Space planning topographic survey device and method

Abstract

The invention relates to a space planning topographic measurement device and method, a gap is formed in the front side of a multifunctional box body, a telescopic topographic measurement instrument is installed in the gap, a controller with a networking module is installed in a second cavity, and a telescopic driving motor is arranged on one side of the controller; the output end of the telescopic driving motor is connected with a telescopic driving gear installed in the first cavity, the telescopic driving gear is matched with the rotating shaft through a linkage gear, a balancing weight and a direction control motor are installed on the rear side of the second cavity, a buoyancy block is arranged at the bottom of the multifunctional box body, and a propelling cavity is formed in the rear end of the buoyancy block. A propeller is mounted in the propelling cavity, and a rudder blade connected with the output end of the direction control motor is arranged on the outer side of the propeller, so that the measurement requirements under special complex working conditions and different working conditions can be met, and the working operation efficiency is high.

Description

Technical Field

[0001] The present invention relates to the technical field of topographic surveying and mapping, and in particular to a spatial planning topographic surveying device and method. Background Art

[0002] Topographic surveying refers to the work of surveying and mapping topographic maps. That is, the projection position and elevation of the objects and terrain on the earth's surface on the horizontal plane are measured, and then reduced to a certain scale and drawn into a topographic map with symbols and annotations. In the process of spatial planning and layout, it is necessary to use a topographic survey device to measure the topographic map. Traditional topographic survey devices have the following defects during use: First, there are many types of traditional topographic surveying devices, including those with mobile trolley bearing structures, those with drone bearing structures, and some measuring devices used under special working conditions. These measuring devices can generally only be used under one working condition. In actual surveying operations, we often encounter some special and complex working conditions and measurement requirements under different working conditions. Traditional measuring devices have single functions and weak ability to cope with multiple working conditions and complex working conditions. Therefore, there are certain disadvantages, which leads to reduced work efficiency. Secondly, the transmitter of traditional measuring devices is mostly a fixed structure, or a relative motion structure implemented by a rotating device. When in use, the transmitter measurement operation is carried out in a handheld or airborne manner. During use, it is subject to many restrictions during the operation of the airborne equipment, which often leads to a reduction in the measurement efficiency of the transmitter. Thirdly, traditional measuring equipment is inconvenient to transport and carry. No matter what form of airborne or handheld method is adopted, it requires a special box structure for reprinting. During the use of multi-fusion measurement operations, installation and disassembly are relatively inconvenient, and it is inconvenient to carry during reprinting, causing many inconveniences during use.

[0003] In view of the above problems, the present invention provides a spatial planning topographic measurement device and method, aiming to solve the problems that need to be solved urgently, such as low working and operation efficiency, inconvenient reprinting, single function, inability to cope with various working conditions or special working conditions, and installation defects at the transmitting end, etc. of traditional equipment and methods. Summary of the invention

[0004] The present invention provides a spatial planning topographic measurement device and method with simple structure, convenient operation, high working and operating efficiency, high intelligence, diverse functions, ability to be used under different and special working conditions, convenient carrying and reloading, high measurement efficiency, simple and easy operation, which is used to overcome the defects in the prior art.

[0005] The technical solution of the present invention is achieved as follows: a spatial planning topographic measurement device comprises a multifunctional box, wherein the multifunctional box is provided with an independent first cavity and a second cavity, a flight telescopic opening is provided on the side wall of the multifunctional box, a rotating shaft is installed in the first cavity inside the flight telescopic opening, a wing motor is installed at the end of the rotating shaft, the output end of the wing motor is connected to the wing, a notch is provided on the front side of the multifunctional box, a retractable topographic telescopic measurement instrument is installed in the notch, a controller with a networking module is installed in the second cavity, a telescopic drive motor is provided on one side of the controller, the output end of the telescopic drive motor is connected to the telescopic active gear installed in the first cavity, the telescopic active gear cooperates with the rotating shaft through a linkage gear, a counterweight block and a direction control motor are installed on the rear side of the second cavity, a buoyancy block is provided at the bottom of the multifunctional box, a propulsion cavity is provided at the rear end of the buoyancy block, a propeller is installed in the propulsion cavity, and a rudder blade connected to the output end of the direction control motor is provided on the outside of the propeller.

[0006] The buoyancy block is a block structure or a cavity structure made of buoyancy material. A first connecting buckle and a second connecting buckle are fixedly installed on the bottom surface of the buoyancy block. A shoulder strap clamping block is clamped on the first connecting buckle, and a shoulder strap adjustment seat is clamped on the second connecting buckle. The shoulder strap adjustment seat is connected to the shoulder strap clamping block through an adjustment ring and a shoulder strap, and a handle is provided on the outside of the shoulder strap clamping block.

