CN114572411A - Unmanned aerial vehicle mapping device that takes photo by plane - Google Patents
Unmanned aerial vehicle mapping device that takes photo by plane Download PDFInfo
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- CN114572411A CN114572411A CN202210392512.1A CN202210392512A CN114572411A CN 114572411 A CN114572411 A CN 114572411A CN 202210392512 A CN202210392512 A CN 202210392512A CN 114572411 A CN114572411 A CN 114572411A
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- 238000013507 mapping Methods 0.000 title claims abstract description 92
- 230000000087 stabilizing effect Effects 0.000 claims abstract description 6
- 230000035939 shock Effects 0.000 claims description 6
- 238000010030 laminating Methods 0.000 claims description 3
- 238000010521 absorption reaction Methods 0.000 claims 1
- 238000013016 damping Methods 0.000 abstract description 14
- 238000010276 construction Methods 0.000 description 3
- 238000011161 development Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 241000883990 Flabellum Species 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 238000005381 potential energy Methods 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
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- 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
- B64C25/62—Spring shock-absorbers; Springs
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
Abstract
The invention provides an unmanned aerial vehicle aerial photography surveying and mapping device which comprises a flight surveying and mapping component, a stable gyroscope component and a damping component, wherein the flight surveying and mapping component lifts the stable gyroscope component and the damping component to the air, so that the stable gyroscope component can be conveniently observed and surveyed, the stable gyroscope component is used for stabilizing the angle and quality of surveying and mapping shooting, and can be used for conveniently storing and protecting equipment for shooting and surveying and mapping when the flight surveying and mapping component drives the stable gyroscope component to move downwards, and when the flight surveying and mapping component drives the damping component to move towards the ground, the damping component is subjected to damping treatment. According to the invention, through the arrangement of the U-shaped plate body, the square through hole plate body, the square plate body, the fixing plate body, the first dynamic balance calibration block and the second dynamic balance calibration block, when the flight fan blade drives the surveying and mapping machine body to fly under the influence of wind power, the position of the surveying and mapping machine body is shaken, the function of the gyroscope is adopted, the use stability of the camera surveying and mapping head is ensured, and the quality and the efficiency of aerial photography surveying and mapping are improved.
Description
Technical Field
The invention relates to the technical field of surveying, in particular to an unmanned aerial vehicle aerial surveying and mapping device.
Background
The aerial survey of the unmanned aerial vehicle is a powerful supplement of the traditional aerial photogrammetry means, has the characteristics of flexibility, high efficiency, rapidness, fineness, accuracy, low operation cost, wide application range, short production period and the like, the method has obvious advantages in the aspect of fast obtaining high-resolution images in small areas and areas with difficult flight, along with the development of the technologies of the unmanned aerial vehicle and the digital camera, the digital aerial photography technology based on the unmanned aerial vehicle platform has shown unique advantages, the combination of the unmanned aerial vehicle and aerial photogrammetry enables the 'digital low-altitude remote sensing of the unmanned aerial vehicle' to become a brand-new development direction in the field of aerial remote sensing, the aerial photography of the unmanned aerial vehicle can be widely applied to the aspects of national major engineering construction, disaster emergency and treatment, territorial supervision, resource development, new rural areas, small town construction and the like, and the method has wide prospects in the aspects of basic mapping, land resource investigation and monitoring, dynamic monitoring of land utilization, digital city construction, acquisition of emergency disaster relief mapping data and the like;
present unmanned aerial vehicle mapping device that takes photo by plane uses the gyroscope to adjust the survey and drawing when surveying and mapping and take a photograph the camera, because the gyroscope receives wind-force influence easily, causes the survey and drawing to take a photograph the first unstability to can't take a photograph the camera to the survey and drawing and carry out safety protection, cause loss of property, and when descending unmanned aerial vehicle, do not have damping device, thereby cause the descending damage, for this reason, provide an unmanned aerial vehicle mapping device that takes photo by plane.
Disclosure of Invention
In view of the above, embodiments of the present invention are intended to provide an apparatus for aerial surveying and mapping by an unmanned aerial vehicle, so as to solve or alleviate the technical problems in the prior art, and to provide at least one useful choice.
