CN220096661U - Survey and drawing unmanned aerial vehicle with self preservation protects function - Google Patents

Survey and drawing unmanned aerial vehicle with self preservation protects function Download PDF

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Publication number
CN220096661U
CN220096661U CN202321213709.0U CN202321213709U CN220096661U CN 220096661 U CN220096661 U CN 220096661U CN 202321213709 U CN202321213709 U CN 202321213709U CN 220096661 U CN220096661 U CN 220096661U
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China
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fixedly connected
wall
aerial vehicle
unmanned aerial
main body
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CN202321213709.0U
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贺爽
薛飞
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Huaian Construction Engineering Quality Inspection Center Co ltd
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Huaian Construction Engineering Quality Inspection Center Co ltd
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Abstract

The utility model provides a surveying and mapping unmanned aerial vehicle with a self-protection function, which comprises a main body and a supporting plate connected to the side wall of the main body, wherein two to five groups of supporting plates are uniformly distributed on the side wall of the main body, and the surveying and mapping unmanned aerial vehicle further comprises: the protection component comprises a dragging frame which is connected to the inner wall of the main body in a sliding way, sliding blocks are fixedly connected to two sides of the dragging frame, clamping plates are fixedly connected to the inner wall of the sliding blocks in a sliding way, a group of mapping instruments are fixedly connected to the side walls of the clamping plates, electromagnets are fixedly connected to the side walls of the sliding blocks, magnetic attraction stones are fixedly connected to the side walls of the clamping plates, the electromagnets are matched with the magnetic attraction stones, and parachutes are fixedly connected to the top walls of the mapping instruments; the storage component is connected to the inner wall of the main body and is matched with the dragging frame; cleaning component connects in the surveying instrument lateral wall, through setting up electro-magnet and magnetism and inhale the stone, is convenient for protect the surveying instrument when unmanned aerial vehicle breaks down, is convenient for improve the accuracy of survey and drawing through the cleaning rod.

