CN207346091U - A kind of six rotor wing unmanned aerial vehicle system of long endurance - Google Patents
A kind of six rotor wing unmanned aerial vehicle system of long endurance Download PDFInfo
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- CN207346091U CN207346091U CN201721339837.4U CN201721339837U CN207346091U CN 207346091 U CN207346091 U CN 207346091U CN 201721339837 U CN201721339837 U CN 201721339837U CN 207346091 U CN207346091 U CN 207346091U
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Abstract
The utility model discloses a kind of long six rotor wing unmanned aerial vehicle system of endurance,Its structure includes Rotor mount,Rotorshaft,Unmanned plane rack,Power-supply battery,Unmanned aerial vehicle (UAV) control device main body,Solar power supply apparatus,GPS locator,Rotor main body,Fixed link,Stent contiguous block,Support feet buffer protection set,Supporting rack,Three-limb tube,Solar power supply apparatus is by solar panels main body,Solar panels protecting frame,Support column,Power lead,Solar energy protective glass forms,Solar energy protective glass is nested at the top of solar panels protecting frame,Among support column bottom is secured by bolts in above unmanned aerial vehicle (UAV) control device main body,The utility model realizes long six rotor wing unmanned aerial vehicle system of endurance by being provided with solar power supply apparatus,Long six rotor wing unmanned aerial vehicle system of endurance can be powered by solar energy when in use,Six rotor wing unmanned aerial vehicles can be made to carry out long-time use,Improve device practicality.
Description
Technical field
The utility model is a kind of six rotor wing unmanned aerial vehicle system of long endurance, belongs to UAV system field.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft, or fully or intermittently independently operated by car-mounted computer, compared with manned aircraft, nobody
Machine is often more suitable for the task of those too " slow-witted, dirty or dangerous ", and unmanned plane presses application field, can be divided into it is military with civilian,
Military aspect, unmanned plane are divided into reconnaissance plane and target drone, and civilian aspect, unmanned plane+sector application, is that unmanned plane has really just needed,
At present take photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping,
The application in news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, has greatly expanded unmanned plane in itself
Purposes, developed country also actively extension sector application with development unmanned air vehicle technique.
Prior art discloses Application No.：201420657241.9 six rotor wing unmanned aerial vehicle of one kind, including six spiral
Paddle, rigid arm support and master control system, six propellers are connected firmly in rigid arm support mechanism by six independences
Motor driving, the master control system mechanism is arranged on the positive lower end of rigid arm support, and six rotor wing unmanned aerial vehicle is in the air
The hovering that accuracy rating is 1 meter can be achieved, being capable of effectively long-time object observing dynamic, and manipulate flexible, the battery module
For 10000mAh, the cruising ability being thirty minutes long can flight 10km, maximal rate 10m/s, the containing of flying height
Property be 0-1000m, can adapt to temperature range as -10 ° -45 °, its take-off weight 3kg, payload capacity 1kg, can carry
The equipment such as video camera observe the place that the mankind are not easy to observe in detail, but prior art construction is simple, traditional six rotor of long endurance
Cruising time is shorter when in use for UAV system, and much time using, device poor practicability can not be carried out by being limited by continuation of the journey.
Utility model content
In view of the deficienciess of the prior art, the utility model aim is to provide a kind of six rotor wing unmanned aerial vehicle system of long endurance
System, prior art construction is simple to solve, and cruising time is shorter when in use for traditional six rotor wing unmanned aerial vehicle system of long endurance, by
The problem of continuation of the journey limitation can not carry out much time using, device poor practicability.
