CN214325367U - Unmanned aerial vehicle convenient to dismouting solar panel - Google Patents
Unmanned aerial vehicle convenient to dismouting solar panel Download PDFInfo
- Publication number
- CN214325367U CN214325367U CN202120220170.6U CN202120220170U CN214325367U CN 214325367 U CN214325367 U CN 214325367U CN 202120220170 U CN202120220170 U CN 202120220170U CN 214325367 U CN214325367 U CN 214325367U
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- solar panel
- unmanned aerial
- aerial vehicle
- vehicle body
- clamping pieces
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- 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
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- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
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- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
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Abstract
The utility model discloses an unmanned aerial vehicle convenient for dismounting a solar panel, which relates to the field of unmanned aerial vehicles and comprises an unmanned aerial vehicle body, side fasteners and a solar panel, two sides of the unmanned aerial vehicle body are fixedly connected with side clamping pieces, sliding grooves are arranged on the side clamping pieces, the solar panel is clamped in the two chutes in a sliding way, the front end of the solar panel is provided with a fixed ring, the fixing ring is fixed by the positioning component, the solar panel of the utility model can be assembled and disassembled without screws, only the solar panel is horizontally inserted into the chutes of the two side clamping pieces, and the fixing ring is fixed by the positioning component, can be fixed with solar panel and unmanned aerial vehicle body, insert with female simultaneously public inserting and peg graft, solar panel realizes being connected with the battery, does not need extra going to connect solar panel and battery, and easy dismounting has avoided the condition that the bolt fastening appears smooth tooth.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle field, concretely relates to unmanned aerial vehicle convenient to dismouting solar panel.
Background
Unmanned aerial vehicles are widely used in many fields such as aerial photography, agriculture, plant protection, power inspection, disaster relief, movie and television shooting at present; unmanned aerial vehicle mainly realizes the power supply by unmanned aerial vehicle's from the battery of taking, nevertheless because the electric power capacity of battery is limited, so some unmanned aerial vehicles have the problem that duration is low, adds on unmanned aerial vehicle and establishes solar panel and can improve unmanned aerial vehicle's duration to adapt to long-time unmanned aerial vehicle flight task.
At present add to establish solar panel and mainly directly fix through screw and unmanned aerial vehicle body locking, when needing to alleviate unmanned aerial vehicle whole weight and dismantling solar panel, need one pull down the screw can, to the solar panel that often needs the dismouting, the smooth tooth of screw can also appear and dismantle the condition of difficulty.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle convenient to dismouting solar panel to solve the problem of mentioning in the above-mentioned background art.
An unmanned aerial vehicle convenient for dismounting a solar panel comprises an unmanned aerial vehicle body, side clamping pieces and a solar panel, wherein the side clamping pieces are fixedly connected to two sides of the unmanned aerial vehicle body, sliding grooves are formed in the side clamping pieces, the solar panel is clamped in the two sliding grooves in a sliding mode, a fixing ring is arranged at the front end of the solar panel, and the fixing ring is fixed through a positioning component;
the positioning assembly comprises a bolt, a pin sleeve and a fixing piece, the bolt is connected in the pin sleeve in a sliding mode, the pin sleeve is fixedly connected to the fixing piece through a screw, the fixing piece is fixedly connected with the unmanned aerial vehicle body, a spring is arranged in the pin sleeve, the spring is located between the bolt and the fixing piece, a pressing piece is arranged on the outer side of the pin sleeve, and the pressing piece is fixedly connected with the bolt.
Preferably, solar panel's front end is equipped with female inserting, be equipped with public inserting on the unmanned aerial vehicle body.
Preferably, the power public affairs are inserted and are had a battery electric connection with the battery unmanned aerial vehicle body.
Preferably, be equipped with spacing arch on the solar panel, leave the space between solar panel and the unmanned aerial vehicle body.