[0007] An isolation plate is arranged between the first cavity and the second cavity, a telescopic containing box independent of the first cavity is arranged at the inner edge of the flight telescopic opening, a rotating shaft is arranged in the telescopic box, a wing protective cover is fixedly installed on the top of the outer end of the rotating shaft, the wing motor is arranged at the center position of the wing protective cover, a telescopic limit box is fixedly installed on the bottom wall of the telescopic containing box, an electric push rod is installed in the telescopic limit box, and the output end of the electric push rod is connected to the telescopic terrain telescopic measuring instrument through a telescopic rod.

[0008] A rechargeable battery assembly is installed in the second cavity, a bottom sealing plate is arranged at the bottom of the second cavity, and a limiting bracket is fixedly installed on the bottom sealing plate outside the telescopic drive motor.

[0009] The propulsion chamber is arranged below the counterweight block, and a propeller motor is embedded at the rear end of the buoyancy block. The output end of the propeller motor is connected to the propeller, and the output end of the direction control motor faces the propulsion chamber. The rudder blade is connected to the output of the direction control motor through a rotating connecting shaft block, and the outer edge of the rudder blade is arranged on the inner side of the inner edge of the propulsion chamber.

[0010] The isolation plate is arranged below the telescopic accommodating box, a support block is arranged between the telescopic accommodating box and the isolation plate, a through hole for the output shaft of the telescopic driving motor is opened on the isolation plate, a rotating support shaft is fixedly installed at the central axis position of the linkage gear, the upper part of the rotating support shaft is supported by the bottom wall of the telescopic accommodating box, a first bearing supporting the upper part of the rotating support shaft is installed on the bottom wall of the telescopic accommodating box, the lower part of the rotating support shaft is supported by the top wall of the isolation plate, and a second bearing supporting the lower part of the rotating support shaft is installed on the top wall of the isolation plate.

[0011] The bottom wall of the telescopic accommodating box is provided with a limit rotation ring, and the bottom of the rotating shaft is connected with the top of the linkage gear through the limit rotation ring.

[0012] A method for measuring terrain using a spatial planning terrain measuring device, characterized in that the method is divided into three modes: Aerial flight measurement mode: during measurement, the multifunctional box is placed horizontally on the open ground, and the telescopic drive motor is turned on through the remote control tablet. The telescopic drive motor drives the telescopic active gear to rotate, and the telescopic active gear drives the linkage gear to rotate. The linkage gear drives the rotation axis to rotate, and the four wings extend from the flight telescopic opening in pairs. The wing motor is turned on to drive the wing to rotate, and the multifunctional box is slowly lifted off. The retractable terrain telescopic measuring instrument is turned on through the controller, and laser measurement operations are carried out through the retractable terrain telescopic measuring instrument during flight; Water surface driving measurement mode: during measurement, the multifunctional box is placed on the water surface, and the propeller power end is turned on by the remote control tablet to drive the propeller to rotate. Under the action of the counterweight, water is poured into the propulsion chamber, and the propeller rotates in the water to propel the multifunctional box to drive on the water surface. During this period, the rotation angle of the rudder blade is controlled by turning on the direction control motor to realize the direction control of water surface driving. The retractable terrain telescopic measuring instrument is turned on by the controller, and laser measurement operations are carried out through the retractable terrain telescopic measuring instrument during water surface driving; Land-carrying measurement mode: during measurement, the multi-function box is placed on the top of a moving vehicle, and the laser measurement operation is carried out by opening the retractable topographic telescopic measuring instrument while the vehicle is moving, or the shoulder strap clamping block is installed on the first connecting buckle, the shoulder strap adjustment seat is installed on the second connecting buckle, and the adjustment ring and shoulder strap are installed. The multi-function box is carried on the human body through the shoulder strap, and the retractable topographic telescopic measuring instrument is turned on by the controller. During the coating and walking process, the laser topographic measurement operation is carried out through the retractable topographic telescopic measuring instrument.

[0013] The present invention has the following positive effects: 1. The present invention adopts a one-machine-multiple-purpose mode, which is suitable for use under different working conditions. It can provide terrain measurement operations on land, water and air, and is suitable for use in different scenes and working conditions. It implements laser measurement operations through a retractable terrain telescopic measuring instrument, which can meet the measurement needs under special and complex working conditions and different working conditions, and has high working efficiency.