To achieve these goals, the utility model is to realize by the following technical solutions：A kind of long endurance six is revolved
Wing UAV system, its structure include Rotor mount, rotorshaft, unmanned plane rack, power-supply battery, unmanned aerial vehicle (UAV) control device master
Body, solar power supply apparatus, GPS locator, rotor main body, fixed link, stent contiguous block, support feet buffer protection set, support
Frame, three-limb tube, the rotor main body are installed on above rotorshaft by fixed link, and the rotorshaft is connected by machinery
Rotor mount inside groove is connected to, the Rotor mount is installed on unmanned plane rack high order end, and the unmanned plane rack is equidistantly equal
Even to be distributed in unmanned plane holster shell edge, the solar power supply apparatus is installed vertically on unmanned aerial vehicle (UAV) control device master by bolt
Above body, the GPS locator is connected on the right side of unmanned aerial vehicle (UAV) control device main body by electric signal, and the three-limb tube is nested in
Inside supporting rack, the support feet buffer protection set is nested in supporting rack left and right ends, and the solar power supply apparatus is by the sun
Energy plate main body, solar panels protecting frame, support column, power lead, solar energy protective glass composition, the solar energy protective glass
It is nested at the top of solar panels protecting frame, the solar energy protective glass is covered in above solar panels body surfaces, the branch
Dagger is welded among solar panels protecting frame bottom surface, and described power lead one end is welded in solar panels bottom part body, another
With power-supply battery by being electrically connected, the support column bottom is secured by bolts in middle above unmanned aerial vehicle (UAV) control device main body at end.
Further, the unmanned plane rack is equipped with 6 positioned at same level and is parallel to each other.
Further, the rotor main body is mutually perpendicular to rotorshaft.
Further, the stent contiguous block is located at the left and right sides below unmanned aerial vehicle (UAV) control device main body.
Further, support frame as described above is installed on below stent contiguous block by fixing axle.
Further, the unmanned aerial vehicle (UAV) control device body circular structure.
Further, the solar energy protective glass is tempered glass/simple glass/sand blasting glass material.
Beneficial effect
The utility model realizes long six rotor wing unmanned aerial vehicle system of endurance by being provided with solar power supply apparatus, long endurance
Six rotor wing unmanned aerial vehicle systems can be powered by solar energy when in use, and six rotor wing unmanned aerial vehicles can be made make for a long time
With raising device practicality.
Brief description of the drawings
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other spies of the utility model
Sign, objects and advantages will become more apparent upon：
Fig. 1 is a kind of structure diagram of long six rotor wing unmanned aerial vehicle system of endurance of the utility model；
Fig. 2 is the structure diagram of the utility model solar power supply apparatus.
In figure：Rotor mount -1, rotorshaft -2, unmanned plane rack -3, power-supply battery -4, unmanned aerial vehicle (UAV) control device master
Body -5, solar power supply apparatus -6, GPS locator -7, rotor main body -8, fixed link -9, stent contiguous block -10, support feet are delayed
Rush protective case -11, supporting rack -12, three-limb tube -13, solar panels main body -601, solar panels protecting frame -602, support
Column -603, power lead -604, solar energy protective glass -605.
Embodiment
To make the technical means, creative features, achievable purpose and effectiveness that the utility model is realized easy to understand, below
With reference to embodiment, the utility model is expanded on further.
- Fig. 2 is please referred to Fig.1, the utility model provides a kind of long six rotor wing unmanned aerial vehicle system of endurance, its structure includes rotor
Mounting base 1, rotorshaft 2, unmanned plane rack 3, power-supply battery 4, unmanned aerial vehicle (UAV) control device main body 5, solar power supply apparatus 6, GPS
Locator 7, rotor main body 8, fixed link 9, stent contiguous block 10, support feet buffer protection set 11, supporting rack 12, three-limb tube
13, the rotor main body 8 is installed on the top of rotorshaft 2 by fixed link 9, and the rotorshaft 2 is by being mechanically connected to rotation
1 inside groove of wing mounting base, the Rotor mount 1 are installed on 3 high order end of unmanned plane rack, and the unmanned plane rack 3 is equidistantly uniform
3 shell edge of unmanned plane rack is distributed in, the solar power supply apparatus 6 is installed vertically on unmanned aerial vehicle (UAV) control device master by bolt
The top of body 5, the GPS locator 7 are connected to the right side of unmanned aerial vehicle (UAV) control device main body 5, the three-limb tube 13 by electric signal
It is nested in inside supporting rack 12, the support feet buffer protection set 11 is nested in 12 left and right ends of supporting rack, and the solar energy supplies
Electric installation 6 protects glass by solar panels main body 601, solar panels protecting frame 602, support column 603, power lead 604, solar energy
Glass 605 forms, and the solar energy protective glass 605 is nested in the top of solar panels protecting frame 602, the solar energy protective glass
605 are covered in 601 surface of solar panels main body, and the support column 603 is welded in 602 bottom surface of solar panels protecting frame
Between, described 604 one end of power lead is welded in 601 bottom of solar panels main body, the other end with power-supply battery 4 by being electrically connected,
603 bottom of support column is secured by bolts among the top of unmanned aerial vehicle (UAV) control device main body 5, and the unmanned plane rack 3 is equipped with 6
A to be located at same level and be parallel to each other, the rotor main body 8 is mutually perpendicular to rotorshaft 2, the stent contiguous block 10
Positioned at the lower section of unmanned aerial vehicle (UAV) control device main body 5 left and right sides, support frame as described above 12 is installed under stent contiguous block 10 by fixing axle
Side.