The technical scheme of the embodiment of the invention is realized as follows: the utility model provides an unmanned aerial vehicle mapping device that takes photo by plane, including flight survey and drawing subassembly, stabilize gyroscope subassembly and damper assembly, flight survey and drawing subassembly will stabilize gyroscope subassembly and damper assembly and rise to aloft, be convenient for stabilize gyroscope subassembly and observe the survey and drawing, it is used for angle and quality at the shooting of stable survey and drawing to stabilize gyroscope subassembly, can drive when stabilizing gyroscope subassembly downstream at flight survey and drawing subassembly again, be convenient for accomodate the protection to the equipment of shooting survey and drawing, when flight survey and drawing subassembly drives damper assembly and removes to ground, thereby make damper assembly carry out the shock attenuation and handle, the improvement is to the protection of this device, stable gyroscope subassembly and damper assembly are installed respectively to the below of flight survey and drawing subassembly.
Preferably, the stable gyroscope assembly comprises a U-shaped plate body, a differential motor, a first electric push rod, a first slide block, a square through hole plate body, a square plate body, a second electric push rod, a camera surveying and mapping head and a fixed plate body;
lower surface mounting in differential motor's upper surface of survey and drawing fuselage, differential motor's output shaft is installed in the upper surface of U type plate body, the inside wall symmetry of U type plate body is equipped with two first sliders, the bearing rotation is passed through to one side that two first sliders are adjacent is connected in the lateral wall of square through hole plate body, the inside wall of square through hole plate body passes through the bearing rotation and connects in the lateral wall of square plate body, the fixed plate body sets up two altogether, the upper surface symmetry of two fixed plate bodies is installed in the lower surface of square plate body, the bearing rotation is passed through to one side that the fixed plate body is adjacent and is connected in the lateral wall of camera survey and drawing head.
Further preferably, two first chutes are symmetrically formed in the inner side wall of the U-shaped plate body, the inner side wall of each first chute is connected to the outer side wall of the corresponding first sliding block in a sliding mode, two first electric push rods are arranged on the outer side wall of the U-shaped plate body, the upper surfaces of the two first electric push rods are symmetrically arranged on the inner side bottom wall of the U-shaped plate body, and piston rods of the first electric push rods are arranged on the upper surface of the first sliding block.
Further preferably, the lower surface of the square plate body is rotatably connected to the upper surface of the second electric push rod through a bearing, and a piston rod of the second electric push rod is hinged to the upper surface of the camera surveying and mapping head through a pin shaft.
Further preferably, two first dynamic balance calibration blocks are symmetrically installed on the lower surface of the square through hole plate body, and two second dynamic balance calibration blocks are symmetrically installed on the lower surface of the square plate body.
Preferably, the flight mapping assembly comprises a mapping fuselage, a connecting plate body, flight fan blades and a streamline plate body;
the connecting plate body sets up four altogether, and the mutual symmetry in the lateral wall of surveying and mapping fuselage in one side that four connecting plate bodies are adjacent sets up four altogether, and the lower surface of four flight flabellums sets up in the upper surface of four connecting plate bodies.
Further preferably, the upper surface of the surveying and mapping body is mounted to the lower surface of the streamlined plate body.
Further preferably, the damping assembly comprises a circular cylinder, a circular rod body, a spring and a rubber pad;
the circular cylinder sets up four altogether, and four circular cylinder's top is installed in the lower surface of four connection plate bodies, and circular cylinder's inside wall laminating in the lateral wall of the circular body of rod, and the upper surface in the rubber pad is installed to the bottom of the circular body of rod, and the bottom of the circular body of rod is installed in the bottom of spring, and the lower surface in connection plate body is installed to the bottom of spring.
Further preferably, four second chutes are symmetrically formed in the inner side wall of the circular cylinder body, the inner side wall of each second chute is connected with a second sliding block in a sliding mode, and one side, adjacent to each other, of each of the four second sliding blocks is symmetrically arranged on the outer side wall of the circular rod body.
