CN105978458A - Device for supporting charging equipment of adjustable six-rotor aircraft - Google Patents
Device for supporting charging equipment of adjustable six-rotor aircraft Download PDFInfo
- Publication number
- CN105978458A CN105978458A CN201610490989.8A CN201610490989A CN105978458A CN 105978458 A CN105978458 A CN 105978458A CN 201610490989 A CN201610490989 A CN 201610490989A CN 105978458 A CN105978458 A CN 105978458A
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- China
- Prior art keywords
- seat
- adjusting screw
- sleeve
- hole
- screw rod
- 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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- 230000002457 bidirectional effect Effects 0.000 claims abstract description 16
- PEDCQBHIVMGVHV-UHFFFAOYSA-N Glycerine Chemical compound OCC(O)CO PEDCQBHIVMGVHV-UHFFFAOYSA-N 0.000 claims 1
- 238000013519 translation Methods 0.000 abstract description 4
- 238000006243 chemical reaction Methods 0.000 abstract 1
- 238000012544 monitoring process Methods 0.000 description 7
- 230000007613 environmental effect Effects 0.000 description 5
- 230000008859 change Effects 0.000 description 4
- 230000008901 benefit Effects 0.000 description 3
- 238000007689 inspection Methods 0.000 description 2
- 230000001105 regulatory effect Effects 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 241000607479 Yersinia pestis Species 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 201000010099 disease Diseases 0.000 description 1
- 208000037265 diseases, disorders, signs and symptoms Diseases 0.000 description 1
- 239000003814 drug Substances 0.000 description 1
- 229940079593 drug Drugs 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 229910052500 inorganic mineral Inorganic materials 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 239000011707 mineral Substances 0.000 description 1
- 230000000116 mitigating effect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000005070 sampling Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02S—GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
- H02S20/00—Supporting structures for PV modules
- H02S20/30—Supporting structures being movable or adjustable, e.g. for angle adjustment
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/50—Photovoltaic [PV] energy
Abstract
The invention discloses a device for supporting charging equipment of an adjustable six-rotor aircraft, and the device comprises a connecting seat, a sleeve, an adjusting screw, a moving plate, a rotating column, a bidirectional pull rod, a supporting seat, a photovoltaic cell panel, and a locking bolt. The top of the sleeve is provided with an internal thread hole cooperating with the adjusting screw. One end of the adjusting screw is disposed in the internal thread hole at the top of the sleeve, and the other end of the adjusting screw is connected with the moving plate. The lower end of the rotating column is disposed in a vertical steering hole at the center of the upper end of the moving plate, and the central part of the bidirectional pull rod is disposed in a horizontal steering hole at the top of the rotating column. The supporting seat is fixed at an outer end of the bidirectional pull rod, and the photovoltaic cell panel is inserted into a square clamping groove of the supporting seat. The device employs a series structure mode, can achieve one-translation and two-rotation movement in three freedom directions, achieves the adjustment of a light angle at any time, improves the conversion efficiency of solar energy to electric energy, and can be applicable for different types of photovoltaic cell panels in different sizes.
Description
Technical field
The present invention relates to unmanned plane auxiliary equipment field, a kind of adjustable six rotorcraft charger supports dress
Put.
Background technology
Aircraft be by the mankind manufacture, can fly away from ground, space flight and by people control in endoatmosphere or exoatmosphere
The apparatus flying object flown in space (space), aircraft is divided into airborne vehicle, spacecraft, rocket, guided missile and guided weapon；Nothing
Man-machine is also the one of aircraft, and unmanned plane is utilize that radio robot and the presetting apparatus provided for oneself handle the most manned
Aircraft, can be divided into depopulated helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, unmanned airship from technical standpoint definition
With unmanned parasol etc.；Can be divided into military and civilian by application, military aspect unmanned plane is divided into reconnaissance plane and target drone；At present,
Unmanned plane can be widely applied to country's ecological environmental protection, aeroplane photography, mapping, mineral resources exploration, the condition of a disaster supervision, traffic
Patrol, power-line patrolling, security monitoring, emergent mitigation, emergency command, rain making, national defense safety, land resources exploration,
Town planning, seismic survey, environmental monitoring, forest fire protection, Crop Estimation, protection zone wild animal monitoring, air sampling,
Maritime affairs scout, border make an inspection tour, the prohibition of drug scouting, fire inspection, ecological environmental protection, marine environmental monitoring, land use survey,
Water resources development, crop growth monitoring and the yield by estimation, agricultural operation, Natural calamity monitoring and assessment, urban planning and municipal administration pipe
The fields such as the protection of reason, forest disease and pest and monitoring, digital city.
