CN106043719A - Self-powered unmanned aerial vehicle - Google Patents
Self-powered unmanned aerial vehicle Download PDFInfo
- Publication number
- CN106043719A CN106043719A CN201610585975.4A CN201610585975A CN106043719A CN 106043719 A CN106043719 A CN 106043719A CN 201610585975 A CN201610585975 A CN 201610585975A CN 106043719 A CN106043719 A CN 106043719A
- Authority
- CN
- China
- Prior art keywords
- power supply
- aerial vehicle
- unmanned aerial
- unmanned plane
- fan blade
- 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.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/24—Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
Abstract
A self-powered unmanned aerial vehicle comprises a machine body, multiple machine arms disposed on the machine body, and a cover body matched with the machine body, wherein rotors are installed on the machine arms; and a fan blade device is disposed on the cover body and is in an axial connection with a power generation device, and the power generation device provides electricity for a storage battery of the unmanned aerial vehicle so as to implement independent power generation. The unmanned aerial vehicle has the advantages that the structure is simple; safety performance is good; manufacture cost is low; electricity charging can be implemented independently; flight duration can be prolonged; and the electricity charging can be effectively converted, and a battery life of the unmanned aerial vehicle can be increased. Hence, the unmanned aerial vehicle is a product superior in technologies, practicability and economic efficiency.
Description
[technical field]
The present invention relates to the unmanned plane of a kind of autologous power supply.
[background technology]
According to market survey, all employings electric energy of existing unmanned plane is driven, and consumes electricity relatively big during driving, as
What allows the energy of loss can add in accumulator with transform portion, is that user wishes to realize always, and existing unmanned
Machine can not realize autologous power supply, and flying power is not good enough.
In order to overcome above-mentioned problem, we have developed the unmanned plane of a kind of autologous power supply.
[summary of the invention]
Purpose of the present invention technical problem to be solved is intended to provide the unmanned plane of a kind of autologous power supply, its simple in construction, peace
Full performance is good, low cost of manufacture and autologous can realize charging, extends the time of flight, effectively converts charging and realize strengthening unmanned plane
Flying power.Therefore, it is technical, practicality and the product of the equal top grade of economy.
To achieve these goals, the technical solution used in the present invention: the unmanned plane of a kind of autologous power supply, it includes fuselage, sets
In multiple horns of fuselage, horn is equiped with rotor；It is matched with the lid of fuselage；Described lid is provided with fan blade device, wind
Leaf assembly axis sending and receiving electric installation, described TRT is that unmanned plane storage battery power supply is to form autologous power supply.
In one or more embodiments of the invention, the rotating shaft of described fan blade device is arranged at lid center of top.
In one or more embodiments of the invention, the core of described fan blade device is cylindricality, and its side arm is provided with multiple
Gathering sill.
In one or more embodiments of the invention, described fan blade device has multiple blades, and they equally spaced set
It is placed in the side of core.
In one or more embodiments of the invention, described lid has hemispherical surface.
The present invention is produced beneficial effect compared with background technology:
Owing to using above-mentioned technical scheme, its simple in construction, security performance are good, low cost of manufacture and autologous can realize charging,
Extend the time of flight, effectively convert charging and realize strengthening the flying power of unmanned plane.Therefore, it be technical, practicality and
The product of the equal top grade of economy.
[accompanying drawing explanation]
Fig. 1 is the structural representation of the unmanned plane of autologous power supply in one embodiment of the invention；
Fig. 2 is that the fuselage of the unmanned plane of autologous power supply in one embodiment of the invention dissects structural representation；
Fig. 3 is the theory structure schematic diagram of the TRT of autologous power supply in one embodiment of the invention.
[detailed description of the invention]
Embodiments of the invention are described below in detail, and described embodiment example is shown in the drawings, the most identical
Or similar label represents same or similar element or has the element of same or like function.
In describing the invention, it should be noted that for the noun of locality, if any term " " center ", " laterally ", " longitudinally ", " length
Degree ", " width ", " thickness ", " on ", D score, "front", "rear", "left", "right", " vertically ", " level ", " top ", " end ", " interior ",
The indicating position such as " outward ", " clockwise ", " counterclockwise " and position relationship are based on orientation shown in the drawings or position relationship, are only
For the ease of describing the present invention and simplifying description rather than instruction or imply that the device of indication or element must have specific side
Position, with particular orientation structure and operation, it is impossible to be interpreted as limit the present invention concrete protection domain.
Additionally, be only used for describing purpose if any term " first ", " second ", and it is not intended that indicate or hint relative importance
Or imply the quantity indicating technical characteristic.Thus, define " first ", " second " feature can be expressed or implicit include one
Or multiple this feature, in the present description, " at least " is meant that one or more, unless otherwise the most concrete
Limit.In the present invention, except as otherwise clear stipulaties and restriction, " assemble " if any term, broad sense should be made in " being connected ", " connection " term
Go to understand, connect for example, it may be fixing, it is also possible to be to removably connect, or be integrally connected；Can also be to be mechanically connected；
Can be to be joined directly together, it is also possible to be to be connected by intermediary, can be that two element internals are connected.General for this area
For logical technical staff, above-mentioned term concrete meaning in the present invention can be understood as the case may be.
