CN219428390U - Unmanned aerial vehicle for controlling building construction progress - Google Patents
Unmanned aerial vehicle for controlling building construction progress Download PDFInfo
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- CN219428390U CN219428390U CN202223605187.7U CN202223605187U CN219428390U CN 219428390 U CN219428390 U CN 219428390U CN 202223605187 U CN202223605187 U CN 202223605187U CN 219428390 U CN219428390 U CN 219428390U
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- damping
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- aerial vehicle
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- camera
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Abstract
The utility model relates to the technical field of construction progress control, in particular to an unmanned aerial vehicle for building construction progress control; the unmanned aerial vehicle comprises an unmanned aerial vehicle, wherein a camera is arranged at the bottom of the unmanned aerial vehicle through a damping device, the damping device comprises a vertical damping mechanism and a horizontal damping mechanism, the top of the vertical damping mechanism is arranged at the bottom of the unmanned aerial vehicle, the bottom of the vertical damping mechanism is connected with the horizontal damping mechanism, and the camera is arranged at the bottom of the horizontal damping mechanism; this application is equipped with damping device through the bottom at unmanned aerial vehicle, and the camera is installed in damping device's bottom, and wherein damping device includes vertical damper and horizontal damper, and vertical damper can shock attenuation and release the vibrations that produce when reciprocating unmanned aerial vehicle, and horizontal damper can shock attenuation and release when unmanned aerial vehicle carries out horizontal migration or the vibrations that produce at the wind current that meets in the high altitude to the stability of camera has been ensured, the unclear problem of camera shooting image has been solved.
Description
Technical Field
The utility model relates to the technical field of construction progress control, in particular to an unmanned aerial vehicle for building construction progress control.
Background
At present, when a plurality of sites are complex in environment and workers cannot conveniently enter the sites directly or are in dangerous area information collection, such as disaster site rescue information collection, site scheduling assistance, construction site information collection and construction monitoring of dangerous areas and other scenes, information collection and monitoring are often needed by means of unmanned aerial vehicles;
in the construction field, unmanned aerial vehicle can be through taking photo by plane synthetic 3D model, detects the construction progress, but unmanned aerial vehicle need fly to certain altitude and can monitor the construction place, nevertheless receive the influence of wind flow at the high altitude, cause unmanned condition that rocks, and then lead to the camera to rock thereupon, make the image that the camera shot unclear, can't accurate shoot out the construction place image even.
Disclosure of Invention
To above-mentioned problem, provide an unmanned aerial vehicle for construction progress management and control, through being equipped with damping device in unmanned aerial vehicle's bottom, the camera is installed in damping device's bottom, wherein damping device includes vertical damper and horizontal damper, vertical damper can shock attenuation and release the vibrations that produce when unmanned aerial vehicle reciprocates, horizontal damper can shock attenuation and release when unmanned aerial vehicle carries out horizontal migration or the wind stream that meets in the high altitude and the vibrations that produce, thereby ensured the stability of camera, solved the unclear problem of camera shooting image.
In order to solve the problems in the prior art, the utility model adopts the following technical scheme:
the utility model provides an unmanned aerial vehicle for construction progress management and control, includes unmanned aerial vehicle, and unmanned aerial vehicle's bottom is equipped with a pair of bracing piece, and the camera passes through damping device to be installed in unmanned aerial vehicle's bottom and its centre that is located two bracing pieces, and damping device includes vertical damper and horizontal damper, and vertical damper's top is installed in unmanned aerial vehicle's bottom and its bottom is connected with horizontal damper, and the bottom at horizontal damper is installed to the camera.
Preferably, the vertical damping mechanism comprises a first damping cabin, a damping rod, a damping component and a damping spring; the first damping cabin is arranged at the bottom of the unmanned aerial vehicle through a connecting disc, and a cavity is formed in the first damping cabin; the damping rod is vertical and can be installed at the bottom of the first damping cabin in a vertically sliding manner, the top of the damping rod is provided with a first damping piston, and the first damping piston is horizontal and is positioned in a cavity of the first damping cabin; the damping component is arranged at the bottom of the damping rod; the damping spring is sleeved on the damping rod, the top of the damping spring is abutted with the bottom of the first damping cabin, and the bottom of the damping spring is abutted with the top of the damping component.
