CN116750223A - Assembled unmanned aerial vehicle topography measuring device - Google Patents
Assembled unmanned aerial vehicle topography measuring device Download PDFInfo
- Publication number
- CN116750223A CN116750223A CN202310979953.6A CN202310979953A CN116750223A CN 116750223 A CN116750223 A CN 116750223A CN 202310979953 A CN202310979953 A CN 202310979953A CN 116750223 A CN116750223 A CN 116750223A
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- aerial vehicle
- unmanned aerial
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- box body
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- 238000012876 topography Methods 0.000 title claims abstract description 16
- 238000013016 damping Methods 0.000 claims abstract description 28
- 230000007246 mechanism Effects 0.000 claims abstract description 26
- 238000004140 cleaning Methods 0.000 claims abstract description 11
- 230000004224 protection Effects 0.000 claims abstract description 6
- 238000005507 spraying Methods 0.000 claims description 12
- 238000005259 measurement Methods 0.000 claims description 11
- 238000005286 illumination Methods 0.000 claims description 6
- 239000007921 spray Substances 0.000 claims description 4
- 238000013507 mapping Methods 0.000 abstract description 8
- 238000007667 floating Methods 0.000 abstract description 5
- 230000009471 action Effects 0.000 abstract description 2
- 238000013461 design Methods 0.000 description 4
- 239000007788 liquid Substances 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 3
- 229920003023 plastic Polymers 0.000 description 3
- 239000004033 plastic Substances 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 239000006260 foam Substances 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000009979 protective mechanism Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/30—Constructional aspects of UAVs for safety, e.g. with frangible components
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B08—CLEANING
- B08B—CLEANING IN GENERAL; PREVENTION OF FOULING IN GENERAL
- B08B3/00—Cleaning by methods involving the use or presence of liquid or steam
- B08B3/02—Cleaning by the force of jets or sprays
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
- B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/80—Arrangement of on-board electronics, e.g. avionics systems or wiring
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/80—Arrangement of on-board electronics, e.g. avionics systems or wiring
- B64U20/87—Mounting of imaging devices, e.g. mounting of gimbals
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U60/00—Undercarriages
- B64U60/10—Undercarriages specially adapted for use on water
-
- 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
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
- B64U2101/32—UAVs specially adapted for particular uses or applications for imaging, photography or videography for cartography or topography
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Catching Or Destruction (AREA)
Abstract
The invention discloses an assembled unmanned aerial vehicle topography measuring device, which relates to the technical field of mapping equipment, and comprises a main body mechanism, a control box and a control box, wherein the main body mechanism comprises an unmanned aerial vehicle box body and a wireless signal receiving and transmitting control box; the mounting mechanism comprises a groove box arranged on the upper surface of the unmanned aerial vehicle box body; the protection mechanism comprises an electric telescopic rod arranged on the lower surface of the unmanned aerial vehicle box body; the cleaning mechanism comprises a rotating plate arranged above the camera. According to the assembled unmanned aerial vehicle terrain measuring device, air is infused into the air bag through the action of the air pump and the hose, so that the air bag is further expanded and enlarged, wherein the air bag extrudes the supporting hooks by utilizing the characteristic that the damping rotary drum is rotationally connected to the outer surface of the damping shaft rod, and then when the air bag is expanded, the damping rotary drum rotates relative to the damping shaft rod, so that the air bag is conveniently separated from the inside of the constraint housing to be expanded, the inflatable air bag is utilized to play a floating role, and the unmanned aerial vehicle device is prevented from falling into a river.
Description
Technical Field
The invention relates to the technical field of surveying and mapping equipment, in particular to an assembled unmanned aerial vehicle terrain measuring device.
Background
The topographic mapping refers to the operation of mapping topographic map, namely, the projection position and elevation of the ground object and the topography on the horizontal plane of the earth surface are measured, and the operation of drawing the topographic map by using symbols and marks is reduced according to a certain proportion, the topographic map is basically mapped by adopting an aerial photogrammetry method, the aerial photo is mainly used for indoor mapping, the advanced digital aerial photogrammetry technology is widely applied in the mapping geographic information industry along with the continuous development of science and technology, the topographic mapping industry of China also has great progress in the unmanned aerial vehicle field, and the unmanned aerial vehicle aerial photogrammetry system is also vigorously developed.
