CN115230954B - Full-automatic topographic map mapping device and mapping method - Google Patents
Full-automatic topographic map mapping device and mapping method Download PDFInfo
- Publication number
- CN115230954B CN115230954B CN202211059600.6A CN202211059600A CN115230954B CN 115230954 B CN115230954 B CN 115230954B CN 202211059600 A CN202211059600 A CN 202211059600A CN 115230954 B CN115230954 B CN 115230954B
- Authority
- CN
- China
- Prior art keywords
- mapping
- assembly
- clamping
- spherical window
- fuselage
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 238000013507 mapping Methods 0.000 title claims abstract description 92
- 238000000034 method Methods 0.000 title claims abstract description 12
- 238000004140 cleaning Methods 0.000 claims abstract description 31
- 230000007246 mechanism Effects 0.000 claims abstract description 26
- 230000010405 clearance mechanism Effects 0.000 claims abstract description 13
- 238000013016 damping Methods 0.000 claims abstract description 7
- 230000005540 biological transmission Effects 0.000 claims description 36
- 210000000078 claw Anatomy 0.000 claims description 14
- 238000009434 installation Methods 0.000 claims description 3
- 238000002360 preparation method Methods 0.000 claims description 3
- 230000001681 protective effect Effects 0.000 claims description 2
- 230000035939 shock Effects 0.000 claims 2
- 230000008569 process Effects 0.000 abstract description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract description 3
- 230000009286 beneficial effect Effects 0.000 description 5
- 230000000694 effects Effects 0.000 description 4
- 239000012535 impurity Substances 0.000 description 4
- 238000012876 topography Methods 0.000 description 4
- 230000001154 acute effect Effects 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 238000004891 communication Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 230000000630 rising effect Effects 0.000 description 2
- 230000008054 signal transmission Effects 0.000 description 2
- 206010039509 Scab Diseases 0.000 description 1
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 1
- NIXOWILDQLNWCW-UHFFFAOYSA-N acrylic acid group Chemical group C(C=C)(=O)O NIXOWILDQLNWCW-UHFFFAOYSA-N 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- -1 bird droppings Substances 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 210000003608 fece Anatomy 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000003384 imaging method Methods 0.000 description 1
- 230000008595 infiltration Effects 0.000 description 1
- 238000001764 infiltration Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 230000001050 lubricating effect Effects 0.000 description 1
- 239000000741 silica gel Substances 0.000 description 1
- 229910002027 silica gel Inorganic materials 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B08—CLEANING
- B08B—CLEANING IN GENERAL; PREVENTION OF FOULING IN GENERAL
- B08B1/00—Cleaning by methods involving the use of tools
- B08B1/20—Cleaning of moving articles, e.g. of moving webs or of objects on a conveyor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
- Y02A90/00—Technologies having an indirect contribution to adaptation to climate change
- Y02A90/30—Assessment of water resources
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Cleaning In General (AREA)
Abstract
The invention discloses a full-automatic topographic map mapping device, which comprises: fuselage, propeller, wane and mapping assembly; the screw sets up the top of fuselage, the wane passes through damper and sets up the bottom edge of fuselage, survey and drawing subassembly passes through clearance mechanism and sets up the bottom of fuselage. When encountering bad weather in the mapping process and leading to the mapping assembly to be stained and blurred, the cleaning mechanism can be started to clean the mapping assembly so as to meet the mapping conditions, so that the mapping assembly is not required to be repeatedly turned back, the mapping assembly is manually cleaned, the mapping device can continuously conduct mapping work in a harsher environment, when the device is recovered, the falling mapping device is not required to be manually caught, the device can be directly fallen on the ground, the impact on a machine body can be reduced when the device is landed through the damping mechanism, and the rocker can provide a larger contact area so that the device can be forced to fall on the water surface.
Description
Technical Field
The invention relates to the technical field of ground mapping, in particular to a full-automatic topographic map mapping device and a mapping method.
Background
With the development of unmanned aerial vehicles and small aircrafts, the mapping of topography in China is turned to unmanned aerial vehicle scanning mapping at present, the mapping is usually carried by adopting an unmanned aerial vehicle to carry a camera to shoot and scan from high altitude, but once severe weather or special use scenes are met, if the situation that the camera cannot shoot exists in the weather suddenly changed in the mapping process, the situation that the camera cannot shoot is needed to be wetted in the weather suddenly changed in the mapping process, the unmanned aerial vehicle is required to fly back to wipe the camera, and then measurement is continued at a coordinate point marked by the fly back, and in a humid area, the measurement progress on the day is slower due to fog occurring in the time of the flight, and the problem to be solved at present is how to reduce the influence of severe weather on the shooting of the camera. Therefore, there is a need for a fully automated topographic mapping apparatus and method that at least partially addresses the problems of the prior art.
Disclosure of Invention
In the summary, a series of concepts in a simplified form are introduced, which will be further described in detail in the detailed description. The summary of the invention is not intended to define the key features and essential features of the claimed subject matter, nor is it intended to be used as an aid in determining the scope of the claimed subject matter.
To at least partially solve the above problems, the present invention provides a fully automatic topographic mapping apparatus comprising: fuselage, propeller, wane and mapping assembly; the screw sets up the top of fuselage, the wane passes through damper and sets up the bottom edge of fuselage, survey and drawing subassembly passes through clearance mechanism and sets up the bottom of fuselage.
