Laser measuring instrument for highway engineering surveying and mapping

By designing a laser measuring instrument for highway engineering surveying and mapping with autonomous surface travel and flight modes, the problems of low surveying and mapping efficiency and great limitations in the existing technology have been solved, and more efficient and practical surveying and mapping effects have been achieved.

CN119509489AInactive Publication Date: 2025-02-25NANPI COUNTY TRANSPORTATION BUREAU
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Patent Information

Application Number
CN202411436859.7
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2024-10-15
Publication Date
2025-02-25
Estimated Expiration
Not applicable · inactive patent

AI Technical Summary

Technical Problem

The existing laser measuring instruments for highway engineering surveying and mapping require a lot of manual intervention in the mapping process of forming multiple surveying and mapping points, which is inefficient, and have great limitations in complex terrain and building environments; the sustainability of surveying and mapping drones is limited, especially in the complex and chaotic highway surveying and mapping process.

Method used

A laser measuring instrument for highway engineering surveying and mapping is designed, with two modes of autonomous surface travel and flight travel. It realizes autonomous surveying and mapping through image acquisition system and remote control carrier, which is suitable for a variety of terrain and building environments.

Benefits of technology

It improves the efficiency and practicality of surveying and mapping, reduces the limitations of surveying and mapping, and can better adapt to the surveying and mapping needs of complex terrain and building environments.

✦ Generated by Eureka AI based on patent content.

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Abstract

The invention relates to the technical field of surveying and mapping devices, and provides a laser measuring instrument for highway engineering surveying and mapping, which has two advancing modes of autonomous ground surface advancing and flying advancing on the basis of meeting basic surveying and mapping, and is higher in applicability to various terrains and buildings in the actual surveying and mapping process, the surveying and mapping limitation is further reduced, and the surveying and mapping efficiency is improved. The system comprises an information processor, an image acquisition system and a remote control carrier, the image acquisition system comprises a swing arm platform, a camera and a laser surveying and mapping instrument, the swing arm platform is provided with an installation plane, the camera is installed on the installation plane, the laser surveying and mapping instrument is installed on the camera in a matched mode, and the camera is a rotary camera. The laser surveying instrument is matched with the rotation of the camera and rotates synchronously, the coincident overlapping of a camera acquisition area and an area measured by the laser surveying instrument is realized, the remote control carrier comprises a center frame, a mounting cavity is formed in the center frame, the information processor is mounted in the mounting cavity, and a gyroscope and a GPS terminal are mounted in the mounting cavity.
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Description

Technical Field

[0001] The invention relates to the technical field of surveying and mapping devices, and in particular to a laser measuring instrument for surveying and mapping highway projects. Background Art

[0002] As we all know, the laser measuring instrument used for highway engineering surveying is an advanced surveying tool. It can cooperate with highway engineering surveying personnel to carry out on-site auxiliary surveying and mapping operations, making it convenient to conduct surveying and mapping work on the corresponding areas of highway projects.

[0003] After searching, the Chinese patent publication number CN220398565U discloses a laser surveying instrument that is easy to adjust. It is roughly described as including a laser surveying instrument, a laser projector, a tripod, a top seat, and a fitting seat. The outer side of the laser surveying instrument is provided with a connecting mechanism that can quickly and conveniently connect the laser surveying instrument to the fitting seat of the tripod and an adjusting mechanism that can conveniently adjust the laser projection angle of the laser projector. When in use, the rotating shaft is driven by holding the handle, and the ball rotates in the rotating groove to adjust the angle of the laser projector. Through the fitting contact between the damping groove and the damping edge, resistance can be generated during the rotation of the two, thereby preventing the rotating shaft from rotating too fast, effectively improving the accuracy of the angle adjustment of the laser projector, and the rotating shaft is adjusted by twisting the threaded rod under the action of the bearing to push the limit block to fit with the limit groove. The patent with Chinese patent publication number CN218258742U also discloses a surveying and mapping UAV, which is roughly described as comprising a surveying and mapping UAV body, an auxiliary mechanism is arranged on the top of the surveying and mapping UAV body, a USB interface is fixedly connected to the top of the surveying and mapping UAV body and on the front of the auxiliary mechanism, a supporting tripod is fixedly connected to the bottom of the surveying and mapping UAV body, a non-slip pad is fixedly connected to the bottom of the supporting tripod, the auxiliary mechanism comprises an auxiliary frame slidably connected to the top of the surveying and mapping UAV body, a lithium battery is slidably connected inside the auxiliary frame, mounting plates are fixedly connected on both sides of the auxiliary frame, a connecting plate is slidably connected inside the mounting plate, and an additional lithium battery is installed by using the auxiliary mechanism in the device, and when in use, the corresponding surveying and mapping operation is realized by flying the surveying and mapping UAV.