Through retrieving, bulletin number (CN 210133287U) an assembled unmanned aerial vehicle that topography survey and drawing was used relates to mapping equipment technical field, and this assembled unmanned aerial vehicle that topography survey and drawing was used includes the fixed plate, the outside fixedly connected with support frame of fixed plate, the bottom edge fixedly connected with kickboard of fixed plate, the kickboard includes outer, foam inlayer, fixed screw and set screw one of plastics, the outer inside of plastics is provided with the foam inlayer, fixed screw has been seted up to the outer inside of plastics, peg graft in the inside of fixed screw has set screw. The assembled unmanned aerial vehicle that this topography survey and drawing was used, through the setting of kickboard, can effectively prevent that the phenomenon that causes unmanned aerial vehicle to sink into the aquatic because unmanned aerial vehicle trouble or improper operation caused the river to drop when surveying and drawing the river basin area produces, and then causes measuring machine and data loss, makes the device effectively improve the security performance, strengthens the result of use of device.
The device has the following defects in the specific use process: (1) The device has the advantages that the floating plate is arranged, so that the phenomenon that the unmanned aerial vehicle falls into water when the unmanned aerial vehicle is mapped on a river basin area due to faults or improper operation is prevented, however, in a specific use process, the unmanned aerial vehicle can further generate additional resistance when flying due to the fact that the floating plate is arranged, and the flying stability of the unmanned aerial vehicle is reduced; (2) When the unmanned aerial vehicle body rises to the high altitude, dust and dirt can be attached to the surface of the camera lens in the process of carrying out camera measurement by the unmanned aerial vehicle due to large variation difference of high air flow, so that a camera picture blurring phenomenon can be caused; (3) the above-mentioned apparatus is inconvenient for carrying out measurement work at night.
Disclosure of Invention
The invention aims to provide an assembled unmanned aerial vehicle terrain measuring device, which aims to solve the problems in the background technology.
In order to solve the problems, the technical scheme adopted by the invention is as follows:
an assembled unmanned aerial vehicle topography measuring device, include
The main body mechanism comprises an unmanned aerial vehicle box body and a wireless signal receiving and transmitting control box, wherein one side surface of the wireless signal receiving and transmitting control box is fixedly connected with one side surface of the unmanned aerial vehicle box body, one side of the unmanned aerial vehicle box body is provided with an illumination assembly, a camera is arranged below the illumination assembly, one side surface of the unmanned aerial vehicle box body is provided with a mounting slot hole, and one end of the camera is connected with the mounting slot hole;
the mounting mechanism comprises a groove box arranged on the upper surface of the unmanned aerial vehicle box body, an inserting block is inserted and connected in the groove box, a soft lamp strip is fixedly connected to the upper surface of the inserting block, and a plurality of LED lighting lamp holders are mounted in the soft lamp strip;
the protection mechanism comprises an electric telescopic rod arranged on the lower surface of the unmanned aerial vehicle box body, one end of the electric telescopic rod is fixedly connected with a constraint housing, an air bag is arranged in the constraint housing, the outer surface of the air bag is fixedly connected with the inner surface of the constraint housing through a plurality of connecting blocks, and a supporting component is arranged below the air bag;
the cleaning mechanism comprises a rotating plate arranged above the camera, a spraying pipe is fixedly connected to the lower surface of the rotating plate, a storage box is fixedly connected to the upper surface of the rotating plate, and a box cover is arranged on the upper surface of the storage box.
Preferably, the lighting assembly comprises a power supply box, the lower surface of the power supply box is fixedly connected with the upper surface of the unmanned aerial vehicle box body, a front lamp is movably connected inside the power supply box, a plurality of wings are rotatably connected to two sides of the unmanned aerial vehicle box body, and a grounding frame is fixedly connected to the lower surface of the unmanned aerial vehicle box body.
Preferably, a fixing bolt is arranged on one side of the groove box, a first internal thread notch is formed in one side surface of the groove box, a second internal thread notch is formed in one side surface of the insertion block, and one end of the fixing bolt penetrates through the first internal thread notch to be in rotary fit with the second internal thread notch.
Preferably, the constraint housing top is equipped with the subassembly of aerifing, the subassembly of aerifing includes air pump and hose, constraint housing external surface fixedly connected with layer board, air pump surface and layer board upper surface fixed connection, hose one end is connected with air pump one end, gasbag one side intercommunication has the pipe, the hose is kept away from the one end and is connected with the pipe cartridge of air pump.