Preferably, the number of the propellers is four, and the propellers are symmetrically arranged at the edge of the top of the machine body in a cross shape.
Preferably, the number of the seesaw is at least two, and the top surface of the seesaw is connected with the bottom surface of the machine body through two damping mechanisms, and the damping mechanisms comprise an outer tube and an inner rod; the top of outer tube with the bottom of fuselage is connected, the top of interior pole is pegged graft in the storage tank of outer tube bottom, and interior pole through first elastic component with the interior top of storage tank is connected, the bottom of interior pole with the top of wane is connected.
Preferably, the surveying and mapping assembly comprises a spherical window, a transmission assembly, a surveying and mapping instrument and a cleaning mechanism, wherein the surveying and mapping instrument is arranged in the spherical window through a horizontal device, the horizontal device is used for maintaining stability of the surveying and mapping instrument when the spherical window rotates, the cleaning mechanism is arranged at the bottom of the machine body, the spherical window and the transmission assembly are both arranged on the cleaning mechanism, the transmission assembly is connected with the top of the spherical window, and the transmission assembly is used for driving the spherical window to rotate.
Preferably, the cleaning mechanism comprises an annular clamping plate, a mounting plate, a limiting claw and an auxiliary wheel; the top surface of annular cardboard is provided with the mounting bracket, the mounting bracket pass through the installation pole with the fuselage is connected, be provided with the cleaning appliance on the inner ring lateral wall of annular cardboard, spherical window overlap joint is in on the inner ring of annular cardboard, the cleaning appliance with the outer wall butt of spherical window, the mounting panel is located the top of spherical window, and the top of mounting panel pass through the connecting rod with the fuselage is connected, the bottom of mounting panel is provided with at least three spacing claw, the inner wall of spacing claw with the outer wall sliding connection of spherical window, the bottom of spacing claw is provided with the auxiliary wheel, the auxiliary wheel with the outer wall butt of spherical window, drive assembly sets up on the mounting panel.
Preferably, the transmission assembly comprises at least three transmission wheels, a driving motor is arranged on each transmission wheel, each transmission wheel is connected with the mounting plate through a connecting plate, and each transmission wheel is abutted to the corresponding spherical window.
Preferably, the bottom surface of annular cardboard is provided with at least emergent protection subassembly, and emergent protection subassembly is the annular and encircles the spherical window outside, emergent protection subassembly to spherical window slope setting, and with have inclination between the annular cardboard.
Preferably, the emergency protection component comprises a containing box, a shifting block, an ejection column, a first clamping piece, a second clamping piece and an ejection component; the ejector column is arranged in the accommodating box, a sliding groove is formed in the ejector column, one end of the ejector column is conical, a clamping groove is formed in the other end of the ejector column, a clamping table is arranged on the side wall of the ejector column, the first clamping piece and the second clamping piece are arranged in the accommodating box through connecting shafts, the first clamping piece and the second clamping piece are connected with the side wall of the accommodating box through springs, the first clamping piece and the second clamping piece are both used for being clamped with the clamping table, the bottom of the ejector assembly is connected with the ejector column through the sliding groove and the clamping groove, and the top of the ejector assembly is clamped with the shifting block which is in sliding connection with the side wall of the accommodating box.
Preferably, the ejection assembly comprises a first slider and a second slider, the first slider is connected with the second slider through a second elastic piece, the bottom surface of the first slider is connected with the sliding groove through a clamping table, the bottom surface of the second slider is connected with the clamping groove through a clamping table, the bottom surface of the shifting block is provided with clamping protrusions, the first slider and the second slider are respectively located at two ends of the clamping protrusions, the side wall of the shifting block is provided with a sliding groove and a sliding plate, the first clamping piece and the second clamping piece are both located in the sliding groove, the shifting block is connected with the side wall of the containing box in a sliding mode through the sliding plate, and the sliding groove is located below the sliding plate.
A mapping method of a fully automatic topographic mapping apparatus, the steps comprising:
s1: placing the mapping assembly at a lifting point, and starting the mapping assembly through a remote controller;
s2: the emergency protection assembly is retracted to a standby state, the transmission assembly drives the spherical window to rotate, and primary cleaning is carried out on the cleaning mechanism;
s3: preheating a propeller and a surveying instrument, and detecting a video state;
s4: and after preparation, controlling the surveying and mapping assembly to lift off to survey and map through a remote controller.
Compared with the prior art, the invention at least comprises the following beneficial effects:
when surveying and mapping is carried out, at first, let propeller and survey and drawing subassembly preheat through the remote controller, survey and drawing subassembly can clean in order to make full use of preheating through clearance mechanism when preheating, then adjust the rotational speed of propeller through the remote controller in order to reach the purpose of rising this device, after survey and drawing device rises, can receive the image signal of survey and drawing subassembly transmission on remote controller or terminal in order to conveniently control this device, can control survey and drawing subassembly through the remote controller, clearance mechanism and propeller, after reaching appointed survey and drawing point, survey and drawing through survey and drawing subassembly, and transmit image message to remote controller or terminal, and backup up in survey and drawing subassembly is local, backup program sets up to reset after turning on again at every time, in order to save storage space, when survey and drawing subassembly is dirty and blurred in the course of working, can start clearance mechanism and clean survey and drawing subassembly, thereby do not need the survey and drawing device to turn back, and manually clean survey and drawing subassembly, and drawing device can survey and draw by force in succession in the more abominable environment, when this device can be landed on the surface of water directly, can be reduced by landing device when landing on the plane, can be reduced by landing device, can be greatly landed on the surface of the plane by the landing device.
