CN104015915A - Unmanned gas saucer and manufacturing method thereof - Google Patents
Unmanned gas saucer and manufacturing method thereof Download PDFInfo
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- CN104015915A CN104015915A CN201410224204.3A CN201410224204A CN104015915A CN 104015915 A CN104015915 A CN 104015915A CN 201410224204 A CN201410224204 A CN 201410224204A CN 104015915 A CN104015915 A CN 104015915A
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Abstract
本发明公开了一种无人气碟及其制作方法，太阳能电池板附着于新型PVC薄膜材料轻质气囊上表面，气囊底面连接碳纤维拉力承受杆，碳纤维拉力承受杆顶端连接螺旋桨，中间连接处与太阳能稳压电源及缓存组相连，太阳能稳压电源及缓存组上安装有逆变器，太阳能稳压电源及缓存组下端连接起落架，动力方面，主要是由太阳能电池板和充有轻质气体的碟体两方面提供混合动力，达到了长航时的优势。本发明的优点是：（1）在高空无人侦测，无人精确侦测领域广泛应用，拥有非常广阔的市场前景和利用价值；（2）具有零排放太阳能驱动、良好的飞行性能、低成本、在晴天可长航时飞行作业、用途广泛等优点。
The invention discloses an unmanned dish and a manufacturing method thereof. A solar panel is attached to the upper surface of a lightweight airbag made of a new type of PVC film material. The bottom surface of the airbag is connected to a carbon fiber tension bearing rod. The stabilized power supply is connected to the cache group, and the inverter is installed on the solar stabilized power supply and the cache group, and the lower end of the solar stabilized power supply and the cache group is connected to the landing gear. The two sides of the disc body provide hybrid power, achieving the advantage of long endurance. The advantages of the present invention are: (1) widely used in high-altitude unmanned detection and unmanned precise detection, and has very broad market prospects and utilization value; (2) has zero-emission solar energy drive, good flight performance, low It has the advantages of low cost, long-lasting flight operation in sunny days, and wide range of uses.
Description
Technical field
The present invention relates to the utilization field of airborne aircraft, be specifically related to a kind of without popularity dish and preparation method thereof.
Background technology
Now, Global Aviation Industry carbon dioxide isothermal chamber gas purging amount, very important source of pollution are become, develop heliotechnics, to advance greatly the enforcement of national energy-saving reduction of discharging plan, domestic existing Helios, because the packaging technology on wing is immature, causes weight large, aeroperformance loss is serious, flight can not effectively realize long boat time.Based on the bottleneck problem of this unmanned vehicle research, test of many times is passed through by our team, find to adopt PVC lightweight material, adopt the lift-off dish body of the extremely strong hot suturing skill processing and manufacturing of leak tightness, and adopt new cleaning fuel as power resources, solar power and light gas auxiliary lifting are organically combined, the airmanship difficult problem such as while effectively having solved long boat, this lift-off dish body can be widely used in taking photo by plane for a long time, physical features exploration, fire alarm is danger in advance, and the low-latitude flyings such as meteorological survey, also can take and transmit; And can be widely used in agricultural, military affairs, urgent early warning, follow the trail of in high-altitude, meteorological observation, the wedding gauze kerchief aerophotography of daily life etc.
Summary of the invention
The object of the present invention is to provide a kind of without popularity dish, this without popularity dish outward appearance adopt saucer-like configuration, volume is little, quality is light, of many uses, flight provides basis when being essentially long boat.
The present invention is achieved like this, it comprises novel PVC membraneous material lightweight air bag, solar panel, alighting gear, inverter, screw propeller, sun-generated electric power voltage stabilizing and buffer memory group, carbon fiber pulling force bearing bar, it is characterized in that: solar panel is attached to novel PVC membraneous material lightweight air bag upper surface, novel PVC membraneous material lightweight air bag bottom surface connects carbon fiber pulling force bearing bar, carbon fiber pulling force bearing bar top connects screw propeller, described carbon fiber pulling force bearing bar is " ten " font, middle junction is connected with solar power constant voltage power suspply and buffer memory group, in solar power constant voltage power suspply and buffer memory group, inverter is installed, solar power constant voltage power suspply and buffer memory group lower end connect alighting gear, described screw propeller lower end is provided with motor, and combine the characteristic of solar powered aircraft and ascending balloon, cleaning new energy solar power and lighter-than-air gas lift are organically combined.