[0014] 2. The present invention implements the integrated loading operation of the whole components through a multifunctional box, and sets two cavity structures to respectively implement the integrated installation of the flight wing, the flight power element, the telescopic installation of the telescopic terrain telescopic measuring instrument, the controller and the electronic control element, and the propeller power element and other components, which can be used for water, land and air three-purpose measurement. The flight telescopic opening provides an inlet and outlet opening for the rotating shaft that can realize rotation and telescoping. In the open state, the rotating shaft is output to the outside of the flight telescopic opening to implement the operation of the wing. When the flight mode is not adopted, the rotating shaft is input to the outside of the flight telescopic opening to implement the wing contraction. The telescopic terrain telescopic measuring instrument cooperates with the position adjustment operation in different modes to realize the laser emission, reception and corresponding transmission and operation in different measurement modes. The networking module can timely transmit the data through the controller. At the same time, the remote control end can implement the control operation on each power element through the controller, and control the four linkage gears through a telescopic active gear to control the mode of two groups of linkage gears to realize the opening of the corresponding flight mode. The setting of the buoyancy block provides support for water travel, and the propeller and rudder blade are used to implement direction control.

[0015] 3. The retractable terrain telescopic measuring instrument of the present invention is a telescopic structure, which can use an electric push rod to implement displacement at the front end of the telescopic limit box, and implement the moving operation above the isolation plate at the notch position through displacement. It is used to cooperate with the barrier-free measurement operation of the multi-functional box in the process of setting it in different directions such as horizontal, vertical or oblique. Different from the traditional fixed or rotating measurement method, the retractable terrain telescopic measuring instrument of this product can cooperate with the needs of different modes and different working conditions during use to achieve efficient measurement operations.

[0016] 4. The present invention is provided with a detachable shoulder strap. During the process of flying measurement, surface measurement and vehicle-mounted measurement, the shoulder strap is not installed. During the process of manual carrying and short-distance transfer, the shoulder strap can be used for carrying and the measurement can also be carried out, meeting the measurement needs of some operations that cannot fly, cannot travel on the water or cannot be carried out by vehicle.

[0017] 5. The setting of the counterweight block can provide guarantee for the draft operation of the propulsion chamber during the surface operation, and cooperate with the independent first cavity and the second cavity to ensure the buoyancy during the surface operation. The telescopic containing box adopts a cavity structure independent of the first cavity, which is suitable for waterproof protection of internal components under different working conditions. The product has a wide range of uses, high working and operating efficiency, high degree of intelligence, and diverse functions. It can be used under different and special working conditions, is easy to carry and reprint, and has high measurement efficiency. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] Figure 1 It is a schematic diagram of the main structure of the spatial planning topographic surveying device of the present invention.

[0019] Figure 2 It is a rear view structural schematic diagram of the spatial planning topographic measurement device of the present invention.

[0020] Figure 3 This is one of the internal structure schematic diagrams of the spatial planning topographic measurement device of the present invention.

[0021] Figure 4 This is the second schematic diagram of the internal structure of the spatial planning topographic surveying device of the present invention.

[0022] Figure 5 This is the third schematic diagram of the internal structure of the spatial planning topographic surveying device of the present invention.

[0023] Figure 6 This is the fourth schematic diagram of the internal structure of the spatial planning topographic surveying device of the present invention.

[0024] Figure 7 This is one of the schematic diagrams of the use status structure of the spatial planning topographic surveying device of the present invention.

[0025] Figure 8 This is the second schematic diagram of the structure of the spatial planning topographic surveying device of the present invention in use state. DETAILED DESCRIPTION

[0026] 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.

[0027] In the following description of the invention, it should be noted that the terms "upper", "lower", "left", "right", "inner", "outer", etc., indicating directions or positional relationships, are based on directions or positional relationships shown in the drawings, and are only for the convenience of describing the invention and simplifying the description, and do not indicate or imply that the devices or elements referred to must have a specific direction or be constructed and operated in a specific direction. The term "connection" only indicates the connection between devices and has no special meaning.

[0028] Example 1: Figure 1-6 As shown, this embodiment is a land-carrying measurement mode.