Preferably, the damping assembly comprises a second damping cabin and a second damping piston; the second shock absorption cabin is vertical and can be installed at the bottom of the shock absorption rod in a vertical sliding mode, and a cavity is formed in the second shock absorption cabin; the second damping piston is horizontally arranged at the bottom of the damping rod and is positioned in the cavity of the second damping cabin.
Preferably, the horizontal damping mechanism comprises a damping disc; the damping disc is provided with a pair of damping discs and is symmetrically arranged between the camera and the second damping cabin; at least two connecting rods extending outwards are arranged on the surfaces of the two damping disks, and the plurality of connecting rods are uniformly distributed on the surfaces of the damping disks; the upper damping disc and the lower damping disc are respectively connected with the bottom of the second damping cabin and the top of the camera, and a damping ball for damping is arranged between the upper connecting rod and the lower connecting rod.
Preferably, the shock-absorbing ball is made of rubber.
Preferably, the horizontal shock absorbing assembly further comprises a universal joint; the top of the universal joint is connected with the bottom of the second damping cabin, and the bottom of the universal joint is connected with the top of the camera.
Compared with the prior art, the beneficial effects of this application are:
this application is equipped with damping device through the bottom at unmanned aerial vehicle, and the camera is installed in damping device's bottom, and wherein damping device includes vertical damper and horizontal damper, and vertical damper can shock attenuation and release the vibrations that produce when reciprocating unmanned aerial vehicle, and horizontal damper can shock attenuation and release when unmanned aerial vehicle carries out horizontal migration or the vibrations that produce at the wind current that meets in the high altitude to the stability of camera has been ensured, the unclear problem of camera shooting image has been solved.
Drawings
FIG. 1 is a schematic perspective view of a drone for use in building construction progress management;
FIG. 2 is a front view of the structure of a drone for construction progress management and control;
FIG. 3 is a schematic view of a partial perspective view of a drone for controlling progress of building construction;
FIG. 4 is a partial perspective exploded view of a drone for construction progress management;
FIG. 5 is a partial perspective cutaway view of a drone for construction progress management;
fig. 6 is a schematic diagram of a partial perspective view of a unmanned aerial vehicle for controlling progress of building construction.
The reference numerals in the figures are:
1-unmanned aerial vehicle; 11-supporting rods;
2-video camera;
3-a damping device; 31-a vertical shock absorbing mechanism; 311-a first shock absorption cabin; 3111-connection pads; 312-a shock rod; 3121—a first damping piston; 313-damping springs; 314-a shock absorbing assembly; 3141-a second shock absorber pod; 3142-a second damping piston; 32-a horizontal shock absorbing mechanism; 321-damping disc; 322-connecting rod; 323-damping ball; 324-universal joint.
Detailed Description
The utility model will be further described in detail with reference to the drawings and the detailed description below, in order to further understand the features and technical means of the utility model and the specific objects and functions achieved.
Referring to fig. 1 to 6, an unmanned aerial vehicle for controlling the progress of building construction, comprising an unmanned aerial vehicle 1, wherein a pair of support rods 11 are arranged at the bottom of the unmanned aerial vehicle 1, a camera is arranged at the bottom of the unmanned aerial vehicle 1 through a damping device 3 and positioned between the two support rods 11, the damping device 3 comprises a vertical damping mechanism 31 and a horizontal damping mechanism 32, the top of the vertical damping mechanism 31 is arranged at the bottom of the unmanned aerial vehicle 1 and connected with the horizontal damping mechanism 32 at the bottom thereof, and the camera is arranged at the bottom of the horizontal damping mechanism 32.
