CN220448178U - Portable support that unmanned aerial vehicle used - Google Patents
Portable support that unmanned aerial vehicle used Download PDFInfo
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- CN220448178U CN220448178U CN202320736422.XU CN202320736422U CN220448178U CN 220448178 U CN220448178 U CN 220448178U CN 202320736422 U CN202320736422 U CN 202320736422U CN 220448178 U CN220448178 U CN 220448178U
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- stand
- bracket
- aerial vehicle
- unmanned aerial
- support
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- 238000001179 sorption measurement Methods 0.000 claims abstract description 8
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 20
- 238000001931 thermography Methods 0.000 claims description 11
- 229910052742 iron Inorganic materials 0.000 claims description 10
- 230000000149 penetrating effect Effects 0.000 claims description 3
- 238000010276 construction Methods 0.000 description 3
- 238000007689 inspection Methods 0.000 description 2
- 230000005389 magnetism Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000032683 aging Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
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Abstract
The utility model discloses a portable bracket for an unmanned aerial vehicle, which comprises a machine body, wherein a camera bracket device is arranged at the bottom of the machine body, connecting rods are arranged at two ends of the bottom of the machine body, a first bracket is symmetrically arranged on one connecting rod, a second bracket is symmetrically arranged on the other connecting rod, a support frame device is arranged on the connecting rod, the support frame device comprises a rotating part arranged in one end of the connecting rod, a merging part embedded at one side of the first bracket, a magnetic attraction part arranged on the inner wall of the first bracket, and adsorption parts arranged at two sides of the second bracket.
Description
Technical Field
The utility model mainly relates to the technical field of unmanned aerial vehicle supports, in particular to a portable support for an unmanned aerial vehicle.
Background
The heat supply pipeline is large in span, inconvenient in environment, high in patrol work difficulty, difficult in damage and leakage evidence obtaining, and personnel safety risks exist, illegal construction and occupation cannot be found timely, risks and damage can be brought to the heat supply pipeline, the faults and leakage risks are improved along with ageing of the pipeline, patrol frequency needs to be improved, a large amount of manpower is occupied, and therefore unmanned aerial vehicle patrol becomes the current mainstream;
according to the patent document with the application number of CN210175109U, the product comprises a reference appearance structure and a plurality of supporting pieces, wherein the reference appearance structure is arc-shaped, and the supporting pieces are distributed at the bottom of the reference appearance structure at intervals with a certain distance and are respectively connected with the reference appearance structure. The utility model has light structure, high rigidity, and can be suitable for unmanned plane structure, and the connecting hole and the positioning hole are arranged on the structure, thus the whole structure can be calibrated and positioned. The whole structure of the utility model has light weight and high rigidity, can be suitable for unmanned plane structures, and is provided with the connecting holes and the positioning holes, so that the whole structure can be calibrated and positioned. In addition, the bracket support piece structure can provide a firm support, and has the vibration reduction function, so that the unmanned aerial vehicle can fly stably in the flight stage, and the whole structure is light in weight, so that the endurance of the flight can be greatly improved;
the patent can provide a firm support, and simultaneously has the function of vibration reduction, so that the unmanned aerial vehicle can stably fly in the flight stage, and the endurance of the flight is improved, but the patent can not accommodate the bracket, so that the unmanned aerial vehicle can carry out inspection maintenance in a narrow space.
Disclosure of Invention
The utility model mainly provides a portable bracket for an unmanned aerial vehicle, which is used for solving the technical problems in the background technology.
The technical scheme adopted for solving the technical problems is as follows:
the utility model provides a portable support that unmanned aerial vehicle used, includes the fuselage, the fuselage bottom is equipped with the support device that makes a video recording, fuselage bottom both ends are equipped with the connecting rod, one of them the symmetry is equipped with first support on the connecting rod, another the symmetry is equipped with the second support on the connecting rod, be equipped with support frame device on the connecting rod, support frame device is including locating rotating parts in the connecting rod one end inlays to be located the merging part of first support one side, locate the magnetism of first support inner wall is inhaled the part, and locates the adsorption part of second support both sides.