Additional advantages, objects, and features of the invention will be set forth in part in the description which follows and in part will become apparent to those having ordinary skill in the art upon examination of the following or may be learned from practice of the invention.
Drawings
The accompanying drawings are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate the invention and together with the embodiments of the invention, serve to explain the invention. In the drawings:
fig. 1 is a cross-sectional view of a front view of a fully automatic topographic mapping apparatus (emergency protective assembly in an open state) according to the present invention.
Fig. 2 is a cross-sectional view of a left side view of the fully automatic topographic mapping apparatus (emergency guard assembly in a armed state) according to the present invention.
Fig. 3 is a schematic structural view of a cleaning mechanism in the fully automatic topographic mapping apparatus according to the present invention.
Fig. 4 is a schematic structural view of a circular clamping plate in the full-automatic topographic mapping device.
Fig. 5 is a schematic structural view of a transmission assembly in the fully automatic topographic mapping apparatus according to the present invention.
Fig. 6 is a top view of fig. 5.
Fig. 7 is a schematic diagram of an internal structure of an emergency protection component in the fully automatic topographic mapping device according to the present invention.
Fig. 8 is a schematic view of the structure of the accommodating case of fig. 7.
Fig. 9 is a schematic view of the ejection column of fig. 7.
Fig. 10 is a schematic view of the location of the ejection column of fig. 7 within the receiving pocket.
Fig. 11 is a bottom schematic view of the ejection assembly of fig. 7.
Fig. 12 is a schematic view of the ejector assembly of fig. 7 about to move the ejector post.
Fig. 13 is a schematic view of the bottom of the dial in fig. 7.
FIG. 14 is a schematic view of the second clamping member and the shifting block before (A) and after (B) opening the emergency protection module.
FIG. 15 is a schematic view of the first clamping member and the dial block before (A) and after (B) opening the emergency protection assembly.
In the figure: 1 fuselage, 2 screw, 3 wanes, 4 mapping device, 41 spherical window, 5 damper, 51 outer tube, 52 inner rod, 53 first elastic component, 6 clearance mechanism, 61 annular cardboard, 611 cleaning tool, 62 mounting panel, 63 spacing claw, 64 auxiliary wheel, 65 mounting bracket, 7 drive assembly, 71 drive wheel, 72 driving motor, 73 connecting plate, 8 emergency protection assembly, 81 holding box, 82 shifting block, 821 joint protruding, 822 sliding groove, 823 sliding plate, 83 catapulting post, 831 spout, 832 draw-in groove, 833 clamping table, 84 first clamping piece, 85 second clamping piece, 86 first slider, 87 second slider, 88 second elastic component.
Detailed Description
The present invention is described in further detail below with reference to the drawings and examples to enable those skilled in the art to practice the invention by referring to the description.
It will be understood that terms, such as "having," "including," and "comprising," as used herein, do not preclude the presence or addition of one or more other elements or groups thereof.
As shown in fig. 1-15, the present invention provides a fully automatic topographic mapping apparatus comprising: the device comprises a body 1, a propeller 2, a rocker 3 and a mapping assembly 4; the screw 2 sets up the top of fuselage 1, wane 3 sets up through damper 5 the bottom edge of fuselage 1, mapping assembly 4 sets up through clearance mechanism 6 the bottom of fuselage 1.
The technical scheme has the working principle and beneficial effects that: when surveying and mapping is carried out, at first, start this device through the remote controller, let screw 2 and surveying and mapping subassembly 4 preheat, survey and mapping subassembly 4 can clean in order to make full use of preheating through clearance mechanism 6 when preheating, then adjust the rotational speed of screw 2 through the remote controller in order to reach the purpose of rising this device, after the surveying and mapping device rises, can receive the image signal of surveying and mapping subassembly 4 transmission on the remote controller or terminal so as to conveniently control this device, can control surveying and mapping subassembly 4 through the remote controller, clearance mechanism 6 and screw 2, reach the appointed point after, survey and mapping subassembly 4 carries out topography survey and drawing, and with image message to remote controller or terminal transmission, and carry out the backup locally at surveying and mapping subassembly 4, backup program sets up to reset after turning off again at every time, in order to save storage space, when meetting bad weather and leading to surveying and mapping subassembly 4 to be made dirty and blur, can start clearance mechanism 6 and clean surveying and mapping subassembly 4, thereby it is clean to do not need surveying and mapping device reciprocal turn back, can carry out the manual to surveying and mapping subassembly 4, and then can carry out topography survey and mapping device 4, can be carried out topography survey and mapping device in the more severe environment, can be carried out landing can be reduced in the landing device when the landing can be used for the landing device is greatly in the landing device is required to be 1, can be reduced when landing device is landed on the surface of land is 1, can be used for the landing device is directly land on the surface is 1.