Due to the adoption of the technical scheme, the embodiment of the invention has the following advantages:
according to the invention, through the arrangement of the U-shaped plate body, the square through hole plate body, the square plate body, the fixing plate body, the first dynamic balance calibration block and the second dynamic balance calibration block, when the flight fan blade drives the surveying and mapping machine body to fly and is influenced by wind power, the position of the surveying and mapping machine body is rocked, the function of the gyroscope is adopted, the use stability of the camera surveying and mapping head is ensured, and the quality and the efficiency of aerial photography surveying and mapping are improved.
According to the unmanned aerial vehicle aerial photography surveying and mapping system, the problem of the shooting angle of the camera surveying and mapping head is changed conveniently through the arrangement of the differential motor and the second electric push rod, the purpose of full coverage of an unmanned aerial vehicle aerial photography surveying and mapping area is achieved, and the surveying and mapping efficiency is further improved.
The circular cylinder, the circular rod body and the spring are arranged, so that when the surveying and mapping machine body descends, the impact force of the circular rod body is buffered through the elastic potential energy of the spring, the descending protection capability of the device is improved, and the service life of the device is prolonged.
According to the invention, by starting the first electric push rod, when the piston rod of the first electric push rod drives the first slider to move in the first chute, the first slider drives the square through hole plate body, the square plate body and the camera surveying and mapping head to move into the U-shaped plate body, when the surveying and mapping machine body descends, the camera surveying and mapping head can be effectively protected, and the camera surveying and mapping head is prevented from being damaged due to collision of ground stones, so that property loss is avoided.
The foregoing summary is provided for the purpose of description only and is not intended to be limiting in any way. In addition to the illustrative aspects, embodiments, and features described above, further aspects, embodiments, and features of the present invention will be readily apparent by reference to the drawings and following detailed description.
Drawings
In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings needed to be used in the embodiments or technical descriptions will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present application, and for those skilled in the art, other drawings can be obtained according to the drawings without creative efforts.
FIG. 1 is a block diagram of the present invention;
FIG. 2 is a top view of the present invention;
FIG. 3 is a side view structural diagram of the present invention;
FIG. 4 is a view of the internal structure of the stabilized gyroscope assembly of the present invention;
FIG. 5 is a bottom view of the internal portion of the stabilizing gyroscope assembly of the present invention;
FIG. 6 is an enlarged structural view of the area A of FIG. 5 according to the present invention;
fig. 7 is an internal structural view of a shock-absorbing assembly of the present invention.
Reference numerals: 1. a flight mapping assembly; 101. surveying and mapping the fuselage; 102. connecting the plate bodies; 103. flight fan blades; 104. a streamlined plate body; 2. stabilizing the gyroscope assembly; 201. a U-shaped plate body; 202. a differential motor; 203. a first electric push rod; 204. a first slider; 205. a square through hole plate body; 206. a square plate body; 207. a second electric push rod; 208. a camera surveying and mapping head; 209. fixing the plate body; 3. a shock absorbing assembly; 301. a circular cylinder; 302. a circular rod body; 303. a spring; 304. a rubber pad; 4. a first chute; 5. a first dynamic balance calibration block; 6. a second dynamic balance calibration block; 7. a second chute; 8. and a second slider.
Detailed Description
In the following, only certain exemplary embodiments are briefly described. As those skilled in the art will recognize, the described embodiments may be modified in various different ways, all without departing from the spirit or scope of the present invention. Accordingly, the drawings and description are to be regarded as illustrative in nature, and not as restrictive.
Embodiments of the present invention will be described in detail below with reference to the accompanying drawings.
Example one
As shown in fig. 1-7, an embodiment of the invention provides an unmanned aerial vehicle aerial photography surveying and mapping device, which comprises a flight surveying and mapping component 1, a stable gyroscope component 2 and a damping component 3, wherein the flight surveying and mapping component 1 lifts the stable gyroscope component 2 and the damping component 3 into the air, so that the stable gyroscope component 2 can be conveniently observed and surveyed, the stable gyroscope component 2 is used for stably surveying and mapping the angle and the quality of shooting, and can be conveniently stored and protected when the flight surveying and mapping component 1 drives the stable gyroscope component 2 to move downwards, the flight surveying and mapping component 1 drives the damping component 3 to move towards the ground, so that the damping component 3 is subjected to damping treatment, the protection of the device is improved, and the stable gyroscope component 2 and the damping component 3 are respectively installed below the flight surveying and mapping component 1.
