CN213862700U - Electromagnetic anomaly verification device for unmanned aerial vehicle - Google Patents

Electromagnetic anomaly verification device for unmanned aerial vehicle Download PDF

Info

Publication number
CN213862700U
CN213862700U CN202023141603.3U CN202023141603U CN213862700U CN 213862700 U CN213862700 U CN 213862700U CN 202023141603 U CN202023141603 U CN 202023141603U CN 213862700 U CN213862700 U CN 213862700U
Authority
CN
China
Prior art keywords
fixedly connected
aerial vehicle
unmanned aerial
motor
middle end
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN202023141603.3U
Other languages
Chinese (zh)
Inventor
张志宏
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN202023141603.3U priority Critical patent/CN213862700U/en
Application granted granted Critical
Publication of CN213862700U publication Critical patent/CN213862700U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Forklifts And Lifting Vehicles (AREA)

Abstract

The utility model discloses an unmanned aerial vehicle verifies device with electromagnetic anomaly, including the unmanned aerial vehicle body, the middle-end fixedly connected with fixed plate of unmanned aerial vehicle body upper surface, the middle-end fixedly connected with device body of fixed plate upper surface, the middle-end of device body lower surface has been seted up and has been pressed from both sides the groove, the equal fixedly connected with electric telescopic handle of lower extreme of the left and right sides of pressing from both sides groove, electric telescopic handle's top fixedly connected with U type clamp splice, the equal fixedly connected with stand of the left and right sides of device body, the upper end fixedly connected with mounting panel of stand inner chamber, the first motor of middle-end fixedly connected with of mounting panel upper surface, the upper end threaded connection of screw rod surface has the slider. The utility model discloses set up second motor, screw, first motor and electric telescopic handle, reached the purpose that stability is good, solved current unmanned aerial vehicle and verified device poor stability with electromagnetic anomaly, lead to its during operation easily not hard up to drop, influence the problem of unmanned aerial vehicle normal work.