Six rotorcraft belongs to the one of aircraft, six rotorcraft have compact conformation, build less than normal, popular relatively strong,
Motion is widely used in civil and military with the advantage such as flight stability flexibly, and the most popular；But current six rotations
Rotor aircraft faces maximum problem demanding prompt solution and continues a journey exactly, and continuation of the journey decides the time of the flight of six rotorcraft and stablizes
Property, indirectly decide efficiency and the quality of six rotorcraft operation, for the energy supplementary question of six rotorcraft, army
Solve with six rotorcraft many employings air refuelling, owing to this kind of supplementary energy mode spends too big, therefore revolve civilian six
Not application on rotor aircraft, civilian six rotorcraft, the most also without good settling mode, the most also sets up charging
Base station carries out energy supplement to the six rotorcraft of operation on the way, but current six rotorcraft charging base station exists electricity
The problems such as energy source is single, environmental protection and energy saving is poor, set in consideration of it, the invention provides the charging of a kind of adjustable six rotorcraft
Backup support device.
Summary of the invention
In order to make up the deficiencies in the prior art, the invention provides a kind of adjustable six rotorcraft charger support means.
The present invention to solve its technical problem and realize by the following technical solutions.
A kind of adjustable six rotorcraft charger support means, including connect seat, sleeve, adjusting screw rod, movable plate,
Rotational Cylindrical, bidirectional tension rod, support seat, photovoltaic battery panel and clamping screw；Described connection seat is crescent shape structure, sleeve and
Adjusting screw rod quantity is two, and sleeve bottom end is respectively symmetrically along the central transverse axis connecting seat and is fixed on connection seat, sleeve top
Being provided with the internal thread hole matched with adjusting screw rod at end, adjusting screw rod one end is arranged on inside the internal thread hole of sleeve top end,
The adjusting screw rod other end is connected with movable plate, and movable plate upper end center position is provided with vertical duction hole, and Rotational Cylindrical lower end is pacified
Being contained in the vertical duction hole of movable plate upper end center position, Rotational Cylindrical upper end is provided with and is horizontally diverted hole, in the middle part of bidirectional tension rod
Being arranged on being horizontally diverted in hole of Rotational Cylindrical upper end, and bidirectional tension rod two ends adjustable length, supporting seat quantity is two, supports seat solid
It is scheduled on bidirectional tension rod outboard end, supports and on seat, offer square draw-in groove, support and equally spaced on seat front/rear end offer spacing hole,
Photovoltaic battery panel assigns in the square draw-in groove supporting seat, and uses clamping screw to be attached between photovoltaic battery panel and support seat；
Can change, by adjusting screw rod, the distance that the present invention stretches laterally, it is adaptable to the use in different places, and the present invention is at water
All can rotate in plane and in vertical, such that it is able to the angle that the regulation present invention is in horizontal plane and in vertical, enter
And the angle of photovoltaic battery panel comparison sunlight can be changed, effectively raise the power that absorbs solar energy of photovoltaic battery panel, remove
Outside this, two spacing supported between seat can be regulated by bidirectional tension rod, it is simple to the photovoltaic cell of different model size is installed
Plate, the suitability is wider, and the present invention uses the form of cascaded structure, can carry out on a translation two rotation three degree of freedom direction altogether
Motion, can regulate at any time angular, improve solar energy and change into the efficiency of electric energy, and be applicable to different model size
Photovoltaic battery panel.
Compared with prior art, the invention have the advantages that the present invention uses the form of cascaded structure, a translation two can be carried out
Rotate the motion being total on three degree of freedom direction, angular can be regulated at any time, improve solar energy and change into the efficiency of electric energy,
And it is applicable to the photovoltaic battery panel of different model size.
Accompanying drawing explanation
The present invention is further described with embodiment below in conjunction with the accompanying drawings.
Fig. 1 is the perspective view (seeing from front to back) of the present invention；
Fig. 2 is the perspective view (seeing from back to front) of the present invention.