Preferably, the support assembly comprises a fixing plate, a damping shaft rod, a damping rotary drum and a supporting hook, wherein one side surface of each fixing plate is fixedly connected with the inner surface of the constraint housing, two ends of each damping shaft rod are respectively fixedly connected with one side surface of each fixing plate, the damping rotary drum is rotationally connected to the outer surface of the damping shaft rod, and one end of the supporting hook is fixedly connected with the outer surface of the damping rotary drum.
Preferably, the surface of one side of the storage box is communicated with a first drainage tube, the upper surface of the rotating plate is fixedly connected with a pump, one end of the first drainage tube is communicated with the outside of the pump, one end of the pump is provided with a second drainage tube, and one end of the second drainage tube is communicated with the outer surface of the spraying tube.
Preferably, unmanned aerial vehicle box body one side is equipped with drive assembly, drive assembly includes motor and pivot, unmanned aerial vehicle box body one side fixed surface is connected with the diaphragm, motor one side surface and diaphragm one side fixed surface are connected, motor one end is equipped with the main shaft, pivot surface and rotation plate one side fixed surface are connected, main shaft one end and pivot one end fixed connection.
Compared with the prior art, the invention has the following beneficial effects:
according to the invention, the air pump and the hose are used for injecting air into the air bag, so that the air bag is further expanded, wherein the air bag is expanded, and then when the air bag is expanded, the air bag extrudes the supporting hooks, so that the damping rotary drum rotates relative to the damping shaft rod, the air bag is conveniently separated from the inside of the constraint housing to be expanded, the inflatable air bag is used for playing a floating role, and the unmanned aerial vehicle device is prevented from falling into a river.
According to the invention, the motor is utilized to drive the main shaft and the rotating shaft to rotate, so that the positions of the rotating plate and the spraying pipe are convenient to adjust, one end of the spraying pipe faces the surface of the camera lens, the pump is further driven, the cleaning liquid in the storage box is conveyed into the spraying pipe through the first drainage pipe and the second drainage pipe by the pump, the cleaning liquid is conveniently sprayed to the surface of the camera lens by the spraying pipe for cleaning, and the structural design is humanized.
According to the invention, a worker uses the characteristic that one end of the fixing bolt penetrates through the first internal thread notch and the second internal thread notch to be in rotary fit, then uses the insert block in the groove box to fix the one end of the fixing bolt through the rotary fixing bolt, so that the insert block is prevented from being separated from the groove box, the assembly work of the mounting mechanism is completed, the soft lamp strip and the unmanned aerial vehicle box body are assembled conveniently, the LED lighting lamp cap in the soft lamp strip is used for warning and lighting at night conveniently, and the structural design is humanized.
Drawings
FIG. 1 is a schematic view of the external overall structure of an assembled unmanned aerial vehicle terrain measuring device;
fig. 2 is a schematic structural diagram of a main body mechanism of an assembled unmanned aerial vehicle terrain measuring device;
fig. 3 is a schematic front view of an assembled unmanned aerial vehicle terrain measuring device;
fig. 4 is a schematic view of a first view angle structure of a protection mechanism of an assembled unmanned aerial vehicle terrain measurement device;
fig. 5 is a schematic view of a second view angle structure of a protection mechanism of an assembled unmanned aerial vehicle terrain measurement device;
FIG. 6 is an enlarged view of a portion of the assembled unmanned aerial vehicle terrain measuring device at A in FIG. 5;
fig. 7 is an enlarged view of part B of fig. 3 of an assembled unmanned aerial vehicle topography measuring device.
In the figure: 100. a main body mechanism; 101. the unmanned aerial vehicle box body; 102. a wireless signal receiving and transmitting control box; 103. a camera; 104. a power supply box; 105. a head lamp; 106. a wing; 107. a grounding frame; 200. a mounting mechanism; 201. a slot box; 202. inserting blocks; 203. soft lamp strip; 204. a fixing bolt; 300. a protective mechanism; 301. an electric telescopic rod; 302. a constraining enclosure; 303. an air bag; 304. an air pump; 305. a hose; 306. a supporting plate; 307. a round tube; 308. a fixing plate; 309. damping shaft lever; 310. a damping drum; 311. a supporting hook; 400. a cleaning mechanism; 401. a rotating plate; 402. a spray tube; 403. a storage box; 404. a first drainage tube; 405. a pump machine; 406. a second drainage tube; 407. a motor; 408. a rotating shaft; 409. and a transverse plate.