The utility model has the advantages that: the utility model discloses a need not use the screw during solar panel dismouting, only need push down the pressing piece, make the bolt move down, insert the spout of two side fasteners with the solar panel level, when spacing arch is supported on the side fastener, solid fixed ring just in time is located the top of bolt, loosen the pressing piece this moment, the bolt moves up under the spring action, insert in the fixed ring, the side fastener has restricted solar panel's horizontal and vertical motion, and the bolt has restricted solar panel's longitudinal movement, so solar panel can fix, meanwhile public inserting is pegged graft with female, solar panel realizes being connected with the battery, do not need extra to connect solar panel and battery, easy dismounting, avoid the condition that smooth tooth appears in the fix with screw.
Drawings
Fig. 1 is a schematic structural diagram of the present invention.
Fig. 2 is a schematic structural view of the solar panel removed.
Fig. 3 is a schematic structural diagram of the positioning assembly.
Fig. 4 is a schematic structural diagram of a solar panel.
Fig. 5 is a schematic structural view of the positioning assembly after the pressing member is hidden.
In the figure: unmanned aerial vehicle body 1, public inserting 11, side fastener 2, solar panel 3, solid fixed ring 31, female 32 of inserting, spacing arch 33, locating component 4, bolt 41, cotter 42, mounting 43, spring 44, pressing member 45.
Detailed Description
In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention is further described below with reference to the following embodiments.
As shown in fig. 1 to 5, an unmanned aerial vehicle convenient for dismounting a solar panel comprises an unmanned aerial vehicle body 1, side clamping pieces 2 and a solar panel 3, wherein the side clamping pieces 2 are fixedly connected to two sides of the unmanned aerial vehicle body 1, sliding grooves are formed in the side clamping pieces 2, the solar panel 3 is slidably clamped in the two sliding grooves, a fixing ring 31 is arranged at the front end of the solar panel 3, and the fixing ring 31 is fixed through a positioning component 4;
locating component 4 includes bolt 41, cotter 42 and mounting 43, bolt 41 sliding connection is in cotter 42, cotter 42 passes through screw fixed connection on mounting 43, mounting 43 and unmanned aerial vehicle body 1 fixed connection, be equipped with spring 44 in the cotter 42, spring 44 is located between bolt 41 and the mounting 43, and the cotter 42 outside is equipped with pressing piece 45, pressing piece 45 and bolt 41 fixed connection.
In this embodiment, solar panel 3's front end is equipped with female 32 of inserting, be equipped with public 11 of inserting on the unmanned aerial vehicle body 1. The female plug 32 and the male plug 11 can be communicated while the solar panel 3 is fixed, so that the step of connecting the solar panel 3 with a battery is reduced.
In this embodiment, the power public affairs insert 11 and the battery electric connection of battery unmanned aerial vehicle body 1.
In this embodiment, be equipped with spacing arch 33 on solar panel 3, leave the space between solar panel 3 and the unmanned aerial vehicle body 1. The limiting protrusions 33 are used to ensure that the solar panel 3 is just inserted into the fixing ring 31 and the plug pins 41 are concentric. Leave the space between solar panel 3 and the unmanned aerial vehicle body 1 and increase solar panel's radiating efficiency.
The working process and the principle thereof are as follows:
when the solar panel 3 needs to be installed, the pressing piece 45 is pressed downwards, and the pressing piece 45 is fixedly connected with the part of the plug pin 41, which protrudes out of the pin sleeve 42, so that the plug pin 41 slides downwards in the pin sleeve 42 under the action of the pressing piece 45. The spring 44 is compressed until the latch 41 slides down into the pin sleeve 42, and then the solar panel 3 is inserted between the two side clamping pieces 2 along the sliding grooves of the two side clamping pieces 2 and pushed towards the direction of the positioning component 4, and when the limiting protrusion 33 on the solar panel 3 is in contact with the side clamping pieces 2, the pressing piece 45 is released. The pressing piece 45 is loosened, the spring 44 is reset, the bolt 41 is ejected out, the ejected bolt 41 is inserted into the fixing ring 31, the fixing ring 31 is fixed, the side clamping piece 2 limits the transverse movement and the vertical movement of the solar panel 3 at the moment, the bolt 41 limits the longitudinal movement of the solar panel 3, and therefore the solar panel 3 is fixed on the unmanned aerial vehicle body 1. When solar panel 3 is fixed, insert 11 with public being connected of battery on the unmanned aerial vehicle body 1 and insert 32 switch-ons with the mother on solar panel 3, the electric quantity that produces on solar panel 3 can be through mother insert 32 with public inserting 11 and store in the battery. The solar panel 3 and the battery are connected without additionally using a wire.