When unmanned aerial vehicle 1 shoots in high altitude flight, camera 2 can rock along with it, in order to make camera 2 keep stable, install the bottom at unmanned aerial vehicle 1 with the camera through damping device 3, damping device 3 is including vertical damper 31 and horizontal damper 32, vertical damper 31 can carry out the shock attenuation to vertical direction's that causes in the vertical movement in-process and unload the power when unmanned aerial vehicle 1 carries out the reciprocating flight, make camera 2 keep stable in-process that reciprocates, horizontal damper 32 can carry out horizontal migration at unmanned aerial vehicle 1, or when unmanned aerial vehicle 1 runs into the influence of high altitude wind stream, horizontal damper 32 can carry out the shock attenuation with horizontal rocking and unload the power, thereby the stability of camera 2 has been kept, the unclear problem of camera 2 shooting image has been solved.
Referring to fig. 3 to 5, the vertical damping mechanism 31 includes a first damping compartment 311, a damping rod 312, a damping assembly 314, and a damping spring 313; the first shock absorption cabin 311 is arranged at the bottom of the unmanned aerial vehicle 1 through a connecting disc 3111, and a cavity is formed in the first shock absorption cabin 311; the damping rod 312 is vertically arranged at the bottom of the first damping cabin 311 in a manner of sliding up and down, the top of the damping rod 312 is provided with a first damping piston 3121, and the first damping piston 3121 is horizontally arranged in the cavity of the first damping cabin 311; shock assembly 314 is mounted to the bottom of shock rod 312; the damping spring 313 is sleeved on the damping rod 312, the top of the damping spring 313 is abutted with the bottom of the first damping cabin 311, and the bottom of the damping spring 313 is abutted with the top of the damping assembly 314.
When unmanned aerial vehicle 1 carries out the reciprocates, the camera 2 of unmanned aerial vehicle 1 bottom can exert certain thrust to unmanned aerial vehicle 1, can cause the rocking of camera 2 this moment, in order to keep the steady of camera 2, install the bottom at unmanned aerial vehicle 1 and its inside cavity with first shock attenuation cabin 311 through connection pad 3111, the top of shock attenuation pole 312 is installed in the inside cavity of first shock attenuation dish 321 and its can slide from top to bottom through first shock attenuation piston 3121, shock attenuation spring 313 cover is established on shock attenuation pole 312, shock attenuation spring 313's top and first shock attenuation cabin 311 butt, shock attenuation cabin 311 butt is gone up with shock attenuation subassembly 314 to the bottom of shock attenuation spring 313, camera 2 can upwards strike because of inertia when unmanned aerial vehicle 1 removes the back, the upward strike of camera 2 can make shock attenuation pole 312 upwards remove, shock attenuation spring 313 takes place to extrude for the first shock attenuation piston 3121 carries out the upward movement in the inside of first shock attenuation cabin 311 this moment, shock attenuation spring 313 can make the upward impact force cushion, first shock attenuation pole 312 drives first piston 3121 and carries out the upward movement 311 in the inside of first shock attenuation cabin 311, thereby the problem of vibration damping force has been solved, thereby the problem of vibration of the camera 2 has been solved, the upward force of vibration is overcome.
Referring to fig. 4-5, shock assembly 314 includes a second shock pod 3141 and a second shock piston 3142; the second damping cabin 3141 is vertically and slidably installed at the bottom of the damping rod 312, and a cavity is formed in the second damping cabin 3141; second damping piston 3142 is horizontally mounted at the bottom of damping rod 312 and is located in the cavity of second damping chamber 3141.
In order to reduce the rocking of unmanned aerial vehicle 1 to camera 2 in the reciprocates the in-process, increase the release of force simultaneously, through being equipped with second shock attenuation cabin 3141 in the bottom of shock attenuation pole 312, the inside of second shock attenuation cabin 3141 is equipped with second shock attenuation piston 3142, second shock attenuation cabin 3141 and shock attenuation pole 312 sliding connection, the bottom and the second shock attenuation piston 3142 of shock attenuation pole 312 are connected, when unmanned aerial vehicle 1's removal makes second shock attenuation cabin 3141 upwards move, shock attenuation pole 312 and second shock attenuation piston 3142 are motionless, the air in the second shock attenuation cabin 3141 upwards moves and can make its cavity compress, thereby can make the power conversion of upwards moving heat, realized the release to the force, camera 2's stability has been kept.
