CN213057509U - Aerial throwing device of unmanned aerial vehicle - Google Patents

Aerial throwing device of unmanned aerial vehicle Download PDF

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Publication number
CN213057509U
CN213057509U CN202021358527.9U CN202021358527U CN213057509U CN 213057509 U CN213057509 U CN 213057509U CN 202021358527 U CN202021358527 U CN 202021358527U CN 213057509 U CN213057509 U CN 213057509U
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China
Prior art keywords
unmanned aerial
aerial vehicle
movable rod
battery
fixed mounting
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CN202021358527.9U
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Chinese (zh)
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董平均
高平
李�浩
罗会
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Hebei Yinglan Automation Technology Co ltd
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Hebei Yinglan Automation Technology Co ltd
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Abstract

The utility model discloses an aerial ware of jettisoninging of unmanned aerial vehicle, including the unmanned aerial vehicle organism, unmanned aerial vehicle organism upper end central point puts fixed mounting and is provided with the battery, battery upper end position level fixed mounting is provided with solar cell panel, solar cell panel and battery electric connection, unmanned aerial vehicle organism lower extreme central point puts fixed mounting and is provided with hollow block, the spout is passed respectively to the movable rod both sides, both sides are all fixed the stopper that is provided with about the movable rod. The utility model discloses a remote control unit control starts the electro-magnet for the electro-magnet attracts the magnetic metal piece, makes the movable rod be the clamping motion, utilizes the grip block can the fixed article of centre gripping, and extension spring when the movable rod removes simultaneously, later when the unmanned aerial vehicle organism removes to the destination point, the user utilizes remote control unit to close the electro-magnet, makes the electro-magnet lose magnetism, and the spring drives the movable rod and resets, makes article deviate from, prevents that article from breaking away from the too big problem of error that drops that the time delay caused.