The saucer-like configuration that is easy to flight that adopts without popularity dish profile of the present invention, encapsulation adopts novel PVC membraneous material, and in conjunction with the novel encapsulated technique of independent research, air bag upper surface entirety is provided with solar panel; This design has improved structure strength-weight ratio on the one hand, has alleviated to greatest extent body weight, has optimized the integral structure of aircraft, can convert solar energy into electrical energy to greatest extent on the other hand, improves greatly the flying power of aircraft.
Of the present inventionly be full of light gas helium without popularity dish dish body inside, contained lighter-than-air gas helium provides rising power also to produce to have alleviated dish body overall weight, combine the characteristic of solar powered aircraft and ascending balloon, cleaning new energy solar power and lighter-than-air gas lift are organically combined, and by meeting the configuration design of flight dynamics principle, reduce to greatest extent flight resistance, flight while making the less power of multiaxis flying platform consumption realize long boat; Dish body has carried solar panel and multiaxis flying platform, and existing enough strength and stabilities are enough to again bear predetermined load; Dish is in meeting under force request in addition, and dish body has been expanded load weight to greatest extent, and its function, to hold multiple airborne equipment, has expanded field of application and field.
Screw propeller of the present invention is by gas dish take-off weight and flying speed requirement, and by adjusting multiaxis wheelbase, footpath, dish body hole, determines that dish body center-of-gravity position selects a set of efficient multiaxis engine installation to determine.
The hovered multiaxis flying platform that adopts efficient stable without popularity dish of the present invention, has realized vertical takeoff and landing, spot hover and stable control.
The present invention, aspect energy conversion efficiency, for improving transmission voltage, designs and has improved efficient power conversion combination, greatly improves the trans-utilization rate of solar power.
The present invention, aspect flight active force, works power consumption greatly in view of multiple motors simultaneously, goes out a set of efficient low energy consumption multiaxis power system, to improve the flying power of gas dish through Research on experiment design.
Of the present inventionly without popularity dish internal circuit control principle be: the electric current that solar panel produces obtains direct current (DC) by photoelectric conversion and enters controller, controller can mutually be exchanged direct current (DC) is stored in storage battery by charging and discharging, converting direct-current power into alternating-current power is entered to AC load with inverter, again alternating current is offered to brushless AC motor, thereby make motor rotation work; On the one hand, brushless electricity is adjusted the alternating-current voltage/AC voltage of controlling output according to the signal of receiver throttle channel, thereby controls the rotating speed of motor, the pulling force of propeller blades; By receiver, flight attitude and the direction of aircraft are controlled in the output of the electric current to steering wheel, voltage on the other hand, realize the effective control to aircraft by this two aspect.
Principle of work of the present invention is: the characteristic that combines solar powered aircraft and ascending balloon, cleaning new energy solar power and lighter-than-air gas lift are organically combined, and integrate four axle flying platforms, solar power provides continuation of the journey power, and light gas can provide part lift, offsets part and bears a heavy burden, reduce the power consumption of four axle flying platforms, radius flight far away while realizing long boat, four axle flying platforms can be realized spot hover awing, can carrying equipment system carry out correlated activation.
Advantage of the present invention is: (1) is unmanned detecting in high-altitude, and unmanned accurately detecting field widespread use, has boundless market outlook and value; (2) fine day there is zero-emission Driven by Solar Energy, good airworthiness, low cost, the operation of flying, the advantage such as of many uses in the time that can be grown boat.
Brief description of the drawings
Fig. 1 is structural representation of the present invention.
Fig. 2 is birds-eye view of the present invention.
Fig. 3 is internal circuit control principle of the present invention.
Fig. 4 is four axis platform constructional drawing of the present invention.
