CN210196889U - Construction progress monitoring system - Google Patents
Construction progress monitoring system Download PDFInfo
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- CN210196889U CN210196889U CN201921118288.7U CN201921118288U CN210196889U CN 210196889 U CN210196889 U CN 210196889U CN 201921118288 U CN201921118288 U CN 201921118288U CN 210196889 U CN210196889 U CN 210196889U
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Abstract
The utility model relates to a construction progress monitored control system, it includes the mounting bracket, mounting bracket upper portion is fixed with driving motor, the vertical setting of driving motor's axis, be fixed with the installation piece on driving motor's the output shaft, the installation piece is located driving motor's top, the top of installation piece is provided with the camera, the upper portion of camera is connected with the aircraft, the mounting hole has been seted up to the upper surface of installation piece, the lower surface of camera is provided with the double-screw bolt, the vertical setting of double-screw bolt, the inside of installation piece is provided with the rolling disc, the rolling disc is connected with rotating device, sliding connection has two semi-arc pieces on the rolling disc, two semi-arc pieces are connected with the drive arrangement who drives two relative or back-to-back motion of semi-arc pieces, the line of two semi-arc piece central point puts passes through the mounting hole round hole, two semi-arc pieces inboard have been provided with double. The utility model discloses have the aircraft and install the piece and be connected more convenient effect.
Description
Technical Field
The utility model belongs to the technical field of a construction progress supervision's technique and specifically relates to a construction progress monitored control system is related to.
Background
In the supervision process of the project, most of the personnel monitor the construction site, the personnel consume manpower resources very much during operation, along with the development, the development of the camera monitoring technology is rapid, and the monitoring on the construction site is also very convenient.
The patent document with the publication number of CN207820109U discloses a construction progress monitoring system for construction engineering, which includes a camera arranged on a construction site for monitoring, and an installation frame arranged on the construction site, wherein an installation block for placing the camera is installed at the upper end of the installation frame, and a driving motor for driving the installation block to rotate around an axis is fixedly installed below the installation block; still including being used for receiving the image information that the camera was shot and carrying out wireless transmission's wireless transceiver, receive the image information that wireless transceiver transmitted and carry out remote display's display device, be provided with the aircraft in the top of mounting bracket, the lower surface of aircraft is used for fixing the upper portion at the camera, the aircraft can take the camera to remove the control after flight, return the back at the aircraft, be provided with coupling assembling between installation piece and aircraft, coupling assembling is including installation pipe and installation pole, the lower surface at the aircraft is fixed to the installation pipe, the upper surface at the installation piece is fixed to the installation pole, after the aircraft descends, the installation pipe box is on the installation pole, make the aircraft connect on the installation piece.
In the structure, when the aircraft is connected to the mounting block through the connecting assembly, the mounting pipe is difficult to be matched with the mounting rod in an inserting manner, so that the aircraft is difficult to be connected to the mounting block.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing a construction progress monitored control system, it has the aircraft and is connected more convenient effect with the installation piece.
The above object of the present invention is achieved by the following technical solutions:
a construction progress monitoring system comprises a mounting frame, a driving motor is fixed on the upper portion of the mounting frame, the axis of the driving motor is vertically arranged, a mounting block is fixed on an output shaft of the driving motor and located above the driving motor, a camera is arranged above the mounting block, an aircraft is connected to the upper portion of the camera, the upper surface of the mounting block is provided with a mounting hole, the lower surface of the camera is provided with a stud which is vertically arranged, the inside of installation piece is provided with the rolling disc, and the rolling disc is connected with rotating device, and sliding connection has two half-arc pieces on the rolling disc, and two half-arc pieces set up relatively, and two half-arc pieces are connected with the drive arrangement who drives two half-arc pieces relative or back-to-back motion, and the line that the central point of two half-arc pieces put is through the mounting hole round hole, and two half-arc piece inboard is opened be provided with double-screw bolt complex screw thread, the diameter of mounting hole is greater than the double-screw bolt diameter and is less than the double-screw bolt diameter.