Example two
As shown in fig. 1 to 7, an embodiment of the present invention provides a stable gyroscope assembly 2, which includes a U-shaped plate 201, a differential motor 202, a first electric push rod 203, a first slider 204, a square through-hole plate 205, a square plate 206, a second electric push rod 207, a camera surveying and mapping head 208, and a fixed plate 209;
the lower surface of the surveying and mapping machine body 101 is arranged on the upper surface of a differential motor 202, the output shaft of the differential motor 202 is arranged on the upper surface of a U-shaped plate body 201, two first sliding blocks 204 are symmetrically arranged on the inner side wall of the U-shaped plate body 201, one side adjacent to the two first sliding blocks 204 is rotatably connected with the outer side wall of a square through-hole plate body 205 through a bearing, the inner side wall of the square through-hole plate body 205 is rotatably connected with the outer side wall of a square plate body 206 through a bearing, two fixing plate bodies 209 are symmetrically arranged on the lower surface of the square plate body 206, one side adjacent to the fixing plate body 209 is rotatably connected with the outer side wall of a camera surveying and mapping head 208 through a bearing, the U-shaped plate body 201, the square through-hole plate body 205, the square plate body 206, a second electric push rod 207 and the camera surveying and mapping head 208 are rotatably connected with each other through a bearing for adjusting the position of the camera surveying and mapping head 208, wherein the fixing plate 209 can fix the position of the camera 208 and adjust the position of the camera 208.
In one embodiment, two first sliding grooves 4 are symmetrically formed in the inner side wall of the U-shaped plate 201, the inner side wall of each first sliding groove 4 is slidably connected to the outer side wall of the first sliding block 204, two first electric push rods 203 are provided, the upper surfaces of the two first electric push rods 203 are symmetrically installed on the inner bottom wall of the U-shaped plate 201, the piston rods of the first electric push rods 203 are installed on the upper surfaces of the first sliding blocks 204, by sliding the first sliding block 204 in the first sliding groove 4, the position of the square through hole plate 205 can be moved, thereby facilitating the adjustment of the position of the square through hole plate body 205 driving the camera surveying and mapping head 208, due to the arrangement of the first electric push rod 203, a piston rod of the first electric push rod 203 drives the first sliding block 204 to slide up and down in the first sliding groove 4, so that the position of the first sliding block 204 is further assisted to move, and the position of the square through hole plate body 205 is assisted to move.
In one embodiment, the lower surface of the square plate 206 is rotatably connected to the upper surface of the second electric push rod 207 through a bearing, the piston rod of the second electric push rod 207 is hinged to the upper surface of the camera surveying and mapping head 208 through a pin shaft, and the up-down angle of the camera surveying and mapping head 208 is adjusted by starting the second electric push rod 207, so that the surveying range is increased.
In one embodiment, two first dynamic balance calibration blocks 5 are symmetrically installed on the lower surface of the square through hole plate 205, two second dynamic balance calibration blocks 6 are symmetrically installed on the lower surface of the square plate 206, and are used for adjusting and balancing the position of the square through hole plate 205 through the setting of the first dynamic balance calibration blocks 5, wherein the setting of the second dynamic balance calibration blocks 6 is used for adjusting and balancing the position of the square plate 206, so as to perform balance adjustment on the position of the camera mapping head 208.
EXAMPLE III
As shown in fig. 1-7, the flight mapping assembly 1 according to the present embodiment of the invention includes a mapping fuselage 101, a connecting plate 102, a flight blade 103, and a streamlined plate 104;
the connecting plate bodies 102 are four in number, one side of each of the four adjacent connecting plate bodies 102 is symmetrically arranged on the outer side wall of the surveying and mapping machine body 101, the four flight fan blades 103 are four in number, the lower surfaces of the four flight fan blades 103 are arranged on the upper surfaces of the four connecting plate bodies 102, and the surveying and mapping machine body 101 is driven to lift off conveniently through the arrangement of the flight fan blades 103.
In one embodiment, the upper surface of the surveying and mapping body 101 is mounted on the lower surface of the streamlined plate 104, and the streamlined plate 104 is used to guide air conveniently, so as to stabilize the position of the surveying and mapping body 101.