Inverter in the drawings, 1, novel PVC membraneous material lightweight air bag, 2, solar panel, 3, alighting gear, 4,, 5, screw propeller, 6, sun-generated electric power voltage stabilizing and buffer memory group, 7, carbon fiber pulling force bearing bar, 8, controller, 9, storage battery, 10, AC load, 11, motor.
Detailed description of the invention
As Fig. 1, Fig. 2, shown in Fig. 4, the present invention is achieved like this, it comprises novel PVC membraneous material lightweight air bag 1, solar panel 2, alighting gear 3, inverter 4, screw propeller 5, sun-generated electric power voltage stabilizing and buffer memory group 6, carbon fiber pulling force bearing bar 7, it is characterized in that: solar panel 2 is attached to novel PVC membraneous material lightweight air bag 1 upper surface, novel PVC membraneous material lightweight air bag 1 bottom surface connects carbon fiber pulling force bearing bar 7, carbon fiber pulling force bearing bar 7 tops connect screw propeller 5, described carbon fiber pulling force bearing bar 7 is " ten " font, middle junction is connected with solar power constant voltage power suspply and buffer memory group 6, in solar power constant voltage power suspply and buffer memory group 6, inverter 4 is installed, solar power constant voltage power suspply and buffer memory group 6 lower ends connect alighting gear 3, described screw propeller 5 lower ends are provided with motor 11.
As shown in Figure 3, of the present inventionly without popularity dish internal circuit control principle be: the electric current that solar panel 2 produces obtains direct current (DC) by photoelectric conversion and enters controller 8, controller 8 can mutually be exchanged direct current (DC) is stored in storage battery 9 by charging and discharging, converting direct-current power into alternating-current power is entered to AC load 10 with inverter 4, again alternating current is offered to brushless AC motor, thereby make motor rotation work; On the one hand, brushless electricity is adjusted the alternating-current voltage/AC voltage of controlling output according to the signal of receiver throttle channel, thereby controls the rotating speed of motor, the pulling force of propeller blades; By receiver, flight attitude and the direction of aircraft are controlled in the output of the electric current to steering wheel, voltage on the other hand, realize the effective control to aircraft by this two aspect.
Principle of work of the present invention is: the characteristic that combines solar powered aircraft and ascending balloon, cleaning new energy solar power and lighter-than-air gas lift are organically combined, and integrate four axle flying platforms, solar power provides continuation of the journey power, and light gas can provide part lift, offsets part and bears a heavy burden, reduce the power consumption of four axle flying platforms, radius flight far away while realizing long boat, four axle flying platforms can be realized spot hover awing, can carrying equipment system carry out correlated activation.
On four axle flying platforms of the present invention, four motors that are cross arrangement are installed, the distance of drive motor wheelbase geometric centre equates, when the lift that produces when diagonal angle diaxon is identical, just can ensure balance, can not tilt to either direction; And four a pair of forwards of motor, the mode of a pair of reversion makes the reactive torque balance around vertical axes direction rotation, ensure the stable of four axle courses, what motor adopted is constant force 4822,690 KV, the APC multiaxis oar of 16 cun, the dish body of gas dish, also to a certain extent for four axles provide lift, is realized long boat.
The arrangement mode that MK specifies four spindle motors as shown in Figure 4, front (A), rear (C), right (B), left (D), A, the rotation of C motor clockwise direction, B, D motor left-hand revolution; The rotating speed of four motors does corresponding variation can realize four axles, motion laterally, longitudinally, on vertical direction and yaw direction, in the time that four axles need to forwards move, B, D motor keeps rotating speed constant, A motor speed declines, and C motor speed rises, and the lift that now C motor produces is greater than the lift of A motor, four axles will tilt forward along geometric centre, and blade lift component longitudinally moves before driving four-axial; In the time that four axles want port to turn to, A, C motor speed rise, B, D motor speed decline, make anti-twisted distance left be greater than reactive torque to the right, four axles under the effect of anti-twisted distance to anticlockwise.