Through adopting the above technical scheme, during the use, the mounting bracket is placed subaerial, driving motor fixes on the mounting bracket, driving motor during operation, driving motor's output can drive the installation piece and rotate, thereby make the camera on the installation piece carry out the multi-angle and shoot, when being connected camera and installation piece, insert the double-screw bolt of camera lower surface in the mounting hole, drive arrangement drives two half-arc piece relative movement on the rolling disc, make screw thread and double-screw bolt cooperation on two half-arc pieces, thereby lock the screw bolt, and the diameter of mounting hole is greater than the diameter of double-screw bolt, make the double-screw bolt more conveniently insert in the mounting hole, it is more convenient to make the camera be connected with the installation piece.
Simultaneously, when the driving device drives the two half-arc pieces on the rotating disc to move back to back, the stud is loosened by the two half-arc pieces, and the aircraft can directly drive the camera to move and shoot.
The utility model discloses further set up to: the driving device comprises a screw, two connecting pieces and a rotating motor, the rotating motor is fixed in the rotating disc, the screw is coaxially fixed at the output end of the driving motor, the thread turning directions of the two ends of the screw are opposite, the two connecting pieces are respectively fixed on the two semi-arc pieces, and the two connecting pieces are respectively in thread fit with the two ends of the screw.
By adopting the technical scheme, the rotating motor is started, the output end of the rotating motor drives the screw rod to rotate, the thread turning directions at two ends of the screw rod are opposite, so that two connecting pieces on the screw rod move oppositely or oppositely, the connecting pieces drive the half-arc piece to move, the half-arc piece is loosened or the stud is clamped, and the stud is accurately positioned at the center of the mounting hole.
The utility model discloses further set up to: the rotary disc is provided with a guide hole, the back of the semi-arc piece is fixedly provided with a guide rod, and the guide rod is in sliding fit in the guide hole.
Through adopting above-mentioned technical scheme, seted up the guiding hole on the rolling disc, set up the guide bar on the semi-arc piece, guide bar and guiding hole sliding fit make the semi-arc piece remove along the length direction of guiding hole under the guide bar and the cooperation of guiding hole.
The utility model discloses further set up to: the rotating device comprises a locking motor, the locking motor is fixedly arranged on the mounting block, the output end of the locking motor is arranged on the lower surface of the rotating disc, and the central line of the output shaft of the locking motor is overlapped with the central line of the mounting hole.
Through adopting above-mentioned technical scheme, the locking motor is fixed on the installation piece, and the locking motor during operation drives the rolling disc and rotates to two half arc pieces on making the rolling disc lock the screw post, make the camera install on the installation piece.
The utility model discloses further set up to: the lower end of the stud is provided with a binding post, the binding post is vertically downward, the rotating disc is provided with an electric slip ring, the inner ring of the electric slip ring is provided with a conducting strip, the outer ring of the electric slip ring is fixed on the rotating disc, and the conducting strip extends to the position of the binding post.
Through adopting above-mentioned technical scheme, the lower extreme of double-screw bolt sets up the terminal, and the outer lane and the rolling disc of electric sliding ring rotate, and the conducting strip that the circle was gone up in the electric sliding ring is behind the double-screw bolt locking, and the conducting strip is connected with the terminal electricity to can be connected with camera or aircraft to the terminal and charge.
The utility model discloses further set up to: the upper surface of the mounting block is provided with a blocking block, the lower surface of the aircraft is provided with a blocking column, the blocking column is vertically arranged, and the distance between the blocking column and the stud is equal to the distance between the blocking block and the center of the mounting hole.
Through adopting above-mentioned technical scheme, the upper surface of installation piece sets up blocks the piece, and the lower surface of aircraft sets up blocks the post, and when double-screw bolt and half-arc piece carried out threaded connection, the post that blocks kept off in the position that blocks the piece, makes things convenient for the rotation of half-arc piece for the double-screw bolt.
The utility model discloses further set up to: the two blocking columns are located in the circumferential direction of the stud and are evenly distributed.
Through adopting above-mentioned technical scheme, stop the post and have two, stop post evenly distributed in the circumference of double-screw bolt on two, make two stop the post can be faster with block piece looks butt, simultaneously, two stop the post and can keep the balance of aircraft.
The utility model discloses further set up to: the upper part of the blocking block is arranged to be triangular.
