CN211167425U - Unmanned aerial vehicle article carry structure - Google Patents

Unmanned aerial vehicle article carry structure Download PDF

Info

Publication number
CN211167425U
CN211167425U CN201922190942.1U CN201922190942U CN211167425U CN 211167425 U CN211167425 U CN 211167425U CN 201922190942 U CN201922190942 U CN 201922190942U CN 211167425 U CN211167425 U CN 211167425U
Authority
CN
China
Prior art keywords
connecting plate
unmanned aerial
aerial vehicle
plate
pad
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
CN201922190942.1U
Other languages
Chinese (zh)
Inventor
边文婷
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 CN201922190942.1U priority Critical patent/CN211167425U/en
Application granted granted Critical
Publication of CN211167425U publication Critical patent/CN211167425U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Vibration Dampers (AREA)

Abstract

The utility model discloses an unmanned aerial vehicle article carry structure, including crossbeam, connecting plate and pinch-off blades, the quantity of crossbeam has two, the welding of crossbeam lower extreme one side has backup pad one, there is the connecting plate through bolted connection on the backup pad one-to-one lateral wall, there is backup pad two connecting plate one end through bolted connection. Has the advantages that: the utility model discloses a set up backup pad one at two crossbeam lower extremes, backup pad two, the connecting plate, the clamp plate, guide bar and lead screw, when needs carry article on unmanned aerial vehicle, can arrange article in between connecting plate and the clamp plate, then rotate the lead screw through the handle, make the clamp plate move up through slide rail one and slide rail two, then clamp plate and connecting plate accessible shock pad one and shock pad two firmly fix article, the clamp plate and the connecting plate of two crossbeam lower extremes can cooperate fixed great article, also can fix different article respectively, it is very nimble convenient to use.