The terminal of GPS locator 7 described in this patent GPS module that has been built-in and mobile communication module, for by GPS moulds
The location data that block obtains is reached by mobile communication module on a server on Internet, so as to realize in electricity
Terminal location is inquired about on brain or mobile phone.
Carrying out in use, the support column 603 of solar power supply apparatus 6 is installed on unmanned aerial vehicle (UAV) control by fixing bolt
Among 5 upper surface of device main body, power lead 604 and the long six rotor wing unmanned aerial vehicle system of endurance of solar power supply apparatus 6 are utilized
Power-supply battery 4 is by being electrically connected, and solar irradiation is formed on 601 semiconductor p-n junctions of solar panels main body when in use
New electron-hole pair, under the action of p-n junction electric field, hole flows to n areas by p areas, and electronics flows to p areas by n areas, connects electricity
Electric current is just formed behind road and provides electric energy for long six rotor wing unmanned aerial vehicle system of endurance, therefore, by being provided with solar power supply apparatus
6, long six rotor wing unmanned aerial vehicle system of endurance can be powered by solar energy when in use, can carry out six rotor wing unmanned aerial vehicles
Use for a long time, improve device practicality.
Its structure and principle are all that this technology personnel can be learnt by technical manual or be known by normal experiment method,
The utility model solves the problems, such as it is that prior art construction is simple, and traditional six rotor wing unmanned aerial vehicle system of long endurance continues when in use
ETS estimated time of sailing is shorter, and much time using, device poor practicability can not be carried out by being limited by continuation of the journey, and the utility model passes through above-mentioned component
Be combined with each other, long six rotor wing unmanned aerial vehicle system of endurance can be powered by solar energy when in use, can make six rotors
Unmanned plane carries out long-time use, improves device practicality, described in detail below:
The solar energy protective glass 605 is nested in the top of solar panels protecting frame 602, the solar energy protective glass
605 are covered in 601 surface of solar panels main body, and the support column 603 is welded in 602 bottom surface of solar panels protecting frame
Between, described 604 one end of power lead is welded in 601 bottom of solar panels main body, the other end with power-supply battery 4 by being electrically connected,
603 bottom of support column is secured by bolts among the top of unmanned aerial vehicle (UAV) control device main body 5.
First uses the solar energy protective glass of tempered glass material, makes six rotor wing unmanned aerial vehicles using the solar power supply apparatus
Carry out long-time use；
Second uses the solar energy protective glass of simple glass material, makes six rotor wing unmanned aerial vehicles using the solar power supply apparatus
Carry out long-time use；
Third uses the solar energy protective glass of sand blasting glass material, makes six rotor wing unmanned aerial vehicles using the solar power supply apparatus
Carry out long-time use；
| Tempered glass | Simple glass | Sand blasting glass | |
| Rigidity | By force | Generally | Generally |
| Light transmittance | 80% | 75% | 70% |
In conclusion using the solar energy protective glass of tempered glass material, make six rotations using the solar power supply apparatus
Wing unmanned plane carries out the best results used for a long time, and rigidity is strong and light transmittance is good.
The advantages of basic principle and main feature and the utility model of the utility model has been shown and described above, for
For those skilled in the art, it is clear that the utility model is not limited to the details of above-mentioned one exemplary embodiment, and without departing substantially from this
In the case of the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter
From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the utility model is by institute
Attached claim rather than described above limit, it is intended that will fall in the implication and scope of the equivalency of claim
All changes are embraced therein.Any reference numeral in claim should not be considered as to the involved right of limitation
It is required that.