Through adopting above-mentioned technical scheme, block piece upper portion and set to triangle-shaped, when blockking that the post downstream, block the post and block when the piece is relative, block the post and receive the triangle-shaped inclined plane conflict of block piece upper portion, reduce and block the post and support at the upper surface that blocks the piece.
To sum up, the utility model discloses a beneficial technological effect does:
1. when the camera is connected with the mounting block, the stud on the lower surface of the camera is inserted into the mounting hole, the driving device drives the two half-arc pieces on the rotating disc to move relatively, so that threads on the two half-arc pieces are matched with the stud, the stud is locked, the diameter of the mounting hole is larger than that of the stud, the stud is conveniently inserted into the mounting hole, and the camera is conveniently connected with the mounting block;
2. the output end of the rotating motor drives the screw to rotate by starting the rotating motor, and the thread turning directions of the two ends of the screw are opposite, so that two connecting pieces on the screw move oppositely or oppositely, the connecting pieces drive the half-arc pieces to move, and the stud is accurately positioned at the center of the mounting hole;
3. the terminal is arranged at the lower end of the stud, the outer ring of the electric slip ring rotates with the rotating disc, the conducting strip on the inner ring of the electric slip ring is electrically connected with the terminal after the stud is locked, and therefore the camera or the aircraft can be connected with the terminal for charging.
Drawings
Fig. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a schematic illustration of an aircraft and installation block explosion configuration;
FIG. 3 is a schematic view of the structure of the connecting device;
fig. 4 is a schematic view of the internal structure of the mounting block.
In the figure, 1, a mounting frame; 2. a drive motor; 3. mounting blocks; 31. mounting holes; 4. a camera; 5. an aircraft; 6. a connecting device; 61. rotating the disc; 62. a half-arc piece; 63. a guide hole; 64. a guide bar; 65. locking the motor; 7. a stud; 8. a drive device; 81. a screw; 82. connecting sheets; 83. rotating the motor; 91. a binding post; 92. an electrical slip ring; 93. a conductive sheet; 10. a blocking block; 11. blocking the post.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings.
Referring to fig. 1 and 2, in order to provide the utility model discloses a construction progress monitoring system, which comprises a mounting frame 1, wherein the mounting frame 1 is a tripod placed on the ground, a driving motor 2 is arranged on the upper part of the mounting frame 1, the driving motor 2 is fixed on the mounting frame 1, the output end of the driving motor 2 is vertically arranged, the output end of the driving motor 2 is arranged upwards, a mounting block 3 is fixed on the output end of the driving motor 2, and the mounting block 3 can horizontally rotate under the action of the driving motor 2; be provided with camera 4 on installation piece 3, camera 4 is along with installation piece 3 pivoted in-process, can all-round to control many places. The upper portion of camera 4 is connected with aircraft 5, and the lower surface of aircraft 5 is used for fixed camera 4, and camera 4 passes through connecting device 6 and sets up on installation piece 3, and when connecting device 6 opened the back, aircraft 5 can take camera 4 to remove and shoot, improves camera 4's surveillance area.
Referring to fig. 2 and 3, a mounting hole 31 is formed in the center of the upper surface of the mounting block 3, the mounting hole 31 is circular, and the mounting hole 31 is vertically downward. And a stud 7 is fixedly arranged on the lower surface of the camera 4, the stud 7 is vertically downward, and the stud 7 can be vertically inserted into the mounting hole 31. Connecting device 6 includes rolling disc 61 and two half arc pieces 62, and installation piece 3 is inside to be hollow structure, and rolling disc 61 sets up in the inside of installation piece 3, and half arc piece 62 is whole to be the arc, and the arc opening of two half arc pieces 62 sets up relatively to the center line of two half arc pieces 62 passes through the center of mounting hole 31. A guide hole 63 is formed in the mounting block 3, the guide hole 63 is horizontally arranged, a guide rod 64 is arranged in the guide hole 63, the guide rod 64 is in sliding fit in the guide hole 63, one end of the guide rod 64 is inserted into the guide hole 63, and the other end of the guide rod is fixed to the back of the half-arc piece 62. The two half-arc pieces 62 move along the length direction of the guide hole 63 under the action of the guide rod 64 and the guide hole 63. The two half-arc pieces 62 are provided with a driving device 8 for driving the two half-arc pieces 62 to move oppositely or back to back, and the diameter of the mounting hole 31 is larger than that of the stud 7 and smaller than twice of the diameter of the stud 7. When the stud 7 is placed in the mounting hole 31, the center line of the stud 7 is located at the center of the two half-arc pieces 62, and when the two half-arc pieces 62 move relatively, the two half-arc pieces 62 can press the stud 7 to the middle position of the half-arc pieces 62, so that the two half-arc pieces 62 can clamp the stud 7.