Example four
As shown in fig. 1 to 7, the embodiment of the present invention provides a shock absorbing assembly 3 including a circular cylinder 301, a circular rod 302, a spring 303 and a rubber pad 304;
In one embodiment, four second sliding grooves 7 are symmetrically formed in the inner side wall of the circular cylinder 301, a second sliding block 8 is connected to the inner side wall of each second sliding groove 7 in a sliding mode, one side, adjacent to each other, of each second sliding block 8 is symmetrically arranged on the outer side wall of the circular rod body 302, and the second sliding blocks 8 slide in the second sliding grooves 7, so that the circular rod body 302 can be assisted to move, and the position of the circular rod body 302 can be limited.
The invention is in operation: the control module in the surveying and mapping machine body 101 is controlled by a remote controller, so that the control module of the surveying and mapping machine body 101 starts the flight blades 103, the flight blades 103 rotate to drive the flight surveying and mapping component 1, the stabilizing gyroscope component 2 and the damping component 3 to lift off, at the moment, the control module starts the first electric push rod 203, a piston rod of the first electric push rod 203 drives the first slider 204 to move downwards in the first chute 4, the first chute 4 drives the square through hole plate body 205, the square plate body 206, the camera 208 and the fixed plate body 209 to move out of the U-shaped plate body 201, when the air flow in the high air is disordered, the position of the surveying and mapping machine body 101 is unstable, the surveying and mapping machine body 101 drives the U-shaped plate body 201 to incline, at the moment, the square through hole plate body 205 on the U-shaped plate body 201 performs position adjustment with the first dynamic balance calibration block 5 through a bearing, so as to balance the position of the square through hole plate body 205, at this time, the square plate 206 on the square through hole plate 205 is conveniently and stably adjusted through the arrangement of the bearing and the second dynamic balance calibration block 6, when the circumferential angle of the camera surveying and mapping head 208 needs to be adjusted, the differential motor 202 drives the position of the U-shaped plate 201 to rotate, the U-shaped plate 201 sequentially passes through the square through hole plate 205, the square plate 206 and the fixing plate 209 to drive the camera surveying and mapping head 208 to circumferentially rotate, when the camera surveying and mapping head 208 needs to be adjusted in an up-and-down angle, the second electric push rod 207 is started, the output shaft of the second electric push rod 207 drives the camera surveying and mapping head 208 to adjust in an angle, when the device needs to be descended, the first electric push rod 203 is started, the piston rod of the first electric push rod 203 drives the first slide block 204 to move upwards, the first slide block 204 sequentially drives the square through hole plate 205, the second dynamic balance calibration block 6, Square plate body 206, second electric putter 207, camera mapping head 208 and fixed plate body 209 remove to U type plate body 201 in, drive circular barrel 301 and circular body of rod 302 and descend when surveying and mapping fuselage 101 to make rubber pad 304 laminate ground, thereby make rubber pad 304 and the recoil force on ground produce deformation through circular body of rod 302 guide to spring 303, thereby release the recoil force on the circular body of rod 302, improve the absorbing effect of this device.
The above description is only for the specific embodiment of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art can easily conceive various changes or substitutions within the technical scope of the present invention, and these should be covered by the scope of the present invention. Therefore, the protection scope of the present invention shall be subject to the protection scope of the appended claims.
Claims (9)
1. The utility model provides an unmanned aerial vehicle mapping device that takes photo by plane which characterized in that, includes flight mapping subassembly (1), stabilizes gyroscope subassembly (2) and damper assembly (3):
flight survey and drawing subassembly (1) will stabilize gyroscope subassembly (2) and damper assembly (3) and rise to aloft, be convenient for stabilize gyroscope subassembly (2) and observe the survey and drawing, stabilize gyroscope subassembly (2) and be used for angle and quality of shooing at stable survey and drawing, can drive when stabilizing gyroscope subassembly (2) downstream again in flight survey and drawing subassembly (1), be convenient for accomodate the protection to the equipment of shooing the survey and drawing, flight survey and drawing subassembly (1) drives damper assembly (3) when removing to ground, thereby make damper assembly (3) carry out the shock attenuation and handle, improve the protection to this device, stable gyroscope subassembly (2) and damper assembly (3) are installed respectively to the below of flight survey and drawing subassembly (1).