Preferably, the rotating component comprises a micro motor arranged in one end of the first bracket, the executing end of the micro motor is rotationally connected with one end of the connecting rod, the other end of the connecting rod is rotationally connected with the rotating shaft, and the second bracket has the same structure as the first bracket.
Preferably, the combining part comprises a bracket groove penetrating through one side of the first bracket, and the size contained in the bracket groove is the same as that of the second bracket.
Preferably, the magnetic component comprises magnetic pads embedded on two sides of the bracket groove.
Preferably, the adsorption component comprises iron sheets embedded in two sides of the second bracket, and the iron sheets are magnetically connected with the magnetic attraction pad.
Preferably, the camera support device comprises a rectangular support frame arranged at the bottom of the camera body, an infrared thermal imaging machine is arranged in the rectangular support frame, a movable gasket is arranged at the top of the infrared thermal imaging machine, two ends of the movable gasket are slidably connected with the inner wall of the rectangular support frame, bolts are arranged at the bottom of the rectangular support frame, and one ends of the bolts sequentially penetrate through the rectangular support frame and the infrared thermal imaging machine and are in threaded connection with the movable gasket.
Compared with the prior art, the utility model has the beneficial effects that:
through rotating the support that the part rotates to be connected, accomodate the support when being convenient for fly, avoid unmanned aerial vehicle to patrol and examine the in-process and collide with the support, influence unmanned aerial vehicle safety flight, accomodate the support through merging the part, be convenient for reduce support weight, keep flying stably, inhale the part through magnetism and adsorb the support, be convenient for the fixed bolster, make the two elbow system each other, keep balanced, prevent that the support from droing, adopt light iron sheet through the adsorption component, be convenient for reduce weight and can keep better fixed effect again, fix the camera through the support device of making a video recording, be convenient for adjust and remove the gasket and fix the camera of equidimension not.
The utility model will be explained in detail below with reference to the drawings and specific embodiments.
Drawings
FIG. 1 is a side cross-sectional view of the primary structure of the present utility model;
FIG. 2 is a front cross-sectional view of the principal structure of the present utility model;
FIG. 3 is a cross-sectional view of a portion of the construction details of the present utility model;
FIG. 4 is a cross-sectional view of a portion of the construction details of the present utility model;
fig. 5 is an overhead view of the overall structure of the present utility model.
Description of the drawings: 10. a body; 11. a connecting rod; 12. a first bracket; 13. a second bracket; 20. a support frame device; 21. a rotating member; 211. a micro motor; 212. a rotating shaft; 22. a merging section; 221. a bracket groove; 23. a magnetic attraction member; 231. a magnetic suction pad; 24. an adsorption member; 241. iron sheet; 30. a camera support device; 31. a rectangular support frame; 32. an infrared thermal imaging machine; 33. moving the gasket; 34. and (5) a bolt.
Detailed Description
In order that the utility model may be more fully understood, a more particular description of the utility model will be rendered by reference to the appended drawings, in which several embodiments of the utility model are illustrated, but which may be embodied in different forms and are not limited to the embodiments described herein, which are, on the contrary, provided to provide a more thorough and complete disclosure of the utility model.
It will be understood that when an element is referred to as being "mounted" on another element, it can be directly on the other element or intervening elements may be present, and when an element is referred to as being "connected" to the other element, it may be directly connected to the other element or intervening elements may also be present, the terms "vertical", "horizontal", "left", "right" and the like are used herein for the purpose of illustration only.
Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this utility model belongs, and the terms used herein in this description of the utility model are for the purpose of describing particular embodiments only and are not intended to be limiting of the utility model, with the term "and/or" as used herein including any and all combinations of one or more of the associated listed items.
Referring to fig. 1, 2, 3, 4, 5, a portable stand for unmanned aerial vehicle includes a main body 10, a camera bracket device 30 is disposed at the bottom of the main body 10, connecting rods 11 are disposed at two ends of the bottom of the main body 10, one of the connecting rods 11 is symmetrically provided with a first stand 12, the other connecting rod 11 is symmetrically provided with a second stand 13, a stand device 20 is disposed on the connecting rod 11, the stand device 20 includes a rotating member 21 disposed in one end of the connecting rod 11, a combining member 22 embedded in one side of the first stand 12, a magnetic attraction member 23 disposed on an inner wall of the first stand 12, and adsorption members 24 disposed on two sides of the second stand 13, the rotating member 21 includes a micro motor 211 disposed in one end of the first stand 12, an executing end of the micro motor 211 is rotationally connected with one end of the connecting rod 11, another end of the connecting rod 11 is rotationally connected with a rotating shaft 212, and the second stand 13 is identical to the above structure of the first stand 12.
