CN106043719B - Unmanned aerial vehicle of autologous power supply - Google Patents
Unmanned aerial vehicle of autologous power supply Download PDFInfo
- Publication number
- CN106043719B CN106043719B CN201610585975.4A CN201610585975A CN106043719B CN 106043719 B CN106043719 B CN 106043719B CN 201610585975 A CN201610585975 A CN 201610585975A CN 106043719 B CN106043719 B CN 106043719B
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- CN
- China
- Prior art keywords
- aerial vehicle
- unmanned aerial
- fan blade
- power supply
- cover body
- 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.)
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- 238000010248 power generation Methods 0.000 claims abstract description 9
- 238000004519 manufacturing process Methods 0.000 abstract description 4
- 238000010586 diagram Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 230000002035 prolonged effect Effects 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D41/00—Power installations for auxiliary purposes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
An unmanned aerial vehicle with self power supply comprises a body and a plurality of arms arranged on the body, wherein a rotor wing is arranged on each arm; a cover body matched with the machine body; the cover body is provided with a fan blade device, the fan blade device is connected with a power generation device in a shaft way, and the power generation device supplies power for the unmanned aerial vehicle storage battery to form self power supply. The unmanned aerial vehicle charging device is simple in structure, good in safety performance, low in manufacturing cost, capable of realizing charging by itself, capable of prolonging flight time, and capable of effectively converting charging to enhance endurance of the unmanned aerial vehicle. Therefore, it is a product with excellent technical, practical and economical properties.
Description
[ field of technology ]
The invention relates to an unmanned aerial vehicle with self power supply.
[ background Art ]
According to market research, current unmanned aerial vehicle all adopts the electric energy to drive, and at driven in-process consumption electric quantity great, how to let the energy of loss can partly supply to the battery, is that the user hopes to realize always, and current unmanned aerial vehicle can not realize the autologous power supply, and the duration is not good enough.
In order to overcome the problems, we have developed an unmanned aerial vehicle which is self-powered.
[ invention ]
The invention aims to solve the technical problem of providing an unmanned aerial vehicle with self power supply, which has the advantages of simple structure, good safety performance, low manufacturing cost and capability of realizing self charging, prolonging the flight time and effectively converting the charging to realize the enhancement of the cruising ability of the unmanned aerial vehicle. Therefore, it is a product with excellent technical, practical and economical properties.
In order to achieve the above purpose, the present invention adopts the following technical scheme: an unmanned aerial vehicle with self power supply comprises a body and a plurality of arms arranged on the body, wherein a rotor wing is arranged on each arm; a cover body matched with the machine body; the cover body is provided with a fan blade device, the fan blade device is connected with a power generation device in a shaft way, and the power generation device supplies power for the unmanned aerial vehicle storage battery to form self power supply.
In one or more embodiments of the present invention, the rotating shaft of the fan blade device is disposed at the top center of the cover body.
In one or more embodiments of the present invention, the core of the fan blade device is cylindrical, and the side arm thereof is provided with a plurality of guide grooves.
In one or more embodiments of the present invention, the fan blade device has a plurality of blades, they are arranged equidistantly spaced on the side of the core.
In one or more embodiments of the invention, the cover has a hemispherical surface.
Compared with the background technology, the invention has the beneficial effects that:
by adopting the technical scheme, the unmanned aerial vehicle has the advantages of simple structure, good safety performance, low manufacturing cost, capability of realizing self-charging, prolonged flight time, and capability of effectively converting charging to enhance the cruising ability of the unmanned aerial vehicle. Therefore, it is a product with excellent technical, practical and economical properties.
[ description of the drawings ]
FIG. 1 is a schematic diagram of a self-powered unmanned aerial vehicle according to an embodiment of the present invention;
FIG. 2 is a schematic diagram of a fuselage profile of a self-powered unmanned aerial vehicle according to an embodiment of the present invention;
fig. 3 is a schematic structural diagram of a self-powered power generation device according to an embodiment of the present invention.