Description

Electromagnetic anomaly verification device for unmanned aerial vehicle
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle verifies device with electromagnetic anomaly.
Background
The unmanned aerial vehicle is called an unmanned aerial vehicle for short, and is called a UAV (unmanned aerial vehicle) in English for short, and the unmanned aerial vehicle is an unmanned aerial vehicle operated by utilizing a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by a vehicle-mounted computer, and the existing electromagnetic anomaly verification device for the unmanned aerial vehicle is poor in stability, so that the existing electromagnetic anomaly verification device for the unmanned aerial vehicle is easy to loosen and fall off during working, and the normal work of the unmanned aerial vehicle is influenced.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle verifies device with electromagnetic anomaly possesses the good advantage of stability, has solved current unmanned aerial vehicle and has verified device poor stability with electromagnetic anomaly, leads to its during operation easily not hard up to drop, influences the problem of unmanned aerial vehicle normal work.
In order to achieve the above object, the utility model provides a following technical scheme: an electromagnetic anomaly verification device for an unmanned aerial vehicle comprises an unmanned aerial vehicle body, wherein a fixed plate is fixedly connected to the middle end of the upper surface of the unmanned aerial vehicle body, a device body is fixedly connected to the middle end of the upper surface of the fixed plate, a clamping groove is formed in the middle end of the lower surface of the device body, electric telescopic rods are fixedly connected to the lower ends of the left side and the right side of the clamping groove, a U-shaped clamping block is fixedly connected to the top of each electric telescopic rod, stand columns are fixedly connected to the left side and the right side of the device body, a mounting plate is fixedly connected to the upper end of an inner cavity of each stand column, a first motor is fixedly connected to the middle end of the upper surface of the mounting plate, the output end of the first motor penetrates through the middle end of the lower surface of the mounting plate and is fixedly connected with a screw, a sliding block is connected to the upper end of the outer surface of the screw, a lifting arm is fixedly connected to the middle end of the outer side of the sliding block, and a motor box is fixedly connected to the upper surface of the lifting arm, the middle end fixedly connected with second motor of motor box inner chamber bottom, the output of second motor runs through the middle end and the fixedly connected with screw of lift arm lower surface.
Preferably, the middle end of the upper surface of the fixing plate is fixedly connected with a fixing block, and the left side and the right side of the upper surface of the fixing plate are both provided with screw holes.
Preferably, the left side of the upper surface of the device body is fixedly connected with a power supply lamp, and the outer surface of the power supply lamp is provided with a glass cover.
Preferably, the equal swing joint in the left and right sides of unmanned aerial vehicle body upper surface has the screw, the middle-end fixedly connected with camera of unmanned aerial vehicle body lower surface.
Preferably, the equal fixedly connected with supporting leg in the left and right sides of unmanned aerial vehicle body lower surface, the bottom fixedly connected with cushion of supporting leg.
Compared with the prior art, the beneficial effects of the utility model are as follows:
the utility model is provided with a second motor, a screw, a first motor and an electric telescopic rod, the device body is placed at a designated position on the upper surface of a fixed plate, the device body is opened through an external controller to work, when the device body works, a power lamp is blue, the electric telescopic rod is opened through the external controller to stretch, the electric telescopic rod drives a U-shaped clamping block to stretch, a fixed block is clamped, the first motor is opened through the external controller to work, the first motor drives a screw rod to rotate, the screw rod drives a sliding block to slide up and down in an inner cavity of a stand column, the sliding block drives a lifting arm to slide up and down, the second motor is opened through the external controller to work, the second motor drives the screw to rotate, the screw is spirally connected to the inner surface of the screw hole, the purpose of good stability is achieved, the problem that the existing electromagnetic abnormity verification device for unmanned aerial vehicle is poor in stability, and the device is easy to loosen and fall off when working is solved, influence the problem of unmanned aerial vehicle normal work.
Drawings
FIG. 1 is a schematic sectional view of the present invention;
FIG. 2 is an enlarged schematic view of the structure at A of the present invention;
fig. 3 is an enlarged schematic view of the position B of the present invention.
In the figure: 1. an unmanned aerial vehicle body; 2. a power supply lamp; 3. a device body; 4. a column; 5. a second motor; 6. a motor box; 7. a lifting arm; 8. a fixing plate; 9. a screw hole; 10. a screw; 11. a screw; 12. a slider; 13. mounting a plate; 14. a first motor; 15. a clamping groove; 16. an electric telescopic rod; 17. a U-shaped clamping block; 18. a fixed block; 19. a propeller; 20. supporting legs; 21. cushion blocks; 22. a camera is provided.
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.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted", "provided", "connected", and the like are to be construed broadly, 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.
The utility model discloses an unmanned aerial vehicle body 1, the power lamp 2, device body 3, stand 4, second motor 5, motor box 6, lifting arm 7, fixed plate 8, screw 9, screw 10, screw rod 11, slider 12, mounting panel 13, first motor 14, clamping groove 15, electric telescopic handle 16, U type clamp splice 17, fixed block 18, screw 19, supporting leg 20, cushion 21 and camera 22 part are general standard or the part that technical personnel in the field know, its structure and principle all are that this technical personnel all can learn through the technical manual or learn through conventional experimental method.
Referring to fig. 1-3, an electromagnetic anomaly verification device for an unmanned aerial vehicle comprises an unmanned aerial vehicle body 1, propellers 19 are movably connected to the left and right sides of the upper surface of the unmanned aerial vehicle body 1, a camera 22 is fixedly connected to the middle end of the lower surface of the unmanned aerial vehicle body 1, supporting legs 20 are fixedly connected to the left and right sides of the lower surface of the unmanned aerial vehicle body 1, cushion blocks 21 are fixedly connected to the bottoms of the supporting legs 20, a fixing plate 8 is fixedly connected to the middle end of the upper surface of the unmanned aerial vehicle body 1, a fixing block 18 is fixedly connected to the middle end of the upper surface of the fixing plate 8, screw holes 9 are respectively formed in the left and right sides of the upper surface of the fixing plate 8, a device body 3 is fixedly connected to the middle end of the upper surface of the device body 3, a power lamp 2 is fixedly connected to the left side of the upper surface of the device body 3, a glass cover is arranged on the outer surface of the power lamp 2, and a clamping groove 15 is formed in the middle end of the lower surface of the device body 3, the lower ends of the left side and the right side of the clamping groove 15 are fixedly connected with electric telescopic rods 16, the top of each electric telescopic rod 16 is fixedly connected with a U-shaped clamping block 17, the left side and the right side of the device body 3 are fixedly connected with upright posts 4, the upper end of the inner cavity of each upright post 4 is fixedly connected with a mounting plate 13, the middle end of the upper surface of the mounting plate 13 is fixedly connected with a first motor 14, the output end of the first motor 14 penetrates through the middle end of the lower surface of the mounting plate 13 and is fixedly connected with a screw 11, the upper end of the outer surface of the screw 11 is connected with a sliding block 12 in a threaded manner, the middle end of the outer side of the sliding block 12 is fixedly connected with a lifting arm 7, the middle end of the upper surface of the lifting arm 7 is fixedly connected with a motor box 6, the middle end of the bottom of the inner cavity of the motor box 6 is fixedly connected with a second motor 5, the output end of the second motor 5 penetrates through the middle end of the lower surface of the lifting arm 7 and is fixedly connected with a screw 10, the second motor 5, the screw 10, the first motor 14 and the electric telescopic rods 16 are arranged, the device body 3 is placed at a designated position on the upper surface of a fixing plate 8, the device body 3 is opened to work through an external controller, when the device body 3 works, a power lamp 2 is blue, an electric telescopic rod 16 is opened to stretch through the external controller, the electric telescopic rod 16 drives a U-shaped clamping block 17 to stretch, a fixing block 18 is clamped tightly, a first motor 14 is opened to work through the external controller, the first motor 14 drives a screw rod 11 to rotate, the screw rod 11 drives a sliding block 12 to slide up and down in an inner cavity of an upright post 4, the sliding block 12 drives a lifting arm 7 to slide up and down, a second motor 5 is opened to work through the external controller, the second motor 5 drives a screw 10 to rotate, the screw 10 is spirally connected to the inner surface of a screw hole 9, and the purpose of good stability is achieved, the external controller is a PLC (programmable logic controller) controller in the application, and meanwhile, two wiring, and the utility power is adopted for power supply in the application.
When the device is used, the second motor 5, the screw 10, the first motor 14 and the electric telescopic rod 16 are arranged, the device body 3 is placed at a designated position on the upper surface of the fixing plate 8, the device body 3 is started to work through the external controller, when the device body 3 works, the power lamp 2 is blue, the electric telescopic rod 16 is started to stretch through the external controller, the electric telescopic rod 16 drives the U-shaped clamping block 17 to stretch, the fixing block 18 is clamped, the first motor 14 is started to work through the external controller, the first motor 14 drives the screw rod 11 to rotate, the screw rod 11 drives the sliding block 12 to slide up and down in the inner cavity of the upright post 4, the sliding block 12 drives the lifting arm 7 to slide up and down, the second motor 5 is started to work through the external controller, the second motor 5 drives the screw 10 to rotate, the screw 10 is spirally connected to the inner surface of the screw hole 9, the purpose of good stability is achieved, and the problem that the existing unmanned aerial vehicle electromagnetic anomaly verification device is poor in stability is solved, the problem that the normal work of the unmanned aerial vehicle is affected due to the fact that the unmanned aerial vehicle is easy to loosen and fall off in the working process is caused.
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 (5)

