flight; the unmanned aerial vehicle starts to descend with power after climbing to the specific altitude, and the unmanned aerial vehicle starts to slide downwards without power from the moment when the secondary power supply starts to participate in power supply till the unmanned aerial vehicle slides downwards to the normal cruising altitude; and the unmanned aerial vehicle cruises all over the night in a constant-altitude mode at the normal cruising altitude by means of energy provided by the secondary power supply till the sunrise moment of the next day, the circulating cycle of one day is ended, and the next cycle is started. According to the daytime climbing flight method for reducing the weight and size of the solar unmanned aerial vehicle, the flight strategy that the solar unmanned aerial vehicle climbs after noon and then falls, so that the energy demand for the secondary power supply is reduced, the weight of the secondary power supply is reduced to a certain extent, the weight and size of the solar unmanned aerial vehicle are reduced accordingly, and the feasibility of the scheme is improved.

Description

technical field [0001] The invention belongs to the field of aircraft design, and relates to a scheme design of a solar-powered drone, in particular to a daytime climbing flight strategy capable of reducing the design weight of a solar-powered drone, reducing its design size, and improving the feasibility of the scheme. Background technique [0002] A solar-powered drone is an unmanned aerial vehicle that uses solar radiation as propulsion energy. During the day, rely on the photovoltaic cells laid on the surface of the wing and tail to convert solar energy into electrical energy, maintain the operation of the power system, avionics equipment and payload, and use the remaining energy to charge the airborne secondary power supply; at night, use the secondary The energy stored in the power supply maintains the normal operation of the entire drone. If the energy stored during the day can meet the needs of the night, solar-powered drones can theoretically achieve permanent air ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/02B64D41/00
CPCB64C39/02B64D41/00B64U50/19B64D27/353Y02T50/40
Inventor 马东立王少奇杨穆清张良李冠雄
Owner BEIHANG UNIV
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