In one embodiment, the number of the propellers 2 is four, and the propellers are symmetrically arranged at the edge of the top of the body 1 in a cross shape. At least two rocker plates 3 are arranged, the top surface of each rocker plate 3 is connected with the bottom surface of the machine body 1 through two damping mechanisms 5, and each damping mechanism 5 comprises an outer tube 51 and an inner rod 52; the top of the outer tube 51 is connected with the bottom of the body 1, the top of the inner rod 52 is inserted into a containing groove at the bottom of the outer tube 51, the inner rod 52 is connected with the inner top of the containing groove through a first elastic piece 53, and the bottom of the inner rod 52 is connected with the top of the rocker 3. The surveying and mapping assembly 4 comprises a spherical window 41, a transmission assembly 7, a surveying and mapping instrument and a cleaning mechanism 6, wherein the surveying and mapping instrument is arranged in the spherical window 41 through horizontal equipment, the horizontal equipment is used for maintaining stability of the surveying and mapping instrument when the spherical window 41 rotates, the cleaning mechanism 6 is arranged at the bottom of the machine body 1, the spherical window 41 and the transmission assembly 7 are both arranged on the cleaning mechanism 6, the transmission assembly 7 is connected with the top of the spherical window 41, and the transmission assembly 7 is used for driving the spherical window 41 to rotate.
The technical scheme has the working principle and beneficial effects that: the spherical window 41 can be made of glass materials or acrylic materials, a horizontal device is arranged in the spherical window 41, the horizontal device can be a gyroscope-like device, the horizontal device can be used as the horizontal device only by ensuring that the spherical window 41 can not rotate along with the rotation when the spherical window 41 rotates, a surveying instrument is carried on the horizontal device, the surveying instrument comprises special equipment for imaging, surveying, storing, signal transmission, batteries and the like, the surveying instrument is arranged on the horizontal device and can realize the 360-degree rotation effect of a range monitoring camera, the top of the spherical window 41 is provided with a transmission component 7 for enabling the spherical window 41 to rotate, a cleaning mechanism 6 can clean water drops, mud and other impurities affecting surveying and mapping on the spherical window 41, the clear mode of activity, on the contrary, through the spherical window 41 of activity, fixed clean mechanism 6, realize the clean work in surface of spherical window 41, because the super-large survey and drawing angle that surveying instrument itself possesses, the cooperation makes it keep stable horizontal equipment in spherical window 41, when not influencing the survey and drawing, can realize the isolation of surveying instrument and external environment, reduce infiltration, the probability that circumstances such as leaking appear, rotatable spherical window 41 can provide bigger change area than traditional fixed window, when clean mechanism 6 can not be erased impurity appears in a place (like bird's excrement), traditional fixed window survey and drawing then can be influenced by impurity, must fly back through manual cleaning, and the spherical window 41 of activity can rotate the position that can not clean to not influence the survey and drawing, thereby do not influence the survey and drawing progress.
In one embodiment, the cleaning mechanism 6 includes an annular clamping plate 61, a mounting plate 62, a limit pawl 63, and an auxiliary wheel 64; the top surface of annular cardboard 61 is provided with mounting bracket 65, mounting bracket 65 pass through the installation pole with fuselage 1 is connected, be provided with cleaning apparatus 611 on the inner ring lateral wall of annular cardboard 61, spherical window 41 overlap joint is in on the inner ring of annular cardboard 61, cleaning apparatus 611 with the outer wall butt of spherical window 41, mounting panel 62 is located the top of spherical window 41, and the top of mounting panel 62 pass through the connecting rod with fuselage 1 is connected, the bottom of mounting panel 62 is provided with at least three spacing claw 63, the inner wall of spacing claw 63 with the outer wall sliding connection of spherical window 41, the bottom of spacing claw 63 is provided with auxiliary wheel 64, auxiliary wheel 64 with the outer wall butt of spherical window 41, drive assembly 7 sets up on the mounting panel 62. The transmission assembly 7 comprises at least three transmission wheels 71, a driving motor 72 is arranged on the transmission wheels 71, the transmission wheels 71 are connected with the mounting plate 62 through a connecting plate 73, and the transmission wheels 71 are abutted with the spherical window 41.
The technical scheme has the working principle and beneficial effects that: the lower half part of the spherical window 41 is lapped on the inner ring of the annular clamping plate 61, when the spherical window 41 rotates, the cleaning tool 611 on the inner ring of the annular clamping plate 61 can wipe the surface of the spherical window 41, so that the aim of cleaning the spherical window 41 is fulfilled, the inner side wall of the annular clamping plate 61 is clamped between the bottom and the lower hemisphere of the spherical window 41 and is as close to the equatorial line of the spherical window 41 as possible, so that a mapping instrument is provided with a view field as large as possible, meanwhile, an auxiliary wheel 64 is positioned on the lower hemisphere of the spherical window 41, the spherical window 41 can be effectively prevented from falling off, the support can be provided for the spherical window 41 through the auxiliary wheel 41, the weight of the spherical window 41 is prevented from being fully concentrated on the inner ring of the annular clamping plate 61, the spherical window 41 is prevented from being scratched, meanwhile, the contact area between the spherical window 41 and the annular clamping plate 61 can be reduced, the rotation is more convenient, the inner side wall of the limiting claw 63 is provided with a non-greasy lubricating strip, the friction force between the limiting claw 63 and the spherical window 41 can be reduced, the side wall of the limiting claw 63 can scrape scab impurities (such as bird droppings, mud points and the like) which cannot be cleaned by the cleaning tool 611 on the spherical window 41 while limiting the spherical window 41, the transmission assembly 7 at least comprises three transmission wheels 71, a remote controller or a terminal can independently drive the transmission wheels 71 through the driving motor 72, and the transmission wheels 71 drive the spherical window 41 to rotate through the friction force of the remote controller or the terminal, so that the spherical window 41 can rotate in all directions without dead angles under the driving of the transmission wheels 71 when the spherical window 41 is required to be cleaned.
