CN102152854A - Solar thin film cell unmanned aerial vehicle - Google Patents

Solar thin film cell unmanned aerial vehicle Download PDF

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Publication number
CN102152854A
CN102152854A CN2011101216762A CN201110121676A CN102152854A CN 102152854 A CN102152854 A CN 102152854A CN 2011101216762 A CN2011101216762 A CN 2011101216762A CN 201110121676 A CN201110121676 A CN 201110121676A CN 102152854 A CN102152854 A CN 102152854A
Authority
CN
China
Prior art keywords
thin film
aerial vehicle
unmanned aerial
solar thin
film cell
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN2011101216762A
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Chinese (zh)
Inventor
吴德滨
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
HARBIN KAIEN TECHNOLOGY DEVELOPMENT Co Ltd
Original Assignee
HARBIN KAIEN TECHNOLOGY DEVELOPMENT Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by HARBIN KAIEN TECHNOLOGY DEVELOPMENT Co Ltd filed Critical HARBIN KAIEN TECHNOLOGY DEVELOPMENT Co Ltd
Priority to CN2011101216762A priority Critical patent/CN102152854A/en
Publication of CN102152854A publication Critical patent/CN102152854A/en
Pending legal-status Critical Current

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Abstract

The invention belongs to a solar thin film cell unmanned aerial vehicle. A cabin and a wing framework are arranged on the unmanned aerial vehicle. A light material is covered on the lower surface of the framework. A solar thin film cell is covered on the upper surface of the framework. Navigation and remote control equipment, a large energy-saving fuel storage cell and a strong permanent magnet electric motor are arranged in the cabin. The tail part of the unmanned aerial vehicle is provided with a propeller. Guided missiles are hung below wings. The solar thin film cell unmanned aerial vehicle does not need other energy resources and patrols and flies in the air day and night. The electric motor has small rotating sound. No infrared rays are generated. The solar thin film cell can adsorb electromagnetic waves, thereby having good concealment property. The solar thin film cell unmanned aerial vehicle has low manufacturing and using costs. The aircraft creates the future development direction.

Description

The solar film battery unmanned plane
Technical field: the present invention relates to a kind of solar film battery unmanned plane.
Background technology: present unmanned plane all is to adopt fuel oil, or rechargeable unmanned plane, and this unmanned plane need replenish the energy, can not aloft fly for a long time.
Summary of the invention: study a kind of energy that do not need to replenish, aloft the light-duty unmanned plane of permanent patrol aviation day and night.
Technical scheme: do the cabin and the wing skeleton of a unmanned plane, cover light material below the skeleton, cover solar film battery above the skeleton, navigation and telecommand equipment are installed, big energy storage fuel storage battery, strong permanent magnetic electrical motor in the cabin, hang guided missile below the afterbody installation screw propeller, wing.
Description of drawings: Fig. 1 is a solar film battery unmanned plane birds-eye view.
Fig. 2 is a solar film battery unmanned plane lateral plan.
Fig. 3 is a solar film battery unmanned plane section-drawing.
Among the figure, the 1-cabin; The 2-wing; The 3-solar film battery; The 4-light material; The 5-screw propeller; The 6-skeleton; 7-navigation and telecommand equipment; The 8-storage battery; The 9-electrical motor; The 10-guided missile.
The specific embodiment: the cabin of doing a unmanned plane 1. with wing skeleton 2. 6., skeleton following covering light material 6. 4., skeleton top covering solar film battery 4. 6., conventional solar cells is plating one deck metal solar film on glass board, change degree one deck metal solar film on plastic sheeting or canvas now into, this technology is fairly simple, can operate, and abroad produces.In the cabin device navigation and telecommand equipment 7., big energy storage fuel storage battery 8., present bus is brought into use, fills once electricity and travels a plurality of hours.The strong permanent magnetic electrical motor 9., this electrical motor power consumption is few especially, 5. cabin afterbody 1. installs screw propeller, wing following suspension guided missile 2. is 10..
When beginning to take off, storage battery is charging earlier 2., and unmanned plane flies in the air, 3. solar film battery is subjected to the illumination effect to produce electric current, and the area design of wing is bigger, and the electric current of generation is many, 8. electric current accumulators on the one hand charges, and satisfies night flying, uses for unmanned plane during flying on the one hand.
Beneficial effect: 1, do not need to replenish the energy, day and night aloft, especially in the coastal area patrol aviation; 2, motor rotation sound is little; 3, motor rotates and does not produce infrared ray; 4, solar energy hull cell energy electromagnetic wave absorption, hidden performance is good; 5, manufacturing cost and use cost is low, and this aircraft is following developing direction.

Claims (1)

1. solar film battery unmanned plane, it is characterized in that: cabin and the wing skeleton of doing a unmanned plane, cover light material below the skeleton, cover solar film battery above the skeleton, navigation and telecommand equipment are installed in the cabin, hang guided missile below big energy storage fuel storage battery, the strong permanent magnetic electrical motor, afterbody installation screw propeller, wing.
CN2011101216762A 2011-05-12 2011-05-12 Solar thin film cell unmanned aerial vehicle Pending CN102152854A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2011101216762A CN102152854A (en) 2011-05-12 2011-05-12 Solar thin film cell unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2011101216762A CN102152854A (en) 2011-05-12 2011-05-12 Solar thin film cell unmanned aerial vehicle

Publications (1)

Publication Number Publication Date
CN102152854A true CN102152854A (en) 2011-08-17

Family

ID=44434609

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2011101216762A Pending CN102152854A (en) 2011-05-12 2011-05-12 Solar thin film cell unmanned aerial vehicle

Country Status (1)

Country Link
CN (1) CN102152854A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102424107A (en) * 2011-09-29 2012-04-25 北京航空航天大学 Manufacture method of solar airplane
CN102837826A (en) * 2012-10-02 2012-12-26 李万红 Solar unmanned aerial vehicle

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102424107A (en) * 2011-09-29 2012-04-25 北京航空航天大学 Manufacture method of solar airplane
CN102424107B (en) * 2011-09-29 2013-11-27 北京航空航天大学 Manufacture method of solar airplane
CN102837826A (en) * 2012-10-02 2012-12-26 李万红 Solar unmanned aerial vehicle
CN102837826B (en) * 2012-10-02 2014-08-20 李万红 Solar unmanned aerial vehicle

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Legal Events

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C06 Publication
PB01 Publication
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20110817