[0004] Although the above-mentioned existing technical solutions can achieve the purpose of surveying and mapping, the former laser surveying instrument, which is easy to adjust, requires more manual intervention in the process of surveying multiple surveying points, so the efficiency of surveying and mapping needs to be further improved. In addition, once the actual surveying and mapping process is blocked by the surface trend or surface buildings, the corresponding surveying and mapping is difficult to carry out, and the surveying and mapping range is greatly limited. For the latter surveying and mapping drone, its surveying and mapping needs to be kept in flight. Even if it has an additional lithium battery, the sustainability of surveying and mapping is still limited, especially for the surveying and mapping of highways with numerous and complicated surveying and mapping work, the practicality needs to be further enhanced. Summary of the invention

[0005] Technical issues solved

[0006] In view of the shortcomings of the prior art, the present invention provides a laser measuring instrument for highway engineering surveying and mapping, which, on the basis of meeting basic surveying and mapping requirements, has two travel modes: autonomous surface travel and flying travel. In the actual surveying and mapping process, it is more applicable to a variety of terrains and buildings, and the limitations of surveying and mapping are further reduced, making it more practical.

[0007] Technical Solution

[0008] To achieve the above-mentioned purpose, the present invention provides the following technical solutions: a laser surveying instrument for highway engineering surveying and mapping, comprising an information processor, an image acquisition system and a remote control carrier, the image acquisition system comprising a swing arm platform, a camera and a laser surveying and mapping instrument, the swing arm platform is provided with a mounting plane, the camera is mounted on the mounting plane, the laser surveying and mapping instrument is mounted on the camera in a supporting manner, the camera is a rotating camera, the laser surveying and mapping instrument rotates synchronously with the rotation of the supporting camera, so that the camera acquisition area and the area measured by the laser surveying and mapping instrument overlap and are consistent, the remote control carrier comprises a center frame, the center frame is provided with a mounting cavity, the information processor is mounted on the center frame, the information processor is mounted on the center frame, the image acquisition system comprises a swing arm platform, a camera and a laser surveying and mapping instrument are mounted on the swing arm platform, the camera is provided with a mounting cavity, the laser surveying and mapping instrument is mounted on the camera in a supporting manner, the camera is provided with a mounting cavity, the information processor is mounted on the center frame, the image acquisition system comprises a swing arm platform, a camera and a laser surveying and mapping instrument are ... It is installed in the installation cavity, and a gyroscope and a GPS terminal are installed in the installation cavity. The gyroscope, GPS terminal, camera and laser surveying instrument are all electrically connected to the information processor. The left and right ends of the central frame are fixedly connected to the installation barrel frame. The swing arm platform is fixedly connected to two swivel seats, and the two swivel seats are respectively rotatably connected to the two installation barrel frames. Mobile execution components are installed on the two installation barrel frames. An electric telescopic rod is installed at the bottom end of the central frame. The electric telescopic rod forms a synchronous adjustment control of the two mobile execution components. A flip linkage structure is installed in the central frame, and the electric telescopic rod realizes the linkage flipping of the swing arm platform through the flip linkage structure.

[0009] Preferably, the flip linkage structure includes two driving racks, sliding grooves are provided at the left and right ends of the center frame, the two driving racks are respectively slidably connected in the two sliding grooves, and limit bars are fixedly connected in the two sliding grooves. Limiting grooves matching the limit bars are provided on the two driving racks, and the two driving racks are meshed with transmission gear rings, and the two transmission gear rings are respectively fixedly connected to the two rotating ring seats, and a synchronous frame is fixedly connected between the two driving racks, and the synchronous frame is fixedly connected to a connecting spring, and the connecting spring is fixedly connected to a transmission frame, and the transmission frame is connected to the telescopic rod of the electric telescopic rod.

[0010] Preferably, the two moving execution components each include a sliding column, an inner wing arm and an outer wing arm, the two sliding columns are respectively slidably connected to the two mounting cylinder frames, the ends of the two sliding columns close to each other are rotatably connected to a transmission member, the two transmission members are rotatably connected to the transmission frame, the two sliding columns are rotatably connected to an inner rotating frame and an outer rotating frame, the two inner wing arms and the two outer wing arms are both equipped with an electric wheel wing assembly, the two inner wing arms and the two outer wing arms are fixedly connected to threaded rods, the two inner rotating frames and the two outer rotating frames are fixedly connected to threaded sleeves, the four threaded rods are respectively threadedly fitted in the four threaded sleeves, the four threaded rods are rotatably connected to traction rings, and the four traction rings are fixedly connected to maintaining springs, and the four maintaining springs are respectively It is fixedly connected to four threaded sleeves, and two sliding columns are fixedly connected to two ring tracks, and the four traction rings are respectively slidably connected to the four ring tracks, and the two mounting cylinder frames are fixedly connected with an inner traction rope and an outer traction rope, the two inner traction ropes are respectively fixedly connected to the two inner rotating frames, and the two outer traction ropes are respectively fixedly connected to the two outer rotating frames, and the two sliding columns are fixedly connected with guide members, and the two guide members are respectively used for steering guidance of the two outer traction ropes, and the two guide members are also respectively used for steering guidance of the two inner traction ropes, and the two sliding columns are connected with an inner connecting spring and an outer connecting spring, and the two inner connecting springs are respectively connected to the two inner rotating frames, and the two outer connecting springs are respectively connected to the two outer rotating frames.