Description

Aerial throwing device of unmanned aerial vehicle
Technical Field
The utility model relates to an unmanned aerial vehicle equipment field specifically is an unmanned aerial vehicle ware of jettisoninging in air.
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.
Unmanned planes tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than manned aircraft; unmanned aerial vehicles can be classified into military and civil according to application fields; for military use, unmanned aerial vehicles are divided into reconnaissance aircraft and target drone; in the civil aspect, the unmanned aerial vehicle + industry is applied, and is really just needed by the unmanned aerial vehicle.
Unmanned aerial vehicle need utilize the device of jettisoninging to carry out the transportation of goods when using, and current jettisoninging device uses the operability relatively poor, and clamping part can not launch on time sometimes when jettisoninging, leads to jettisoninging place error great to unmanned aerial vehicle duration is shorter, so the above-mentioned problem is solved to urgent needs a device.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an aerial ware of jettisoninging of unmanned aerial vehicle to solve the problem that proposes in the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle aerial jettison device comprises an unmanned aerial vehicle body, wherein a storage battery is fixedly arranged at the central position of the upper end of the unmanned aerial vehicle body, a solar cell panel is horizontally and fixedly arranged at the upper end of the storage battery, the solar cell panel is electrically connected with the storage battery, the solar cell panel is convenient for converting solar energy into electric energy to be stored in the storage battery, so that the cruising time of the unmanned aerial vehicle body is effectively prolonged, and the transportation capacity of the unmanned aerial vehicle body is improved, a hollow block is fixedly arranged at the central position of the lower end of the unmanned aerial vehicle body, a sliding groove is horizontally formed in the central position of the front end of the hollow block, a movable rod is vertically movably and alternately arranged in the hollow block, two side ends of the movable rod respectively penetrate through the sliding groove, the movable rod slides left and right along the sliding groove, limit, left side horizontal fixed connection in position between movable rod left side end and the inside left side wall of hollow block is provided with the spring, the right side horizontal fixed connection in position between movable rod right side end position and the inside right side wall of hollow block is provided with the spring, and the spring is convenient for the movable rod to reset, the left side horizontal fixed mounting in movable rod central point position is provided with the electro-magnet, the right side the movable rod left side end central point puts and inlays fixedly to be provided with magnetic metal piece, the inside fixed mounting of unmanned aerial vehicle organism is provided with the control box, the control box is provided with remote control unit through wireless connection, and remote control unit is convenient for through the motion of control box control unmanned aerial vehicle organism, stopper lower extreme welded fastening is provided with the extension rod, the inboard welded fastening of extension rod lower extreme is provided with the grip block.
Preferably, battery and unmanned aerial vehicle organism electric connection utilize the battery to supply power for the unmanned aerial vehicle organism.
Preferably, the sliding groove is communicated with the inside of the hollow block.
Preferably, the electromagnet is electrically connected with the storage battery.
Preferably, the control box is electrically connected with the electromagnet.
Preferably, the outer surface of the non-slip mat is provided with non-slip bulges.
Compared with the prior art, the beneficial effects of the utility model are that:
1. the solar cell panel of the utility model is convenient for converting solar energy into electric energy to be stored in the internal position of the storage battery, thereby effectively improving the endurance time of the unmanned aerial vehicle body and further improving the transport capacity of the unmanned aerial vehicle body;
2. the utility model discloses a remote control unit control starts the electro-magnet for the electro-magnet attracts the magnetic metal piece, makes the movable rod be the clamping motion, utilizes the grip block can the fixed article of centre gripping, and extension spring when the movable rod removes simultaneously, later when the unmanned aerial vehicle organism removes to the destination point, the user utilizes remote control unit to close the electro-magnet, makes the electro-magnet lose magnetism, and the spring drives the movable rod and resets, makes article deviate from, prevents that article from breaking away from the too big problem of error that drops that the time delay caused.
Drawings
Fig. 1 is a schematic view of the overall structure of an unmanned aerial vehicle aerial throwing device of the utility model;
fig. 2 is a schematic structural view of a hollow block of the unmanned aerial vehicle aerial throwing device of the present invention;
fig. 3 is the utility model relates to a system diagram of aerial ware of jettisoninging of unmanned aerial vehicle.
In the figure: 1. an unmanned aerial vehicle body; 2. a storage battery; 3. a solar panel; 4. a hollow block; 5. a chute; 6. a limiting block; 7. an extension rod; 8. a clamping plate; 9. a non-slip mat; 10. a movable rod; 11. an electromagnet; 12. a spring; 13. a magnetic metal sheet; 14. a control box; 15. a remote control device.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-3, the present invention provides a technical solution: an unmanned aerial vehicle aerial jettison device comprises an unmanned aerial vehicle body 1, a storage battery 2 is fixedly arranged at the central position of the upper end of the unmanned aerial vehicle body 1, the storage battery 2 is electrically connected with the unmanned aerial vehicle body 1, the storage battery 2 is used for supplying power to the unmanned aerial vehicle body 1, a solar cell panel 3 is horizontally and fixedly arranged at the upper end position of the storage battery 2, the solar cell panel 3 is electrically connected with the storage battery 2, the solar cell panel 3 is convenient for converting solar energy into electric energy to be stored at the internal position of the storage battery 2, so that the endurance time of the unmanned aerial vehicle body 1 is effectively improved, the transportation capability of the unmanned aerial vehicle body 1 is improved, a hollow block 4 is fixedly arranged at the central position of the lower end of the unmanned aerial vehicle body 1, a chute 5 is horizontally arranged at the central position of the front end of the hollow block 4, the chute 5 is, the movable rod 10 slides left and right along the sliding chute 5, the upper and lower side ends of the movable rod 10 are respectively welded and fixed with a limiting block 6, the limiting blocks 6 prevent the movable rod 10 from separating from the hollow block 4, a spring 12 is horizontally and fixedly connected between the left side end of the left movable rod 10 and the left side wall inside the hollow block 4, a spring 12 is horizontally and fixedly connected between the right side end of the right movable rod 10 and the right side wall inside the hollow block 4, the spring 12 facilitates the reset of the movable rod 10, an electromagnet 11 is horizontally and fixedly installed at the center position of the left movable rod 10, the electromagnet 11 is electrically connected with the storage battery 2, a magnetic metal sheet 13 is embedded and fixed at the center position of the left side end of the right movable rod 10, a control box 14 is fixedly installed inside the unmanned aerial vehicle body 1, the control box 14 is electrically connected with the electromagnet 11, the control box 14 is wirelessly connected with a remote, an extension rod 7 is fixedly welded at the lower end of the limiting block 6, a clamping plate 8 is fixedly welded at the inner side of the lower end of the extension rod 7, an anti-skid pad 9 is fixedly bonded on the surface of the inner side end of the clamping plate 8, and an anti-skid bump is arranged on the outer surface of the anti-skid pad 9.
The working principle is as follows: the utility model discloses a solar cell panel 3 is convenient for change solar energy and is stored in battery 2 internal position for the electric energy, thereby effectively improve the duration of a journey of unmanned aerial vehicle organism 1, thereby improve the transportation ability of unmanned aerial vehicle organism 1, the article that will wait to transport during the use is settled between grip block 8 position, then start electromagnet 11 through remote control equipment 15 control, make electromagnet 11 attract magnetic metal piece 13, make movable rod 10 be the centre gripping motion, utilize grip block 8 can centre gripping fixed article, simultaneously extension spring 12 when movable rod 10 removes, later when unmanned aerial vehicle organism 1 removes to the destination point, the user utilizes remote control equipment 15 to close electromagnet 11, make electromagnet 11 lose magnetism, spring 12 drives movable rod 10 and resets, make article deviate from, prevent that article from the too big problem of drop error that the time delay caused, and have simple structure, convenient to use, The use effect is good.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims (6)

1. The utility model provides an aerial jettison ware of unmanned aerial vehicle, includes unmanned aerial vehicle organism (1), its characterized in that: unmanned aerial vehicle organism (1) upper end central point puts fixed mounting and is provided with battery (2), battery (2) upper end position horizontal fixed mounting is provided with solar cell panel (3), solar cell panel (3) and battery (2) electric connection, unmanned aerial vehicle organism (1) lower extreme central point puts fixed mounting and is provided with hollow block (4), spout (5) have been seted up to hollow block (4) front end central point level, the inside vertical movement interlude of hollow block (4) is provided with movable rod (10), spout (5) are passed respectively to movable rod (10) both sides end, both sides end is all fixed about movable rod (10) and is provided with stopper (6), the left side between movable rod (10) left side end and the inside left side wall of hollow block (4) horizontal fixed connection of position is provided with spring (12), right side between movable rod (10) right side position and the inside right side wall of hollow block (4) position level (6), left side Fixed connection is provided with spring (12), left side the horizontal fixed mounting of movable rod (10) central point position is provided with electro-magnet (11), right side movable rod (10) left side end central point puts fixed magnetic metal piece (13) of being provided with, unmanned aerial vehicle organism (1) inside fixed mounting is provided with control box (14), control box (14) are provided with remote control unit (15) through wireless connection, stopper (6) lower extreme is fixed and is provided with extension rod (7), extension rod (7) lower extreme inboard is fixed and is provided with grip block (8), grip block (8) medial extremity fixed surface is provided with slipmat (9).
2. An unmanned aerial vehicle aerial tosser as claimed in claim 1, wherein: battery (2) and unmanned aerial vehicle organism (1) electric connection.
3. An unmanned aerial vehicle aerial tosser as claimed in claim 1, wherein: the sliding groove (5) is communicated with the inside of the hollow block (4).
4. An unmanned aerial vehicle aerial tosser as claimed in claim 1, wherein: the electromagnet (11) is electrically connected with the storage battery (2).
5. An unmanned aerial vehicle aerial tosser as claimed in claim 1, wherein: the control box (14) is electrically connected with the electromagnet (11).
6. An unmanned aerial vehicle aerial tosser as claimed in claim 1, wherein: and the outer surface of the non-slip mat (9) is provided with non-slip bulges.
CN202021358527.9U 2020-07-10 2020-07-10 Aerial throwing device of unmanned aerial vehicle Active CN213057509U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202021358527.9U CN213057509U (en) 2020-07-10 2020-07-10 Aerial throwing device of unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202021358527.9U CN213057509U (en) 2020-07-10 2020-07-10 Aerial throwing device of unmanned aerial vehicle

Publications (1)

Publication Number Publication Date
CN213057509U true CN213057509U (en) 2021-04-27

Family

ID=75572800

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202021358527.9U Active CN213057509U (en) 2020-07-10 2020-07-10 Aerial throwing device of unmanned aerial vehicle

Country Status (1)

Country Link
CN (1) CN213057509U (en)

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