In one embodiment, at least 4 emergency protection components 8 are arranged on the bottom surface of the annular clamping plate 61, the emergency protection components 8 are annularly encircling the outer side of the spherical window 41, and the emergency protection components 8 are obliquely arranged towards the spherical window 41 and have an inclination angle with the annular clamping plate 61. The emergency protection component 8 comprises a containing box 81, a shifting block 82, an ejection column 83, a first clamping piece 84, a second clamping piece 85 and an ejection component; the ejector column 83 is arranged in the accommodating box 81, a sliding groove 831 is formed in the ejector column 83, one end of the ejector column 83 is conical, a clamping groove 832 is formed in the other end of the ejector column 83, a clamping table 833 is arranged on the side wall of the ejector column 83, a first clamping piece 84 and a second clamping piece 85 are arranged in the accommodating box 81 through connecting shafts, the first clamping piece 84 and the second clamping piece 85 are connected with the side wall of the accommodating box 81 through springs, the first clamping piece 84 and the second clamping piece 85 are used for being clamped with the clamping table 833, the bottom of the ejector assembly is connected with the ejector column 83 through the sliding groove 831 and the clamping groove 832, the top of the ejector assembly is clamped with the shifting block 82, and the shifting block 82 is slidably connected with the side wall of the accommodating box 81. The ejection assembly comprises a first sliding block 86 and a second sliding block 87, the first sliding block 86 is connected with the second sliding block 87 through a second elastic piece 88, the bottom surface of the first sliding block 86 is connected with a sliding groove 831 through a clamping table, the bottom surface of the second sliding block 87 is connected with a clamping groove 832 through a clamping table, the bottom surface of a shifting block 82 is provided with clamping protrusions 821, the first sliding block 86 and the second sliding block 87 are respectively located at two ends of the clamping protrusions 821, the side wall of the shifting block 82 is provided with a sliding groove 822 and a sliding plate 823, the first clamping piece 84 and the second clamping piece 85 are both located in the sliding groove 822, the shifting block 82 is in sliding connection with the side wall of the containing box 81 through the sliding plate 823, and the sliding groove 822 is located below the sliding plate 823.
The technical scheme has the working principle and beneficial effects that: at least 4 emergency protection components 8 are arranged at the bottom of the annular clamping plate 61, when the device is not used, the emergency protection components 8 are in an open state, one conical end of the ejection column 83 is positioned outside the spherical window 41 to prevent the spherical window 41 from being scratched or damaged when collision occurs, after the device is started by a remote controller, the emergency protection components 8 are changed to a standby state, the ejection column 83 is retracted into the accommodating box 81, during the flying process of the device, once the situation of disconnection from the remote controller occurs, although the built-in return system of the surveying instrument can automatically return, because the return is in an unmanned monitoring state, the possibility of a frying machine is thrown, the emergency protection components 8 are arranged to be automatically opened once the surveying instrument is disconnected from the remote controller or the terminal or the machine body 1 is suddenly dropped, when the situation occurs, the sensing module arranged in the driving device driving the shifting block 82 to move senses that the emergency protection component 8 needs to be started, the driving device is internally provided with a battery and the sensing module for ensuring the starting of the emergency protection component 8, the sensing module comprises a gravity sensing device (used for judging whether the situation of the falling of the frying machine occurs) and a signal receiving device (used for judging whether the signal transmission with a remote controller or a terminal is disconnected), the driving device can drive the shifting block 82 to slide along the side wall of the accommodating box 81, the shifting block 82 is positioned at one side of the sliding groove 822 and is in sliding connection with the side wall of the accommodating box 81 through the sliding plate 823, the sliding groove 822 is positioned below the sliding plate 823, so that the sliding plate 823 is not contacted with the first clamping piece 84 and the second clamping piece 85 when the shifting block 82 slides, the two side walls of the clamping protrusion 821 on the bottom surface of the shifting block 82 are respectively abutted against the first sliding block 86 and the second sliding block 87, in the standby state, the second clamping piece 85 is jacked by the spring to be clamped on one side of the clamping table 833 of the ejection column 83, the first clamping piece 84 is positioned at one end of the sliding groove 822 and is in a pressed state, the thickness of the first clamping piece 84 and the second clamping piece 85 is the sum of the thickness of the ejection column 83 and the thickness of the sliding groove 822, along with the movement of the shifting block 82, the first sliding block 86 slides along the sliding groove 831 under the pushing of the clamping protrusion 821, the clamping table of the second sliding block 87 is clamped by the clamping groove 832 to be unable to move, so that the second elastic piece 88 is elongated and generates a tensile force, meanwhile, the other side of the sliding groove 822 also gradually slides towards the second clamping piece 85, because the two ends of the sliding groove 822 are arc-shaped, as shown in fig. 13, the second clamping piece 85 can be pressed by the sliding groove 822, until the second clamping piece 85 is separated from the clamping table 833 of the ejection column 83, under the action of the pull force of the second elastic piece 88, the second sliding block 87 drives the ejection column 83 to eject rapidly, until the clamping table 833 is impacted onto the limiting platform at the end part of the accommodating box 81, the connection angle between the first clamping piece 84 and the second clamping piece 85 through the spring and the side wall of the accommodating box 81 is an acute angle, the acute angle of the first clamping piece 84 is consistent with the ejecting direction of the ejection column 83, the acute angle of the second clamping piece 85 is consistent with the retracting direction of the ejection column 83, as shown in fig. 7-10, therefore, when the clamping table 833 translates, the first clamping piece 84 is extruded firstly to prevent the ejection of the ejection column 83, when one side of the clamping table 833 is clamped on the limiting platform, the other side of the clamping table 833 just passes through the first clamping piece 84, and the first clamping piece 84 is sprung to prevent the clamping table 833 from rebounding, the schematic diagrams of the first clamping member 84 and the second clamping member 85 before and after ejection are shown in fig. 14 and 15, therefore, when the emergency protection assembly 8 is started, the driving device only needs to drive the shifting block 82 to move a short distance to realize quick ejection of the ejection column 83, so that the spherical window 41 can be protected by the ejection column 83 almost instantaneously when the emergency protection assembly 8 is started, the principle that the emergency protection assembly 8 becomes standby state is the same as that of ejection, the ejection column 83 can be made of elastic silica gel and other materials, the sliding chute 831 not only provides a limiting function for the first sliding block 86, but also can play a role of buffering and damping, the emergency protection assembly 8 does not take the spherical window 41 as a first requirement, but rather takes the relatively expensive mapping instrument inside the emergency protection assembly to protect the spherical window 41 from dropping, losing and damaging after the frying, the spherical window 41 is cracked, the obliquely arranged ejection column 83 can protect and bind the mapping instrument in the machine body 1, so that the mapping instrument is prevented from being lost in the process of falling, the mapping instrument can be conveniently searched, and the loss of the mapping can be recovered when the frying machine can be recovered.