[ detailed description ] of the invention
Embodiments of the present invention are described in detail below, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to like or similar elements or elements having like or similar functions throughout.
In the description of the present invention, it should be noted that, for the azimuth words such as "center", "lateral", "longitudinal", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", etc., the azimuth and positional relationships are based on the azimuth or positional relationships shown in the drawings, it is merely for convenience of describing the present invention and simplifying the description, and it is not to be construed as limiting the specific scope of protection of the present invention that the device or element referred to must have a specific azimuth configuration and operation.
Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features. Thus, the definition of "a first", "a second" feature may explicitly or implicitly include one or more of such features, and in the description of the invention, "at least" means one or more, unless clearly specifically defined otherwise. In the present invention, unless explicitly stated and limited otherwise, the terms "assembled," "connected," and "connected" are to be construed broadly, e.g., as being either fixedly connected, detachably connected, or integrally connected; or may be a mechanical connection; can be directly connected or connected through an intermediate medium, and can be communicated with the inside of the two elements. The specific meaning of the above terms in the present invention can be understood by those of ordinary skill in the art according to the specific circumstances.
In the present invention, unless specified and limited otherwise, a first feature "above" or "below" a second feature may include both the first and second features being in direct contact, as well as the first and second features not being in direct contact but being in contact with each other through additional features therebetween. Moreover, a first feature being "above," "below," and "above" a second feature includes the first feature being directly above and obliquely above the second feature, or simply representing the first feature as having a higher level than the second feature. The first feature being "above," "below," and "beneath" the second feature includes the first feature being directly below or obliquely below the second feature, or simply indicating that the first feature is level below the second feature.
In view of the foregoing, those skilled in the art will appreciate and understand that, together with the drawings accompanying the specification, by further describing the specific embodiments of the invention, the technical scheme and the beneficial effects of the invention are clearer and more definite. The embodiments described below are exemplary by referring to the drawings for the purpose of illustrating the invention and are not to be construed as limiting the invention.
Referring to fig. 1-3, a preferred embodiment of the present invention is an unmanned aerial vehicle with self-powered, which comprises a body 1, a plurality of arms 2 arranged on the body 1, wherein a rotor 3 is arranged on the arms 2; a cover 4 fitted over the body 1; the cover body 4 is provided with a fan blade device 5, the fan blade device 51 is connected with a power generation device 6 in a shaft mode, and the power generation device 6 supplies power for the unmanned aerial vehicle storage battery 7 to form self power supply.
The rotating shaft 51 of the fan blade device 5 is arranged at the center of the top of the cover body 4. The core 52 of the fan blade device 5 is cylindrical, and a plurality of guide grooves 53 are formed in the side wall of the core. The fan blade unit 5 has six blades 54, and may be three or more, which are disposed at equidistant intervals on the side of the core 52. The cover body 4 has a hemispherical surface, and may have a regular or irregular shape such as an arc surface.
During operation, the rotor 3 is started to rotate to enable the unmanned aerial vehicle to fly, the fan blade device 5 is rotated under the pressure action of air fluid in the flying process, the fan blade device 5 drives the generator 6 to work to generate electricity, the power is supplied to the storage battery 7 to the control system 8 and the motor 9, because the rotating shaft 51 of the fan blade device 5 is arranged at the center of the top of the cover body 4, the air flow generated by rotation of the fan blade device 5 does not influence the stability of the direction control of the aircraft, the effect of the guide grooves 53 is that the air flow can be led in to form the self-air-guiding to effectively reduce the resistance and increase the power in rotation, and the unmanned aerial vehicle has the advantages of simple structure, good safety performance, low manufacturing cost, self realization of charging, prolonged flying time, effective conversion of charging and realization of enhancing the endurance of the unmanned aerial vehicle. Therefore, it is a product with excellent technical, practical and economical properties.
In the description of the present invention, a description of the terms "one embodiment," "preferred," "example," "specific example," or "some examples," etc., means that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention, and a schematic representation of the terms described above in the present specification does not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
From the above description of the structure and principles, it should be understood by those skilled in the art that the present invention is not limited to the above-described embodiments, but rather that modifications and substitutions using known techniques in the art on the basis of the present invention fall within the scope of the present invention, which is defined by the appended claims.