Referring to fig. 5 to 6, the horizontal damping mechanism 32 includes a damping disk 321; the shock absorbing disc 321 has a pair and is symmetrically disposed in the middle of the camera 2 and the second shock absorbing compartment 3141; the surfaces of the two shock-absorbing discs 321 are respectively provided with at least two connecting rods 322 extending outwards, and the plurality of connecting rods 322 are uniformly distributed on the surfaces of the shock-absorbing discs 321; the upper and lower shock absorbing discs 321 are respectively connected with the bottom of the second shock absorbing cabin 3141 and the top of the camera 2, and a shock absorbing ball 323 for shock absorption is installed between the upper and lower connecting rods 322.
When unmanned aerial vehicle 1 carries out horizontal migration, perhaps when the high altitude runs into the windstream, in order to reduce the rocking of camera 2, through being equipped with two shock attenuation discs 321 in the bottom of second shock attenuation cabin 3141, two shock attenuation discs 321 symmetry set up the bottom at camera 2 top and second shock attenuation cabin 3141, the surface of two shock attenuation discs 321 is equipped with a plurality of connecting rods 322 that extend to the outside, connect through shock attenuation ball 323 between two upper and lower connecting rods 322, when unmanned aerial vehicle 1 produced the horizontal rocking, through two shock attenuation discs 321 and shock attenuation ball 323 that upper and lower symmetry set up, the power that can make rocking is buffered, make unmanned aerial vehicle 1 when rocking, the rocking of camera 2 has been reduced, thereby can make camera 2 keep stable, the definition of picture when having increased the shooting.
Referring to fig. 5, the shock absorbing ball 323 is made of rubber.
When unmanned aerial vehicle 1 takes place to rock, can reduce the rocking of camera 2 through upper and lower two shock attenuation discs 321 and shock attenuation ball 323, can make the connection between two shock attenuation discs 321 have elasticity through setting up shock attenuation ball 323 to the rubber material to when unmanned aerial vehicle takes place to rock, can have certain shock attenuation effect.
Referring to fig. 5-6, horizontal damping assembly 314 further includes universal joint 324; the top of the universal joint 324 is connected to the bottom of the second damping compartment 3141, and the bottom of the universal joint 324 is connected to the top of the camera 2.
Two shock attenuation discs 321 in the top of camera 2 pass through shock attenuation ball 323 to be connected, in order to increase the fastness between camera 2 and the vertical damper 31, camera 2 passes through universal joint 324 and is connected with the second shock attenuation cabin 3141 in the vertical damper 31, when unmanned aerial vehicle 1 rocks, shock attenuation is carried out through shock attenuation ball 323 between two shock attenuation discs 321, there is rocking between the camera 2 of bottom and the second shock attenuation cabin 3141 this moment, so just connect through universal joint 324, when rocking the production, universal joint 324 can make all the time keep being connected between camera 2 and the second shock attenuation cabin 3141, thereby the fastness when having increased camera 2 and vertical damper 31 to be connected.
The foregoing examples merely illustrate one or more embodiments of the utility model, which are described in greater detail and are not to be construed as limiting the scope of the utility model. It should be noted that it will be apparent to those skilled in the art that several variations and modifications can be made without departing from the spirit of the utility model, which are all within the scope of the utility model. Accordingly, the scope of protection of the present utility model is to be determined by the appended claims.
Claims (6)
1. The utility model provides an unmanned aerial vehicle for construction progress management and control, including unmanned aerial vehicle (1), the bottom of unmanned aerial vehicle (1) is equipped with a pair of bracing piece (11), its characterized in that, the camera passes through damping device (3) to be installed in the bottom of unmanned aerial vehicle (1) and its centre that is located two bracing pieces (11), damping device (3) are including vertical damper (31) and horizontal damper (32), the bottom at unmanned aerial vehicle (1) is installed at the top of vertical damper (31) and its bottom is connected with horizontal damper (32), the bottom at horizontal damper (32) is installed to the camera.