[0029] A spatial planning topographic measurement device comprises a multifunctional box 1, wherein the multifunctional box 1 is provided with an independent first cavity 37 and a second cavity 38, a side wall of the multifunctional box 1 is provided with a flight telescopic opening 12, a rotating shaft 16 is installed in the first cavity 37 inside the flight telescopic opening 12, a wing motor 18 is installed at the end of the rotating shaft 16, an output end of the wing motor 18 is connected to a wing 19, a notch 3 is provided at the front side of the multifunctional box 1, a telescopic topographic telescopic measurement instrument 2 is installed in the notch 3, and a controller 2 with a networking module is installed in the second cavity 38 3. A telescopic driving motor 27 is arranged on one side of the controller 23. The output end of the telescopic driving motor 27 is connected to the telescopic driving gear 28 installed in the first cavity 37. The telescopic driving gear 28 cooperates with the rotating shaft 16 through the linkage gear 29. A counterweight block 24 and a direction control motor 25 are installed on the rear side of the second cavity 38. A buoyancy block 4 is arranged at the bottom of the multifunctional box 1. A propulsion chamber 30 is opened at the rear end of the buoyancy block 4. A propeller 32 is installed in the propulsion chamber 30. A rudder blade 33 connected to the output end of the direction control motor 25 is arranged on the outside of the propeller 32. The buoyancy block 4 is a block structure or a cavity structure made of buoyancy material. A first connecting buckle 35 and a second connecting buckle 36 are fixedly installed on the bottom surface of the buoyancy block 4. A shoulder strap clamping block 5 is clamped on the first connecting buckle 35, and a shoulder strap adjustment seat 8 is clamped on the second connecting buckle 36. The shoulder strap adjustment seat 8 is connected to the shoulder strap clamping block 5 through an adjusting ring 9 and a shoulder strap 7. A handle 6 is provided on the outer side of the shoulder strap clamping block 5.

[0030] During the operation of this embodiment, when used in the vehicle-mounted measurement mode, the strap clamp block 5, the handle 6, the strap 7 and the adjustment ring 9 may not be installed. The product can be fixedly installed on the top of the vehicle, and the multifunctional box is placed horizontally or vertically.

[0031] Specifically, an isolation plate 11 is provided between the first cavity 37 and the second cavity 38, a telescopic housing box 13 independent of the first cavity 37 is provided at the inner edge of the flight telescopic opening 12, a rotating shaft 16 is provided in the telescopic housing box 13, a wing shield 17 is fixedly installed on the top of the outer end of the rotating shaft 16, a wing motor 18 is provided at the center of the wing shield 17, a telescopic limit box 14 is fixedly installed on the bottom wall of the telescopic housing box 13, an electric push rod 15 is installed in the telescopic limit box 14, and the output end of the electric push rod 15 is connected to the telescopic terrain telescopic measuring instrument 2 through the telescopic rod 10. A rechargeable battery assembly 22 is installed in the second cavity 38, a bottom sealing plate 21 is provided at the bottom of the second cavity 38, and a limit bracket 26 is fixedly installed on the bottom sealing plate 21 outside the telescopic drive motor 27. The propulsion chamber 30 is arranged below the counterweight block 24, and a propeller motor 31 is embedded at the rear end of the buoyancy block 4. The output end of the propeller motor 31 is connected to the propeller 32, and the output end of the direction control motor 25 faces the propulsion chamber 30. The rudder blade 33 is connected to the output of the direction control motor 25 through a rotating connecting shaft block 34, and the outer edge of the rudder blade 33 is arranged on the inner side of the inner edge of the propulsion chamber 30.

[0032] Specifically, the isolation plate 11 is arranged below the telescopic accommodating box 13, a support block is arranged between the telescopic accommodating box 13 and the isolation plate 11, a through hole for the output shaft of the telescopic drive motor 27 is provided on the isolation plate 11, a rotating support shaft is fixedly installed at the central axis position of the linkage gear 29, the upper part of the rotating support shaft is supported by the bottom wall of the telescopic accommodating box 13, a first bearing supporting the upper part of the rotating support shaft is installed on the bottom wall of the telescopic accommodating box 13, the lower part of the rotating support shaft is supported by the top wall of the isolation plate 11, and a second bearing supporting the lower part of the rotating support shaft is installed on the top wall of the isolation plate 11. The bottom wall of the telescopic accommodating box 13 is provided with a limited rotation ring 20, and the bottom of the rotating shaft 16 is connected to the top of the linkage gear 29 through the limited rotation ring 20.