Description

Unmanned aerial vehicle article carry structure
Technical Field
The utility model relates to an unmanned aerial vehicle equipment technical field, concretely relates to unmanned aerial vehicle article carry structure.
Background
An unmanned aerial vehicle is called an unmanned aerial vehicle for short, and is called a UAV (unmanned aerial vehicle) in English, 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, an article mounting structure of the unmanned aerial vehicle is generally called a tripod head, and the tripod head is supporting equipment for mounting and fixing a camera and is divided into a fixed tripod head and an electric tripod head.
The existing unmanned aerial vehicle article mounting structure is difficult to fix articles conveniently, is fixed inconveniently for a plurality of articles, is short of protective measures for the mounted articles and is not enough in practicability.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
In order to overcome prior art not enough, now provide an unmanned aerial vehicle article carry structure, solved current unmanned aerial vehicle article carry structure and be difficult to convenient fix article, and to the fixed inconvenient problem of a plurality of article.
(II) technical scheme
The utility model discloses a following technical scheme realizes: the utility model provides an unmanned aerial vehicle article carry structure, including crossbeam, connecting plate and pinch-off blades, the quantity of crossbeam has two, the welding of crossbeam lower extreme one side has backup pad one, there is the connecting plate through bolted connection on the backup pad one-to-one lateral wall, there is backup pad two connecting plate one end through bolted connection, the shaping has slide rail one in the backup pad one, the shaping has slide rail two in the backup pad two, sliding connection has on the slide rail one the pinch-off blades, sliding connection has the guide bar on the pinch-off blades, guide bar one side be provided with the pinch-off blades passes through threaded connection's lead screw.
Furthermore, the lower end of the guide rod is formed with a limiting piece, the lower end of the screw rod is provided with a handle, the middle of the lower end of the connecting plate is provided with a first shock pad, the middle of the upper end of the clamping plate is provided with a second shock pad, the two ends of the cross beam are provided with support frames, and the lower end of each support frame is provided with a third shock pad.
Through adopting above-mentioned technical scheme, when needs carry article on unmanned aerial vehicle, can arrange article in the connecting plate with between the clamp plate, then pass through the handle rotates the lead screw makes the clamp plate passes through slide rail one with two shifts up of slide rail, then the clamp plate with the connecting plate accessible the shock pad one with two firmly fix article, two the crossbeam lower extreme the clamp plate with the connecting plate can cooperate fixed great article, also can fix different article respectively, and it is very nimble convenient to use.
Furthermore, the clamping plate is connected with the second sliding rail in a sliding mode, and the guide rod is connected with the connecting plate in an interference mode.
By adopting the technical scheme, the guide rod plays a role in guiding and stabilizing the movement of the clamping plate, and the clamping plate can conveniently move up and down between the first supporting plate and the second supporting plate through the first sliding rail and the second sliding rail.
Furthermore, the screw rod is connected with the connecting plate through a bearing, and the handle is welded with the screw rod.
By adopting the technical scheme, the screw rod is connected with the clamping plate through the threads, so that the clamping plate can move up and down along the screw rod when the screw rod is rotated through the handle.
Furthermore, the first damping pad is connected with the connecting plate in a glued mode, and the second damping pad is connected with the clamping plate in a glued mode.
By adopting the technical scheme, the first shock pad and the second shock pad have better skid resistance and shock absorption, and can protect objects after the connecting plate and the clamping plate fix the objects.
Furthermore, the support frame is welded with the cross beam, and the shock pad III is glued with the support frame.
Through adopting above-mentioned technical scheme, the shock pad three can reduce the vibrations that unmanned aerial vehicle received when descending.
(III) advantageous effects
Compared with the prior art, the utility model, following beneficial effect has:
1. in order to solve the problems that the existing unmanned aerial vehicle article hanging structure is difficult to fix articles conveniently and is inconvenient to fix a plurality of articles, the utility model discloses a first supporting plate, a second supporting plate, a connecting plate, a clamping plate, a guide rod and a lead screw are arranged at the lower ends of two cross beams, when the unmanned aerial vehicle needs to hang articles, the articles can be arranged between the connecting plate and the clamping plate, then the lead screw is rotated through a handle, the clamping plate moves upwards through a first sliding rail and a second sliding rail, then the clamping plate and the connecting plate can firmly fix the articles through a first damping pad and a second damping pad, the clamping plate and the connecting plate at the lower ends of the two cross beams can be matched with and fix larger articles, and different articles can also be fixed respectively, so that the use;
2. for solving current unmanned aerial vehicle article carry structure and lack the safeguard measure to carry article, the not enough problem of practicality, the utility model discloses a shock pad one and shock pad two that the setting has better non-skid property and shock attenuation nature can be fixed back with article at connecting plate and clamp plate and play the guard action, very practical to article.
Drawings
Fig. 1 is a schematic structural view of an article mounting structure of an unmanned aerial vehicle according to the present invention;
fig. 2 is a schematic structural view of a cross beam and a support frame in an article mounting structure of an unmanned aerial vehicle according to the present invention;