[0011] Preferably, the four electric wheel wing assemblies all include terminal frames, and the four terminal frames are respectively fixedly connected to the two inner wing arms and the two outer wing arms, and a central shaft is rotatably connected in each of the four terminal frames, and a variable frequency motor is installed in each of the four terminal frames. The four variable frequency motors are respectively used for rotational driving of the four central shafts, and a rotating part is installed on each of the four central shafts, and a plurality of fixed rotors are fixedly connected to each of the four rotating parts, and the plurality of fixed rotors on the same rotating part are fixedly connected to a wheel rim, and a plurality of circular holes are opened on the four wheel rims, and sliding rotors are slidably connected in the plurality of circular holes, and retractable parts are installed in the plurality of fixed rotors, and the plurality of retractable parts are respectively matched with the plurality of sliding rotors.

[0012] Preferably, the multiple retractable parts all include flexible springs and permanent magnets, the multiple flexible springs are respectively fixedly connected in the multiple fixed rotors, the multiple flexible springs are respectively fixedly connected to the multiple sliding rotors, the multiple permanent magnets are respectively fixedly connected in the multiple fixed rotors, the multiple sliding rotors are each provided with a magnetic block, the multiple magnetic blocks are respectively matched with the multiple permanent magnets, and the multiple sliding rotors are each made of a material that cannot be attracted by magnetism.

[0013] Preferably, a plugging plate is fixedly connected to each of the plurality of sliding rotors, the plurality of plugging plates are respectively matched with the plurality of circular holes, and the plurality of plugging plates are made of a material that can be magnetically attracted by a permanent magnet.

[0014] Preferably, the two inner rotating frames and the two outer rotating frames each include an upper assembly frame and a lower assembly frame, the two inner traction ropes and the two outer traction ropes are respectively fixedly connected to the four upper assembly frames, the four upper assembly frames are respectively fixedly connected to the four lower assembly frames, the threaded sleeve is fixedly connected between the upper assembly frame and the lower assembly frame fixedly connected to each other, and the two inner connecting springs and the two outer connecting springs are respectively fixedly connected to the four upper assembly frames.

[0015] Preferably, the guide member is provided with an inner turning hole, an outer turning hole and a return hole, the two inner turning holes are respectively used for passing through the two inner traction ropes, the two outer turning holes are respectively used for passing through the two outer traction ropes, the two return holes are respectively used for passing through the two inner traction ropes, and the two return holes are also respectively used for passing through the two outer traction ropes.

[0016] Preferably, the information processor includes a control terminal, a communication module, a storage module and a power module. The communication module is used to realize wireless communication with the control terminal held by the operator to ensure the accurate transmission of instructions and the real-time return of data. The instructions received by the supporting communication module of the control terminal form a matching conversion and output of the instructions to form the corresponding operation of the camera, laser surveying instrument, electric telescopic rod and variable frequency motor. The storage module stores the operation data of the camera, laser surveying instrument, electric telescopic rod and variable frequency motor. The power module provides the necessary power supply for the gyroscope, GPS terminal, information processor, camera, laser surveying instrument, electric telescopic rod and variable frequency motor.

[0017] Preferably, storage grooves are provided on the plurality of fixed rotors, the plurality of storage grooves are matched with the plurality of sliding rotors respectively, and a plurality of anti-skid ridges are provided on the four wheel rims.

[0018] Beneficial Effects

[0019] Compared with the prior art, the present invention provides a laser measuring instrument for highway engineering surveying and mapping, which has the following beneficial effects:

[0020] (1) In the present invention, a specific surveying and mapping functional component is formed by configuring an image acquisition system, which can realize the acquisition of images of the corresponding measurement area while realizing the specific data measurement. On the basis of satisfying basic surveying and mapping, the data acquisition is richer and the functionality is stronger.

[0021] (2) In the present invention, through the design of a remote control carrier, a carrier is formed for the image acquisition system and the information processor, which has two travel modes: autonomous surface travel and flying travel. In the actual surveying and mapping process, it is more applicable to various terrains and buildings, and the limitations of surveying and mapping are further reduced, making it more practical. BRIEF DESCRIPTION OF THE DRAWINGS

[0022] Figure 1 It is a schematic diagram of the overall three-dimensional structure of the present invention;

[0023] Figure 2 For the present invention Figure 1 A schematic diagram of the local enlarged structure at point A in the middle;

[0024] Figure 3 For the present invention Figure 1 A schematic diagram of the local enlarged structure at B in the middle;

[0025] Figure 4 It is a partially cutaway three-dimensional structural schematic diagram of the cooperation of the center frame, the mounting cylinder frame and the swivel seat of the present invention;

[0026] Figure 5 It is a schematic diagram of the three-dimensional structure of the wheel rim, sliding rotor and flexible spring of the present invention;

[0027] Figure 6 It is a schematic diagram of the three-dimensional structure of the rotating member, the fixed rotor and the magnetic suction block of the present invention;

[0028] Figure 7 It is a schematic diagram of an exploded three-dimensional structure of the threaded rod, threaded sleeve and traction ring of the present invention;

[0029] Figure 8 It is a schematic diagram of the three-dimensional structure of the center frame and the mounting cylinder frame of the present invention;

[0030] Fig. 9 It is a schematic diagram of the three-dimensional structure of the connection spring, the transmission frame and the sliding column of the present invention;

[0031] Fig.10 It is a schematic diagram of the overall three-dimensional structure of the present invention when viewed from above;

[0032] Fig.11 It is a schematic diagram of the three-dimensional structure of the terminal frame, the central axis and the variable frequency motor of the present invention;

[0033] Fig.12 It is a partially cutaway three-dimensional structural schematic diagram of the threaded rod, threaded sleeve, traction ring, etc. of the present invention.