In the present invention, unless otherwise prescribed and limit, fisrt feature second feature it " on " or D score can include the
One directly contacts with second feature, it is also possible to include that fisrt feature and second feature are not directly contact but by between them
Other characterisation contact.And, fisrt feature second feature " on ", " under " and " above " include that fisrt feature is second
Directly over feature and oblique upper, or be only the height representing fisrt feature level height higher than second feature.Fisrt feature exists
Second feature " on ", " under " and " below " include that fisrt feature immediately below second feature or obliquely downward, or is merely representative of
Fisrt feature level height is less than second feature.
Being incorporated into foregoing, those skilled in the art can carry out adaptive regulation and understanding, in the lump with reference to explanation
The accompanying drawing of book, by being further described the detailed description of the invention of the present invention, makes technical scheme and useful
Effect is clearer, clear and definite.It is exemplary for describing embodiment below with reference to accompanying drawing, it is intended to explain the present invention, and can not
It is interpreted as limitation of the present invention.
Refer to shown by Fig. 1-3, it provides preferably embodiment to be the unmanned plane of a kind of autologous power supply for the present invention,
It includes fuselage 1, is located at multiple horns 2 of fuselage 1, and horn 2 is equiped with rotor 3；It is matched with the lid 4 above fuselage 1；Institute
State lid 4 and be provided with fan blade device 5, fan blade device 51 axle sending and receiving electric installation 6, TRT 6 for unmanned plane accumulator 7 power with
Form autologous power supply.
The rotating shaft 51 of described fan blade device 5 is arranged at lid 4 center of top.The core 52 of described fan blade device 5 is cylindricality,
Its sidewall is provided with multiple gathering sill 53.Described fan blade device 5 has six blades 54, it is of course possible to be set to three or three with
On, they are equally spaced arranged at the side of core 52.Described lid 4 has hemispherical surface, it is also possible to for cambered surface etc.
Regular or irregular form.
During work, starting rotor 3 and rotate and make unmanned plane during flying, in flight course, fan blade device 5 is bullied the pressure effect of fluid
Rotating, fan blade device 5 drives electromotor 6 work generating, flows to accumulator 7 and powers, due to wind to control system 8 and motor 9
The rotating shaft 51 of leaf device 5 is arranged at lid 4 center of top, and such fan blade device 5 rotates the air-flow produced does not affects the side of aircraft
To manipulation stability, the effect of multiple gathering sills 53 is, can allow air-flow import formed autologous wind-guiding effectively reduce resistance and
Increase rotate time power, integral face say, its simple in construction, security performance are good, low cost of manufacture and can autologous realize charging, prolong
The time of long flight, effectively convert charging and realize strengthening the flying power of unmanned plane.Therefore, it is technical, practicality and warp
The product of the equal top grade of Ji property.
In the description of description, reference term " embodiment ", " preferably ", " example ", " concrete example " or " one
A little examples " etc. description means to combine this embodiment or example describes specific features, structure, material or feature, be contained in
In at least one embodiment of the present invention or example, the schematic representation for above-mentioned term not necessarily refers in this manual
It is identical embodiment or example.And, the specific features of description, structure, material or feature can at any one or
Multiple embodiments or example combine in a suitable manner.
By above-mentioned structure and the description of principle, person of ordinary skill in the field should be appreciated that the present invention not office
It is limited to above-mentioned detailed description of the invention, uses the improvement of techniques well known and replacement to all fall within this on the basis of the present invention
Bright protection domain, should be limited it by each claim.
Claims (5)
1. the unmanned plane of an autologous power supply, it is characterised in that it includes fuselage, is located at multiple horns of fuselage, horn fills
It is provided with rotor；It is matched with the lid of fuselage；Described lid is provided with fan blade device, fan blade device axle sending and receiving electric installation, described
Denso is set to unmanned plane storage battery power supply to form autologous power supply.
The unmanned plane of autologous power supply the most according to claim 1, it is characterised in that: the rotating shaft of described fan blade device is arranged at
Lid center of top.
The unmanned plane of autologous power supply the most according to claim 2, it is characterised in that: the core of described fan blade device is post
Shape, its sidewall is provided with multiple gathering sill.
The unmanned plane of autologous power supply the most according to claim 3, it is characterised in that: described fan blade device has multiple blades,
They are equally spaced arranged at the side of core.
The unmanned plane of autologous power supply the most according to claim 4, it is characterised in that: described lid has hemispherical table
Face.
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 true CN106043719A (en) | 2016-10-26 |
| CN106043719B CN106043719B (en) | 2023-08-29 |
Family
ID=57418444
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) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106741885A (en) * | 2016-11-23 | 2017-05-31 | 上海卫星工程研究所 | Using the autogyro and its application method of martian atmosphere circulation random probing |
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| 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 |
| US20150097071A1 (en) * | 2013-04-04 | 2015-04-09 | Sunlight Photonics Inc. | Airborne kinetic energy conversion system |
| 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 |
-
2016
- 2016-07-22 CN CN201610585975.4A patent/CN106043719B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20150097071A1 (en) * | 2013-04-04 | 2015-04-09 | Sunlight Photonics Inc. | Airborne kinetic energy conversion system |
| 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 |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106741885A (en) * | 2016-11-23 | 2017-05-31 | 上海卫星工程研究所 | Using the autogyro and its application method of martian atmosphere circulation random probing |
| 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 |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106043719B (en) | 2023-08-29 |
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| SE01 | Entry into force of request for substantive examination | ||
| CB02 | Change of applicant information | ||
| CB02 | Change of applicant information |
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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