Detailed description of the invention
For the technological means making the present invention realize, creation characteristic, reach purpose and be easy to understand with effect, below in conjunction with tool
Body illustrates, and the present invention is expanded on further.
As depicted in figs. 1 and 2, a kind of adjustable six rotorcraft charger support means, including connecting seat 21, set
Cylinder 22, adjusting screw rod 23, movable plate 24, Rotational Cylindrical 25, bidirectional tension rod 26, support seat 27, photovoltaic battery panel 28 and lock
Tight bolt 29；Described connection seat 21 is in crescent shape structure, and sleeve 22 and adjusting screw rod 23 quantity are two, sleeve 22 end
End is respectively symmetrically along the central transverse axis connecting seat 21 and is fixed on connection seat 21, and sleeve 22 top end is provided with and regulates spiral shell
The internal thread hole that bar 23 matches, adjusting screw rod 23 one end is arranged on inside the internal thread hole of sleeve 22 top end, adjusting screw rod
23 other ends are connected with movable plate 24, and movable plate 24 upper end center position is provided with vertical duction hole, Rotational Cylindrical 25 times
End is arranged in the vertical duction hole of movable plate 24 upper end center position, and Rotational Cylindrical 25 upper end is provided with and is horizontally diverted hole, double
In the middle part of pull bar 26, it is arranged on being horizontally diverted in hole of Rotational Cylindrical 25 upper end, and bidirectional tension rod 26 two ends adjustable length, supports seat
27 quantity are two, support seat 27 and are fixed on bidirectional tension rod 26 outboard end, support and offer square draw-in groove on seat 27, support seat
The equally spaced spacing hole that offers on 27 front/rear ends, photovoltaic battery panel 28 assigns in the square draw-in groove supporting seat 27, and light
Clamping screw 29 is used to be attached between volt cell panel 28 and support seat 27；The present invention can be changed by adjusting screw rod 23
The distance stretched laterally, it is adaptable to the use in different places, and and all can the entering in vertical in horizontal plane of the present invention
Row rotates, such that it is able to the angle that the regulation present invention is in horizontal plane and in vertical, and then it is right to change photovoltaic battery panel 28
According to the angle of sunlight, effectively raise the power that absorbs solar energy of photovoltaic battery panel 28, in addition, pass through bidirectional tension rod
26 can regulate two spacing supported between seat 27, it is simple to installing the photovoltaic battery panel 28 of different model size, the suitability is more
Extensively, the present invention uses the form of cascaded structure, can carry out a translation two and rotate the motion being total on three degree of freedom direction, to optic angle
Degree can regulate at any time, improves solar energy and changes into the efficiency of electric energy, and is applicable to the photovoltaic battery panel of different model size
28。
The ultimate principle of the present invention, principal character and advantage have more than been shown and described.Skilled person will appreciate that of the industry,
The present invention is not restricted to the described embodiments, the principle that the present invention is simply described of the description in above-described embodiment and description,
Without departing from the spirit and scope, the present invention also has various changes and modifications, and these changes and improvements both fall within
In scope of the claimed invention.Claimed scope is defined by appending claims and equivalent thereof.