Description

Survey and drawing unmanned aerial vehicle with self preservation protects function
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a surveying and mapping unmanned aerial vehicle with a self-protection function.
Background
The unmanned aerial vehicle is a unmanned aerial vehicle operated by using radio remote control equipment and a self-provided program control device, and has the advantages of small volume, low cost, convenient use, low requirement on battle environment, stronger battlefield survivability and the like compared with a manned aerial vehicle.
Through retrieving, chinese patent application number is CN 202220003584.8's patent, a topography is unmanned aerial vehicle for survey and drawing with self preservation protects function is disclosed, belong to unmanned aerial vehicle technical field, including the unmanned aerial vehicle main part, unmanned aerial vehicle main part both sides lateral wall bottom transversely punishment is equipped with electric telescopic machine, electric telescopic machine's urceolus limit department is equipped with rotor subassembly, and be equipped with the buffer board in electric telescopic machine's tip department, drive crashproof buffer unit through electric telescopic machine and remove when will bump, reducible collision, can play the function of buffering through crashproof buffer unit when bumping, crashproof buffer unit also plays the function of protection rotor subassembly when rotor subassembly rotates, prevent that rotor subassembly from bumping, result in unmanned aerial vehicle accident to descend, can realize shooting the function to different angles through taking a picture the subassembly, play the regulation is convenient, the effectual effect of use, realize the function of falling to the ground buffering through descending buffer unit unmanned aerial vehicle when unmanned aerial vehicle descends, can be in the buffering with the power between the ground.
The above patents have the following disadvantages: 1. when the unmanned aerial vehicle crashes in a high altitude, the unmanned aerial vehicle is inconvenient to protect the camera and the mapping data, the damage to the mapping data and the camera is easy to cause after the unmanned aerial vehicle crashes, and the unmanned aerial vehicle is inconvenient to use; 2. when the camera is used, because dust exists in the air, a large amount of dust is easily attached to the camera, so that the accuracy of mapping is affected.
Therefore, a mapping unmanned aerial vehicle with self-protection function is needed to solve the above problems.
Disclosure of Invention
The utility model aims at: aiming at the existing situation that when the unmanned aerial vehicle breaks down and crashes in the high air at present, the unmanned aerial vehicle is inconvenient to protect a camera and mapping data, the damage to the mapping data and the camera is easy to cause after the unmanned aerial vehicle crashes, and the unmanned aerial vehicle is inconvenient to use; when the camera is used, because dust exists in the air, a large amount of dust is easily attached to the camera, so that the accuracy of mapping is affected.
In order to achieve the above object, the present utility model provides the following technical solutions:
survey and drawing unmanned aerial vehicle with self preservation protects function to improve above-mentioned problem.
The utility model is specifically as follows:
survey and drawing unmanned aerial vehicle with self preservation protects function, include the main part and connect in the backup pad of main part lateral wall, the backup pad has two to five groups about main part lateral wall evenly distributed, still includes:
the protection component comprises a dragging frame which is connected to the inner wall of the main body in a sliding way, sliding blocks are fixedly connected to two sides of the dragging frame, clamping plates are connected to the inner wall of the sliding blocks in a sliding way, a group of mapping instruments are fixedly connected to the side walls of the clamping plates, electromagnets are fixedly connected to the side walls of the sliding blocks, magnetic attraction stones are fixedly connected to the side walls of the clamping plates, the electromagnets are matched with the magnetic attraction stones, and parachutes are fixedly connected to the top walls of the mapping instruments;
the storage component is connected to the inner wall of the main body and is matched with the dragging frame;
cleaning component is connected in the surveying instrument lateral wall.
As the preferable technical scheme of the utility model, the top wall of the parachute is fixedly connected with a pull rope, and one end of the pull rope far away from the parachute is also connected with a dragging frame.
As the preferable technical scheme of the utility model, the containing part comprises a lifting screw rod rotatably connected to the inner wall of the main body, the inner wall of the main body is fixedly connected with a sliding frame, the lifting screw rod is in threaded connection with the dragging frame, and the sliding frame is in sliding connection with the dragging frame.
As the preferable technical scheme of the utility model, the cleaning component comprises an air cylinder fixedly connected with the side wall of the surveying instrument, the side wall of the surveying instrument is slidably connected with the cleaning rod, and the output end of the air cylinder is fixedly connected with the cleaning rod.
As the preferable technical scheme of the utility model, the side wall of the supporting plate is connected with the supporting frame, the side wall of the supporting frame is connected with the propeller, the side wall of the main body is fixedly connected with the landing gear, the top wall of the main body is fixedly connected with the solar panel, the inner wall of the main body is fixedly connected with the storage battery, and the propeller is not specifically described in detail in the prior art.
In the scheme of the utility model:
1. through setting up protection component, through being on to the electro-magnet, thereby make the electro-magnet produce magnetism, inhale and the principle of repulsion through magnetism mutually, thereby promote magnetism stone to push out the cardboard in the sliding block, drop the surveying instrument through the cardboard, when the surveying instrument is kept away from dragging the frame, thereby open the parachute through the stay cord, play the effect of buffering protection when falling the surveying instrument through the parachute, when preventing that unmanned aerial vehicle from breaking down, lead to survey and drawing data damage, more facilitate the use, when having solved in the prior art in carrying out survey and drawing work, when unmanned aerial vehicle breaks down and crash in the high altitude, be inconvenient for protecting camera and survey and drawing data, easily lead to unmanned aerial vehicle crash after, survey and drawing data and camera damage, inconvenient use's problem;
2. through setting up the clearance part, through starting the cylinder, the cylinder promotes the cleaning rod and cleans the position of making a video recording to clear away the dust, improved the accuracy of survey and drawing, solved among the prior art when using, because there is the dust in the air, lead to adhering to a large amount of dust on the camera easily, thereby influenced the problem of the accuracy of survey and drawing.
Drawings
Fig. 1 is a schematic diagram of the overall structure of a mapping unmanned aerial vehicle with a self-protection function;
FIG. 2 is a second schematic diagram of the overall structure of the mapping unmanned aerial vehicle with self-protection function according to the present utility model;
fig. 3 is a schematic diagram of a part of a mapping unmanned aerial vehicle with a self-protection function according to the present utility model;
FIG. 4 is a second schematic diagram of a part of a mapping unmanned aerial vehicle with self-protection function according to the present utility model;
fig. 5 is a third schematic diagram of a part of a mapping unmanned aerial vehicle with a self-protection function according to the present utility model.