Detailed Description
The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
Embodiment one:
referring to FIGS. 1-7, the present invention is an assembled unmanned aerial vehicle terrain measuring device, comprising
The main body mechanism 100 comprises an unmanned aerial vehicle box body 101 and a wireless signal receiving and transmitting control box 102, wherein one side surface of the wireless signal receiving and transmitting control box 102 is fixedly connected with one side surface of the unmanned aerial vehicle box body 101, one side of the unmanned aerial vehicle box body 101 is provided with a lighting assembly, a camera 103 is arranged below the lighting assembly, one side surface of the unmanned aerial vehicle box body 101 is provided with a mounting slot hole, and one end of the camera 103 is connected with the mounting slot hole;
the mounting mechanism 200 comprises a groove box 201 arranged on the upper surface of the unmanned aerial vehicle box body 101, an inserting block 202 is inserted and connected in the groove box 201, a soft lamp strip 203 is fixedly connected to the upper surface of the inserting block 202, and a plurality of LED lighting lamp holders are mounted in the soft lamp strip 203;
the protection mechanism 300 comprises an electric telescopic rod 301 arranged on the lower surface of the unmanned aerial vehicle box body 101, a constraint housing 302 is fixedly connected to one end of the electric telescopic rod 301, an air bag 303 is arranged in the constraint housing 302, the outer surface of the air bag 303 is fixedly connected with the inner surface of the constraint housing 302 through a plurality of connecting blocks, and a supporting component is arranged below the air bag 303;
the cleaning mechanism 400 comprises a rotating plate 401 arranged above the camera 103, a spraying pipe 402 is fixedly connected to the lower surface of the rotating plate 401, a storage box 403 is fixedly connected to the upper surface of the rotating plate 401, and a box cover is arranged on the upper surface of the storage box 403.
As can be seen from fig. 1 and 3, a fixing bolt 204 is disposed on one side of the slot box 201, a first internal thread slot is disposed on one side surface of the slot box 201, a second internal thread slot is disposed on one side surface of the insert block 202, and one end of the fixing bolt 204 passes through the first internal thread slot and is rotationally matched with the second internal thread slot.
From the above, during the use, the staff is connected with the characteristic of inserted block 202 through utilizing the inside cartridge 201 to insert, then insert the inserted block 202 and cartridge 201 to be connected, after the grafting, further the staff passes first internal thread notch and second internal thread notch swivelling fit's characteristic through utilizing fixing bolt 204 one end, then utilize fixing bolt 204 one end to fix with the inside inserted block 202 of cartridge 201 through rotatory fixing bolt 204, prevent the separation of inserted block 202 and cartridge 201, accomplish the equipment work of installation mechanism 200, be convenient for assemble soft lamp strip 203 and unmanned aerial vehicle box 101, be convenient for utilize the inside LED lighting lamp holder of soft lamp strip 203 to play night warning and illumination effect, structural design is humanized.
Specifically, regarding the main body mechanism 100, referring to fig. 1 and 2, the lighting assembly includes a power box 104, the lower surface of the power box 104 is fixedly connected with the upper surface of the unmanned aerial vehicle box 101, the inside of the power box 104 is movably connected with a headlight 105, both sides of the unmanned aerial vehicle box 101 are rotatably connected with a plurality of wings 106, and the lower surface of the unmanned aerial vehicle box 101 is fixedly connected with a grounding frame 107.
From the above, during the use, the staff rotates and opens unmanned aerial vehicle box body 101 both sides wing 106, utilizes wireless signal to send out control box 102 long-range drive unmanned aerial vehicle to fly afterwards, when unmanned aerial vehicle device risees to the high altitude, makes a video recording the ground through camera 103, is convenient for expand measurement work, wherein, power supply box 104 inside swing joint has head lamp 105, and power supply box 104 is provided with the head lamp 105 through the power supply, is convenient for utilize head lamp 105 to play the illumination effect.
Embodiment two:
referring to fig. 1, fig. 4, fig. 5 and fig. 6, an inflation assembly is arranged above the constraint housing 302, the inflation assembly comprises an air pump 304 and a hose 305, a supporting plate 306 is fixedly connected to the outer surface of the constraint housing 302, the outer surface of the air pump 304 is fixedly connected with the upper surface of the supporting plate 306, one end of the hose 305 is connected with one end of the air pump 304, one side of the air bag 303 is communicated with a circular tube 307, and one end, far away from the air pump 304, of the hose 305 is connected with the circular tube 307 in an inserting manner.