When the solar panel 3 needs to be detached, the pressing piece 45 is pressed down, so that the bolt 41 is separated from the fixing ring 31, and then the solar panel 3 can be taken down by drawing out the solar panel 3 from the two side clamping pieces 2.
Based on the above: the utility model discloses a need not use the screw during the dismouting of solar panel 3, only need, insert in the spout of two side fasteners 2 with 3 levels of solar panel, recycle locating component 4 and fix solid fixed ring 31, can be fixed with solar panel 3 and unmanned aerial vehicle body 1, insert 11 with mother simultaneously and peg graft 32, solar panel 3 realizes with the battery to be connected, does not need extra going to connect solar panel 3 and battery, easy dismounting has avoided the condition that smooth tooth appears in the fix with screw.
It will be appreciated by those skilled in the art that the invention may be embodied in other specific forms without departing from the spirit or essential characteristics thereof. The embodiments disclosed above are therefore to be considered in all respects as illustrative and not restrictive. All changes which come within the scope of the invention or which are equivalent to the scope of the invention are embraced by the invention.
Claims (4)
1. The unmanned aerial vehicle convenient for dismounting the solar panel is characterized by comprising an unmanned aerial vehicle body (1), side clamping pieces (2) and the solar panel (3), wherein the side clamping pieces (2) are fixedly connected to two sides of the unmanned aerial vehicle body (1), sliding grooves are formed in the side clamping pieces (2), the solar panel (3) is slidably clamped in the two sliding grooves, a fixing ring (31) is arranged at the front end of the solar panel (3), and the fixing ring (31) is fixed through a positioning assembly (4);
locating component (4) include bolt (41), round pin cover (42) and mounting (43), bolt (41) sliding connection is in round pin cover (42), round pin cover (42) pass through screw fixed connection on mounting (43), mounting (43) and unmanned aerial vehicle body (1) fixed connection, be equipped with spring (44) in round pin cover (42), spring (44) are located between bolt (41) and mounting (43), the round pin cover (42) outside is equipped with pressing piece (45), pressing piece (45) and bolt (41) fixed connection.
2. The unmanned aerial vehicle convenient to dismouting solar panel of claim 1, characterized in that, solar panel (3)'s front end is equipped with female (32), be equipped with public (11) of inserting on unmanned aerial vehicle body (1).
3. The unmanned aerial vehicle convenient to dismouting solar panel of claim 2, characterized in that, the public affair plug (11) and the battery electric connection of battery unmanned aerial vehicle body (1).
4. The unmanned aerial vehicle convenient to dismouting solar panel of claim 1, characterized in that, be equipped with spacing arch (33) on solar panel (3), leave the space between solar panel (3) and unmanned aerial vehicle body (1).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN202120220170.6U CN214325367U (en) | 2021-01-27 | 2021-01-27 | Unmanned aerial vehicle convenient to dismouting solar panel |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN202120220170.6U CN214325367U (en) | 2021-01-27 | 2021-01-27 | Unmanned aerial vehicle convenient to dismouting solar panel |
Publications (1)
Publication Number | Publication Date |
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CN214325367U true CN214325367U (en) | 2021-10-01 |
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CN202120220170.6U Active CN214325367U (en) | 2021-01-27 | 2021-01-27 | Unmanned aerial vehicle convenient to dismouting solar panel |
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CN (1) | CN214325367U (en) |
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2021
- 2021-01-27 CN CN202120220170.6U patent/CN214325367U/en active Active
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