The thrusts that four oars produce, exceed or can realize lower than the gravity of four axles own time the motion of vertical direction rise and fall, realize hovering in the time that the lift of oar equates with the gravity of four axles itself; Four axles are combined into one by bindiny mechanism and gas dish dish body, in the time that four axles carry out various flare maneuver, be with the dish of taking offence to do identical action and complete a whole set of flight, without popularity dish, solar panel adds four axles, can follow-on mission when sunny more than 6 hours.
The above; be only the detailed description of the invention in the present invention, but protection scope of the present invention is not limited to this, any people who is familiar with this technology is in the disclosed technical scope of the present invention; the conversion that can expect easily or replacement, all should be encompassed in of the present invention comprise scope within.
Claims (5)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410224204.3A CN104015915A (en) | 2014-05-26 | 2014-05-26 | Unmanned gas saucer and manufacturing method thereof |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410224204.3A CN104015915A (en) | 2014-05-26 | 2014-05-26 | Unmanned gas saucer and manufacturing method thereof |
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| Publication Number | Publication Date |
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| CN104015915A true CN104015915A (en) | 2014-09-03 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201410224204.3A Pending CN104015915A (en) | 2014-05-26 | 2014-05-26 | Unmanned gas saucer and manufacturing method thereof |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104908955A (en) * | 2015-05-22 | 2015-09-16 | 中国科学院物理研究所 | Multi-shaft unmanned aerial vehicle |
| WO2017067412A1 (en) * | 2015-10-22 | 2017-04-27 | 深圳光启合众科技有限公司 | Multi-rotor aircraft |
| WO2017107781A1 (en) * | 2015-12-21 | 2017-06-29 | 深圳光启空间技术有限公司 | Multi-rotor air vehicle |
| CN110712736A (en) * | 2019-11-11 | 2020-01-21 | 青田极石航空科技有限公司 | A kind of aviation equipment counterweight adjustment equipment |
| CN111645854A (en) * | 2020-03-30 | 2020-09-11 | 上海交通大学医学院附属瑞金医院 | Unmanned aerial vehicle monitoring and sampling system for high-infectivity environment medical treatment |
| CN113377126A (en) * | 2021-05-31 | 2021-09-10 | 湖北君邦环境技术有限责任公司 | Site survey stationing point location generation method, device, equipment and storage medium |
-
2014
- 2014-05-26 CN CN201410224204.3A patent/CN104015915A/en active Pending
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104908955A (en) * | 2015-05-22 | 2015-09-16 | 中国科学院物理研究所 | Multi-shaft unmanned aerial vehicle |
| CN104908955B (en) * | 2015-05-22 | 2017-04-12 | 中国科学院物理研究所 | Multi-shaft unmanned aerial vehicle |
| WO2017067412A1 (en) * | 2015-10-22 | 2017-04-27 | 深圳光启合众科技有限公司 | Multi-rotor aircraft |
| CN106608350A (en) * | 2015-10-22 | 2017-05-03 | 深圳光启合众科技有限公司 | Multi-rotor type aircraft |
| CN106608350B (en) * | 2015-10-22 | 2024-03-15 | 深圳光启合众科技有限公司 | Multi-rotor aircraft |
| WO2017107781A1 (en) * | 2015-12-21 | 2017-06-29 | 深圳光启空间技术有限公司 | Multi-rotor air vehicle |
| CN110712736A (en) * | 2019-11-11 | 2020-01-21 | 青田极石航空科技有限公司 | A kind of aviation equipment counterweight adjustment equipment |
| CN110712736B (en) * | 2019-11-11 | 2020-10-27 | 青田极石航空科技有限公司 | Balancing weight adjusting equipment for aviation equipment |
| CN111645854A (en) * | 2020-03-30 | 2020-09-11 | 上海交通大学医学院附属瑞金医院 | Unmanned aerial vehicle monitoring and sampling system for high-infectivity environment medical treatment |
| CN111645854B (en) * | 2020-03-30 | 2022-04-15 | 上海交通大学医学院附属瑞金医院 | A UAV monitoring and sampling system for medical treatment of highly infectious environments |
| CN113377126A (en) * | 2021-05-31 | 2021-09-10 | 湖北君邦环境技术有限责任公司 | Site survey stationing point location generation method, device, equipment and storage medium |
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Application publication date: 20140903 |
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