CN212195948U - Unmanned aerial vehicle solar cell panel fixed knot constructs - Google Patents

Unmanned aerial vehicle solar cell panel fixed knot constructs Download PDF

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Publication number
CN212195948U
CN212195948U CN202020976703.9U CN202020976703U CN212195948U CN 212195948 U CN212195948 U CN 212195948U CN 202020976703 U CN202020976703 U CN 202020976703U CN 212195948 U CN212195948 U CN 212195948U
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CN
China
Prior art keywords
aerial vehicle
unmanned aerial
cell panel
fixedly connected
solar cell
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Expired - Fee Related
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CN202020976703.9U
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Chinese (zh)
Inventor
王云川
李万江
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Chongqing Weici Intelligent Control Technology Co ltd
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Chongqing Weici Intelligent Control Technology Co ltd
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Priority to CN202020976703.9U priority Critical patent/CN212195948U/en
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    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/50Photovoltaic [PV] energy
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/50On board measures aiming to increase energy efficiency

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Abstract

The utility model discloses a fixed framework of unmanned aerial vehicle solar cell panel belongs to unmanned air vehicle technical field, a fixed framework of unmanned aerial vehicle solar cell panel, including the unmanned aerial vehicle body, the top fixedly connected with fixed plate of unmanned aerial vehicle body, two through-holes have been seted up at the top of fixed plate. The utility model discloses a, through rotating the panel cassette one side that has the draw-in groove and overturning to the front, because the draw-in groove up, so the staff can very easy alignment insert accomplish fixed, rotate two battery board cassette to relative direction simultaneously, solar cell panel can aim at another draw-in groove and fix the opposite side inserting the completion into, rotatory lead screw, the movable block can drive montant relative movement, the lantern ring on the montant can be fixed to it through the mounting, this process easy operation is convenient, the angle of adjustable cell panel cassette is very convenient to insert solar cell panel into and fixes, the in-process also can not cause the damage to solar cell panel.