2. Unmanned aerial vehicle mapping device that takes photo by plane of claim 1, characterized in that: the stable gyroscope component (2) comprises a U-shaped plate body (201), a differential motor (202), a first electric push rod (203), a first slide block (204), a square through hole plate body (205), a square plate body (206), a second electric push rod (207), a camera surveying and mapping head (208) and a fixed plate body (209);
lower surface mounting in the upper surface of differential motor (202) of survey and drawing fuselage (101), the output shaft of differential motor (202) is installed in the upper surface of U type plate body (201), the inside wall symmetry of U type plate body (201) is equipped with two first sliders (204), the lateral wall in square through hole plate body (205) is connected in through bearing rotation to the adjacent one side of two first sliders (204), the lateral wall in square through hole plate body (205) is connected in the lateral wall of square plate body (206) through bearing rotation, fixed plate body (209) set up two altogether, the upper surface symmetry of two fixed plate bodies (209) is installed in the lower surface of square plate body (206), the adjacent one side of fixed plate body (209) is passed through bearing rotation and is connected in the lateral wall of taking a photograph of survey and drawing head (208).
3. Unmanned aerial vehicle mapping device that takes photo by plane of claim 2, characterized in that: two first chutes (4) are symmetrically arranged on the inner side wall of the U-shaped plate body (201), the inner side wall of each first chute (4) is connected to the outer side wall of the corresponding first sliding block (204) in a sliding mode, the two first electric push rods (203) are arranged on the outer side wall of the U-shaped plate body (201) in a sharing mode, the upper surfaces of the two first electric push rods (203) are symmetrically arranged on the inner side bottom wall of the U-shaped plate body (201), and piston rods of the first electric push rods (203) are arranged on the upper surface of the first sliding block (204).
4. Unmanned aerial vehicle mapping device that takes photo by plane of claim 2, characterized in that: the lower surface of the square plate body (206) is rotatably connected to the upper surface of the second electric push rod (207) through a bearing, and a piston rod of the second electric push rod (207) is hinged to the upper surface of the camera surveying and mapping head (208) through a pin shaft.
5. Unmanned aerial vehicle mapping device that takes photo by plane of claim 2, characterized in that: two first dynamic balance calibration blocks (5) are symmetrically installed on the lower surface of the square through hole plate body (205), and two second dynamic balance calibration blocks (6) are symmetrically installed on the lower surface of the square plate body (206).
6. Unmanned aerial vehicle mapping device that takes photo by plane of claim 1, characterized in that: the flight mapping assembly (1) comprises a mapping fuselage (101), a connecting plate body (102), flight fan blades (103) and a streamline-shaped plate body (104);
the four connecting plate bodies (102) are arranged in total, one adjacent sides of the four connecting plate bodies (102) are symmetrically arranged on the outer side wall of the surveying and mapping machine body (101), the four flying fan blades (103) are arranged in total, and the lower surfaces of the four flying fan blades (103) are arranged on the upper surfaces of the four connecting plate bodies (102).
7. Unmanned aerial vehicle mapping device that takes photo by plane of claim 6, characterized in that: the upper surface of the surveying and mapping machine body (101) is arranged on the lower surface of the streamline plate body (104).
8. Unmanned aerial vehicle mapping device that takes photo by plane of claim 1, characterized in that: the shock absorption assembly (3) comprises a circular cylinder (301), a circular rod body (302), a spring (303) and a rubber pad (304);
circular cylinder (301) set up four altogether, and the lower surface in four connection plate bodies (102) is installed on the top of four circular cylinder (301), and the inside wall laminating of circular cylinder (301) is in the lateral wall of the circular body of rod (302), and the upper surface in rubber pad (304) is installed to the bottom of the circular body of rod (302), and the bottom in spring (303) is installed on the top of the circular body of rod (302), and the lower surface in connection plate body (102) is installed to the bottom of spring (303).