The invention provides a mapping method of a full-automatic topographic map mapping device, which comprises the following steps:
s1: placing the mapping assembly 4 at a lifting point, and starting the mapping assembly 4 through a remote controller;
s2: the emergency protection component 8 is retracted to a standby state, the transmission component 7 drives the spherical window 41 to rotate, and primary cleaning is carried out on the cleaning mechanism 6;
s3: preheating a propeller 2 and a surveying instrument, and detecting a video state;
s4: and after the preparation, the surveying and mapping assembly 4 is controlled to lift off by a remote controller to survey and map.
In the description of the present invention, it should be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", "axial", "radial", "circumferential", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings are merely for convenience in describing the present invention and simplifying the description, and do not indicate or imply that the device or element being referred to must have a specific orientation, be configured and operated in a specific orientation, and therefore should not be construed as limiting the present invention.
In the present invention, unless explicitly specified and limited otherwise, the terms "mounted," "connected," "secured," and the like are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally formed; may be mechanically connected, may be electrically connected or may be in communication with each other; either directly or indirectly, through intermediaries, or both, may be in communication with each other or in interaction with each other, unless expressly defined otherwise. The specific meaning of the above terms in the present invention can be understood by those of ordinary skill in the art according to the specific circumstances.
Although embodiments of the present invention have been disclosed above, it is not limited to the details and embodiments shown and described, it is well suited to various fields of use for which the invention would be readily apparent to those skilled in the art, and accordingly, the invention is not limited to the specific details and illustrations shown and described herein, without departing from the general concepts defined in the claims and their equivalents.
Claims (9)
1. A fully automatic topographic mapping apparatus, comprising: the device comprises a machine body (1), a propeller (2), a wane (3) and a mapping assembly (4); the screw propeller (2) is arranged at the top of the machine body (1), the rocker (3) is arranged at the bottom edge of the machine body (1) through a damping mechanism (5), and the mapping assembly (4) is arranged at the bottom of the machine body (1) through a cleaning mechanism (6);
the utility model provides a surveying and mapping subassembly (4) is including spherical window (41), drive assembly (7), surveying instrument with clearance mechanism (6), surveying instrument passes through level equipment setting in spherical window (41), level equipment is used for maintaining surveying instrument's stability when spherical window (41) rotate, clearance mechanism (6) set up the bottom of fuselage (1), spherical window (41) with drive assembly (7) all set up on clearance mechanism (6), drive assembly (7) with the top of spherical window (41) is connected, drive assembly (7) are used for driving spherical window (41) rotate.
2. The full-automatic topographic mapping device according to claim 1, wherein the number of propellers (2) is four, and the propellers are symmetrically arranged at the edge of the top of the machine body (1) in a cross shape.
3. The full-automatic topographic mapping device according to claim 1, characterized in that there are at least two of the rocker plates (3), and the top surface of the rocker plates (3) is connected with the bottom surface of the fuselage (1) through two shock absorbing mechanisms (5), the shock absorbing mechanisms (5) comprising an outer tube (51) and an inner rod (52); the top of the outer tube (51) is connected with the bottom of the machine body (1), the top of the inner rod (52) is inserted into a containing groove at the bottom of the outer tube (51), the inner rod (52) is connected with the inner top of the containing groove through a first elastic piece (53), and the bottom of the inner rod (52) is connected with the top of the rocker (3).