Claims (1)
1. an adjustable six rotorcraft charger support means, it is characterised in that: include connecting seat, sleeve, tune
Joint screw rod, movable plate, Rotational Cylindrical, bidirectional tension rod, support seat, photovoltaic battery panel and clamping screw；Described connection seat is the moon
Tooth shape structure, sleeve and adjusting screw rod quantity are two, and sleeve bottom end is respectively symmetrically along the central transverse axis connecting seat and is fixed on
Connecting on seat, sleeve top end is provided with the internal thread hole matched with adjusting screw rod, and adjusting screw rod one end is arranged on sleeve top
Inside the internal thread hole at place, the adjusting screw rod other end is connected with movable plate, and movable plate upper end center position is provided with vertical turning
Xiang Kong, Rotational Cylindrical lower end is arranged in the vertical duction hole of movable plate upper end center position, and Rotational Cylindrical upper end is provided with level and turns
Xiang Kong, is arranged on being horizontally diverted in hole of Rotational Cylindrical upper end, and bidirectional tension rod two ends adjustable length in the middle part of bidirectional tension rod, support seat
Quantity is two, supports seat and is fixed on bidirectional tension rod outboard end, supports and offers square draw-in groove on seat, supports seat front/rear end first-class
Spacing offer spacing hole, photovoltaic battery panel assigns in the square draw-in groove supporting seat, and between photovoltaic battery panel and support seat
Employing clamping screw is attached.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610490989.8A CN105978458B (en) | 2016-06-28 | 2016-06-28 | A kind of adjustable supporting |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610490989.8A CN105978458B (en) | 2016-06-28 | 2016-06-28 | A kind of adjustable supporting |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105978458A true CN105978458A (en) | 2016-09-28 |
| CN105978458B CN105978458B (en) | 2017-11-07 |
Family
ID=57020197
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610490989.8A Active CN105978458B (en) | 2016-06-28 | 2016-06-28 | A kind of adjustable supporting |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105978458B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108336958A (en) * | 2018-02-26 | 2018-07-27 | 海宁市海创通日用品科技有限公司 | One kind installing common support frame structure based on solar energy |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201926930U (en) * | 2010-11-25 | 2011-08-10 | 贵州航天凯山石油仪器有限公司 | Angle adjusting device for solar panel on indicator diagram instrument |
| CN202546577U (en) * | 2012-03-27 | 2012-11-21 | 西安博深半导体照明有限公司 | Solar energy LED (light emitting diode) point light source |
| CN103092215A (en) * | 2013-01-11 | 2013-05-08 | 太原理工大学 | Double-shaft sun position tracking device and forecast disturbance control method thereof |
| CN204707084U (en) * | 2015-05-05 | 2015-10-14 | 浙江欧宝能源有限公司 | A kind of solar cell panel assembly corner protector |
| KR101617160B1 (en) * | 2014-03-18 | 2016-05-02 | 강우이엔지(주) | Solar elevation angle of the solar panel according to the season |
-
2016
- 2016-06-28 CN CN201610490989.8A patent/CN105978458B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201926930U (en) * | 2010-11-25 | 2011-08-10 | 贵州航天凯山石油仪器有限公司 | Angle adjusting device for solar panel on indicator diagram instrument |
| CN202546577U (en) * | 2012-03-27 | 2012-11-21 | 西安博深半导体照明有限公司 | Solar energy LED (light emitting diode) point light source |
| CN103092215A (en) * | 2013-01-11 | 2013-05-08 | 太原理工大学 | Double-shaft sun position tracking device and forecast disturbance control method thereof |
| KR101617160B1 (en) * | 2014-03-18 | 2016-05-02 | 강우이엔지(주) | Solar elevation angle of the solar panel according to the season |
| CN204707084U (en) * | 2015-05-05 | 2015-10-14 | 浙江欧宝能源有限公司 | A kind of solar cell panel assembly corner protector |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105978458B (en) | 2017-11-07 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| CB03 | Change of inventor or designer information |
Inventor after: Liu Xuefeng Inventor before: Wu Yan |
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| CB03 | Change of inventor or designer information | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20170913 Address after: 312080 Zhejiang Province, Shaoxing city Keqiao District Anchang town Shuguang Road No. 603 2-1 Applicant after: Shaoxing Xinjiang Network Technology Service Co., Ltd. Address before: 246001 Xinzhou in Anhui province Anqing City Yingjiang District Town Comprehensive Building 3 floor Applicant before: Anqing Baisite Electronic Technology Co., Ltd. |
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| TA01 | Transfer of patent application right | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20180925 Address after: 313000 2599 Hu Jie Avenue, Huzhou, Zhejiang Patentee after: Zhejiang Dadongwu Group Construction New Materials Co., Ltd. Address before: 312080 No. 2-1, Shuguang Road, Keqiao Town, Keqiao District, Shaoxing, Zhejiang Patentee before: Shaoxing Xinjiang Network Technology Service Co., Ltd. |
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| TR01 | Transfer of patent right |
Effective date of registration: 20201021 Address after: Wu Jiawang District Deer Village 221000 Jiangsu city of Xuzhou Province Patentee after: Xuzhou Wanming Precision Casting Co.,Ltd. Address before: 313000 No. 2599 weaving Avenue, Huzhou City, Zhejiang Province Patentee before: ZHEJIANG DADONGWU GROUP CONSTRUCTION OF THE NEW MATERIAL Ltd. |
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| TR01 | Transfer of patent right |