Referring to fig. 2 and 3, threads matched with the stud 7 are formed on the inner sides of the two half-arc pieces 62, a locking motor 65 is arranged on the lower surface of the rotating disc 61, the locking motor 65 is fixed in the mounting block 3, the output end of the locking motor 65 is fixed on the rotating disc 61, and the central line of the output shaft of the locking motor 65 is overlapped with the central line of the mounting hole 31. The locking motor 65 is started, the locking motor 65 drives the rotating disc 61 to rotate, the half-arc sheet 62 is enabled to lock the stud 7, and therefore the stud 7 is fixed on the mounting block 3. Two blocking blocks 10 are arranged on the upper surface of the mounting block 3, the blocking blocks 10 are uniformly distributed on the circumferential direction of the mounting hole 31, and the upper parts of the blocking blocks 10 are arranged into a triangle; two blocking columns 11 are arranged on the lower surface of the aircraft 5, the blocking columns 11 are vertically arranged, the two blocking columns 11 are uniformly distributed on the circumference of the stud 7, and the distance between the blocking columns 11 and the center of the stud 7 is equal to the distance between the blocking block 10 and the center of the mounting hole 31. When the rotating disc 61 rotates, the stop post 11 stops at the position of the stop block 10, and the stud 7 is prevented from rotating along with the rotating disc 61.
Referring to fig. 3, the driving device 8 includes a screw 81, two connecting pieces 82 and a rotating motor 83, the rotating motor 83 is fixed in the rotating disc 61, the screw 81 is coaxially fixed at the output end of the driving motor 2, the thread directions of the two ends of the screw 81 are opposite, the two connecting pieces 82 are provided, the two connecting pieces 82 are respectively fixed on the two half-arc pieces 62, the screw 81 simultaneously penetrates through the two connecting pieces 82, and the two connecting pieces 82 are respectively in thread fit with the two ends of the screw 81. When the rotating motor 83 is started, the rotating motor 83 can drive the two connecting pieces 82 to move oppositely or oppositely along the length direction of the screw 81, so that the two half-arc pieces 62 clamp the stud 7 relatively or loosen the stud 7.
Referring to fig. 3 and 4, a terminal 91 is arranged at the lower end of the stud 7, the terminal 91 is vertically downward, the terminal 91 is electrically connected with the camera 4 and an electric storage component of the aircraft, an electric slip ring 92 is arranged on the rotating disc 61, the center of the electric slip ring 92 coincides with the center of the rotating disc 61, a conducting strip 93 is arranged on the inner ring of the electric slip ring 92, the conducting strip 93 extends to the position of the terminal 91 to electrically connect the conducting strip 93 with the corresponding terminal 91, and the outer ring of the electric slip ring 92 is fixed on the rotating disc 61. When rotating disc 61 moves, the outer ring of electrical slip ring 92 rotates with rotating disc 61, and the inner ring of electrical slip ring 92 is blocked by conducting strip 93. After the stud 7 is locked with the semi-arc piece 62, the terminal post 91 at the lower end of the stud 7 is electrically connected with the conducting strip 93, so that the aircraft and the camera 4 can be charged.
The embodiment of this specific implementation mode is the preferred embodiment of the present invention, not limit according to this the utility model discloses a protection scope, so: all equivalent changes made according to the structure, shape and principle of the utility model are covered within the protection scope of the utility model.
