CN215753081U - Support unmanned aerial vehicle honeycomb that solar energy independently charges - Google Patents

Support unmanned aerial vehicle honeycomb that solar energy independently charges Download PDF

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Publication number
CN215753081U
CN215753081U CN202122394969.XU CN202122394969U CN215753081U CN 215753081 U CN215753081 U CN 215753081U CN 202122394969 U CN202122394969 U CN 202122394969U CN 215753081 U CN215753081 U CN 215753081U
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honeycomb
fixing
solar energy
shaft
fixed
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石建迈
靳晓洁
孙伟昌
郑龙
黄魁华
刘瑶
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National University of Defense Technology
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National University of Defense Technology
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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

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Abstract

The utility model discloses an unmanned aerial vehicle honeycomb supporting solar autonomous charging, which comprises a honeycomb main body, wherein fixing plates are fixedly connected to the upper parts of the left side and the right side of the honeycomb main body, shaft holes are formed in the middle parts of the fixing plates, rotating shafts are arranged in the shaft holes, and the rotating shafts are fixedly connected to the middle parts of the fixing frames, which are close to one end of the honeycomb main body. According to the solar energy collecting device, the fixing plates are fixed on two sides of the honeycomb main body, the fixing frame and the fixing plates can be connected through the rotating shaft, the rotating shaft can be pulled out of the shaft hole by one section, the fixing frame can rotate, so that the angle of the solar panel is adjusted, when the solar energy collecting device is used, the fixing frame is pressed down towards the direction of the fixing plates after the approximate angle is selected, the clamping columns can be inserted into the clamping holes, the fixing frame can be fixed through the clamping columns and the clamping holes, a person can adjust the angle of the solar panel, the solar panel can be better collected, and the solar energy collecting device is worthy of great popularization.