1. The utility model provides an unmanned aerial vehicle verifies device with electromagnetic anomaly, includes unmanned aerial vehicle body (1), its characterized in that: the middle end of the upper surface of the unmanned aerial vehicle body (1) is fixedly connected with a fixing plate (8), the middle end of the upper surface of the fixing plate (8) is fixedly connected with a device body (3), the middle end of the lower surface of the device body (3) is provided with a clamping groove (15), the lower ends of the left side and the right side of the clamping groove (15) are fixedly connected with an electric telescopic rod (16), the top of the electric telescopic rod (16) is fixedly connected with a U-shaped clamping block (17), the left side and the right side of the device body (3) are fixedly connected with a stand column (4), the upper end of the inner cavity of the stand column (4) is fixedly connected with a mounting plate (13), the middle end of the upper surface of the mounting plate (13) is fixedly connected with a first motor (14), the output end of the first motor (14) penetrates through the middle end of the lower surface of the mounting plate (13) and is fixedly connected with a screw rod (11), and the upper end of the outer surface of the screw rod (11) is connected with a sliding block (12) in a threaded manner, the middle end fixedly connected with lifting arm (7) in slider (12) outside, the middle end fixedly connected with motor box (6) of lifting arm (7) upper surface, the middle end fixedly connected with second motor (5) of motor box (6) inner chamber bottom, the output of second motor (5) runs through the middle end and fixedly connected with screw (10) of lifting arm (7) lower surface.
2. The electromagnetic anomaly verification apparatus for unmanned aerial vehicle according to claim 1, characterized in that: the middle end of the upper surface of the fixing plate (8) is fixedly connected with a fixing block (18), and the left side and the right side of the upper surface of the fixing plate (8) are both provided with screw holes (9).
3. The electromagnetic anomaly verification apparatus for unmanned aerial vehicle according to claim 1, characterized in that: the device is characterized in that a power lamp (2) is fixedly connected to the left side of the upper surface of the device body (3), and a glass cover is arranged on the outer surface of the power lamp (2).
4. The electromagnetic anomaly verification apparatus for unmanned aerial vehicle according to claim 1, characterized in that: the equal swing joint in the left and right sides of unmanned aerial vehicle body (1) upper surface has screw (19), middle-end fixedly connected with camera (22) of unmanned aerial vehicle body (1) lower surface.
5. The electromagnetic anomaly verification apparatus for unmanned aerial vehicle according to claim 1, characterized in that: the equal fixedly connected with supporting leg (20) of the left and right sides of unmanned aerial vehicle body (1) lower surface, the bottom fixedly connected with cushion (21) of supporting leg (20).
CN202023141603.3U 2020-12-23 2020-12-23 Electromagnetic anomaly verification device for unmanned aerial vehicle Expired - Fee Related CN213862700U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202023141603.3U CN213862700U (en) 2020-12-23 2020-12-23 Electromagnetic anomaly verification device for unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202023141603.3U CN213862700U (en) 2020-12-23 2020-12-23 Electromagnetic anomaly verification device for unmanned aerial vehicle