Claims (8)
1. The utility model provides a construction progress monitored control system, includes mounting bracket (1), mounting bracket (1) upper portion is fixed with driving motor (2), the vertical setting of axis of driving motor (2), is fixed with installation piece (3) on the output shaft of driving motor (2), and installation piece (3) are located the top of driving motor (2), and the top of installation piece (3) is provided with camera (4), and the upper portion of camera (4) is connected with aircraft (5), its characterized in that: mounting hole (31) have been seted up to the upper surface of installation piece (3), the lower surface of camera (4) is provided with double-screw bolt (7), double-screw bolt (7) vertical setting, the inside of installation piece (3) is provided with rolling disc (61), rolling disc (61) are connected with rotating device, sliding connection has two half-arc pieces (62) on rolling disc (61), two half-arc pieces (62) set up relatively, two half-arc pieces (62) are connected with drive arrangement (8) that drive two half-arc pieces (62) relative or carried on the back the body motion, the line that the central point of two half-arc pieces (62) put is through mounting hole (31) round hole, two half-arc piece (62) inboard are seted up have with double-screw bolt (7) complex screw thread, the diameter of mounting hole (31) is greater than double-screw bolt (7) diameter and is less than the twice of double-screw bolt (7.
2. The construction progress monitoring system according to claim 1, characterized in that: drive arrangement (8) include screw rod (81), connection piece (82) and rotate motor (83), rotate motor (83) and fix on rolling disc (61), and the output at driving motor (2) is fixed to screw rod (81) coaxial, and the screw thread direction of turning at screw rod (81) both ends is opposite, and connection piece (82) have two, and two connection pieces (82) are fixed respectively on two half arc pieces (62), and two connection pieces (82) are respectively with the both ends screw-thread fit of screw rod (81).
3. A construction progress monitoring system according to claim 1 or 2, characterized in that: a guide hole (63) is formed in the rotating disc (61), a guide rod (64) is fixedly arranged on the back face of the half-arc piece (62), and the guide rod (64) is in sliding fit in the guide hole (63).
4. A construction progress monitoring system according to claim 3, characterized in that: the rotating device comprises a locking motor (65), the locking motor (65) is fixedly arranged on the mounting block (3), the output end of the locking motor (65) is arranged on the lower surface of the rotating disc (61), and the central line of the output shaft of the locking motor (65) is overlapped with the central line of the mounting hole (31).
5. The construction progress monitoring system according to claim 4, characterized in that: the lower end of the stud (7) is provided with a binding post (91), the binding post (91) is vertically downward, an electric slip ring (92) is arranged on the rotating disc (61), a conducting strip (93) is arranged on the inner ring of the electric slip ring (92), the outer ring of the electric slip ring (92) is fixed on the rotating disc (61), and the conducting strip (93) extends to the position of the binding post (91).
6. The construction progress monitoring system according to claim 1, characterized in that: the upper surface of installation piece (3) is provided with blocks (10), and the lower surface of aircraft (5) is provided with blocks post (11), blocks the vertical setting of post (11), blocks the distance of post (11) and double-screw bolt (7) and equals to block the distance at block (10) apart from mounting hole (31) center.
7. The construction progress monitoring system according to claim 6, characterized in that: the number of the blocking columns (11) is two, and the two blocking columns (11) are located in the circumferential direction of the stud (7) and are evenly distributed.
8. The construction progress monitoring system according to claim 7, characterized in that: the upper part of the stop block (10) is arranged in a triangle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921118288.7U CN210196889U (en) | 2019-07-16 | 2019-07-16 | Construction progress monitoring system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921118288.7U CN210196889U (en) | 2019-07-16 | 2019-07-16 | Construction progress monitoring system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210196889U true CN210196889U (en) | 2020-03-27 |
Family
ID=69867884
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921118288.7U Expired - Fee Related CN210196889U (en) | 2019-07-16 | 2019-07-16 | Construction progress monitoring system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210196889U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112849423A (en) * | 2021-02-07 | 2021-05-28 | 广东金筑工程管理有限公司 | Unmanned aerial vehicle building engineering supervision system |
-
2019
- 2019-07-16 CN CN201921118288.7U patent/CN210196889U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112849423A (en) * | 2021-02-07 | 2021-05-28 | 广东金筑工程管理有限公司 | Unmanned aerial vehicle building engineering supervision system |
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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: 20200327 |