fig. 3 is a connection relation sketch map of backup pad one, connecting plate, backup pad two, pinch-off blades, guide bar, lead screw, shock pad one and shock pad two among unmanned aerial vehicle article carry structure.
The reference numerals are explained below:
1. a cross beam; 2. a first support plate; 3. a connecting plate; 4. a second support plate; 5. a first slide rail; 6. a second slide rail; 7. a clamping plate; 8. a guide bar; 9. a screw rod; 10. a limiting sheet; 11. a handle; 12. a first shock absorption pad; 13. a second damping pad; 14. a support frame; 15. and a third shock absorption pad.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more clearly understood, the present invention is further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
As shown in fig. 1-3, the article mounting structure of the unmanned aerial vehicle in this embodiment includes two cross beams 1, two connecting plates 3 and two clamping plates 7, a first supporting plate 2 is welded on one side of the lower end of the cross beam 1, a connecting plate 3 is connected on one side wall of the first supporting plate 2 through a bolt, a second supporting plate 4 is connected on one end of the connecting plate 3 through a bolt, a first slide rail 5 is formed on the first supporting plate 2, a second slide rail 6 is formed on the second supporting plate 4, a clamping plate 7 is slidably connected on the first slide rail 5, a guide rod 8 is slidably connected on the clamping plate 7, a lead screw 9 in threaded connection with the clamping plate 7 is arranged on one side of the guide rod 8, a limiting piece 10 is formed on the lower end of the guide rod 8, a handle 11 is arranged on the lower end of the lead screw 9, a first damping pad 12 is arranged in the middle of the lower end of the connecting, the lower end of the supporting frame 14 is provided with a third shock pad 15, when articles need to be hung on the unmanned aerial vehicle, the articles can be placed between the connecting plate 3 and the clamping plate 7, then the screw rod 9 is rotated through the handle 11, the clamping plate 7 moves upwards through the first sliding rail 5 and the second sliding rail 6, then the clamping plate 7 and the connecting plate 3 can firmly fix the articles through the first shock pad 12 and the second shock pad 13, the clamping plate 7 and the connecting plate 3 at the lower ends of the two cross beams 1 can be matched with and fix larger articles and can also respectively fix different articles, the use is very flexible and convenient, the clamping plate 7 is in sliding connection with the second sliding rail 6, the guide rod 8 is in interference connection with the connecting plate 3, the guide rod 8 plays a role in guiding and stabilizing the movement of the clamping plate 7, the clamping plate 7 can conveniently move up and down between the first supporting plate 2 and the second supporting plate 4 through the first sliding rail 5 and, handle 11 and lead screw 9 welding, because lead screw 9 and clamp plate 7 pass through threaded connection, when rotating lead screw 9 through handle 11, clamp plate 7 can reciprocate along lead screw 9, shock pad one 12 splices with connecting plate 3, two 13 splices with clamp plate 7 of shock pad, shock pad one 12 and two 13 shock pads have better non-skid property and shock attenuation nature, can play the guard action to article after connecting plate 3 and clamp plate 7 are fixed with article, support frame 14 welds with crossbeam 1, three 15 and support frame 14 splices of shock pad, three 15 shock pads can reduce the vibrations that unmanned aerial vehicle received when descending.
As shown in fig. 1-3, in this embodiment, when articles need to be mounted on the unmanned aerial vehicle, the articles can be placed between the connecting plate 3 and the clamping plate 7, then the screw rod 9 is rotated through the handle 11, so that the clamping plate 7 moves upwards through the first sliding rail 5 and the second sliding rail 6, then the clamping plate 7 and the connecting plate 3 can firmly fix the articles through the first damping pad 12 and the second damping pad 13, the clamping plate 7 and the connecting plate 3 at the lower ends of the two beams 1 can be matched with and fix large articles, and different articles can be fixed respectively, so that the unmanned aerial vehicle is very flexible and convenient to use.
As shown in fig. 1-3, in the present embodiment, the first cushion 12 and the second cushion 13 have better anti-skid and shock-absorbing properties, and can protect the article after the article is fixed by the connecting plate 3 and the clamping plate 7.
The specific implementation process of this embodiment is as follows: because the screw rod 9 is connected with the clamping plate 7 through the screw thread, when the screw rod 9 is rotated through the handle 11, the clamping plate 7 can move up and down along the screw rod 9, the clamping plate 7 can conveniently move up and down between the support plate one 2 and the support plate two 4 through the slide rail one 5 and the slide rail two 6, when an object needs to be hung on the unmanned aerial vehicle, the object can be placed between the connecting plate 3 and the clamping plate 7, then the screw rod 9 is rotated through the handle 11, the clamping plate 7 can move up through the slide rail one 5 and the slide rail two 6, then the clamping plate 7 and the connecting plate 3 can firmly fix the object through the shock pad one 12 and the shock pad two 13, the clamping plate 7 and the connecting plate 3 at the lower ends of the two cross beams 1 can be matched with and fix larger objects, different objects can also be respectively fixed, the guide rod 8 plays a role in guiding and stabilizing for the movement of the clamping plate 7, the shock pad one 12 and the shock, the article can be protected after the connecting plate 3 and the clamping plate 7 fix the article.
The above-described embodiments are merely illustrative of the preferred embodiments of the present invention and are not intended to limit the spirit and scope of the present invention. Without departing from the design concept of the present invention, various modifications and improvements made by the technical solution of the present invention by those skilled in the art should fall into the protection scope of the present invention, and the technical contents claimed by the present invention have been fully recorded in the claims.