Description

Support unmanned aerial vehicle honeycomb that solar energy independently charges
Technical Field
The utility model relates to the field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle honeycomb supporting solar autonomous charging.
Background
The unmanned plane is called as an unmanned plane for short, is an unmanned aerial vehicle operated by utilizing a radio remote control device and a self-contained program control device, is a general name of the unmanned aerial vehicle in practice, and can be defined as follows from the technical point of view: compared with manned aircraft, the unmanned fixed wing aircraft has the advantages of small volume, low manufacturing cost, convenient use, low requirement on the operational environment, strong battlefield viability and the like.
At the in-process that uses the unmanned aerial vehicle honeycomb that supports solar energy autonomous charging, the unmanned aerial vehicle honeycomb that supports solar energy autonomous charging that has now on the market often still has two shortcomings when using, firstly it is owing to need satisfy the requirement of charging when using for it needs polylith solar panel, makes its volume too big, and occupation space is many, is difficult for depositing and shifting, secondly it can not carry out angle modulation to solar panel when using, makes its moment to the sun.
SUMMERY OF THE UTILITY MODEL
The utility model aims to solve the defects in the prior art, and provides an unmanned aerial vehicle honeycomb supporting solar autonomous charging.
In order to achieve the purpose, the utility model adopts the following technical scheme: the utility model provides a support unmanned aerial vehicle honeycomb that solar energy independently charges, includes the honeycomb main part, the equal fixedly connected with fixed plate in honeycomb main part left and right sides upper portion, the fixed plate middle part all is provided with the shaft hole, the inside pivot that all is provided with in shaft hole, the equal fixed connection in the one end middle part of fixed frame near the honeycomb main part of pivot, the middle part all is provided with the fixed axle between the fixed frame, the equal threaded connection of lower extreme has fixed cover on the fixed axle, the fixed axle middle part all is provided with the rotation cover, the fixed axle sheathes in with the rotation the lower part and all is provided with evenly distributed's locating hole, it all is provided with the stopper to rotate cover front side middle part, the equal fixedly connected with locating pin of lower part on the stopper rear end.
As a further description of the above technical solution:
the left side and the right side of the top end of the honeycomb main body are both connected with end covers in a sliding mode.
As a further description of the above technical solution:
the fixed plate is kept away from the one end middle part outside of honeycomb main part and all is provided with evenly distributed's card hole.
As a further description of the above technical solution:
the upper side and the lower side of the rotating shaft are provided with clamping columns.
As a further description of the above technical solution:
the inside solar panel that all fixedly connected with of fixed frame.
As a further description of the above technical solution:
the fixed sleeves are fixedly connected with the fixed frame.
As a further description of the above technical solution:
the locating pin keeps away from the one end of stopper and all sets up inside the locating hole.
As a further description of the above technical solution:
the positioning pins penetrate through the positioning holes.
The utility model has the following beneficial effects:
1. according to the honeycomb solar panel fixing device, the solar panel is arranged in the fixing frame, the solar panel can be conveniently fixed and connected through the fixing frame, the fixing sleeve and the rotating sleeve are arranged between the fixing frames, the fixing shafts are arranged in the middle of the fixing frames, the two solar panels can rotate relatively through the fixing shafts, the solar panels can be folded and extended, the limiting block is arranged at the front part of the rotating sleeve, the fixing frame can be fixed and limited through the fixing pins at the rear parts of the limiting blocks, the two solar panels can be fixed at an angle, and the honeycomb can be used in a small space, so that the honeycomb solar panel fixing device has good adaptability.
2. According to the solar energy collecting device, the fixing plates are fixed on two sides of the honeycomb main body, the fixing frame and the fixing plates can be connected through the rotating shaft, the rotating shaft can be pulled out of the shaft hole by one section, the fixing frame can rotate, so that the angle of the solar panel is adjusted, the clamping columns are arranged on the upper portion and the lower portion of the rotating shaft, the clamping holes are evenly distributed in the fixing plates, when the solar energy collecting device is used, the fixing frame is pressed down towards the direction of the fixing plate after the approximate angle is selected, the clamping columns can be inserted into the clamping holes, the fixing frame can be fixed through the clamping columns and the clamping holes, so that a person can adjust the angle of the solar panel, the solar energy collecting device can better collect solar energy, and the solar energy collecting device is worthy of great popularization.
Drawings
Fig. 1 is a perspective view of an unmanned aerial vehicle honeycomb supporting solar autonomous charging according to the present invention;
fig. 2 is a side view of a fixing plate of a honeycomb of an unmanned aerial vehicle supporting solar autonomous charging according to the present invention;
fig. 3 is a schematic structural view of a fixing shaft of a honeycomb of an unmanned aerial vehicle supporting solar autonomous charging according to the present invention;