It should be noted that, in this embodiment, when the ground, the first support 12 and the second support 13 are in a vertical state with the ground, and support the airframe 10, when the unmanned aerial vehicle patrols and protects the heat supply pipeline, because many times the unmanned aerial vehicle needs to be close to detection or the space is limited, the unmanned aerial vehicle support is easy to collide with, in order to reduce unnecessary loss, when the unmanned aerial vehicle takes off, trigger the corresponding button of remote control, the electric signal of the PLC controller triggers the corresponding micro motor 211 to execute the end and drives the pivot 212 connected with the first support 12 to rotate earlier, make the first support 12 fold with the airframe 10, then the PLC controller triggers the corresponding micro motor 211 to execute the end and drives the pivot 212 connected with the second support 13 again to rotate, when the unmanned aerial vehicle falls, trigger the corresponding button, the electric signal of PLC controller triggers the corresponding micro motor 211 to execute the end to drive the pivot 212 connected with the second support 13 to rotate earlier, make it perpendicular to the airframe 10, then the PLC controller triggers the corresponding micro motor 211 to execute the end to drive the pivot 212 connected with the first support 12 to rotate, make it perpendicular to the airframe 10, and support the unmanned aerial vehicle falls.
Referring to fig. 1, 2, 3, 4, and 5, the combining component 22 includes a bracket groove 221 penetrating through one side of the first bracket 12, the size of the bracket groove 221 is the same as that of the second bracket 13, the magnetic component 23 includes magnetic pads 231 embedded on two sides of the bracket groove 221, the adsorbing component 24 includes iron pieces 241 embedded on two sides of the second bracket 13, and the iron pieces 241 are magnetically connected with the magnetic pads 231.
In this embodiment, the second bracket 13 is inserted into the bracket groove 221 and is integrated with the first bracket 12, the bracket groove 221 increases stability when contacting with the ground, and the magnetic pad 231 in the first bracket 12 adsorbs the iron sheets on both sides of the second bracket 13, thereby increasing fixity, making the two mutually toggle and not easy to fall.
Referring to fig. 1, 2 and 3, the camera support device 30 includes a rectangular support frame 31 disposed at the bottom of the body 10, an infrared thermal imaging machine 32 is disposed in the rectangular support frame 31, a moving pad 33 is disposed at the top of the infrared thermal imaging machine 32, two ends of the moving pad 33 are slidably connected to the inner wall of the rectangular support frame 31, a bolt 34 is disposed at the bottom of the rectangular support frame 31, and one end of the bolt 34 sequentially penetrates through the rectangular support frame 31 and the infrared thermal imaging machine 32 and is in threaded connection with the moving pad 33.
In this embodiment, a moving space is reserved between the rectangular support frame 31 and the moving pad 33, the infrared thermal imaging machine 32 smaller than the rectangular support frame 31 and having different sizes can be installed, and then the rectangular support frame 31 and the moving pad 33 are clamped and fixed, and then fastened by bolts 34, so that the device is firm and convenient.
The specific flow of the utility model is as follows:
the model number of the PLC is S7-300.