9. Unmanned aerial vehicle mapping device that takes photo by plane of claim 8, characterized in that: four second chutes (7) are symmetrically arranged on the inner side wall of the circular cylinder body (301), the inner side wall of each second chute (7) is connected with a second sliding block (8) in a sliding mode, and one side, adjacent to each other, of each second sliding block (8) is symmetrically arranged on the outer side wall of the circular rod body (302).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN202210392512.1A CN114572411A (en) | 2022-04-15 | 2022-04-15 | Unmanned aerial vehicle mapping device that takes photo by plane |
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| Application Number | Priority Date | Filing Date | Title |
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| CN202210392512.1A CN114572411A (en) | 2022-04-15 | 2022-04-15 | Unmanned aerial vehicle mapping device that takes photo by plane |
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| CN202210392512.1A Pending CN114572411A (en) | 2022-04-15 | 2022-04-15 | Unmanned aerial vehicle mapping device that takes photo by plane |
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Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106892095A (en) * | 2017-02-21 | 2017-06-27 | 宿州瑞丰农业科技有限公司 | A kind of many rotor plant protection unmanned planes |
| CN206900674U (en) * | 2017-06-05 | 2018-01-19 | 北京凌云智信科技有限公司 | A kind of gyroplane remote sensing system |
| KR101932929B1 (en) * | 2018-04-18 | 2018-12-27 | (주)더모스트 | Unmanned aerial vehicle for image shooting of surveying coast |
| CN209112436U (en) * | 2018-09-07 | 2019-07-16 | 广东诚进科技股份有限公司 | A kind of police unmanned plane big data acquisition device |
| CN211543925U (en) * | 2020-04-09 | 2020-09-22 | 海南迪奥普科技有限公司 | A camera for unmanned aerial vehicle flight survey and drawing |
| CN212195955U (en) * | 2020-05-09 | 2020-12-22 | 广西秀山水勘测设计有限公司 | But angle regulation's remote sensing survey and drawing unmanned aerial vehicle |
| US20200407077A1 (en) * | 2018-01-10 | 2020-12-31 | Ford Global Technologies, Llc | Moveable mounting structure for uav |
| CN215514171U (en) * | 2021-07-26 | 2022-01-14 | 深圳市卓锐通电子有限公司 | Adjustable limit structure of surveying and mapping unmanned aerial vehicle camera |
| CN216154024U (en) * | 2021-09-09 | 2022-04-01 | 江慧萍 | Possesses folding remote sensing survey and drawing unmanned aerial vehicle of being convenient for to accomodate of intelligence |
-
2022
- 2022-04-15 CN CN202210392512.1A patent/CN114572411A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106892095A (en) * | 2017-02-21 | 2017-06-27 | 宿州瑞丰农业科技有限公司 | A kind of many rotor plant protection unmanned planes |
| CN206900674U (en) * | 2017-06-05 | 2018-01-19 | 北京凌云智信科技有限公司 | A kind of gyroplane remote sensing system |
| US20200407077A1 (en) * | 2018-01-10 | 2020-12-31 | Ford Global Technologies, Llc | Moveable mounting structure for uav |
| KR101932929B1 (en) * | 2018-04-18 | 2018-12-27 | (주)더모스트 | Unmanned aerial vehicle for image shooting of surveying coast |
| CN209112436U (en) * | 2018-09-07 | 2019-07-16 | 广东诚进科技股份有限公司 | A kind of police unmanned plane big data acquisition device |
| CN211543925U (en) * | 2020-04-09 | 2020-09-22 | 海南迪奥普科技有限公司 | A camera for unmanned aerial vehicle flight survey and drawing |
| CN212195955U (en) * | 2020-05-09 | 2020-12-22 | 广西秀山水勘测设计有限公司 | But angle regulation's remote sensing survey and drawing unmanned aerial vehicle |
| CN215514171U (en) * | 2021-07-26 | 2022-01-14 | 深圳市卓锐通电子有限公司 | Adjustable limit structure of surveying and mapping unmanned aerial vehicle camera |
| CN216154024U (en) * | 2021-09-09 | 2022-04-01 | 江慧萍 | Possesses folding remote sensing survey and drawing unmanned aerial vehicle of being convenient for to accomodate of intelligence |
Non-Patent Citations (1)
| Title |
|---|
| 孙毅: "《无人机驾驶员航空知识手册》", 中国民航出版社, pages: 218 - 220 * |
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