fig. 4 is a schematic structural view of a positioning pin of a honeycomb of an unmanned aerial vehicle supporting solar autonomous charging according to the present invention;
fig. 5 is an enlarged view of a portion a in fig. 4.
Illustration of the drawings:
1. a honeycomb body; 2. an end cap; 3. a solar panel; 4. a fixing plate; 5. a rotating shaft; 6. fixing a sleeve; 7. clamping the column; 8. a clamping hole; 9. a shaft hole; 10. a fixing frame; 11. positioning holes; 12. rotating the sleeve; 13. a fixed shaft; 14. a limiting block; 15. and a positioning pin.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc., indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplicity of description, but do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention; the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance, and furthermore, unless otherwise explicitly stated or limited, the terms "mounted," "connected," and "connected" are to be construed broadly and may be, for example, 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 meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Referring to fig. 1-5, an embodiment of the present invention is provided: an unmanned aerial vehicle honeycomb supporting solar autonomous charging comprises a honeycomb main body 1, wherein the upper parts of the left side and the right side of the honeycomb main body 1 are fixedly connected with a fixed plate 4 for connecting a fixed frame 10, the middle parts of the fixed plates 4 are respectively provided with a shaft hole 9 for arranging a rotating shaft 5, the rotating shafts 5 are respectively arranged in the shaft holes 9, the rotating shafts 5 can be pulled out from the shaft holes 9 to enable the fixed frame 10 to rotate, the rotating shafts 5 are respectively fixedly connected with the middle part of one end, close to the honeycomb main body 1, of the fixed frame 10, the middle parts between the fixed frames 10 are respectively provided with a fixed shaft 13, the two solar panels 3 can relatively rotate through the fixed shafts 13 to enable the two solar panels to be folded and extended, the upper end and the lower end of each fixed shaft 13 are respectively in threaded connection with a fixed sleeve 6 to enable the fixed frames to be fixed, the middle parts of the fixed shafts 13 are respectively provided with a rotating sleeve 12 in a rotating connection way, and are rotatably connected between the fixed shafts, the fixed shaft 13 and the upper and lower parts of the rotating sleeve 12 are provided with uniformly distributed positioning holes 11 for matching with positioning pins 15, the middle part of the front side of the rotating sleeve 12 is provided with a limiting block 14, the upper and lower parts of the rear end of the limiting block 14 are fixedly connected with the positioning pins 15, and the fixing frame 10 can be fixed and limited by the positioning pins 15 at the rear part of the limiting block 14.
The left side and the right side of the top end of the honeycomb main body 1 are respectively connected with the end cover 2 in a sliding way so as to be convenient for opening, the middle outer side of one end of the fixed plate 4 far away from the honeycomb main body 1 is respectively provided with the clamping holes 8 which are uniformly distributed, when in use, the fixed frame 10 is pressed down towards the direction of the fixed plate 4 after selecting an approximate angle, the clamping posts 7 can be inserted into the clamping holes 8, the fixed frame 10 can be fixed through the clamping posts 7 and the clamping holes 8, so that a person can adjust the angle of the solar panel 3, the solar panel can better collect solar energy, the clamping posts 7 are respectively arranged at the upper side and the lower side of the rotating shaft 5 and are used for being matched with the clamping holes 8, the solar panel 3 is respectively and fixedly connected in the fixed frame 10, the solar panel 3 can be conveniently fixed and connected through the fixed frame 10, the fixed sleeve 6 is respectively and fixedly connected with the fixed frame 10, one end of the positioning pin 15 far away from the limiting block 14 is respectively arranged in the positioning hole 11, locating pin 15 all runs through locating hole 11, and locating pin 15 through stopper 14 rear portion can fix fixed frame 10 spacing, makes and can fix at an angle between its two solar panel 3 for the honeycomb can use in less space, makes it can have better adaptability.
The working principle is as follows: firstly, the solar panels 3 are arranged inside a fixed frame 10, the solar panels 3 can be conveniently fixed and connected through the fixed frame 10, a fixed sleeve 6 and a rotating sleeve 12 are arranged between the fixed frames 10, a fixed shaft 13 is arranged at the middle parts of the fixed frames and the rotating sleeve 12, the two solar panels 3 can relatively rotate through the fixed shaft 13 to be folded and extended, a limit block 14 is arranged at the front part of the rotating sleeve 12, the fixed frame 10 can be fixed and limited through a positioning pin 15 at the rear part of the limit block 14, so that the two solar panels 3 can be fixed at an angle, the honeycomb can be used in a small space and has good adaptability, fixed plates 4 are fixed at both sides of a honeycomb main body 1, the fixed frame 10 and the fixed plates 4 can be connected through a rotating shaft 5, and the rotating shaft 5 can be pulled out a section from a shaft hole 9, make fixed frame 10 can rotate, thereby adjust solar panel 3's angle, all be provided with card post 7 in the upper and lower portion of pivot 5 simultaneously, be provided with evenly distributed's card hole 8 on fixed plate 4, when using, press fixed frame 10 to fixed plate 4's direction after choosing approximate angle, can insert card post 7 inside card hole 8, can fix fixed frame 10 through card post 7 and card hole 8, make the people can carry out angle modulation to solar panel 3, make its collection solar energy that can be better, be worth wideling popularize.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments or portions thereof without departing from the spirit and scope of the utility model.