Claims (3)
1. The unmanned aerial vehicle is characterized by comprising a body and a plurality of arms arranged on the body, wherein a rotor wing is arranged on each arm; a cover body matched with the machine body; the cover body is provided with a fan blade device which is connected with a power generation device in a shaft way, and the power generation device supplies power for the unmanned aerial vehicle storage battery to form self power supply; the rotating shaft of the fan blade device is arranged in the center of the top of the cover body; the core of fan blade device is cylindricality, and its lateral wall is equipped with a plurality of guide slots.
2. The self-powered drone of claim 1, wherein: the fan blade device is provided with a plurality of blades which are equidistantly arranged on the side face of the core part.
3. The self-powered drone of claim 2, wherein: the cover body is provided with a hemispherical surface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610585975.4A CN106043719B (en) | 2016-07-22 | 2016-07-22 | Unmanned aerial vehicle of autologous power supply |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610585975.4A CN106043719B (en) | 2016-07-22 | 2016-07-22 | Unmanned aerial vehicle of autologous power supply |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106043719A CN106043719A (en) | 2016-10-26 |
| CN106043719B true CN106043719B (en) | 2023-08-29 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610585975.4A Active CN106043719B (en) | 2016-07-22 | 2016-07-22 | Unmanned aerial vehicle of autologous power supply |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106043719B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106741885B (en) * | 2016-11-23 | 2019-08-23 | 上海卫星工程研究所 | Utilize the autogyro and its application method of martian atmosphere circulation random probing |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103523236A (en) * | 2013-10-25 | 2014-01-22 | 苏州艾锐泰克无人飞行器科技有限公司 | Unmanned aerial vehicle wind energy recycling device |
| CN204660029U (en) * | 2015-05-22 | 2015-09-23 | 北京汉能光伏投资有限公司 | A kind of unmanned plane |
| CN204776037U (en) * | 2015-06-19 | 2015-11-18 | 沈全贵 | Solar powered aircraft |
| CN204956939U (en) * | 2015-08-05 | 2016-01-13 | 深圳市顶逸创新科技有限公司 | Unmanned aerial vehicle's mechanical motion battery charging configuration |
| CN105253307A (en) * | 2015-10-21 | 2016-01-20 | 黄彰标 | Unmanned aerial vehicle with fly-back charging function |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10040561B2 (en) * | 2013-04-04 | 2018-08-07 | Sunlight Photonics Inc. | Airborne kinetic energy conversion system |
-
2016
- 2016-07-22 CN CN201610585975.4A patent/CN106043719B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103523236A (en) * | 2013-10-25 | 2014-01-22 | 苏州艾锐泰克无人飞行器科技有限公司 | Unmanned aerial vehicle wind energy recycling device |
| CN204660029U (en) * | 2015-05-22 | 2015-09-23 | 北京汉能光伏投资有限公司 | A kind of unmanned plane |
| CN204776037U (en) * | 2015-06-19 | 2015-11-18 | 沈全贵 | Solar powered aircraft |
| CN204956939U (en) * | 2015-08-05 | 2016-01-13 | 深圳市顶逸创新科技有限公司 | Unmanned aerial vehicle's mechanical motion battery charging configuration |
| CN105253307A (en) * | 2015-10-21 | 2016-01-20 | 黄彰标 | Unmanned aerial vehicle with fly-back charging function |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106043719A (en) | 2016-10-26 |
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Address after: 519000 Guangdong city of Zhuhai province Pingsha Town New Road No. 305 building a building area of A Applicant after: ZHUHAI YINTONG UAV TECHNOLOGY CO.,LTD. Address before: 519000 Guangdong city of Zhuhai province Pingsha Town New Road No. 305 building a building area of A Applicant before: ZHUHAI YINTONG AGRICULTURAL SCIENCE AND TECHNOLOGY Co.,Ltd. |
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