[0034] In the figure: 1. swing arm platform; 2. camera; 3. laser mapping instrument; 4. center frame; 5. installation cavity; 6. installation cylinder frame; 7. swivel seat; 8. electric telescopic rod; 9. driving rack; 10. sliding groove; 11. limit strip; 12. limit groove; 13. transmission gear ring; 14. synchronous frame; 15. connecting spring; 16. transmission frame; 17. sliding column; 18. transmission part; 19. inner wing arm; 20. outer wing arm; 21. threaded rod; 22. threaded sleeve; 23. traction ring; 24. ring track ; 25. External traction rope; 26. Internal traction rope; 27. Guide; 28. Internal connecting spring; 29. ​​External connecting spring; 30. Terminal frame; 31. Central axis; 32. Frequency conversion motor; 33. Rotating member; 34. Fixed rotor; 35. Wheel rim; 36. Sliding rotor; 37. Flexible spring; 38. Permanent magnet; 39. Magnetic block; 40. Plug plate; 41. Upper assembly frame; 42. Lower assembly frame; 43. External steering hole; 44. Internal steering hole; 45. Return hole; 46. Storage tank; 47. Anti-slip ridge. DETAILED DESCRIPTION

[0035] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0036] Example

[0037] See also Figure 1 -Attached Fig.12A laser surveying instrument for highway engineering surveying and mapping includes an information processor, an image acquisition system and a remote control carrier. The image acquisition system includes a swing arm platform 1, a camera 2 and a laser surveying and mapping instrument 3. The swing arm platform 1 is provided with a mounting plane, the camera 2 is mounted on the mounting plane, and the laser surveying and mapping instrument 3 is mounted on the camera 2 in a supporting manner. The camera 2 is a rotating camera 2, and the laser surveying and mapping instrument 3 rotates synchronously with the rotation of the camera 2 to achieve the overlap between the acquisition area of ​​the camera 2 and the area measured by the laser surveying and mapping instrument 3. Through the configuration of the image acquisition system, a specific surveying and mapping functional component is formed, and the image of the corresponding measurement area can be acquired while the specific data is measured. On the basis of meeting the basic surveying and mapping requirements, the data acquisition is richer and the functionality is stronger. The remote control carrier includes a central frame 4, in which a mounting cavity 5 is provided, in which an information processor is installed, in which a gyroscope and a GPS terminal are installed, and the gyroscope, the GPS terminal, the camera 2 and the laser surveying instrument 3 are electrically connected to the information processor, and the left and right ends of the central frame 4 are fixedly connected to mounting barrel frames 6, and the swing arm platform 1 is fixedly connected to two swivel seats 7, and the two swivel seats 7 are rotatably connected to the two mounting barrel frames 6 respectively, and mobile execution components are installed on the two mounting barrel frames 6, and an electric telescopic rod 8 is installed at the bottom end of the central frame 4, and the electric telescopic rod 8 forms a synchronous adjustment control of two mobile execution components. Through the design of the remote control carrier, a carrier is formed for the image acquisition system and the information processor, and has the ability of autonomous surface movement and flight. There are two travel modes. In the actual surveying and mapping process, it is more applicable to various terrains and buildings, the surveying and mapping limitations have been further reduced, and it is more practical. The two mobile execution components include a sliding column 17, an inner wing arm 19 and an outer wing arm 20. The two sliding columns 17 are slidably connected to the two mounting cylinder frames 6 respectively, and the ends of the two sliding columns 17 close to each other are rotatably connected with a transmission member 18, and the two transmission members 18 are rotatably connected to the transmission frame 16. The two sliding columns 17 are rotatably connected with an inner rotating frame and an outer rotating frame. The two inner wing arms 19 and the two outer wing arms 20 are installed with electric wheel wing assemblies. The two inner wing arms 19 and the two outer wing arms 20 are fixedly connected with threaded rods 21. The two inner rotating frames and the two outer rotating frames are fixedly connected with threaded rods. The sleeve 22, the four threaded rods 21 are respectively threadedly fitted in the four threaded sleeves 22, the four threaded rods 21 are rotatably connected with traction rings 23, and the four traction rings 23 are fixedly connected with maintaining springs, the four maintaining springs are respectively fixedly connected with the four threaded sleeves 22, the two sliding columns 17 are respectively fixedly connected with two ring tracks 24, the four traction rings 23 are respectively slidably connected to the four ring tracks 24, the two mounting cylinder frames 6 are respectively fixedly connected with inner traction ropes 26 and outer traction ropes 25, the two inner traction ropes 26 are respectively fixedly connected with the two inner rotating frames, the two outer traction ropes 25 are respectively fixedly connected with the two outer rotating frames, the two sliding columns 17 are respectively fixedly connected with guide members 27, and the two guide members 27 are respectively used for steering guidance of the two outer traction ropes 25,The two guide members 27 are also used for steering the two inner traction ropes 26. The two sliding columns 17 are connected with inner connecting springs 28 and outer connecting springs 29. The two inner connecting springs 28 are connected with the two inner rotating frames, and the two outer connecting springs 29 are connected with the two outer rotating frames.