The figures indicate: 100. a main body; 101. a support plate; 110. a dragging frame; 111. a sliding block; 112. a clamping plate; 113. a mapping instrument; 114. an electromagnet; 115. magnetic stone; 116. a parachute; 117. a pull rope; 120. lifting screw rods; 121. a carriage; 130. a cylinder; 131. a cleaning rod; 140. a support frame; 141. a propeller; 142. landing gear; 143. a solar panel.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present utility model more clear, the technical solutions of the embodiments of the present utility model will be clearly and completely described below with reference to the accompanying drawings. It will be apparent that the described embodiments are some, but not all, embodiments of the utility model.
Thus, the following detailed description of the embodiments of the utility model is not intended to limit the scope of the utility model, as claimed, but is merely representative of some embodiments of the utility model. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
It should be noted that, under the condition of no conflict, the embodiments of the present utility model and the features and technical solutions in the embodiments may be combined with each other.
It should be noted that: like reference numerals and letters denote like items in the following figures, and thus once an item is defined in one figure, no further definition or explanation thereof is necessary in the following figures.
In the description of the present utility model, it should be noted that, the terms "upper", "lower", and the like indicate an azimuth or a positional relationship based on the azimuth or the positional relationship shown in the drawings, or an azimuth or a positional relationship conventionally put in use of the inventive product, or an azimuth or a positional relationship conventionally understood by those skilled in the art, such terms are merely for convenience of describing the present utility model and simplifying the description, and do not indicate or imply that the apparatus or element to be referred must have a specific azimuth, be constructed and operated in a specific azimuth, and thus should not be construed as limiting the present utility model. Furthermore, the terms "first," "second," and the like, are used merely to distinguish between descriptions and should not be construed as indicating or implying relative importance.
As shown in fig. 1-4, this embodiment provides a mapping unmanned aerial vehicle with self-protection function, including main part 100 and connect in the backup pad 101 of main part 100 lateral wall, backup pad 101 has two to five groups about main part 100 lateral wall evenly distributed, still includes:
the protection component comprises a dragging frame 110 which is connected to the inner wall of the main body 100 in a sliding way, sliding blocks 111 are fixedly connected to two sides of the dragging frame 110, clamping plates 112 are fixedly connected to the inner wall of the sliding blocks 111, a group of mapping instruments 113 are fixedly connected to the side walls of the clamping plates 112, electromagnets 114 are fixedly connected to the side walls of the sliding blocks 111, magnetic attractors 115 are fixedly connected to the side walls of the clamping plates 112, the electromagnets 114 are matched with the magnetic attractors 115, and parachutes 116 are fixedly connected to the top walls of the mapping instruments 113;
the storage component is connected to the inner wall of the main body 100 and is matched with the dragging frame 110;
cleaning component connects in the surveying instrument 113 lateral wall, through setting up electro-magnet 114 and magnetism and inhale stone 115, is convenient for when unmanned aerial vehicle breaks down, drops through surveying instrument 113, can effectually protect surveying and mapping data, convenient to use more.
As shown in fig. 1 to 3, as a preferred embodiment, further, based on the above manner, a pull rope 117 is fixedly connected to the top wall of the parachute 116, one end of the pull rope 117 away from the parachute 116 is also connected to the dragging frame 110, and when the surveying instrument 113 falls off, the parachute 116 is opened by the pull rope 117 under the action of gravity, so that the practicability is improved.
As shown in fig. 1 to 5, as a preferred embodiment, based on the above manner, further, the storage component includes a lifting screw 120 rotatably connected to an inner wall of the main body 100, a sliding frame 121 is fixedly connected to the inner wall of the main body 100, the lifting screw 120 is in threaded connection with the dragging frame 110, the sliding frame 121 is slidably connected to the dragging frame 110, and by setting the lifting screw 120, the storage of the surveying instrument 113 is facilitated, and the carrying is facilitated.
As shown in fig. 1-3, as a preferred embodiment, on the basis of the above manner, the cleaning component further includes a cylinder 130 fixedly connected to the side wall of the surveying instrument 113, the side wall of the surveying instrument 113 is slidably connected with a cleaning rod 131, the output end of the cylinder 130 is fixedly connected with the cleaning rod 131, and cleaning of the surveying instrument 113 is facilitated when in use by the arrangement of the cylinder 130 and the cleaning rod 131, so that accuracy of surveying and mapping is facilitated to be improved.
As shown in fig. 1-2, as a preferred embodiment, on the basis of the above manner, further, the side wall of the supporting plate 101 is connected with the supporting frame 140, the side wall of the supporting frame 140 is connected with the propeller 141, the side wall of the main body 100 is fixedly connected with the landing gear 142, the top wall of the main body 100 is fixedly connected with the solar panel 143, the inner wall of the main body 100 is fixedly connected with the storage battery, the propeller 141 is not described in detail herein for the prior art, and by arranging the solar panel 143, a part of electric power can be provided for the storage battery when in use, thereby improving the adaptability.
Specifically, this survey and drawing unmanned aerial vehicle with self preservation protects function when using: thereby having driven main part 100 through start screw 141 and having risen, when rising suitable position on, through starting elevating screw 120, drive and drag frame 110 downstream, drag frame 110 and slide down at carriage 121 outer wall, thereby it goes out main part 100 to have driven surveying instrument 113 downstream, then survey work, when the position is made a video recording to surveying instrument 113 during the use, when adhering to the dust, through starting cylinder 130, cylinder 130 promotes cleaning rod 131 and cleans the position of making a video recording, thereby the dust is cleared, the accuracy of survey and drawing has been improved, when unmanned aerial vehicle breaks down, through being circular telegram to electro-magnet 114, thereby make electro-magnet 114 produce magnetism, attract and repel the principle through magnetism, thereby promote magnetism magnet 115 to release cardboard 112 in sliding block 111, drop surveying instrument 113 through cardboard 112, thereby when surveying instrument 113 keeps away from surveying instrument 113, open parachute 116 through stay cord 117, play the effect of buffering protection when having played the parachute 116 to surveying instrument 113, when preventing that the dragging machine breaks down, lead to the survey and drawing data damage, convenient for use is provided with the electric power to the outdoor condition that does not have the battery under the part through setting up, the outdoor power that is favorable to improve practicality.
The above embodiments are only for illustrating the present utility model and not for limiting the technical solutions described in the present utility model, and although the present utility model has been described in detail in the present specification with reference to the above embodiments, the present utility model is not limited to the above specific embodiments, and thus any modifications or equivalent substitutions are made to the present utility model; all technical solutions and modifications thereof that do not depart from the spirit and scope of the utility model are intended to be included in the scope of the appended claims.