[0033] A method for measuring terrain using a space planning terrain measuring device, during measurement, a multifunctional box 1 is placed on top of a moving vehicle, and a retractable terrain telescopic measuring instrument 2 is opened to perform laser measurement during vehicle travel, or a shoulder strap clamping block 5 is installed on a first connecting buckle 35, a shoulder strap adjustment seat 8 is installed on a second connecting buckle 36, and an adjustment ring 9 and a shoulder strap 7 are installed, and the multifunctional box 1 is carried on a human body via the shoulder strap 7, and the retractable terrain telescopic measuring instrument 2 is opened via a controller 23, and laser terrain measurement is performed via the retractable terrain telescopic measuring instrument 2 during coating and walking.

[0034] Example 2: Figure 1-7 As shown, this embodiment is an aerial flight measurement mode.

[0035] A spatial planning topographic measurement device comprises a multifunctional box 1, wherein the multifunctional box 1 is provided with an independent first cavity 37 and a second cavity 38, a side wall of the multifunctional box 1 is provided with a flight telescopic opening 12, a rotating shaft 16 is installed in the first cavity 37 inside the flight telescopic opening 12, a wing motor 18 is installed at the end of the rotating shaft 16, an output end of the wing motor 18 is connected to a wing 19, a notch 3 is provided at the front side of the multifunctional box 1, a telescopic topographic telescopic measurement instrument 2 is installed in the notch 3, and a controller 2 with a networking module is installed in the second cavity 38 3. A telescopic drive motor 27 is provided on one side of the controller 23. The output end of the telescopic drive motor 27 is connected to the telescopic driving gear 28 installed in the first cavity 37. The telescopic driving gear 28 cooperates with the rotating shaft 16 through the linkage gear 29. A counterweight block 24 and a direction control motor 25 are installed on the rear side of the second cavity 38. A buoyancy block 4 is provided at the bottom of the multifunctional box 1. A propulsion chamber 30 is provided at the rear end of the buoyancy block 4. A propeller 32 is installed in the propulsion chamber 30. A rudder blade 33 connected to the output end of the direction control motor 25 is provided on the outside of the propeller 32. The buoyancy block 4 is a block structure or a cavity structure made of buoyancy material. A first connecting buckle 35 and a second connecting buckle 36 are fixedly installed on the bottom surface of the buoyancy block 4.

[0036] During the operation of this embodiment, the shoulder strap clamping block 5, the handle 6, the shoulder strap 7 and the adjustment ring 9 are not installed.

[0037] Specifically, an isolation plate 11 is provided between the first cavity 37 and the second cavity 38, a telescopic housing box 13 independent of the first cavity 37 is provided at the inner edge of the flight telescopic opening 12, a rotating shaft 16 is provided in the telescopic housing box 13, a wing shield 17 is fixedly installed on the top of the outer end of the rotating shaft 16, a wing motor 18 is provided at the center of the wing shield 17, a telescopic limit box 14 is fixedly installed on the bottom wall of the telescopic housing box 13, an electric push rod 15 is installed in the telescopic limit box 14, and the output end of the electric push rod 15 is connected to the telescopic terrain telescopic measuring instrument 2 through the telescopic rod 10. A rechargeable battery assembly 22 is installed in the second cavity 38, a bottom sealing plate 21 is provided at the bottom of the second cavity 38, and a limit bracket 26 is fixedly installed on the bottom sealing plate 21 outside the telescopic drive motor 27. The propulsion chamber 30 is arranged below the counterweight block 24, and a propeller motor 31 is embedded at the rear end of the buoyancy block 4. The output end of the propeller motor 31 is connected to the propeller 32, and the output end of the direction control motor 25 faces the propulsion chamber 30. The rudder blade 33 is connected to the output of the direction control motor 25 through a rotating connecting shaft block 34, and the outer edge of the rudder blade 33 is arranged on the inner side of the inner edge of the propulsion chamber 30.

[0038] Specifically, the isolation plate 11 is arranged below the telescopic accommodating box 13, a support block is arranged between the telescopic accommodating box 13 and the isolation plate 11, a through hole for the output shaft of the telescopic drive motor 27 is provided on the isolation plate 11, a rotating support shaft is fixedly installed at the central axis position of the linkage gear 29, the upper part of the rotating support shaft is supported by the bottom wall of the telescopic accommodating box 13, a first bearing supporting the upper part of the rotating support shaft is installed on the bottom wall of the telescopic accommodating box 13, the lower part of the rotating support shaft is supported by the top wall of the isolation plate 11, and a second bearing supporting the lower part of the rotating support shaft is installed on the top wall of the isolation plate 11. The bottom wall of the telescopic accommodating box 13 is provided with a limited rotation ring 20, and the bottom of the rotating shaft 16 is connected to the top of the linkage gear 29 through the limited rotation ring 20.