[0038] It should be further explained that the four electric wheel wing assemblies each include a terminal frame 30, the four terminal frames 30 are respectively fixedly connected to the two inner wing arms 19 and the two outer wing arms 20, the four terminal frames 30 are rotatably connected with a central shaft 31, the four terminal frames 30 are each installed with a variable frequency motor 32, the four variable frequency motors 32 are respectively used for the rotation drive of the four central shafts 31, the four central shafts 31 are each installed with a rotating member 33, the four rotating members 33 are each fixedly connected with a plurality of fixed rotors 34, the plurality of fixed rotors 34 on the same rotating member 33 are fixedly connected with a wheel rim 35, the four wheel rims 35 are each provided with a plurality of circular holes, and the plurality of circular holes are each slidingly connected. A sliding rotor 36 is connected, and a plurality of fixed rotors 34 are each installed with a retractable member, and the plurality of retractable members are respectively matched with the plurality of sliding rotors 36, and the plurality of retractable members each include a flexible spring 37 and a permanent magnet 38, and the plurality of flexible springs 37 are respectively fixedly connected in the plurality of fixed rotors 34, and the plurality of flexible springs 37 are respectively fixedly connected with the plurality of sliding rotors 36, and the plurality of permanent magnets 38 are respectively fixedly connected in the plurality of fixed rotors 34, and a magnetic suction block 39 is provided on the plurality of sliding rotors 36, and the plurality of magnetic suction blocks 39 are respectively matched with the plurality of permanent magnets 38, and the plurality of sliding rotors 36 are all made of a material that cannot be attracted by magnetism, so as to facilitate the relative adjustment process between the sliding rotor 36 and the fixed rotor 34 Auxiliary limit, multiple sliding rotors 36 are fixedly connected with plugging plates 40, multiple plugging plates 40 are respectively matched with multiple circular holes, multiple plugging plates 40 are made of materials that can be magnetically attracted by permanent magnets 38, when the sliding rotor 36 is retracted relative to the fixed rotor 34, the plugging plates 40 are convenient for blocking the circular holes, and also convenient for the auxiliary limit after the sliding rotor 36 is retracted relative to the fixed rotor 34, a flip linkage structure is installed in the center frame 4, and the electric telescopic rod 8 realizes the linkage flipping of the swing arm platform 1 through the flip linkage structure, and the flip linkage structure includes two driving racks 9, and the left and right ends of the center frame 4 are provided with sliding grooves 10, and the two driving racks 9 are respectively slidably connected in two sliding grooves 10, and the two sliding grooves 10 are fixedly connected with limit strips 11, and the two driving racks 9 are provided with limit slots 12 matching the limit strips 11, and the two driving racks 9 are meshed with transmission gear rings 13, and the two transmission gear rings 13 are respectively fixedly connected to the two swivel seats 7, and a synchronous frame 14 is fixedly connected between the two driving racks 9, and the synchronous frame 14 is fixedly connected with a connecting spring 15, and the connecting spring 15 is fixedly connected with a transmission frame 16, and the transmission frame 16 is connected with the telescopic rod of the electric telescopic rod 8, forming a specific display of the flip linkage structure, and the purpose of controlling the linkage movement of the swing arm platform 1 can be achieved through the operation of the electric telescopic rod 8.

[0039] It should be further explained that the two inner rotating frames and the two outer rotating frames each include an upper assembly frame 41 and a lower assembly frame 42, the two inner traction ropes 26 and the two outer traction ropes 25 are respectively fixedly connected to the four upper assembly frames 41, the four upper assembly frames 41 are respectively fixedly connected to the four lower assembly frames 42, the threaded sleeve 22 is fixedly connected between the upper assembly frames 41 and the lower assembly frames 42 fixedly connected to each other, the two inner connecting springs 28 and the two outer connecting springs 29 are respectively fixedly connected to the four upper assembly frames 41, the inner rotating frame and the outer rotating frame adopt a split design, comprehensively considering the processability, facilitating subsequent production and assembly, the guide member 27 is provided with an inner steering hole 44, an outer steering hole 43 and a return hole 45, the two inner steering holes 44 are respectively used for the passage of the two inner traction ropes 26, the two outer steering holes 43 are respectively used for the passage of the two outer traction ropes 25, the two return holes 45 are respectively used for the passage of the two inner traction ropes 26, and the two return holes 45 are also respectively used for the two outer traction ropes The rope 25 passes through, the information processor includes a control terminal, a communication module, a storage module and a power module, the communication module is used to realize wireless communication with the control terminal held by the operator, to ensure the accurate transmission of instructions and the real-time return of data, the instructions received by the control terminal supporting the communication module form a matching conversion and output of the instructions, so as to form the corresponding operation of the camera 2, the laser surveying instrument 3, the electric telescopic rod 8, and the variable frequency motor 32, the storage module stores the operation data of the camera 2, the laser surveying instrument 3, the electric telescopic rod 8 and the variable frequency motor 32, the power module provides the necessary power supply for the gyroscope, the GPS terminal, the information processor, the camera 2, the laser surveying instrument 3, the electric telescopic rod 8 and the variable frequency motor 32, and the multiple fixed rotors 34 are provided with storage tanks 46, and the multiple storage tanks 46 are respectively matched with the multiple sliding rotors 36, and the four rims 35 are provided with multiple anti-skid ridges 47 to improve the anti-skid effect of the rims 35 when traveling.

