CN104029820A - Solar flying saucer capable of flying for long time - Google Patents

Solar flying saucer capable of flying for long time Download PDF

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Publication number
CN104029820A
CN104029820A CN201410256723.8A CN201410256723A CN104029820A CN 104029820 A CN104029820 A CN 104029820A CN 201410256723 A CN201410256723 A CN 201410256723A CN 104029820 A CN104029820 A CN 104029820A
Authority
CN
China
Prior art keywords
flying
solar
empennage
motor
flying saucer
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
CN201410256723.8A
Other languages
Chinese (zh)
Inventor
徐洪寿
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.)
QINGDAO YUTAI NEW ENERGY SCIENCE AND TECHNOLOGY Co Ltd
Original Assignee
QINGDAO YUTAI NEW ENERGY SCIENCE AND TECHNOLOGY 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 QINGDAO YUTAI NEW ENERGY SCIENCE AND TECHNOLOGY Co Ltd filed Critical QINGDAO YUTAI NEW ENERGY SCIENCE AND TECHNOLOGY Co Ltd
Priority to CN201410256723.8A priority Critical patent/CN104029820A/en
Publication of CN104029820A publication Critical patent/CN104029820A/en
Pending legal-status Critical Current

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Abstract

The invention discloses a solar flying saucer capable of flying for a long time. A thin solar battery component is arranged on the upper surface of a carrying plate with a symmetric structure; one end of the carrying plate is connected with an auxiliary wing, and the other end of the carrying plate is connected with an empennage; the thin solar battery component is connected with a storage battery; the storage battery is connected with a controller; the controller is connected with a signal transceiver, shooting detection equipment and a motor respectively; the motor is connected with the auxiliary wing and the empennage. The solar flying saucer has the technical effects that solar energy supplies a power source, the structure is simple, and the solar flying saucer is convenient to carry and practical.

Description

A kind of solar power flying saucer that can flying for long time
Technical field
The present invention relates to a kind of solar powered aircraft, relate in particular to a kind of solar power flying saucer that can flying for long time.
Background technology
At present, conventionally adopt that the aircraft such as helicopter, fire balloon, dirigible are taken photo by plane, explore, investigate, surveyed and drawn, meteorological, environmental protection on market, but it all exists the shortcoming that can not fly for a long time aloft, use cost is high.
Summary of the invention
The object of the present invention is to provide a kind of solar power flying saucer that can flying for long time, this solar power flying saucer has zero-emission Driven by Solar Energy, good airworthiness, low cost, the operation of flying when fine day can be grown boat, the advantage such as of many uses.
The present invention is achieved like this, it comprises support plate, thin solar module, aileron, empennage, storage battery, controller, signal receiving-transmitting device, shot detection equipment, motor, the upper surface that it is characterized in that the support plate of symmetrical configuration is provided with thin solar module, one end of support plate is connected with aileron, the other end of support plate is connected with empennage, described thin solar module connects storage battery, storage battery connects controller, controller connects respectively signal receiving-transmitting device, shot detection equipment and motor, and motor connects respectively aileron and empennage.
Technique effect of the present invention is: rely on solar power that power source is provided, knot simple structure, practicality easy to carry.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention
Fig. 2 is functional-block diagram of the present invention
Support plate 2, thin solar module 3, aileron 4, empennage 5, storage battery 6, controller 7, signal receiving-transmitting device 8, shot detection equipment 9, motor in the drawings, 1.
The specific embodiment
As shown in Figure 1 and Figure 2, the present invention is achieved like this, the upper surface of the support plate 1 of symmetrical configuration is provided with thin solar module 2, one end of support plate 1 is connected with aileron 3, the other end of support plate 1 is connected with empennage 4, and described thin solar module 2 connects storage battery 5, and storage battery 5 connects controller 6, controller 6 connects respectively signal receiving-transmitting device 7, shot detection equipment 8 and motor 9, and motor 9 connects respectively aileron 3 and empennage 4.Utilizing frivolous solar module to accept solar energy generates electricity and supplies with flying saucer motor and make screw propeller rotation produce flying power flying saucer is aloft flown, and by the rotation that empennage is controlled on ground, control flying saucer heading, on flying saucer take photo by plane and miscellaneous equipment can be taken photo by plane, makes a video recording, investigated, exploration etc.
Principle of work: accept solar energy by solar module and generate electricity, and charge and power to flying saucer motor to energy-storage travelling wave tube, making the rotation of driven by motor screw propeller produce flying power flies flying saucer aloft, and by the rotation that empennage is controlled on ground, control flying saucer heading, on flying saucer take photo by plane and miscellaneous equipment can be taken photo by plane, makes a video recording, investigated, exploration etc.

Claims (1)

  1. One kind can flying for long time solar power flying saucer, it comprises support plate, thin solar module, aileron, empennage, storage battery, controller, signal receiving-transmitting device, shot detection equipment, motor, the upper surface that it is characterized in that the support plate of symmetrical configuration is provided with thin solar module, one end of support plate is connected with aileron, the other end of support plate is connected with empennage, described thin solar module connects storage battery, storage battery connects controller, controller connects respectively signal receiving-transmitting device, shot detection equipment and motor, and motor connects respectively aileron and empennage.
CN201410256723.8A 2014-06-11 2014-06-11 Solar flying saucer capable of flying for long time Pending CN104029820A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410256723.8A CN104029820A (en) 2014-06-11 2014-06-11 Solar flying saucer capable of flying for long time

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410256723.8A CN104029820A (en) 2014-06-11 2014-06-11 Solar flying saucer capable of flying for long time

Publications (1)

Publication Number Publication Date
CN104029820A true CN104029820A (en) 2014-09-10

Family

ID=51460873

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410256723.8A Pending CN104029820A (en) 2014-06-11 2014-06-11 Solar flying saucer capable of flying for long time

Country Status (1)

Country Link
CN (1) CN104029820A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2585245A1 (en) * 2016-03-23 2016-10-04 Manuel Torres Martinez Low load aircraft alar (Machine-translation by Google Translate, not legally binding)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2585245A1 (en) * 2016-03-23 2016-10-04 Manuel Torres Martinez Low load aircraft alar (Machine-translation by Google Translate, not legally binding)

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WD01 Invention patent application deemed withdrawn after publication
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20140910