[0039] A method for measuring terrain using a space planning terrain measuring device, during measurement, a multifunctional box 1 is horizontally placed in an open space, a telescopic driving motor 27 is turned on by a remote control tablet, the telescopic driving motor 27 drives a telescopic active gear 28 to rotate, the telescopic active gear 28 drives a linkage gear 29 to rotate, the linkage gear 29 drives a rotating shaft 16 to rotate, four wings 19 extend from a flight telescopic opening 12 in pairs, the wing motor 18 is turned on to drive the wings 19 to rotate, the multifunctional box 1 is slowly lifted off, a telescopic terrain telescopic measuring instrument 2 is turned on by a controller 23, and laser measurement operations are performed by the telescopic terrain telescopic measuring instrument 2 during flight.

[0040] Example 3: Figure 1-8 As shown, this embodiment is a water surface traveling measurement mode.

[0041] A spatial planning topographic measurement device comprises a multifunctional box 1, wherein the multifunctional box 1 is provided with an independent first cavity 37 and a second cavity 38, a side wall of the multifunctional box 1 is provided with a flight telescopic opening 12, a rotating shaft 16 is installed in the first cavity 37 inside the flight telescopic opening 12, a wing motor 18 is installed at the end of the rotating shaft 16, an output end of the wing motor 18 is connected to a wing 19, a notch 3 is provided at the front side of the multifunctional box 1, a telescopic topographic telescopic measurement instrument 2 is installed in the notch 3, and a controller 2 with a networking module is installed in the second cavity 38 3. A telescopic driving motor 27 is arranged on one side of the controller 23. The output end of the telescopic driving motor 27 is connected to the telescopic driving gear 28 installed in the first cavity 37. The telescopic driving gear 28 cooperates with the rotating shaft 16 through the linkage gear 29. A counterweight block 24 and a direction control motor 25 are installed on the rear side of the second cavity 38. A buoyancy block 4 is arranged at the bottom of the multifunctional box 1. A propulsion chamber 30 is opened at the rear end of the buoyancy block 4. A propeller 32 is installed in the propulsion chamber 30. A rudder blade 33 connected to the output end of the direction control motor 25 is arranged on the outside of the propeller 32.

[0042] During the operation of this embodiment, the shoulder strap clamping block 5, the handle 6, the shoulder strap 7 and the adjustment ring 9 are not installed.

[0043] Specifically, the buoyancy block 4 is a block structure or a cavity structure made of buoyancy material, and a first connecting buckle 35 and a second connecting buckle 36 are fixedly installed on the bottom surface of the buoyancy block 4. A shoulder strap clamping block 5 is clamped on the first connecting buckle 35, and a shoulder strap adjustment seat 8 is clamped on the second connecting buckle 36. The shoulder strap adjustment seat 8 is connected to the shoulder strap clamping block 5 through an adjusting ring 9 and a shoulder strap 7, and a handle 6 is provided on the outer side of the shoulder strap clamping block 5. An isolation plate 11 is provided between the first cavity 37 and the second cavity 38, a telescopic housing box 13 independent of the first cavity 37 is provided at the inner edge of the flight telescopic opening 12, a rotating shaft 16 is provided in the telescopic housing box 13, a wing shield 17 is fixedly installed on the top of the outer end of the rotating shaft 16, a wing motor 18 is provided at the center of the wing shield 17, a telescopic limit box 14 is fixedly installed on the bottom wall of the telescopic housing box 13, an electric push rod 15 is installed in the telescopic limit box 14, and the output end of the electric push rod 15 is connected to the telescopic terrain telescopic measuring instrument 2 through the telescopic rod 10. A rechargeable battery assembly 22 is installed in the second cavity 38, a bottom sealing plate 21 is provided at the bottom of the second cavity 38, and a limit bracket 26 is fixedly installed on the bottom sealing plate 21 outside the telescopic drive motor 27. The propulsion chamber 30 is arranged below the counterweight block 24, and a propeller motor 31 is embedded at the rear end of the buoyancy block 4. The output end of the propeller motor 31 is connected to the propeller 32, and the output end of the direction control motor 25 faces the propulsion chamber 30. The rudder blade 33 is connected to the output of the direction control motor 25 through a rotating connecting shaft block 34, and the outer edge of the rudder blade 33 is arranged on the inner side of the inner edge of the propulsion chamber 30.