[0040] To sum up, the working process of the laser measuring instrument for highway engineering surveying and mapping is as follows: when not in use, the remote control carrier in the laser measuring instrument for highway engineering surveying and mapping is in a retracted state as a whole. In this state, the telescopic rod of the electric telescopic rod 8 pushes the transmission frame 16 to form a relative displacement in the center frame 4. The displaced transmission frame 16 forms a traction effect relative to the transmission member 18, prompting the two sliding columns 17 to approach each other. Under the cooperation of the inner connecting spring 28 and the outer connecting spring 29, the two inner wing arms 19 are respectively rotated synchronously relative to the two outer wing arms 20 and the two inner wing arms 19 and the two outer wing arms 20 are brought together, so as to achieve the folding of the laser measuring instrument for highway engineering surveying and mapping. After folding, the overall size is greatly reduced, thereby achieving the effect of convenient carrying and storage. When in use, the electric telescopic rod 8 controls the transmission frame 16 to move toward the two inner wings in the aforementioned steps. The arms 19 and the two outer wing arms 20 are pushed in the opposite direction of the closing direction. Under the synchronous pushing action of the transmission frame 16 on the two transmission members 18, the two sliding columns 17 will be pushed to form a relative distance. Due to the traction action of the inner traction rope 26 and the outer traction rope 25, when the two sliding columns 17 move away from each other, the two inner wing arms 19 will form a relative rotation adjustment relative to the two outer wing arms 20, so as to ensure that the two inner wing arms 19 are respectively rotated and unfolded relative to the two outer wing arms 20, so as to achieve the four wheel rims 35 can be relatively separated, so as to form a stable support for the center frame 4. When it is necessary to travel on the surface, the rotation amplitude of the inner wing arm 19 and the outer wing arm 20 is controlled so that the traction ring 23 has not yet entered the corresponding reduced diameter area on the ring track 24. In this way, under the elastic pushing action of the maintaining spring, the wheel rim 35 remains in an upright state. At this time, the state is as shown in the attached figure. Figure 1 As shown, when flying is required, the electric telescopic rod 8 continues to work to form a relative push between the two sliding columns 17, so that the traction of the inner traction rope 26 and the outer traction rope 25 causes the rotation amplitude of the inner rotating frame and the outer rotating frame to be larger, until the traction ring 23 enters the corresponding reduced diameter area on the ring track 24. Under the traction effect of the corresponding reduced diameter area on the ring track 24 on the traction ring 23, a relative drive will be formed between the threaded rod 21 and the threaded sleeve 22 that are threadedly matched with each other, which will cause the threaded rod 21 to rotate relative to the threaded sleeve 22, prompting the wheel 35 to enter the horizontal state from the upright state, which is convenient for the laser measuring instrument for highway engineering surveying and mapping to enter the flying state.

[0041] Furthermore, the swing arm platform 1 is coordinated with the operation of the electric telescopic rod 8. Due to the transmission effect of the driving rack 9, the transmission gear ring 13, the synchronous frame 14, the connecting spring 15 and the transmission frame 16, when the electric telescopic rod 8 controls the folding of the two inner wing arms 19 and the two outer wing arms 20, the swing arm platform 1 also forms a lying posture relative to the center frame 4. When the electric telescopic rod 8 controls the laser measuring instrument for highway engineering surveying and mapping to enter the attached Figure 1In the state shown, under the push of the transmission connecting frame 16, the swing arm platform 1 is above the center frame 4 relative to the center frame 4, which is convenient for the camera 2 and the laser surveying instrument 3 to be in a relatively high position relative to the center frame 4 to facilitate the acquisition of surveying and mapping graphics. When the highway engineering surveying and mapping laser measuring instrument enters the flying state, under the push of the transmission connecting frame 16, the swing arm platform 1 is below the center frame 4 relative to the center frame 4, which is convenient for the camera 2 and the laser surveying instrument 3 to be in a relatively low position relative to the center frame 4 to facilitate the acquisition of surveying and mapping graphics. The limit range of the swing arm platform 1 is limited by the relative sliding limit between the limiting strip 11 and the limiting groove 12. Due to the connection spring 15 When the swing arm platform 1 enters the limited position, the transmission frame 16 can also form a linkage adjustment with the transmission member 18 to enrich the adjustable range of the remote control carrier. When entering the flight state, the variable frequency motor 32 drives the rotating member 33 to rotate. When the rotating member 33 is driven to a certain speed by the variable frequency motor 32, the rotating sliding rotor 36 can overcome the relative magnetic attraction between the permanent magnet 38 and the plug plate 40 under the action of centrifugal force, so that the sliding rotor 36 can slide out relative to the fixed rotor 34. When the centrifugal force borne by the rotating sliding rotor 36 increases again, the sliding rotor 36 can overcome the elastic pulling force of the flexible spring 37 and move outward relative to the fixed rotor 34, so that the sliding rotor 36 and the fixed rotor 34 can be moved outward. 4, when the magnetic block 39 is relatively close to the permanent magnet 38, under the action of the relative magnetic force between the magnetic block 39 and the permanent magnet 38 and the rotational centrifugal force of the sliding rotor 36, the position of the sliding rotor 36 and the fixed rotor 34 after sliding out relative to each other is stabilized, that is, when the centrifugal force borne by the sliding rotor 36 is greater than a certain range of values, the sliding rotor 36 will not slide back relative to the fixed rotor 34, and when the centrifugal force borne by the sliding rotor 36 is less than a certain range of values, the sliding rotor 36 will slide back relative to the fixed rotor 34 under the traction of the flexible spring 37, so as to facilitate the transition between the two modes of surface travel and flight travel. Automatic switching, during the movement of the remote control carrier, when it enters a suitable surveying and mapping coordinate point, it enters a parked state. If it is moving on the surface, it is not moving relative to the surface. If it is flying and cannot land, it adopts a suspended and stationary parking mode. The camera 2 forms an image acquisition for the corresponding target acquisition area, and the laser surveying and mapping instrument 3 performs quantitative measurement of specific data of the corresponding points of the camera 2 image acquisition to cooperate with the camera 2 to form a supplement to the matching acquisition information. At the same time, the gyroscope stabilizes the overall movement posture of the center frame 4. The GPS terminal can realize the auxiliary positioning of the spatial position of the laser surveying and mapping instrument for highway engineering surveying and mapping, so as to facilitate the determination of the position of the laser surveying and mapping instrument for highway engineering surveying and mapping.