When the ground, first support 12 and second support 13 are in the vertical state with the ground, support fuselage 10, when unmanned aerial vehicle is to heat supply pipeline inspection time, because need press close to when many detect or the space is restricted, unmanned aerial vehicle support is very easy to collide with, in order to reduce unnecessary loss, when unmanned aerial vehicle takes off, trigger the remote control and correspond the button, the PLC controller signal of telecommunication triggers and corresponds micro motor 211 actuating end and drive the pivot 212 that is connected with first support 12 earlier rotate, make first support 12 and fuselage 10 parallel folding, then the PLC controller triggers again and corresponds micro motor 211 actuating end and drive the pivot 212 that is connected with second support 13 again and rotate, make second support 13 get into in the support recess 221, and be incorporated as an organic wholely with first support 12, support recess 221 has increased the stability when contacting with the ground, the magnetic absorption pad 231 in the first support 13 both sides's iron sheet, the fixed nature has been increased, make the two control each other, when unmanned aerial vehicle descends, trigger the remote control corresponds the button, the PLC controller signal of telecommunication triggers and corresponds micro motor 211 actuating end and drives and is connected with the pivot 212 earlier, make second support 13 and rotate with the pivot 212, then the frame 31 can not move with the rectangle frame 31 with the first support 10, then the rectangle frame is moved with the vertical support 31, and the frame is fixed with the rectangle frame is moved down, then, it is convenient for the frame is moved with the frame is 31, and can be moved with the rectangle frame 31, then, and can be moved with the frame 31 is moved down, and is convenient to move the frame is moved, and is moved down to the frame is moved and is moved.
While the utility model has been described above with reference to the accompanying drawings, it will be apparent that the utility model is not limited to the embodiments described above, but is intended to be within the scope of the utility model, as long as such insubstantial modifications are made by the method concepts and technical solutions of the utility model, or the concepts and technical solutions of the utility model are applied directly to other occasions without any modifications.
Claims (6)
1. The portable bracket for the unmanned aerial vehicle comprises a machine body (10), and is characterized in that a camera shooting bracket device (30) is arranged at the bottom of the machine body (10), connecting rods (11) are arranged at two ends of the bottom of the machine body (10), a first bracket (12) is symmetrically arranged on one connecting rod (11), a second bracket (13) is symmetrically arranged on the other connecting rod (11), and a supporting frame device (20) is arranged on the connecting rod (11);
the support frame device (20) comprises a rotating part (21) arranged in one end of the connecting rod (11), a combining part (22) embedded in one side of the first support (12), a magnetic attraction part (23) arranged on the inner wall of the first support (12), and adsorption parts (24) arranged on two sides of the second support (13).
2. The portable stand for the unmanned aerial vehicle according to claim 1, wherein the rotating member (21) comprises a micro motor (211) provided in one end of the first stand (12), the actuating end of the micro motor (211) is rotatably connected to one end of the connecting rod (11), the other end of the connecting rod (11) is rotatably connected to the rotating shaft (212), and the second stand (13) has the same structure as the first stand (12).
3. A portable stand for unmanned aerial vehicle according to claim 1, wherein the merging means (22) comprises a stand recess (221) penetrating one side of the first stand (12), the stand recess (221) having the same size as the second stand (13).
4. A portable stand for unmanned aerial vehicle according to claim 3, wherein the magnetic attraction means (23) comprises magnetic attraction pads (231) embedded on both sides of the stand recess (221).
5. The portable stand for the unmanned aerial vehicle according to claim 4, wherein the adsorption member (24) comprises iron pieces (241) embedded at both sides of the second stand (13), and the iron pieces (241) are magnetically connected with the magnetic pad (231).
6. The portable bracket for the unmanned aerial vehicle according to claim 1, wherein the camera shooting bracket device (30) comprises a rectangular bracket frame (31) arranged at the bottom of the body (10), an infrared thermal imaging machine (32) is arranged in the rectangular bracket frame (31), a movable gasket (33) is arranged at the top of the infrared thermal imaging machine (32), two ends of the movable gasket (33) are slidably connected with the inner wall of the rectangular bracket frame (31), a bolt (34) is arranged at the bottom of the rectangular bracket frame (31), and one end of the bolt (34) sequentially penetrates through the rectangular bracket frame (31) and the infrared thermal imaging machine (32) and is in threaded connection with the movable gasket (33).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320736422.XU CN220448178U (en) | 2023-04-06 | 2023-04-06 | Portable support that unmanned aerial vehicle used |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320736422.XU CN220448178U (en) | 2023-04-06 | 2023-04-06 | Portable support that unmanned aerial vehicle used |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220448178U true CN220448178U (en) | 2024-02-06 |
Family
ID=89726107
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202320736422.XU Active CN220448178U (en) | 2023-04-06 | 2023-04-06 | Portable support that unmanned aerial vehicle used |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220448178U (en) |
-
2023
- 2023-04-06 CN CN202320736422.XU patent/CN220448178U/en active Active
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