Moreover, it will be appreciated that although the present specification is described in terms of embodiments, not each embodiment is only wrapped
Containing an independent technical solution, this narrating mode of specification is only that those skilled in the art should for clarity
Using specification as an entirety, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
It is appreciated that other embodiment.
Claims (5)
1. a kind of six rotor wing unmanned aerial vehicle system of long endurance, its structure includes Rotor mount (1), rotorshaft (2), unmanned plane machine
Frame (3), power-supply battery (4), unmanned aerial vehicle (UAV) control device main body (5), solar power supply apparatus (6), GPS locator (7), rotor main body
(8), fixed link (9), stent contiguous block (10), support feet buffer protection set (11), supporting rack (12), three-limb tube (13),
It is characterized in that：
The rotor main body (8) is installed on above rotorshaft (2) by fixed link (9), and the rotorshaft (2) passes through machinery
Rotor mount (1) inside groove is connected to, the Rotor mount (1) is installed on unmanned plane rack (3) high order end, the unmanned plane
Rack (3) is equidistantly uniformly distributed in unmanned plane rack (3) shell edge, and the solar power supply apparatus (6) is vertical by bolt
It is installed on above unmanned aerial vehicle (UAV) control device main body (5), the GPS locator (7) is connected to unmanned aerial vehicle (UAV) control device master by electric signal
On the right side of body (5), the three-limb tube (13) is nested in supporting rack (12) inside, and the support feet buffer protection set (11) is nested
In supporting rack (12) left and right ends；
The solar power supply apparatus (6) by solar panels main body (601), solar panels protecting frame (602), support column (603),
Power lead (604), solar energy protective glass (605) composition, the solar energy protective glass (605) are nested in solar panels guarantor
Protect at the top of frame (602), the solar energy protective glass (605) is covered in solar panels main body (601) surface, the support
Column (603) is welded among solar panels protecting frame (602) bottom surface, and described power lead (604) one end is welded in solar panels
Main body (601) bottom, with power-supply battery (4) by being electrically connected, support column (603) bottom is secured by bolts in the other end
Among above unmanned aerial vehicle (UAV) control device main body (5).
A kind of 2. long six rotor wing unmanned aerial vehicle system of endurance according to claim 1, it is characterised in that：The unmanned plane rack
(3) 6 are equipped with positioned at same level and be parallel to each other.
A kind of 3. long six rotor wing unmanned aerial vehicle system of endurance according to claim 1, it is characterised in that：The rotor main body
(8) it is mutually perpendicular to rotorshaft (2).
A kind of 4. long six rotor wing unmanned aerial vehicle system of endurance according to claim 1, it is characterised in that：The stent contiguous block
(10) left and right sides below unmanned aerial vehicle (UAV) control device main body (5).
A kind of 5. long six rotor wing unmanned aerial vehicle system of endurance according to claim 1, it is characterised in that：Support frame as described above (12)
It is installed on by fixing axle below stent contiguous block (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721339837.4U CN207346091U (en) | 2017-10-18 | 2017-10-18 | A kind of six rotor wing unmanned aerial vehicle system of long endurance |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721339837.4U CN207346091U (en) | 2017-10-18 | 2017-10-18 | A kind of six rotor wing unmanned aerial vehicle system of long endurance |
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| Publication Number | Publication Date |
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| CN207346091U true CN207346091U (en) | 2018-05-11 |
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| CN201721339837.4U Active CN207346091U (en) | 2017-10-18 | 2017-10-18 | A kind of six rotor wing unmanned aerial vehicle system of long endurance |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111268091A (en) * | 2020-02-20 | 2020-06-12 | 南京航空航天大学 | Four rotor unmanned aerial vehicle of folded cascade of high continuation of journey |
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2017
- 2017-10-18 CN CN201721339837.4U patent/CN207346091U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111268091A (en) * | 2020-02-20 | 2020-06-12 | 南京航空航天大学 | Four rotor unmanned aerial vehicle of folded cascade of high continuation of journey |
| CN111268091B (en) * | 2020-02-20 | 2021-05-11 | 南京航空航天大学 | A high-endurance foldable quadrotor unmanned aerial vehicle |
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