[0042] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A laser measuring instrument for highway engineering surveying and mapping, comprising an information processor, characterized in that: The device also comprises an image acquisition system and a remote control carrier, wherein the image acquisition system comprises a swing arm platform (1), a camera (2) and a laser mapper (3), wherein a mounting plane is arranged on the swing arm platform (1), the camera (2) is mounted on the mounting plane, the laser mapper (3) is mounted on the camera (2), the camera (2) is a rotating camera (2), and the laser mapper (3) rotates synchronously with the rotation of the camera (2), so that the acquisition area of ​​the camera (2) and the area measured by the laser mapper (3) overlap and are consistent, and the remote control carrier comprises a central frame (4), wherein a mounting cavity (5) is provided in the central frame (4), the information processor is mounted in the mounting cavity (5), and a rotor is mounted in the mounting cavity (5). The invention relates to a gyroscope and a GPS terminal, wherein the gyroscope, the GPS terminal, the camera (2) and the laser surveying instrument (3) are all electrically connected to the information processor, the left and right ends of the central frame (4) are fixedly connected to the mounting barrel frame (6), the swing arm platform (1) is fixedly connected to two swivel seats (7), the two swivel seats (7) are respectively rotatably connected to the two mounting barrel frames (6), the two mounting barrel frames (6) are both installed with a mobile execution component, the bottom end of the central frame (4) is installed with an electric telescopic rod (8), the electric telescopic rod (8) forms a synchronous adjustment control of the two mobile execution components, and a flip linkage structure is installed in the central frame (4), and the electric telescopic rod (8) realizes the linkage flipping of the swing arm platform (1) through the flip linkage structure.

2. A laser measuring instrument for highway engineering surveying and mapping according to claim 1, characterized in that: The flip linkage structure comprises two driving racks (9), the left and right ends of the central frame (4) are provided with sliding grooves (10), the two driving racks (9) are respectively slidably connected in the two sliding grooves (10), the two sliding grooves (10) are fixedly connected with limit bars (11), the two driving racks (9) are provided with limit grooves (12) matching the limit bars (11), the two driving racks (9) are meshed with transmission gear rings (13), the two transmission gear rings (13) are respectively fixedly connected to the two rotating ring seats (7), a synchronous frame (14) is fixedly connected between the two driving racks (9), the synchronous frame (14) is fixedly connected with a connecting spring (15), the connecting spring (15) is fixedly connected with a transmission frame (16), and the transmission frame (16) is connected to the telescopic rod of the electric telescopic rod (8).

3. A laser measuring instrument for highway engineering surveying and mapping according to claim 2, characterized in that: The two moving execution components each include a sliding column (17), an inner wing arm (19) and an outer wing arm (20), the two sliding columns (17) are respectively slidably connected to the two mounting cylinder frames (6), the ends of the two sliding columns (17) close to each other are rotatably connected to a transmission member (18), the two transmission members (18) are rotatably connected to the transmission frame (16), the two sliding columns (17) are rotatably connected to an inner rotating frame and an outer rotating frame, the two inner wing arms (19) and the two outer wing arms (20) are rotatably connected to the inner rotating frame and the outer rotating frame, and the two inner wing arms (19) and the two outer wing arms (20) are rotatably connected to the inner rotating frame and the outer rotating frame. The wing arms (20) are all equipped with electric wheel wing assemblies, the two inner wing arms (19) and the two outer wing arms (20) are all fixedly connected with threaded rods (21), the two inner rotating frames and the two outer rotating frames are all fixedly connected with threaded sleeves (22), the four threaded rods (21) are respectively threadedly engaged in the four threaded sleeves (22), the four threaded rods (21) are all rotatably connected with traction rings (23), and the four traction rings (23) are all fixedly connected with maintenance springs, and the four maintenance springs are respectively connected with the four The two sliding columns (17) are fixedly connected with two ring tracks (24), and the four traction rings (23) are respectively slidably connected to the four ring tracks (24). The two mounting cylinder frames (6) are fixedly connected with inner traction ropes (26) and outer traction ropes (25). The two inner traction ropes (26) are respectively fixedly connected with the two inner rotating frames, and the two outer traction ropes (25) are respectively fixedly connected with the two outer rotating frames. The two sliding columns (17) are fixedly connected with guide members (27). The two guide members (27) are respectively used for steering guidance of the two outer traction ropes (25). The two guide members (27) are also respectively used for steering guidance of the two inner traction ropes (26). The two sliding columns (17) are connected with inner connecting springs (28) and outer connecting springs (29). The two inner connecting springs (28) are respectively connected with the two inner rotating frames, and the two outer connecting springs (29) are respectively connected with the two outer rotating frames.