Claims (6)

1. The utility model provides an unmanned aerial vehicle article carry structure which characterized in that: including crossbeam (1), connecting plate (3) and clamp plate (7), the quantity of crossbeam (1) has two, crossbeam (1) lower extreme one side welding has backup pad (2), there is connecting plate (3) through bolted connection on backup pad (2) the lateral wall, there is backup pad two (4) connecting plate (3) one end through bolted connection, the shaping has slide rail one (5) on backup pad one (2), the shaping has slide rail two (6) on backup pad two (4), sliding connection has on slide rail one (5) clamp plate (7), sliding connection has guide bar (8) on clamp plate (7), guide bar (8) one side be provided with lead screw (9) that clamp plate (7) pass through threaded connection.
2. The unmanned aerial vehicle article mounting structure of claim 1, wherein: guide bar (8) lower extreme shaping has spacing piece (10), lead screw (9) lower extreme is provided with handle (11), connecting plate (3) lower extreme middle part is provided with shock pad (12), grip block (7) upper end middle part is provided with shock pad two (13), crossbeam (1) both ends are provided with support frame (14), support frame (14) lower extreme is provided with shock pad three (15).
3. The unmanned aerial vehicle article mounting structure of claim 1, wherein: the clamping plate (7) is in sliding connection with the second sliding rail (6), and the guide rod (8) is in interference connection with the connecting plate (3).
4. The unmanned aerial vehicle article mounting structure of claim 2, wherein: the screw rod (9) is connected with the connecting plate (3) through a bearing, and the handle (11) is welded with the screw rod (9).
5. The unmanned aerial vehicle article mounting structure of claim 4, wherein: the damping pad I (12) is connected with the connecting plate (3) in a glued mode, and the damping pad II (13) is connected with the clamping plate (7) in a glued mode.
6. The unmanned aerial vehicle article mounting structure of claim 5, wherein: the supporting frame (14) is welded with the cross beam (1), and the shock pad III (15) is connected with the supporting frame (14) in a gluing mode.
CN201922190942.1U 2019-12-10 2019-12-10 Unmanned aerial vehicle article carry structure Expired - Fee Related CN211167425U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201922190942.1U CN211167425U (en) 2019-12-10 2019-12-10 Unmanned aerial vehicle article carry structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201922190942.1U CN211167425U (en) 2019-12-10 2019-12-10 Unmanned aerial vehicle article carry structure

Publications (1)

Publication Number Publication Date
CN211167425U true CN211167425U (en) 2020-08-04

Family

ID=71829113

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201922190942.1U Expired - Fee Related CN211167425U (en) 2019-12-10 2019-12-10 Unmanned aerial vehicle article carry structure

Country Status (1)

Country Link
CN (1) CN211167425U (en)

Similar Documents

Publication Publication Date Title
CN211167425U (en) Unmanned aerial vehicle article carry structure
CN204847852U (en) Hoist collision device
CN210232781U (en) Clamp for machining shock absorber
CN110635373A (en) Electric power box base with good stability
CN211853243U (en) Positioning device for big data all-in-one machine
CN103639743A (en) Swinging clamping device
CN213109420U (en) Quick transfer trolley for tool
CN211029146U (en) Material loading frame material blocking device
CN219192284U (en) Electronic information test platform convenient to remove
CN209811007U (en) Perforating device of motor car door body guide rail
CN213502438U (en) Rolling device for carrying civil air defense equipment
CN214134629U (en) Moving frame for welding robot
CN202572179U (en) Quick clamp with movable clamping head
CN217683963U (en) Equipment bottom thickening device for intermittent relocation of equipment
CN217901963U (en) Circuit board detection device
CN211880741U (en) Floating damping electrical cabinet for electronic information engineering
CN216462707U (en) Tourist bus distance rod beam assembly welding frock
CN204973968U (en) Mount for pipettor
CN215499118U (en) Integrated vehicle-mounted support
CN205279914U (en) Utensil is examined to automobile shock absorber ware
CN213243301U (en) Power dispatching emergency device
CN214750141U (en) Adjustable portable diesel engine tail gas detection device
CN220497879U (en) Carriage board cutting machine
CN203843281U (en) Movable cutting support
CN218715743U (en) Safety protection frame convenient to move

Legal Events

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

Granted publication date: 20200804

Termination date: 20201210

CF01 Termination of patent right due to non-payment of annual fee