[0044] Specifically, the isolation plate 11 is arranged below the telescopic accommodating box 13, a support block is arranged between the telescopic accommodating box 13 and the isolation plate 11, a through hole for the output shaft of the telescopic drive motor 27 is provided on the isolation plate 11, a rotating support shaft is fixedly installed at the central axis position of the linkage gear 29, the upper part of the rotating support shaft is supported by the bottom wall of the telescopic accommodating box 13, a first bearing supporting the upper part of the rotating support shaft is installed on the bottom wall of the telescopic accommodating box 13, the lower part of the rotating support shaft is supported by the top wall of the isolation plate 11, and a second bearing supporting the lower part of the rotating support shaft is installed on the top wall of the isolation plate 11. The bottom wall of the telescopic accommodating box 13 is provided with a limited rotation ring 20, and the bottom of the rotating shaft 16 is connected to the top of the linkage gear 29 through the limited rotation ring 20.

[0045] A method for measuring terrain using a spatial planning terrain measuring device, during measurement, a multifunctional box 1 is placed on the water surface, a power end of a propeller 32 is turned on by a remote control tablet to drive the propeller 32 to rotate, water is poured into a propulsion chamber 30 under the action of a counterweight 24, the propeller 32 rotates in the water and then propels the multifunctional box 1 to travel on the water surface, during which the rotation angle of a rudder blade 33 is controlled by turning on a direction control motor 25 to achieve direction control of travel on the water surface, a retractable terrain telescopic measuring instrument 2 is turned on by a controller 23, and laser measurement operations are performed by the retractable terrain telescopic measuring instrument 2 during travel on the water surface.

[0046] During the operation of the above embodiment, the controller 23 is connected to the remote control tablet through the networking module to implement data transmission operations, and the measurement data is transmitted to the remote control tablet in real time for calculation. At the same time, the remote control tablet can issue control commands to the controller 23 through the networking module.

[0047] The above is only a preferred embodiment of the present invention, and does not limit the present invention in other forms. Any technician familiar with the profession may use the above disclosed technical content to change or modify it into an equivalent embodiment with equivalent changes. However, any simple modification, equivalent change and modification made to the above embodiment according to the technical essence of the present invention without departing from the technical solution of the present invention still belongs to the protection scope of the technical solution of the present invention.

Claims

1. A spatial planning topographic survey device, comprising a multifunctional housing (1), characterized in that: The multifunctional box (1) is provided with an independent first cavity (37) and a second cavity (38). The side wall of the multifunctional box (1) is provided with a flight telescopic opening (12). A rotating shaft (16) is installed in the first cavity (37) inside the flight telescopic opening (12). A wing motor (18) is installed at the end of the rotating shaft (16). The output end of the wing motor (18) is connected to the wing (19). A notch (3) is provided on the front side of the multifunctional box (1). A telescopic terrain telescopic measuring instrument (2) is installed in the notch (3). A controller (23) with a networking module is installed in the second cavity (38). One side of the controller (23) is provided with A telescopic drive motor (27) is provided, the output end of the telescopic drive motor (27) is connected to a telescopic driving gear (28) installed in a first cavity (37), the telescopic driving gear (28) cooperates with a rotating shaft (16) through a linkage gear (29), a counterweight block (24) and a direction control motor (25) are installed on the rear side of the second cavity (38), a buoyancy block (4) is provided at the bottom of the multifunctional box (1), a propulsion chamber (30) is provided at the rear end of the buoyancy block (4), a propeller (32) is installed in the propulsion chamber (30), and a rudder blade (33) connected to the output end of the direction control motor (25) is provided on the outer side of the propeller (32).

2. The spatial planning topographic surveying device according to claim 1, characterized in that: The buoyancy block (4) is a block structure or a cavity structure made of a buoyancy material. A first connecting buckle (35) and a second connecting buckle (36) are fixedly mounted on the bottom surface of the buoyancy block (4). A shoulder strap clamping block (5) is clamped on the first connecting buckle (35), and a shoulder strap adjustment seat (8) is clamped on the second connecting buckle (36). The shoulder strap adjustment seat (8) is connected to the shoulder strap clamping block (5) via an adjustment ring (9) and a shoulder strap (7). A handle (6) is arranged on the outer side of the shoulder strap clamping block (5).

3. The spatial planning topographic surveying device according to claim 1, characterized in that: An isolation plate (11) is provided between the first cavity (37) and the second cavity (38); a telescopic accommodating box (13) independent of the first cavity (37) is provided at the inner edge of the flight telescopic opening (12); a rotating shaft (16) is provided in the telescopic box (13); a wing protective cover (17) is fixedly installed on the top of the outer end of the rotating shaft (16); a wing motor (18) is provided at the center of the wing protective cover (17); a telescopic limit box (14) is fixedly installed on the bottom wall of the telescopic accommodating box (13); an electric push rod (15) is installed in the telescopic limit box (14); and an output end of the electric push rod (15) is connected to the telescopic terrain telescopic measuring instrument (2) through a telescopic rod (10).