4. A laser measuring instrument for highway engineering surveying and mapping according to claim 3, characterized in that: The four electric wheel wing assemblies each comprise a terminal frame (30), the four terminal frames (30) being respectively fixedly connected to the two inner wing arms (19) and the two outer wing arms (20), the four terminal frames (30) being rotatably connected with a central shaft (31), the four terminal frames (30) being installed with a variable frequency motor (32), the four variable frequency motors (32) being respectively used for rotationally driving the four central shafts (31), the four central shafts (31) being installed with a rotating member (33), the four rotating members (33) being fixedly connected with a plurality of fixed rotors (34), the plurality of fixed rotors (34) on the same rotating member (33) being fixedly connected with a wheel rim (35), the four wheel rims (35) being provided with a plurality of circular holes, the plurality of circular holes being slidably connected with sliding rotors (36), the plurality of fixed rotors (34) being installed with a retractable member, the plurality of retractable members being respectively matched with the plurality of sliding rotors (36).

5. A laser measuring instrument for highway engineering surveying and mapping according to claim 4, characterized in that: The plurality of retractable components all include flexible springs (37) and permanent magnets (38); the plurality of flexible springs (37) are respectively fixedly connected in the plurality of fixed rotors (34); the plurality of flexible springs (37) are respectively fixedly connected to the plurality of sliding rotors (36); the plurality of permanent magnets (38) are respectively fixedly connected in the plurality of fixed rotors (34); the plurality of sliding rotors (36) are each provided with a magnetic attraction block (39); the plurality of magnetic attraction blocks (39) are respectively matched with the plurality of permanent magnets (38); and the plurality of sliding rotors (36) are each made of a material that cannot be attracted by magnetism.

6. A laser measuring instrument for highway engineering surveying and mapping according to claim 5, characterized in that: A plugging plate (40) is fixedly connected to each of the plurality of sliding rotors (36), and each of the plurality of plugging plates (40) matches each of the plurality of circular holes. Each of the plurality of plugging plates (40) is made of a material that can be magnetically attracted by the permanent magnet (38).

7. A laser measuring instrument for highway engineering surveying and mapping according to claim 6, characterized in that: The two inner rotating frames and the two outer rotating frames each comprise an upper assembly frame (41) and a lower assembly frame (42); the two inner traction ropes (26) and the two outer traction ropes (25) are respectively connected to the four upper assembly frames (41); the four upper assembly frames (41) are respectively fixedly connected to the four lower assembly frames (42); the threaded sleeve (22) is fixedly connected between the upper assembly frames (41) and the lower assembly frames (42) that are fixedly connected to each other; and the two inner connecting springs (28) and the two outer connecting springs (29) are respectively fixedly connected to the four upper assembly frames (41).

8. A laser measuring instrument for highway engineering surveying and mapping according to claim 7, characterized in that: The guide member (27) is provided with an inner turning hole (44), an outer turning hole (43) and a return hole (45); the two inner turning holes (44) are respectively used for passing through the two inner traction ropes (26); the two outer turning holes (43) are respectively used for passing through the two outer traction ropes (25); the two return holes (45) are respectively used for passing through the two inner traction ropes (26); and the two return holes (45) are also respectively used for passing through the two outer traction ropes (25).

9. A laser measuring instrument for highway engineering surveying and mapping according to claim 8, characterized in that: The information processor comprises a control terminal, a communication module, a storage module and a power module. The communication module is used to realize wireless communication with the control terminal held by the operator to ensure accurate transmission of instructions and real-time return of data. The control terminal matches the instructions received by the communication module to form a matching conversion and output of the instructions to form the corresponding operation of the camera (2), the laser surveying instrument (3), the electric telescopic rod (8) and the variable frequency motor (32). The storage module stores the operation data of the camera (2), the laser surveying instrument (3), the electric telescopic rod (8) and the variable frequency motor (32). The power module provides the necessary power supply for the gyroscope, the GPS terminal, the information processor, the camera (2), the laser surveying instrument (3), the electric telescopic rod (8) and the variable frequency motor (32).

10. A laser measuring instrument for highway engineering surveying and mapping according to claim 9, characterized in that: The plurality of fixed rotors (34) are each provided with a storage groove (46), the plurality of storage grooves (46) are respectively matched with the plurality of sliding rotors (36), and the four wheel rims (35) are each provided with a plurality of anti-skid ridges (47).

Citation Information

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