4. The fully automatic topographic mapping apparatus according to claim 1, wherein the cleaning mechanism (6) includes a ring-shaped clamping plate (61), a mounting plate (62), a limiting pawl (63) and an auxiliary wheel (64); the utility model discloses a cleaning device for the automobile, including annular cardboard (61), fuselage (1), mounting bracket (61), mounting bracket (65), mounting bracket (62) and fuselage (1) are connected through the installation pole, be provided with cleaning apparatus (611) on the inner ring lateral wall of annular cardboard (61), spherical window (41) overlap joint is in on the inner ring of annular cardboard (61), cleaning apparatus (611) with the outer wall butt of spherical window (41), mounting panel (62) are located the top of spherical window (41), and the top of mounting panel (62) pass through the connecting rod with fuselage (1) are connected, the bottom of mounting panel (62) is provided with at least three spacing claw (63), the inner wall of spacing claw (63) with the outer wall sliding connection of spherical window (41), the bottom of spacing claw (63) is provided with auxiliary wheel (64), auxiliary wheel (64) with the outer wall butt of spherical window (41), drive assembly (7) set up on mounting panel (62).
5. The full-automatic topographic mapping device according to claim 4, characterized in that the transmission assembly (7) comprises at least three transmission wheels (71), a driving motor (72) is arranged on the transmission wheels (71), the transmission wheels (71) are connected with the mounting plate (62) through a connecting plate (73), and the transmission wheels (71) are abutted with the spherical window (41).
6. The full-automatic topographic mapping device according to claim 4, wherein at least 4 emergency protection components (8) are arranged on the bottom surface of the annular clamping plate (61), the emergency protection components (8) are annularly encircling the outer side of the spherical window (41), and the emergency protection components (8) are obliquely arranged towards the spherical window (41) and are obliquely arranged with the annular clamping plate (61).
7. The fully automatic topographic mapping apparatus of claim 6, wherein the emergency protective assembly (8) includes a containment box (81), a dial block (82), an ejection post (83), a first snap-in member (84), a second snap-in member (85), and an ejection assembly; the ejector column (83) is arranged in the accommodating box (81), a sliding groove (831) is formed in the ejector column (83), one end of the ejector column (83) is conical, a clamping groove (832) is formed in the other end of the ejector column, a clamping table (833) is arranged on the side wall of the ejector column (83), a first clamping piece (84) and a second clamping piece (85) are arranged in the accommodating box (81) through connecting shafts, the first clamping piece (84) and the second clamping piece (85) are connected with the side wall of the accommodating box (81) through springs, the first clamping piece (84) and the second clamping piece (85) are both used for being clamped with the clamping table (833), the bottom of the ejector assembly is connected with the ejector column (83) through the sliding groove (831) and the clamping groove (832), and the top of the ejector assembly is clamped with the poking block (82), and the poking block (82) is connected with the side wall of the accommodating box (81) in a sliding mode.
8. The full-automatic topographic mapping device according to claim 7, wherein the ejection assembly comprises a first slider (86) and a second slider (87), the first slider (86) is connected with the second slider (87) through a second elastic member (88), the bottom surface of the first slider (86) is connected with the chute (831) through a clamping table, the bottom surface of the second slider (87) is connected with the clamping groove (832) through a clamping table, the bottom surface of the shifting block (82) is provided with a clamping protrusion (821), the first slider (86) and the second slider (87) are respectively located at two ends of the clamping protrusion (821), the side wall of the shifting block (82) is provided with a sliding groove (822) and a sliding plate (823), the first clamping member (84) and the second clamping member (85) are both located in the sliding groove (822), and the shifting block (82) is located in the sliding groove (823) through the sliding plate (823) and is connected with the side wall (81) in the sliding groove (823).
9. A mapping method using the fully automatic topographic mapping apparatus of claim 8, characterized by the steps of:
s1: the mapping assembly (4) is placed at a lifting point, and the mapping assembly (4) is started through a remote controller;
s2: the emergency protection assembly (8) is retracted to a standby state, the transmission assembly (7) drives the spherical window (41) to rotate, and primary cleaning is carried out on the cleaning mechanism (6);
s3: preheating a propeller (2) and a surveying instrument, and detecting a video state;
s4: and after the preparation, controlling the surveying and mapping assembly (4) to lift off through a remote controller to survey and map.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202211059600.6A CN115230954B (en) | 2022-08-31 | 2022-08-31 | Full-automatic topographic map mapping device and mapping method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202211059600.6A CN115230954B (en) | 2022-08-31 | 2022-08-31 | Full-automatic topographic map mapping device and mapping method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN115230954A CN115230954A (en) | 2022-10-25 |
| CN115230954B true CN115230954B (en) | 2023-05-30 |
Family
ID=83681904