Claims (5)

1. Survey and drawing unmanned aerial vehicle with self preservation protects function, including main part (100) and connect in backup pad (101) of main part (100) lateral wall, a serial communication port, backup pad (101) have two to five group about main part (100) lateral wall evenly distributed, still include:
the protection component comprises a dragging frame (110) which is connected to the inner wall of the main body (100) in a sliding mode, sliding blocks (111) are fixedly connected to two sides of the dragging frame (110), clamping plates (112) are connected to the inner wall of the sliding blocks (111) in a sliding mode, a group of mapping instruments (113) are fixedly connected to the side walls of the clamping plates (112), electromagnets (114) are fixedly connected to the side walls of the sliding blocks (111), magnetic attraction stones (115) are fixedly connected to the side walls of the clamping plates (112), the electromagnets (114) are matched with the magnetic attraction stones (115), and parachutes (116) are fixedly connected to the top walls of the mapping instruments (113).
The storage component is connected to the inner wall of the main body (100) and is matched with the dragging frame (110);
and the cleaning component is connected to the side wall of the surveying instrument (113).
2. The surveying and mapping unmanned aerial vehicle with the self-protection function according to claim 1, wherein a pull rope (117) is fixedly connected to the top wall of the parachute (116), and one end, far away from the parachute (116), of the pull rope (117) is further connected with a dragging frame (110).
3. The surveying and mapping unmanned aerial vehicle with the self-protection function according to claim 1, wherein the accommodating part comprises a lifting screw (120) rotatably connected to the inner wall of the main body (100), the inner wall of the main body (100) is fixedly connected with a sliding frame (121), the lifting screw (120) is in threaded connection with the dragging frame (110), and the sliding frame (121) is in sliding connection with the dragging frame (110).
4. The surveying and mapping unmanned aerial vehicle with the self-protection function according to claim 1, wherein the cleaning component comprises a cylinder (130) fixedly connected to the side wall of the surveying and mapping instrument (113), the side wall of the surveying and mapping instrument (113) is slidably connected with a cleaning rod (131), and the output end of the cylinder (130) is fixedly connected with the cleaning rod (131).
5. The surveying and mapping unmanned aerial vehicle with self-protection function according to claim 4, wherein the side wall of the supporting plate (101) is connected with a supporting frame (140), the side wall of the supporting frame (140) is connected with a propeller (141), the side wall of the main body (100) is fixedly connected with a landing gear (142), the top wall of the main body (100) is fixedly connected with a solar panel (143), and the inner wall of the main body (100) is fixedly connected with a storage battery.
CN202321213709.0U 2023-05-19 2023-05-19 Survey and drawing unmanned aerial vehicle with self preservation protects function Active CN220096661U (en)

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CN202321213709.0U CN220096661U (en) 2023-05-19 2023-05-19 Survey and drawing unmanned aerial vehicle with self preservation protects function

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Application Number Priority Date Filing Date Title
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117818928A (en) * 2024-03-04 2024-04-05 厦门精导数字技术有限公司 Unmanned aerial vehicle for surveying and mapping

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117818928A (en) * 2024-03-04 2024-04-05 厦门精导数字技术有限公司 Unmanned aerial vehicle for surveying and mapping
CN117818928B (en) * 2024-03-04 2024-05-28 厦门精导数字技术有限公司 Unmanned aerial vehicle for surveying and mapping

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GR01 Patent grant
GR01 Patent grant
PE01 Entry into force of the registration of the contract for pledge of patent right

Denomination of utility model: A surveying drone with self-protection function

Granted publication date: 20231128

Pledgee: Huaian Qingjiang puyintai financing Company limited by guarantee

Pledgor: HUAIAN CONSTRUCTION ENGINEERING QUALITY INSPECTION CENTER Co.,Ltd.

Registration number: Y2024980006864

PE01 Entry into force of the registration of the contract for pledge of patent right