The support assembly comprises a fixed plate 308, a damping shaft rod 309, a damping rotary drum 310 and a supporting hook 311, wherein one side surface of the two fixed plates 308 is fixedly connected with the inner surface of the constraint housing 302, two ends of the damping shaft rod 309 are respectively fixedly connected with one side surface of the two fixed plates 308, the damping rotary drum 310 is rotationally connected to the outer surface of the damping shaft rod 309, and one end of the supporting hook 311 is fixedly connected with the outer surface of the damping rotary drum 310.
It can be seen from the above that, when the unmanned aerial vehicle is about to fall into a river, at this time, the worker transmits a signal to the wireless signal receiving and transmitting control box 102 remotely, and further drives the air pump 304 by the wireless signal receiving and transmitting control box 102, and infuses air into the air bag 303 through the action of the air pump 304 and the hose 305, so that the air bag 303 is further expanded, wherein the air bag 303 is further expanded, and then when the air bag 303 is expanded, the air bag 303 presses the supporting hooks 311, so that the damping drum 310 rotates relative to the damping shaft 309, the air bag 303 is conveniently unfolded from the inside of the constraint housing 302, the air bag 303 plays a floating role, and the unmanned aerial vehicle device is prevented from falling into the river.
Embodiment III:
referring to fig. 1, 3 and 7, a first drainage tube 404 is communicated with one side surface of the storage box 403, a pump 405 is fixedly connected with the upper surface of the rotating plate 401, one end of the first drainage tube 404 is communicated with the outside of the pump 405, a second drainage tube 406 is arranged at one end of the pump 405, and one end of the second drainage tube 406 is communicated with the outer surface of the spray tube 402.
The unmanned aerial vehicle box 101 one side is equipped with drive assembly, and drive assembly includes motor 407 and pivot 408, and unmanned aerial vehicle box 101 one side surface fixed connection has diaphragm 409, and motor 407 one side surface and diaphragm 409 one side surface fixed connection, motor 407 one end are equipped with the main shaft, pivot 408 surface and pivot 401 one side surface fixed connection, main shaft one end and pivot 408 one end fixed connection.
It is known from the above that, when the dirt is attached to the surface of the lens of the camera 103, at this time, the worker uses the remote transmitting signal to drive the motor 407 for the wireless signal receiving and transmitting control box 102, and further uses the wireless signal receiving and transmitting control box 102 to drive the motor 407, and uses the motor 407 to drive the spindle and the rotating shaft 408 to rotate, so as to facilitate adjusting the rotation plate 401 and the direction of the spraying tube 402, so that one end of the spraying tube 402 faces the surface of the lens of the camera 103, further drives the pump 405, uses the pump 405 to convey the cleaning liquid in the storage box 403 to the spraying tube 402 through the first drainage tube 404 and the second drainage tube 406, and is convenient to spray the cleaning liquid to the surface of the lens of the camera 103 for cleaning by using the spraying tube 402, and the structural design is humanized.
Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. Assembled unmanned aerial vehicle topography measuring device, its characterized in that: comprising
The main body mechanism (100) comprises an unmanned aerial vehicle box body (101) and a wireless signal receiving and transmitting control box (102), wherein one side surface of the wireless signal receiving and transmitting control box (102) is fixedly connected with one side surface of the unmanned aerial vehicle box body (101), an illumination assembly is arranged on one side of the unmanned aerial vehicle box body (101), a camera (103) is arranged below the illumination assembly, a mounting slot hole is formed in one side surface of the unmanned aerial vehicle box body (101), and one end of the camera (103) is connected with the mounting slot hole;
the mounting mechanism (200) comprises a groove box (201) arranged on the upper surface of the unmanned aerial vehicle box body (101), an inserting block (202) is inserted and connected in the groove box (201), a soft lamp strip (203) is fixedly connected to the upper surface of the inserting block (202), and a plurality of LED lighting lamp holders are mounted in the soft lamp strip (203);
the protection mechanism (300) comprises an electric telescopic rod (301) arranged on the lower surface of the unmanned aerial vehicle box body (101), one end of the electric telescopic rod (301) is fixedly connected with a constraint housing (302), an air bag (303) is arranged in the constraint housing (302), the outer surface of the air bag (303) is fixedly connected with the inner surface of the constraint housing (302) through a plurality of connecting blocks, and a supporting component is arranged below the air bag (303);
the cleaning mechanism (400) comprises a rotating plate (401) arranged above a camera (103), a spraying pipe (402) is fixedly connected to the lower surface of the rotating plate (401), a storage box (403) is fixedly connected to the upper surface of the rotating plate (401), and a box cover is arranged on the upper surface of the storage box (403).