4. The spatial planning topographic surveying device according to claim 1, characterized in that: A rechargeable battery assembly (22) is installed in the second cavity (38), a bottom sealing plate (21) is provided at the bottom of the second cavity (38), and a limit bracket (26) is fixedly installed on the bottom sealing plate (21) outside the telescopic drive motor (27).

5. The spatial planning topographic surveying device according to claim 1, characterized in that: The propulsion chamber (30) is arranged below the counterweight block (24), a propeller motor (31) is embedded at the rear end of the buoyancy block (4), the output end of the propeller motor (31) is connected to the propeller (32), the output end of the direction control motor (25) faces the propulsion chamber (30), the rudder blade (33) is connected to the output of the direction control motor (25) via a rotating connection shaft block (34), and the outer edge of the rudder blade (33) is arranged inside the inner edge of the propulsion chamber (30).

6. The spatial planning topographic surveying device according to claim 3, characterized in that: The isolation plate (11) is arranged below the telescopic accommodating box (13), a support block is arranged between the telescopic accommodating box (13) and the isolation plate (11), a through hole for receiving the output shaft of the telescopic drive motor (27) is opened on the isolation plate (11), a rotating support shaft is fixedly installed at the center axis position of the linkage gear (29), the upper part of the rotating support shaft is supported by the bottom wall of the telescopic accommodating box (13), a first bearing supporting the upper part of the rotating support shaft is installed on the bottom wall of the telescopic accommodating box (13), the lower part of the rotating support shaft is supported by the top wall of the isolation plate (11), and a second bearing supporting the lower part of the rotating support shaft is installed on the top wall of the isolation plate (11).

7. The spatial planning topographic surveying device according to claim 3, characterized in that: The bottom wall of the telescopic accommodating box (13) is provided with a limit rotation ring (20), and the bottom of the rotating shaft (16) is connected to the top of the linkage gear (29) via the limit rotation ring (20).

8. A method for measuring terrain using a spatial planning terrain measuring device, characterized in that: The method is divided into three modes: Aerial flight measurement mode: during measurement, the multifunctional box (1) is horizontally placed on an open ground, and the telescopic drive motor (27) is turned on through a remote control tablet. The telescopic drive motor (27) drives the telescopic active gear (28) to rotate, and the telescopic active gear (28) drives the linkage gear (29) to rotate. The linkage gear (29) drives the rotation shaft (16) to rotate, and the four wings (19) extend from the flight telescopic opening (12) in pairs. The wing motor (18) is turned on to drive the wings (19) to rotate, and the multifunctional box (1) is slowly lifted off. The telescopic topographic telescopic measuring instrument (2) is turned on through a controller (23), and laser measurement is performed through the telescopic topographic telescopic measuring instrument (2) during the flight. Water surface travel measurement mode: during measurement, the multifunctional housing (1) is placed on the water surface, the power end of the propeller (32) is turned on by a remote control tablet to drive the propeller (32) to rotate, water is poured into the propulsion chamber (30) under the action of the counterweight (24), the propeller (32) rotates in the water and then propels the multifunctional housing (1) to travel on the water surface, during which the direction of travel is controlled by turning on the direction control motor (25) to control the rotation angle of the rudder blade (33), thereby realizing the direction control of the travel on the water surface, the retractable terrain telescopic measuring instrument (2) is turned on by the controller (23), and laser measurement is performed by the retractable terrain telescopic measuring instrument (2) during the travel on the water surface; Land-carrying measurement mode: during measurement, the multifunctional box (1) is placed on top of a moving vehicle, and a laser measurement operation is performed by opening the retractable topographic telescopic measuring instrument (2) while the vehicle is moving, or the shoulder strap clamping block (5) is installed on the first connecting buckle (35), the shoulder strap adjustment seat (8) is installed on the second connecting buckle (36), and the adjustment ring (9) and the shoulder strap (7) are installed, and the multifunctional box (1) is carried on the human body via the shoulder strap (7), and the retractable topographic telescopic measuring instrument (2) is opened via the controller (23), and a laser topographic measurement operation is performed via the retractable topographic telescopic measuring instrument (2) during the coating and walking process.

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