Publications (1)

Publication Number Publication Date
CN213862700U true CN213862700U (en) 2021-08-03

Family

ID=77043105

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202023141603.3U Expired - Fee Related CN213862700U (en) 2020-12-23 2020-12-23 Electromagnetic anomaly verification device for unmanned aerial vehicle

Country Status (1)

Country Link
CN (1) CN213862700U (en)

Similar Documents

Publication Publication Date Title
CN207995520U (en) A kind of electronic circuit board welding mechanism
CN110142547B (en) Regulator cubicle welding auxiliary device
CN211991050U (en) Transformer shell drilling equipment
CN213862700U (en) Electromagnetic anomaly verification device for unmanned aerial vehicle
CN116393970A (en) Automatic screwing device for dust cover of shock absorber
CN214815993U (en) Clean room equipment production is with automatic welding robot
CN214275013U (en) Automatic control maintenance device for electromechanical equipment
CN211465164U (en) Multi-angle cutting device is used in door and window production and processing
CN210732663U (en) PCB (printed circuit board) drilling device
CN215581942U (en) Device for correcting mounting height of LED lamp
CN216421658U (en) Numerical control machining center that work efficiency is high
CN215200628U (en) Intelligent manufacturing production equipment based on Internet of things
CN215217641U (en) Detecting instrument for precision machining of sensor part framework
CN217688400U (en) Lifting mechanism for insulator thermal shock testing machine
CN215148803U (en) Coal fired boiler dust remover assembly structure
CN218335765U (en) Power supply device for testing high-power frequency converter
CN214769105U (en) Fixing device is used in production of microelectronic component
CN215953330U (en) Automatic detection device of electrical engineering
CN214185381U (en) Panel drilling equipment for machining
CN213809945U (en) Compact composite clamping module
CN211332910U (en) Frock clamp system
CN218503624U (en) Electric connector electronic component welding set
CN214623662U (en) ID card reader
CN214043813U (en) Shell battery convenient to maintain and used for automobile
CN212253891U (en) Hole site detection jig

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20210803

Termination date: 20211223