2. The assembled unmanned aerial vehicle topography measurement device of claim 1, wherein: the illuminating assembly comprises a power supply box (104), the lower surface of the power supply box (104) is fixedly connected with the upper surface of an unmanned aerial vehicle box body (101), a head lamp (105) is movably connected inside the power supply box (104), a plurality of wings (106) are rotatably connected to two sides of the unmanned aerial vehicle box body (101), and a grounding frame (107) is fixedly connected to the lower surface of the unmanned aerial vehicle box body (101).
3. The assembled unmanned aerial vehicle topography measurement device of claim 1, wherein: the fixed bolt is arranged on one side of the groove box (201), a first internal thread notch is formed in the surface of one side of the groove box (201), a second internal thread notch is formed in the surface of one side of the insert block (202), and one end of the fixed bolt (204) penetrates through the first internal thread notch and is in rotary fit with the second internal thread notch.
4. The assembled unmanned aerial vehicle topography measurement device of claim 1, wherein: the utility model discloses a restraint housing, including air pump (304), hose (305), restraint housing (302) surface fixedly connected with layer board (306), air pump (304) surface and layer board (306) upper surface fixed connection, hose (305) one end is connected with air pump (304) one end, gasbag (303) one side intercommunication has pipe (307), the one end that air pump (304) was kept away from to hose (305) is connected with pipe (307) cartridge.
5. The assembled unmanned aerial vehicle topography measurement device of claim 1, wherein: the support assembly comprises fixing plates (308), damping shaft rods (309), damping rotating cylinders (310) and supporting hooks (311), wherein one side surfaces of the fixing plates (308) are fixedly connected with the inner surface of the constraint housing (302), two ends of each damping shaft rod (309) are fixedly connected with one side surface of each fixing plate (308), the damping rotating cylinders (310) are rotationally connected to the outer surfaces of the damping shaft rods (309), and one ends of the supporting hooks (311) are fixedly connected with the outer surfaces of the damping rotating cylinders (310).
6. The assembled unmanned aerial vehicle topography measurement device of claim 1, wherein: the storage box (403) one side surface intercommunication has first drainage tube (404), fixed surface is connected with pump machine (405) on rotating plate (401), first drainage tube (404) one end and the outside intercommunication of pump machine (405), pump machine (405) one end is equipped with second drainage tube (406), second drainage tube (406) one end and spray tube (402) surface intercommunication.
7. The assembled unmanned aerial vehicle topography measurement device of claim 1, wherein: the unmanned aerial vehicle box body (101) one side is equipped with drive assembly, drive assembly includes motor (407) and pivot (408), unmanned aerial vehicle box body (101) one side fixed surface is connected with diaphragm (409), motor (407) one side surface and diaphragm (409) one side fixed surface are connected, motor (407) one end is equipped with the main shaft, pivot (408) surface and pivot (401) one side fixed surface are connected, main shaft one end and pivot (408) one end fixed surface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310979953.6A CN116750223A (en) | 2023-08-04 | 2023-08-04 | Assembled unmanned aerial vehicle topography measuring device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202310979953.6A CN116750223A (en) | 2023-08-04 | 2023-08-04 | Assembled unmanned aerial vehicle topography measuring device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN116750223A true CN116750223A (en) | 2023-09-15 |
Family
ID=87948083
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202310979953.6A Withdrawn CN116750223A (en) | 2023-08-04 | 2023-08-04 | Assembled unmanned aerial vehicle topography measuring device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN116750223A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117775335A (en) * | 2024-02-27 | 2024-03-29 | 利华兴业(大连)新能源有限公司 | Unmanned aerial vehicle panorama camera device |
-
2023
- 2023-08-04 CN CN202310979953.6A patent/CN116750223A/en not_active Withdrawn
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117775335A (en) * | 2024-02-27 | 2024-03-29 | 利华兴业(大连)新能源有限公司 | Unmanned aerial vehicle panorama camera device |
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| WW01 | Invention patent application withdrawn after publication |