2. The unmanned aerial vehicle for construction progress control according to claim 1, wherein the vertical damping mechanism (31) comprises a first damping cabin (311), a damping rod (312), a damping assembly (314) and a damping spring (313); the first damping cabin (311) is arranged at the bottom of the unmanned aerial vehicle (1) through a connecting disc (3111), and a cavity is formed in the first damping cabin (311); the damping rod (312) is vertically arranged at the bottom of the first damping cabin (311) in a sliding manner, a first damping piston (3121) is arranged at the top of the damping rod (312), and the first damping piston (3121) is horizontally arranged and is positioned in the cavity of the first damping cabin (311); the damping component (314) is arranged at the bottom of the damping rod (312); the damping spring (313) is sleeved on the damping rod (312), the top of the damping spring (313) is abutted with the bottom of the first damping cabin (311), and the bottom of the damping spring (313) is abutted with the top of the damping component (314).
3. The unmanned aerial vehicle for construction progress control according to claim 2, wherein the damping assembly (314) comprises a second damping cabin (3141) and a second damping piston (3142); the second damping cabin (3141) is vertically arranged at the bottom of the damping rod (312) in a sliding manner, and a cavity is formed in the second damping cabin (3141); the second damping piston (3142) is horizontally mounted at the bottom of the damping rod (312) and is located in the cavity of the second damping chamber (3141).
4. A drone for construction progress management according to claim 1, characterized in that the horizontal shock absorbing mechanism (32) comprises a shock absorbing disc (321); the damping disc (321) is provided with a pair of damping discs and is symmetrically arranged between the camera (2) and the second damping cabin (3141); the surfaces of the two shock absorption discs (321) are respectively provided with at least two connecting rods (322) extending outwards, and the plurality of connecting rods (322) are uniformly distributed on the surfaces of the shock absorption discs (321); the upper damping disc (321) and the lower damping disc are respectively connected with the bottom of the second damping cabin (3141) and the top of the video camera (2), and a damping ball (323) for damping is arranged between the upper connecting rod (322) and the lower connecting rod (322).
5. The unmanned aerial vehicle for controlling the progress of building construction according to claim 4, wherein the shock absorbing balls (323) are made of rubber.
6. The unmanned aerial vehicle for construction progress control according to claim 1, wherein the horizontal damping assembly (314) further comprises a universal joint (324); the top of the universal joint (324) is connected with the bottom of the second damping cabin (3141), and the bottom of the universal joint (324) is connected with the top of the camera (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223605187.7U CN219428390U (en) | 2022-12-30 | 2022-12-30 | Unmanned aerial vehicle for controlling building construction progress |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223605187.7U CN219428390U (en) | 2022-12-30 | 2022-12-30 | Unmanned aerial vehicle for controlling building construction progress |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219428390U true CN219428390U (en) | 2023-07-28 |
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ID=87335496
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202223605187.7U Active CN219428390U (en) | 2022-12-30 | 2022-12-30 | Unmanned aerial vehicle for controlling building construction progress |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219428390U (en) |
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2022
- 2022-12-30 CN CN202223605187.7U patent/CN219428390U/en active Active
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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder |
Address after: Room 1520, financial building, 171 Haibin Road, Nansha District, Guangzhou, Guangdong 510000 Patentee after: CHINA RAILWAY 25TH BUREAU GROUP Co.,Ltd. Patentee after: Guangdong Qingtianzhu Intelligent Construction Technology Co.,Ltd. Address before: Room 1520, financial building, 171 Haibin Road, Nansha District, Guangzhou, Guangdong 510000 Patentee before: CHINA RAILWAY 25TH BUREAU GROUP Co.,Ltd. Patentee before: Guangdong Qingtianzhu Intelligent Technology Co.,Ltd. |
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| CP01 | Change in the name or title of a patent holder |