Description

Unmanned aerial vehicle solar cell panel fixed knot constructs
Technical Field
The utility model relates to an unmanned air vehicle technique field, more specifically say, relate to a fixed framework of unmanned aerial vehicle solar cell panel.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.
At present taking photo by plane, agriculture, plant protection, electric power is patrolled and examined, the relief of disaster, the application in numerous fields such as movie & TV shooting is very extensive, add on current unmanned aerial vehicle and establish solar cell panel and supply power and make its power consumption convenient, environmental protection and energy saving, more obtain extensive popularization and application, solar cell panel generally all is the snap-on the support frame, then install on the fuselage the support frame, but ordinary support can be more troublesome when fixing installation and dismantlement solar cell panel, and current fixed architecture that can adjust the solar cell panel size installs through using machinery, very easily cause the damage to solar cell panel, so need an unmanned aerial vehicle solar cell panel fixed architecture.
SUMMERY OF THE UTILITY MODEL
1. Technical problem to be solved
To the problem that exists among the prior art, the utility model aims to provide an unmanned aerial vehicle solar cell panel fixed framework, the convenience that possesses dismantles the installation advantage to solar cell panel, has solved the problem that above-mentioned background art mentioned.
2. Technical scheme
In order to solve the above problems, the utility model adopts the following technical proposal.
An unmanned aerial vehicle solar cell panel fixing framework comprises an unmanned aerial vehicle body, wherein a fixing plate is fixedly connected to the top of the unmanned aerial vehicle body, two through holes are formed in the top of the fixing plate, lifting rods are respectively and slidably connected to the inner walls of the two through holes, springs are respectively and fixedly connected to the inner bottom walls of the two through holes, the other ends of the two springs are respectively and fixedly connected with the two lifting rods, sliding rods fixedly connected with the lifting rods are respectively inserted into the two lifting rods, two sliding rods are respectively sleeved with two sliding blocks slidably connected with the sliding rods, a cell panel clamping seat is respectively and rotatably connected between the two sliding blocks on the left side and the two sliding blocks on the right side, a through groove is formed in the top of the fixing plate, a lead screw is rotatably connected to the inner wall of the through groove, the right end of the lead screw penetrates through and extends to, the battery board clamping device comprises two movable blocks, wherein the tops of the movable blocks are fixedly connected with vertical rods, the vertical rods are sleeved with lantern rings which are connected with the vertical rods in a sliding mode, one side, opposite to the lantern rings, of each lantern ring is integrally formed with a fixing piece, and the fixing pieces are clamped with two battery board clamping seats respectively.
Preferably, the opposite sides of the two battery panel clamping seats are provided with clamping grooves, and the clamping grooves are matched with the solar battery panels.
Preferably, bolt pieces are integrally formed on the opposite sides of the two battery plate clamping seats, and the two bolt pieces are respectively clamped with the two fixing pieces.
Preferably, two the mounting all is the N font, two the relative one side of mounting and two bolt spare one side of carrying on the back of the body all is the arc.
Preferably, the inner wall of the through groove is embedded with two bearings, and the inner rings of the two bearings are fixedly connected with the screw rod.
Preferably, the two ends of the sliding rod are fixedly connected with limiting blocks, and one side of each limiting block is fixedly connected with a rubber pad.
Preferably, the top end of the vertical rod is fixedly connected with a stop block, and the bottom of the stop block is fixedly connected with an elastic pad.
Preferably, the lifting rod is T-shaped.
3. Advantageous effects
Compared with the prior art, the utility model has the advantages of:
(1) the scheme can turn the side with the clamping groove to the front by rotating the cell panel clamping seat, a worker inserts the solar cell panel into the clamping groove for fixing, because the clamping groove is upward, the worker can easily align and insert the solar cell panel to complete the fixing, then pulls the cell panel clamping seat at the other side to the other side of the solar cell panel, simultaneously rotates the two cell panel clamping seats in opposite directions, the solar cell panel can align to the other clamping groove to complete the fixing of the other side after being inserted, through rotating the lead screw, the two moving blocks can drive the two vertical rods to move relatively, the lantern ring on the vertical rod can fix the cell panel clamping seat through the fixing piece, the fixing of the solar cell panel can be completed, the spring connected with the bottom of the lifting rod can buffer and absorb shock to protect the cell panel clamping seat, thereby protecting the solar cell panel, and the process is simple and, the angle of adjustable cell panel cassette is very convenient inserts solar cell panel into and fixes, can not cause the damage to solar cell panel, and two lantern rings can be quick carry on spacingly to the cell panel cassette, and the staff can be very convenient and fast when installing and dismantling solar cell panel.
(2) This scheme can grasp solar cell panel through the draw-in groove that relative one side of two panel cassette was all seted up and fix it, reachs the fixed purpose to solar cell panel, improves the convenience of device.
(3) Inside this scheme can insert the mounting through the fashioned bolt spare of the homogeneous body in the one side of carrying on the back of the body of two panel cassettes, reach the spacing fixed effect of panel cassette for the panel cassette can not slide on the slide bar again, improves the convenience of device.
(4) This scheme all is the N font through two mountings and can clip the bolt piece, reaches the purpose of fixing it, and relative one side of two mountings and the mutually backing on the back of the body one side of two bolt pieces all are the arc and can order about bolt piece and accomplish the purpose that the card sister is fixed in inserting the mounting, improves the practicality of device.
(5) This scheme inlays two bearings of establishing through the inner wall that leads to the groove and can reduce the friction between lead screw and the fixed plate, can let the quick control mounting of lead screw remove to the bolt spare and fix it, improves the practicality of device.
(6) This scheme can prevent through the equal fixed connection's in both ends stopper of slide bar that the slide bar is drawn to the slider, and the rubber pad can reduce because of the wearing and tearing that the contact produced between slider and the stopper, improves the life of device.
(7) The dog that this scheme passes through the top fixed connection of montant can prevent the lantern ring roll-off montant, and the cushion can cushion the impact of the lantern ring striking dog, improves the practicality of device.
(8) This scheme is the T font through the lifter and can prevents the lifter roll-off through-hole, improves the practicality of device.
Drawings
Fig. 1 is a schematic structural view of the present invention;
FIG. 2 is an enlarged view of portion A of FIG. 1 according to the present invention;
fig. 3 is a top view of the fixing plate of the present invention;
fig. 4 is a cross-sectional view of the middle fixing member and the battery panel clamping seat of the present invention.
The reference numbers in the figures illustrate:
1. an unmanned aerial vehicle body; 2. a fixing plate; 3. a through hole; 4. a lifting rod; 5. a spring; 6. a slide bar; 601. a limiting block; 602. a rubber pad; 7. a slider; 8. a battery plate clamping seat; 801. a card slot; 802. a latch member; 9. a through groove; 901. a bearing; 10. a screw rod; 11. a moving block; 12. a vertical rod; 13. a collar; 131. a stopper; 132. an elastic pad; 14. and a fixing member.
Detailed Description
The technical solution in the embodiment of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiment of the present invention; obviously, the described embodiments are only a part of the embodiments of the present invention, and not all embodiments, and all other embodiments obtained by those skilled in the art without any inventive work are within the scope of the present invention based on the embodiments of the present invention.
In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "top/bottom", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted", "provided", "sleeved/connected", "connected", and the like are to be understood in a broad sense, such as "connected", which may be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Referring to fig. 1-4, an unmanned aerial vehicle solar panel fixing framework comprises an unmanned aerial vehicle body 1, a fixing plate 2 is fixedly connected to the top of the unmanned aerial vehicle body 1, two through holes 3 are formed in the top of the fixing plate 2, lifting rods 4 are slidably connected to the inner walls of the two through holes 3, springs 5 are fixedly connected to the inner bottom walls of the two through holes 3, the other ends of the two springs 5 are respectively fixedly connected to the two lifting rods 4, slide rods 6 fixedly connected to the two lifting rods 4 are respectively inserted into the two lifting rods 4, two slide blocks 7 slidably connected to the two slide rods 6 are respectively sleeved on the two slide rods 6, a panel clamping seat 8 is rotatably connected between the two left slide blocks 7 and between the two right slide blocks 7, a through groove 9 is formed in the top of the fixing plate 2, a lead screw 10 is rotatably connected to the inner wall of the through groove 9, the lead screw 10 is sleeved with two moving blocks 11 in threaded connection with the lead screw, the tops of the two moving blocks 11 are fixedly connected with vertical rods 12, the two vertical rods 12 are sleeved with lantern rings 13 in sliding connection with the vertical rods, fixing pieces 14 are integrally formed on one opposite sides of the two lantern rings 13, the two fixing pieces 14 are respectively clamped with two battery plate clamping seats 8, one side with a clamping groove 801 can be turned to the front side by rotating the battery plate clamping seats 8, a worker inserts the solar battery plate into the clamping groove 801 to fix the solar battery plate, the worker can very easily align to insert the solar battery plate to complete the fixation because the clamping groove 801 is upward, then the battery plate clamping seat 8 on the other side is pulled to the other side of the solar battery plate, the two battery plate clamping seats 8 are rotated towards the opposite direction, the solar battery plate can align to the other clamping groove 801 to, through rotatory lead screw 10, two movable blocks 11 can drive two montant 12 relative movement, lantern ring 13 on montant 12 can be fixed the panel cassette 8 through mounting 14, can accomplish the fixed to solar cell panel, the spring 5 of 4 bottom connections of lifter can cushion shock attenuation protection to panel cassette 8, thereby protect solar cell panel, the operation of the process is simple and convenient, the angle of adjustable panel cassette 8 is very convenient to insert solar cell panel into and fix, can not cause the damage to solar cell panel, two lantern rings 13 can be quick carry out spacingly to panel cassette 8, the staff can be very convenient and fast when installing and dismantling solar cell panel.
Further, draw-in groove 801 has all been seted up to two relative one sides of panel cassette 8, draw-in groove 801 and solar cell panel phase-match, and draw-in groove 801 all seted up through two relative one sides of panel cassette 8 can grasp solar cell panel and fix it, reachs the fixed purpose to solar cell panel, improves the convenience of device.
Further, two equal integrated into one piece in the back of the body one side of two panel cassette 8 have bolt piece 802, and two bolt pieces 802 respectively with 14 looks joints of two mountings, through two panel cassette 8 back of the body one side of the back of the body fashioned bolt piece 802 in one side can insert inside 14 mountings, reach the spacing fixed effect to panel cassette 8 for slide on the slide bar 6 can not again in panel cassette 8, improve the convenience of device.
Further, two mountings 14 all are the N font, and relative one side of two mountings 14 and the back of the body one side of two bolt pieces 802 all are the arc, all are the N font through two mountings 14 and can clip bolt piece 802, reach the purpose of fixing it, and relative one side of two mountings 14 and the back of the body one side of two bolt pieces 802 all are the arc and can order about bolt piece 802 and accomplish the purpose that the card sister is fixed in inserting mounting 14, improves the practicality of device.
Further, the inner wall that leads to groove 9 inlays and is equipped with two bearings 901, and the inner circle of two bearings 901 all with lead screw 10 fixed connection, inlays two bearings 901 of establishing through the inner wall that leads to groove 9 and can reduce the friction between lead screw 10 and the fixed plate 2, can let the quick control mounting 14 of lead screw 10 remove to bolt piece 802 and fix it, improves the practicality of device.
Further, the two ends of the sliding rod 6 are fixedly connected with the limiting blocks 601, one side of each limiting block 601 is fixedly connected with the rubber pad 602, the sliding rod 6 can be prevented from being drawn out of the sliding block 7 through the limiting blocks 601 which are fixedly connected with the two ends of the sliding rod 6, the rubber pads 602 can reduce abrasion between the sliding block 7 and the limiting blocks 601 caused by contact, and the service life of the device is prolonged.
Further, the top fixedly connected with dog 131 of montant 12, the bottom fixedly connected with cushion 132 of dog 131, dog 131 through the top fixedly connected of montant 12 can prevent the lantern ring 13 roll-off montant 12, cushion 132 can cushion the impact that the lantern ring 13 strikes dog 131, improves the practicality of device.
Furthermore, lifter 4 is the T font, is the T font through lifter 4 and can prevent 4 roll-off through-holes 3 of lifter, improves the practicality of device.
The working principle is as follows: firstly, the panel clamping seat 8 is turned to the front side with the clamping groove 801, a worker inserts the solar panel into the clamping groove 801 to fix the solar panel, the worker can easily align with the clamping groove 801 to insert the solar panel to complete fixation because the clamping groove 801 is upward, then the panel clamping seat 8 at the other side is pulled to the other side of the solar panel, simultaneously the two panel clamping seats 8 are rotated towards the opposite direction, the solar panel can align with the other clamping groove 801 to complete fixation of the other side after being inserted into the clamping groove, the two movable blocks 11 can drive the two vertical rods 12 to move relatively by rotating the screw rod 10, the lantern ring 13 on the vertical rod 12 can fix the panel clamping seat 8 through the fixing part 14, and then fixation of the solar panel can be completed, the process is simple and convenient to operate, and the angle of the panel clamping seat 8 can be adjusted to conveniently insert the, spring 5 that 4 bottoms of lifter are connected can cushion shock attenuation protection to panel cassette 8, thereby protect solar cell panel, this process easy operation is convenient, the angle of adjustable panel cassette 8 is very convenient inserts solar cell panel into and fixes, can not cause the damage to solar cell panel, two lantern rings 13 can be quick carry on spacingly to panel cassette 8, the staff can be very convenient and fast when installing and dismantling solar cell panel, it can be more troublesome when fixing installation and dismantlement to solar cell panel to have solved ordinary support, and the fixed framework of current adjustable solar cell panel size is installed through using machinery, very easily cause the damage to solar cell panel.
The above is only a preferred embodiment of the present invention; the scope of the present invention is not limited thereto. Any person skilled in the art should also be able to cover the technical scope of the present invention by replacing or changing the technical solution and the improvement concept of the present invention with equivalents and modifications within the technical scope of the present invention.

Claims (8)

1. The utility model provides an unmanned aerial vehicle solar cell panel fixed knot constructs, includes unmanned aerial vehicle body (1), its characterized in that: the top of the unmanned aerial vehicle body (1) is fixedly connected with a fixed plate (2), the top of the fixed plate (2) is provided with two through holes (3), the inner walls of the two through holes (3) are respectively and slidably connected with lifting rods (4), the inner bottom walls of the two through holes (3) are respectively and fixedly connected with springs (5), the other ends of the two springs (5) are respectively and fixedly connected with the two lifting rods (4), the two lifting rods (4) are respectively and penetratingly inserted with sliding rods (6) fixedly connected with the lifting rods, the two sliding rods (6) are respectively sleeved with two sliding blocks (7) slidably connected with the sliding rods, a battery panel clamping seat (8) is rotatably connected between the two sliding blocks (7) on the left side and between the two sliding blocks (7) on the right side, the top of the fixed plate (2) is provided with a through groove (9), and the inner walls of the through groove, the right-hand member of lead screw (10) runs through and extends to the right side of fixed plate (2), the cover is equipped with two movable block (11) rather than threaded connection on lead screw (10), two the equal fixedly connected with montant (12) in top of movable block (11), two all the cover is equipped with the lantern ring (13) rather than sliding connection on montant (12), two the equal integrated into one piece in relative one side of the lantern ring (13) has mounting (14), two mounting (14) are connected with two panel cassette (8) looks joints respectively.
2. The unmanned aerial vehicle solar panel fixed architecture of claim 1, characterized in that: the opposite sides of the two battery panel clamping seats (8) are provided with clamping grooves (801), and the clamping grooves (801) are matched with the solar battery panels.
3. The unmanned aerial vehicle solar panel fixed architecture of claim 1, characterized in that: bolt pieces (802) are integrally formed on the opposite sides of the two battery plate clamping seats (8), and the two bolt pieces (802) are respectively clamped with the two fixing pieces (14).
4. The unmanned aerial vehicle solar panel fixed architecture of claim 3, characterized in that: the two fixing pieces (14) are both in an N shape, and the opposite sides of the two fixing pieces (14) and the opposite sides of the two bolt pieces (802) are both in an arc shape.
5. The unmanned aerial vehicle solar panel fixed architecture of claim 1, characterized in that: two bearings (901) are embedded in the inner wall of the through groove (9), and inner rings of the two bearings (901) are fixedly connected with the screw rod (10).
6. The unmanned aerial vehicle solar panel fixed architecture of claim 1, characterized in that: the two ends of the sliding rod (6) are fixedly connected with limiting blocks (601), and one side of each limiting block (601) is fixedly connected with a rubber pad (602).
7. The unmanned aerial vehicle solar panel fixed architecture of claim 1, characterized in that: the top end of the vertical rod (12) is fixedly connected with a stop block (131), and the bottom of the stop block (131) is fixedly connected with an elastic pad (132).
8. The unmanned aerial vehicle solar panel fixed architecture of claim 1, characterized in that: the lifting rod (4) is T-shaped.
CN202020976703.9U 2020-06-02 2020-06-02 Unmanned aerial vehicle solar cell panel fixed knot constructs Expired - Fee Related CN212195948U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202020976703.9U CN212195948U (en) 2020-06-02 2020-06-02 Unmanned aerial vehicle solar cell panel fixed knot constructs

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202020976703.9U CN212195948U (en) 2020-06-02 2020-06-02 Unmanned aerial vehicle solar cell panel fixed knot constructs

Publications (1)

Publication Number Publication Date
CN212195948U true CN212195948U (en) 2020-12-22

Family

ID=73812458

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202020976703.9U Expired - Fee Related CN212195948U (en) 2020-06-02 2020-06-02 Unmanned aerial vehicle solar cell panel fixed knot constructs

Country Status (1)

Country Link
CN (1) CN212195948U (en)

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