Claims (8)

1.一种支持太阳能自主充电的无人机蜂巢,包括蜂巢主体(1),其特征在于:所述蜂巢主体(1)左右侧上部均固定连接有固定板(4),所述固定板(4)中部均设置有轴孔(9),所述轴孔(9)内部均设置有转轴(5),所述转轴(5)均固定连接在固定框(10)靠近蜂巢主体(1)的一端中部,所述固定框(10)之间中部均设置有固定轴(13),所述固定轴(13)上下端均螺纹连接有固定套(6),所述固定轴(13)中部均设置有转动连接有转动套(12),所述固定轴(13)与转动套(12)上下部均设置有均匀分布的定位孔(11),所述转动套(12)前侧中部均设置有限位块(14),所述限位块(14)后端上下部均固定连接有定位销(15)。1. An unmanned aerial vehicle honeycomb supporting solar energy autonomous charging, comprising a honeycomb body (1), characterized in that: the upper left and right sides of the honeycomb body (1) are fixedly connected with a fixing plate (4), and the fixing plate ( 4) A shaft hole (9) is arranged in the middle, and a rotating shaft (5) is arranged inside the shaft hole (9), and the rotating shaft (5) is fixedly connected to the fixing frame (10) close to the honeycomb body (1). A fixing shaft (13) is arranged in the middle of one end and between the fixing frames (10), the upper and lower ends of the fixing shaft (13) are threadedly connected with fixing sleeves (6), and the middle of the fixing shaft (13) is A rotating sleeve (12) is provided in a rotatable connection, the upper and lower parts of the fixed shaft (13) and the rotating sleeve (12) are provided with evenly distributed positioning holes (11), and the front and middle parts of the rotating sleeve (12) are provided with A limiting block (14), the upper and lower parts of the rear end of the limiting block (14) are fixedly connected with positioning pins (15). 2.根据权利要求1所述的一种支持太阳能自主充电的无人机蜂巢,其特征在于:所述蜂巢主体(1)顶端左右两侧均滑动连接有端盖(2)。2 . The drone honeycomb supporting solar energy autonomous charging according to claim 1 , characterized in that: the top left and right sides of the honeycomb main body (1) are slidably connected with end caps (2). 3 . 3.根据权利要求1所述的一种支持太阳能自主充电的无人机蜂巢,其特征在于:所述固定板(4)远离蜂巢主体(1)的一端中部外侧均设置有均匀分布的卡孔(8)。3. A UAV honeycomb supporting solar energy autonomous charging according to claim 1, characterized in that: the fixing plate (4) is provided with evenly distributed clamping holes on the outer side of one end of the fixing plate (4) away from the honeycomb main body (1). (8). 4.根据权利要求1所述的一种支持太阳能自主充电的无人机蜂巢,其特征在于:所述转轴(5)上下侧均设置有卡柱(7)。4 . The drone honeycomb supporting solar autonomous charging according to claim 1 , wherein the upper and lower sides of the rotating shaft ( 5 ) are provided with clamping posts ( 7 ). 5 . 5.根据权利要求1所述的一种支持太阳能自主充电的无人机蜂巢,其特征在于:所述固定框(10)内部均固定连接有太阳能板(3)。5. A drone honeycomb supporting solar energy autonomous charging according to claim 1, wherein a solar panel (3) is fixedly connected inside the fixing frame (10). 6.根据权利要求1所述的一种支持太阳能自主充电的无人机蜂巢,其特征在于:所述固定套(6)均与固定框(10)固定连接。6 . The drone honeycomb supporting solar energy autonomous charging according to claim 1 , wherein the fixing sleeves ( 6 ) are all fixedly connected with the fixing frame ( 10 ). 7 . 7.根据权利要求1所述的一种支持太阳能自主充电的无人机蜂巢,其特征在于:所述定位销(15)远离限位块(14)的一端均设置在定位孔(11)内部。7. A drone honeycomb supporting solar energy autonomous charging according to claim 1, characterized in that: one end of the positioning pin (15) away from the limit block (14) is arranged inside the positioning hole (11) . 8.根据权利要求1所述的一种支持太阳能自主充电的无人机蜂巢,其特征在于:所述定位销(15)均贯穿定位孔(11)。8 . The drone honeycomb supporting solar energy autonomous charging according to claim 1 , wherein the positioning pins ( 15 ) all pass through the positioning holes ( 11 ). 9 .
CN202122394969.XU 2021-09-30 2021-09-30 Support unmanned aerial vehicle honeycomb that solar energy independently charges Active CN215753081U (en)

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CN202122394969.XU CN215753081U (en) 2021-09-30 2021-09-30 Support unmanned aerial vehicle honeycomb that solar energy independently charges

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Application Number Priority Date Filing Date Title
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