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202211059600.6A Active CN115230954B (en) | 2022-08-31 | 2022-08-31 | Full-automatic topographic map mapping device and mapping method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN115230954B (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN210063387U (en) * | 2019-05-29 | 2020-02-14 | 广东孛特勘测设计有限公司 | Single-camera shooting measuring device for unmanned aerial vehicle |
| CN110823188A (en) * | 2019-11-11 | 2020-02-21 | 河南省聚鑫勘测规划设计有限公司 | Full-automatic topographic map surveying and mapping device and surveying and mapping method |
| CN211139691U (en) * | 2019-10-24 | 2020-07-31 | 广州欧达信息科技有限公司 | Unmanned aerial vehicle for electric power inspection |
| WO2021017017A1 (en) * | 2019-07-30 | 2021-02-04 | 苏州领速电子科技有限公司 | Camera lens for racing unmanned aerial vehicle |
| CN113492977A (en) * | 2020-04-07 | 2021-10-12 | 隆安良 | Full-automatic topographic map mapping device of robot |
| CN214930624U (en) * | 2021-07-15 | 2021-11-30 | 重庆巨海信息技术有限公司 | Unmanned aerial vehicle is camera anti-shake device for survey and drawing |
| CN215098331U (en) * | 2021-07-15 | 2021-12-10 | 河南峥峰勘测设计有限公司 | Be used for dedicated mapping tool of unmanned aerial vehicle survey and drawing |
| CN114802790A (en) * | 2022-05-05 | 2022-07-29 | 常州工学院 | But remote sensing survey and drawing unmanned aerial vehicle of autogiration |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP3224172U (en) * | 2016-11-04 | 2019-12-05 | エックスダイナミクス リミテッド | Unmanned aerial vehicle |
| CN110809110B (en) * | 2019-11-19 | 2020-10-27 | 珠海大横琴科技发展有限公司 | Intelligent road surface information acquisition machine |
| CN211468760U (en) * | 2019-12-18 | 2020-09-11 | 哈尔滨酷迈科技有限公司 | A undercarriage for unmanned aerial vehicle |
| KR102200908B1 (en) * | 2020-06-12 | 2021-01-11 | 조은석 | VRS follow-up system for cadastral survey using by DRON |
| CN212963341U (en) * | 2020-08-21 | 2021-04-13 | 内蒙古中科世源生态科技有限公司 | Recorder cleaning device for unmanned aerial vehicle surveying and mapping |
| CN213414247U (en) * | 2020-10-30 | 2021-06-11 | 深圳市卓影光电有限公司 | Survey and drawing unmanned aerial vehicle camera rotational positioning device |
| CN214824205U (en) * | 2020-12-30 | 2021-11-23 | 南京羽飞电子科技有限公司 | Survey and drawing unmanned aerial vehicle with high definition digtal camera protection machanism |
-
2022
- 2022-08-31 CN CN202211059600.6A patent/CN115230954B/en active Active
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN210063387U (en) * | 2019-05-29 | 2020-02-14 | 广东孛特勘测设计有限公司 | Single-camera shooting measuring device for unmanned aerial vehicle |
| WO2021017017A1 (en) * | 2019-07-30 | 2021-02-04 | 苏州领速电子科技有限公司 | Camera lens for racing unmanned aerial vehicle |
| CN211139691U (en) * | 2019-10-24 | 2020-07-31 | 广州欧达信息科技有限公司 | Unmanned aerial vehicle for electric power inspection |
| CN110823188A (en) * | 2019-11-11 | 2020-02-21 | 河南省聚鑫勘测规划设计有限公司 | Full-automatic topographic map surveying and mapping device and surveying and mapping method |
| CN113492977A (en) * | 2020-04-07 | 2021-10-12 | 隆安良 | Full-automatic topographic map mapping device of robot |
| CN214930624U (en) * | 2021-07-15 | 2021-11-30 | 重庆巨海信息技术有限公司 | Unmanned aerial vehicle is camera anti-shake device for survey and drawing |
| CN215098331U (en) * | 2021-07-15 | 2021-12-10 | 河南峥峰勘测设计有限公司 | Be used for dedicated mapping tool of unmanned aerial vehicle survey and drawing |
| CN114802790A (en) * | 2022-05-05 | 2022-07-29 | 常州工学院 | But remote sensing survey and drawing unmanned aerial vehicle of autogiration |
Also Published As
| Publication number | Publication date |
|---|---|
| CN115230954A (en) | 2022-10-25 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN211391706U (en) | Slow descending device and unmanned aerial vehicle | |
| CN115230954B (en) | Full-automatic topographic map mapping device and mapping method | |
| CN117104560B (en) | Monitoring device for inspection unmanned aerial vehicle | |
| DE102015012369A1 (en) | System for influencing an adaptive chassis of a land vehicle | |
| CN115675958A (en) | Pumped storage power station inspection device based on unmanned aerial vehicle | |
| CN113955031A (en) | Unmanned aerial vehicle storage mechanism for unmanned ship and using method | |
| CN216546771U (en) | Unmanned aerial vehicle's descending platform for survey and drawing data acquisition | |
| CN220374781U (en) | Amphibious inspection device | |
| CN212401587U (en) | Unmanned aerial vehicle with aerial photogrammetry function | |
| CN219313042U (en) | Unmanned aerial vehicle for farmland environment monitoring | |
| CN111891371A (en) | Unmanned aerial vehicle topography survey device | |
| CN116692073A (en) | Substation inspection unmanned aerial vehicle relay charging platform | |
| CN213323689U (en) | Unmanned aerial vehicle water ecology remote sensing monitoring system | |
| CN115817876A (en) | Unmanned aerial vehicle positioner that falls based on computer vision | |
| CN212195850U (en) | Unmanned aerial vehicle buffer stop | |
| CN110958430A (en) | Monitoring system and monitoring method | |
| CN113650777A (en) | Unmanned aerial vehicle undercarriage receive and releases system | |
| CN218052639U (en) | Automatic inspection robot | |
| CN112298555A (en) | A5G unmanned aerial vehicle for high accuracy survey and drawing | |
| CN220948583U (en) | Unmanned aerial vehicle camera protection is with accessory | |
| CN115384774B (en) | Investigation unmanned aerial vehicle is used in actual combat countermeasure | |
| CN111112197A (en) | Vehicle-mounted camera cleaning device | |
| CN219096991U (en) | Automatic line inspection structure of unmanned aerial vehicle | |
| CN220540773U (en) | Adjustable vehicle-mounted camera shooting holder | |
| CN217227908U (en) | Damping device for aerial remote sensing surveying and mapping unmanned aerial vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |