CN114604425B - Three-dimensional low-altitude navigation chart inspection device for unmanned aerial vehicle inspection - Google Patents
Three-dimensional low-altitude navigation chart inspection device for unmanned aerial vehicle inspection Download PDFInfo
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- CN114604425B CN114604425B CN202210148724.5A CN202210148724A CN114604425B CN 114604425 B CN114604425 B CN 114604425B CN 202210148724 A CN202210148724 A CN 202210148724A CN 114604425 B CN114604425 B CN 114604425B
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- Prior art keywords
- strip
- aerial vehicle
- unmanned aerial
- wiper
- panoramic camera
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- 238000007689 inspection Methods 0.000 title claims abstract description 44
- 239000000523 sample Substances 0.000 claims abstract description 23
- 238000007790 scraping Methods 0.000 claims description 36
- 238000005192 partition Methods 0.000 claims description 18
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 18
- 239000003595 mist Substances 0.000 claims description 12
- 238000000034 method Methods 0.000 claims description 7
- 238000001816 cooling Methods 0.000 claims description 5
- 230000000694 effects Effects 0.000 claims description 5
- 230000005540 biological transmission Effects 0.000 claims description 3
- 238000003466 welding Methods 0.000 claims description 3
- 230000017525 heat dissipation Effects 0.000 claims description 2
- 230000002349 favourable effect Effects 0.000 description 6
- 238000010586 diagram Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 241000112598 Pseudoblennius percoides Species 0.000 description 1
- 239000000779 smoke Substances 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
Classifications
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- 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
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- B08B1/165—
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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
- 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
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- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Abstract
The invention discloses a three-dimensional low-altitude aerial image inspection device for unmanned aerial vehicle inspection, which structurally comprises an inspection probe, a vortex press, sliding wings and an unmanned aerial vehicle body, wherein the top end of the inspection probe is connected with the lower end of the front side of the unmanned aerial vehicle body in a nested manner, two sides of the unmanned aerial vehicle body are connected with the tops of the sliding wings in a welded manner, the lower surfaces of the sliding wings are fixed with the top end of the vortex press through bolts, the inner side of the vortex press is in clearance fit with the whole unmanned aerial vehicle body, the inspection probe comprises a wiper, a panoramic camera, a rotating rod and a conducting wire, the inner wall of the wiper is in clearance fit with the surface of the panoramic camera, and the top of the panoramic camera is fixedly connected with the tail end of the rotating rod in a nested manner.
Description
Technical Field
The invention relates to the field of aerial image inspection devices, in particular to a three-dimensional low-altitude aerial image inspection device for unmanned aerial vehicle inspection.
Background
The shipping industry in China is developed, so huge workload is realized, the best supervision effect is difficult to achieve by only carrying out patrol management on the shipping management ships and law enforcement vehicles, and the unmanned aerial vehicle can well supplement the defects of supervision work, so that the unmanned aerial vehicle has the characteristics of flexibility, safety and reliability, and plays an important role in the course patrol;
however, the following disadvantages exist in the prior art: a three-dimensional low altitude aerial image inspection device for unmanned aerial vehicle inspection is because to carrying out low altitude aerial image inspection to each big sea area for inspection probe can be because the refractive sea surface temperature of sun risees in the in-process of operation on the sea, accompanies sea air humidity simultaneously, and outer guard shield surface can form the water smoke under the high temperature that the probe was operated, leads to the probe to be covered by its fog pearl, and then causes three-dimensional aerial image to gather uncleanly.
Disclosure of Invention
Aiming at the defects existing in the prior art, the invention aims to provide a three-dimensional low-altitude aerial image inspection device for unmanned aerial vehicle inspection, so as to solve the problems that the three-dimensional aerial image is not collected clearly because the three-dimensional low-altitude aerial image inspection device for unmanned aerial vehicle inspection in the prior art performs low-altitude aerial image inspection on all sea areas, the temperature of the sea surface of the inspection probe is increased due to refraction of the sun in the process of operation on the sea surface, and water mist is formed on the surface of an outer shield under the high temperature of the operation of the probe along with the air humidity of the sea surface.
In order to achieve the above object, the present invention is realized by the following technical scheme: a three-dimensional low altitude map inspection device for unmanned aerial vehicle inspection, its structure includes inspection probe, scroll press, sliding wing, unmanned aerial vehicle body, inspection probe top and the nested connection of unmanned aerial vehicle body front side lower extreme, unmanned aerial vehicle body both sides and sliding wing top welded connection, sliding wing lower surface and scroll press top bolt fastening, scroll press inboard and the whole clearance fit of unmanned aerial vehicle body, inspection probe includes wiper, panoramic camera, dwang, conducting wire, wiper inner wall and panoramic camera surface movable fit, panoramic camera top and dwang terminal are inlayed fixedly and are connected, the inside whole nested connection of conducting wire of dwang, the conducting wire top is inlayed fixedly and is connected with the panoramic camera inside.
According to a further improvement of the invention, the wiper comprises a wiper strip, a connecting frame and a fixed sleeve ring, wherein the top of the wiper strip is hinged with the tail end of the connecting frame, the top end of the connecting frame is welded with the outer surface of the fixed sleeve ring, the lower end of the fixed sleeve ring is in integral clearance fit with the wiper strip, the whole fixed sleeve ring is in a ring shape, the inside of the fixed sleeve ring is in a hollowed-out shape, the two side surfaces of the fixed sleeve ring are welded with the top of the connecting frame, and the lower end of the fixed sleeve ring is in integral clearance fit with the wiper strip.
According to a further improvement, the wiper strip comprises a strip body, an anti-drop cap, a movable bolt and a spring strip, wherein the top of the strip body is integrally nested and connected with the movable bolt, the outer end of the movable bolt is integrally movably matched with the spring strip, the lower end of the spring strip is integrally clearance matched with the spring strip, the top of the spring strip is integrally clamped and connected with the anti-drop cap, the anti-drop cap is distributed at the top of the strip body, and the anti-drop cap mainly covers the movable bolt and the spring strip and prevents the movable bolt and the spring strip from being lost in the moving process.
The invention is further improved, the strip body comprises an inner cavity, rubber scraping strips and a pressure seat, wherein the inner wall of the inner cavity is fixedly connected with the tail end of the pressure seat in an embedded mode, the surface of the pressure seat is in movable fit with the inner wall of the rubber scraping strips, the inner sides of the rubber scraping strips are in clearance fit with the inner cavity, the four pressure seats are distributed on the surface of the inner wall of the inner cavity and are fixedly connected with the inner wall of the inner cavity in an embedded mode, and the top ends of the four pressure seats are in movable fit with the inner surface of the rubber scraping strips.
The panoramic camera comprises a partition cover, a fixing frame, an inner ring machine and a camera, wherein the partition cover, the inner part and two ends of the fixing frame are fixed through bolts, the lower end of the fixing frame is integrally clamped and connected with the inner ring machine, the inner part of the inner ring machine is integrally movably matched with the camera, the inner ring machine mainly provides the functions of data acquisition and transmission for the camera, and the camera is integrally embedded and fixed on the front end surface of the inner ring machine.
According to the invention, the partition cover comprises a circulation strip, an anti-moving fixing plate and a high-definition transparent plate, wherein the bottom of the circulation strip is fixedly connected with the top end of the high-definition transparent plate in an embedded mode, the inner side of the high-definition transparent plate is in clearance fit with the whole anti-moving fixing plate, the inner wall of the anti-moving fixing plate is connected with the inner wall of the circulation strip in a welding mode, two circulation strips are distributed on the left side and the right side of the top of the high-definition transparent plate and are fixedly connected with the top end of the high-definition transparent plate in an embedded mode, and the inner side of the circulation strip is connected with the inner wall of the anti-moving fixing plate in a welding mode.
The invention is further improved, the circulation strip comprises a wind guide block, a groove body, a limiting block and an outward expansion groove, wherein the inner side of the wind guide block is movably matched with the outward expansion groove integrally, two sides of the outward expansion groove are connected with the limiting block integrally in a clamping manner, the inner wall of the limiting block is fixedly connected with the inner side of the groove body in an embedded manner, the inner side of the groove body is connected with the wind guide block integrally in a clamping manner, the wind guide block is arc-shaped and is distributed in the groove body and fixedly connected with the inner side of the groove body in a embedding manner, and two sides of the wind guide block are connected with the limiting block in a clamping manner.
The invention is further improved, the wind guide block comprises a guide pipe, an air inlet and an outflow cavity, the top end of the guide pipe is fixedly connected with the outer side of the air inlet in a embedding way, the lower end of the air inlet is in clearance fit with the whole outflow cavity, the two sides of the top of the outflow cavity are fixedly connected with the tail end of the guide pipe in a embedding way, the whole guide pipe is in a C-shaped return pipe, the top end of the guide pipe is fixedly connected with the surface of the outer side of the air inlet, and the tail end of the guide pipe is fixedly connected with the side wall of the outflow cavity in a embedding way.
Advantageous effects
Compared with the prior art, the invention has the following beneficial effects;
1. according to the invention, the water mist formed on the partition cover is scraped through the scraping strip in clearance fit with the fixed loop bar, so that in the process of collecting the panoramic three-dimensional image of the panoramic camera through the rotating rod, the water mist on the partition cover is scraped through the rubber scraping strip on the inner wall of the matching strip body under the assistance of rotation, and the problem of unclear three-dimensional image collection caused by the fact that the probe is shielded by the water mist is effectively avoided.
2. According to the invention, the inner ring machine and the camera are protected through the partition cover, the air inlet is reduced under the cooperation of the flow bars, wind power diffused and guided at two sides of the air inlet enters from the reduced air inlet, the wind is conveyed from the outer expansion groove to the inside for cooling and heat dissipation by the cooperation of the C-shaped flow guide pipe, meanwhile, the air inlet is small, the flow is guided by the large flow rate as the internal heat, and meanwhile, the cooling effect is achieved, and the problem of fogging inside the shield is avoided.
Drawings
Fig. 1 is a schematic structural diagram of a three-dimensional low-altitude aerial image inspection device for unmanned aerial vehicle inspection.
Fig. 2 is a schematic diagram of the front view structure of the inspection probe of the present invention.
FIG. 3 is a schematic view showing the internal structure of the wiper of the present invention.
FIG. 4 is a schematic view of the internal structure of the wiper strip of the present invention.
Fig. 5 is a schematic view of the internal structure of the strip body of the present invention.
Fig. 6 is a schematic diagram of an internal structure of the panoramic camera of the present invention.
FIG. 7 is a schematic view showing the internal structure of the partition cover of the present invention.
Fig. 8 is a schematic view of the internal structure of the flow-through strip of the present invention.
FIG. 9 is a schematic view of the internal structure of the wind guiding block of the present invention.
In the figure: the inspection probe-1, the vortex press-2, the sliding wings-3, the unmanned body-4, the wiper-11, the panoramic camera-12, the rotating rod-13, the conducting wire-14, the wiper strip-111, the connecting frame-112, the fixed sleeve ring-113, the strip body-a 1, the anti-drop cap-a 2, the movable bolt-a 3, the spring strip-a 4, the inner cavity-a 11, the rubber wiper strip-a 12, the pressure seat-a 13, the partition cover-121, the fixed frame-122, the inner ring machine-123, the camera-124, the circulation strip-b 1, the anti-moving fixing plate-b 2, the high definition transparent plate-b 3, the wind guide block-b 11, the tank body-b 12, the limiting block-b 13, the outer expansion tank-b 14, the guide pipe-c 1, the air inlet-c 2 and the outflow cavity-c 3.
Detailed Description
The present invention now will be described more fully hereinafter with reference to the accompanying drawings, in which some, but not all embodiments of the invention are shown, and in which all other embodiments of the invention, based on which one skilled in the art may be obtained without making any inventive effort, are within the scope of the invention.
The invention is further described below with reference to the accompanying drawings:
example 1
As shown in fig. 1 to 5:
the structure of the intelligent inspection probe comprises an inspection probe 1, a vortex press 2, sliding wings 3 and an unmanned aerial vehicle body 4, wherein the top end of the inspection probe 1 is connected with the lower end of the front side of the unmanned aerial vehicle body 4 in a nested manner, two sides of the unmanned aerial vehicle body 4 are connected with the tops of the sliding wings 3 in a welded manner, the lower surfaces of the sliding wings 3 are fixed with the top ends of the vortex press 2 through bolts, the inner side of the vortex press 2 is in clearance fit with the whole unmanned aerial vehicle body 4, the inspection probe 1 comprises a wiper 11, a panoramic camera 12, a rotating rod 13 and a conducting wire 14, the inner wall of the wiper 11 is in movable fit with the surface of the panoramic camera 12, the top of the panoramic camera 12 is fixedly connected with the tail end of the rotating rod 13, the inside of the rotating rod 13 is fixedly connected with the conducting wire 14 in a whole nested manner, and the top end of the conducting wire 14 is fixedly connected with the inside of the panoramic camera 12.
The wiper 11 comprises a wiper strip 111, a connecting frame 112 and a fixed collar 113, wherein the top of the wiper strip 111 is hinged to the tail end of the connecting frame 112, the top end of the connecting frame 112 is welded to the outer surface of the fixed collar 113, the lower end of the fixed collar 113 is in clearance fit with the whole wiper strip 111, the whole circular ring shape of the fixed collar 113 is hollowed, the two side surfaces are welded to the top of the connecting frame 112, the lower end of the fixed collar 113 is in clearance fit with the whole wiper strip 111, the fixed collar 113 is favorable for fixing the wiper strip 111 at the lower end, the wiper strip is in an immovable state, and corresponding operation is further carried out on the inner surface of the wiper strip.
The scraping strip 111 comprises a strip body a1, an anti-drop cap a2, a movable bolt a3 and a spring strip a4, wherein the top of the strip body a1 is integrally nested and connected with the movable bolt a3, the outer end of the movable bolt a3 is integrally movably matched with the spring strip a4, the lower end of the spring strip a4 is integrally clearance matched with the spring strip a4, the top end of the spring strip a4 is integrally clamped and connected with the anti-drop cap a2, the anti-drop cap a2 is distributed at the top end of the strip body a1 and mainly covers the movable bolt a3 and the spring strip a4 to prevent the strip body a1 from being lost in the moving process, and the movable bolt a3 and the spring strip a4 are favorable for carrying out angle adjustment under the matching so that the strip body is more attached to the surface of a camera outer cover, and water drops on the outer cover are wiped.
The strip body a1 comprises an inner cavity a11, a rubber scraping strip a12 and a pressure seat a13, wherein the inner wall of the inner cavity a11 is fixedly connected with the tail end of the pressure seat a13 in a embedding mode, the surface of the pressure seat a13 is in clearance fit with the inner wall of the rubber scraping strip a12, the inner side of the rubber scraping strip a12 is in clearance fit with the inner cavity a11, four pressure seats a13 are arranged on the surface of the inner wall of the inner cavity a11 and are fixedly connected with the inner wall of the inner cavity a11 in a embedding mode, the top end of the pressure seat a13 is in movable fit with the inner surface of the rubber scraping strip a12, the rubber scraping strip a12 is favorable for scraping with the surface of an outer cover under the cooperation of the inner cavity a11 and the pressure seat a13, and meanwhile, jacking and depressurization are made through the cooperation of an inner structure, so that the problem that water drops on the outer cover are not cleaned and the outer cover are avoided.
The specific working principle is as follows:
according to the invention, the unmanned aerial vehicle body 4 is driven to fly through the vortex compressor 2, so that the unmanned aerial vehicle body flies to a specified aviation line under the cooperation of the sliding wings 3 to carry out inspection, then three-dimensional images of the unmanned aerial vehicle body are collected by the inspection probe 1, the images of the panoramic camera 12 are transmitted to a terminal through the cooperation of the transmission line, when the unmanned aerial vehicle body flies to the sea area, the sea level temperature of the unmanned aerial vehicle body rises due to refraction of sunlight, and a factor of high humidity is added, so that water mist appears on the partition cover 121 at the outer end of the panoramic camera 12, in order to ensure the high-definition performance of three-dimensional image collection, the wiper 11 which is nested and fixed on the rotating rod 13 is attached to the surface of the partition cover 121, so that the rotating rod 13 is matched with the wiper strip 111 at the outer end of the fixed lantern ring 113 in the auxiliary panoramic camera 12 to scrape the surface of the cover, the movable bolt a3 at the inner side of the anti-release cap a2 is matched with the spring strip a4, the rubber wiper strip body a1 is attached to the surface of the cover, and the rubber wiper strip a12 is attached to the rubber wiper strip a12, so that the water mist is prevented from being attached to the inner wall of the cover 12, and the water mist is prevented from being formed in the process of rotating the auxiliary panoramic camera 12, and the rotating rod is prevented from being matched with the rotating to the wiper strip 121, and the water mist is prevented from being attached to the inner wall of the upper part of the wiper strip and the wiper strip to be attached to the 3.
Example 2:
as shown in fig. 6 to 9:
the strip body a1 comprises an inner cavity a11, a rubber scraping strip a12 and a pressure seat a13, wherein the inner wall of the inner cavity a11 is fixedly connected with the tail end of the pressure seat a13 in a embedding mode, the surface of the pressure seat a13 is in clearance fit with the inner wall of the rubber scraping strip a12, the inner side of the rubber scraping strip a12 is in clearance fit with the inner cavity a11, four pressure seats a13 are arranged on the surface of the inner wall of the inner cavity a11 and are fixedly connected with the inner wall of the inner cavity a11 in a embedding mode, the top end of the pressure seat a13 is in movable fit with the inner surface of the rubber scraping strip a12, the rubber scraping strip a12 is favorable for scraping with the surface of an outer cover under the cooperation of the inner cavity a11 and the pressure seat a13, and meanwhile, jacking and depressurization are made through the cooperation of an inner structure, so that the problem that water drops on the outer cover are not cleaned and the outer cover are avoided.
The strip body a1 comprises an inner cavity a11, a rubber scraping strip a12 and a pressure seat a13, wherein the inner wall of the inner cavity a11 is fixedly connected with the tail end of the pressure seat a13 in a embedding mode, the surface of the pressure seat a13 is in clearance fit with the inner wall of the rubber scraping strip a12, the inner side of the rubber scraping strip a12 is in clearance fit with the inner cavity a11, four pressure seats a13 are arranged on the surface of the inner wall of the inner cavity a11 and are fixedly connected with the inner wall of the inner cavity a11 in a embedding mode, the top end of the pressure seat a13 is in movable fit with the inner surface of the rubber scraping strip a12, the rubber scraping strip a12 is favorable for scraping with the surface of an outer cover under the cooperation of the inner cavity a11 and the pressure seat a13, and meanwhile, jacking and depressurization are made through the cooperation of an inner structure, so that the problem that water drops on the outer cover are not cleaned and the outer cover are avoided.
The strip body a1 comprises an inner cavity a11, a rubber scraping strip a12 and a pressure seat a13, wherein the inner wall of the inner cavity a11 is fixedly connected with the tail end of the pressure seat a13 in a embedding mode, the surface of the pressure seat a13 is in clearance fit with the inner wall of the rubber scraping strip a12, the inner side of the rubber scraping strip a12 is in clearance fit with the inner cavity a11, four pressure seats a13 are arranged on the surface of the inner wall of the inner cavity a11 and are fixedly connected with the inner wall of the inner cavity a11 in a embedding mode, the top end of the pressure seat a13 is in movable fit with the inner surface of the rubber scraping strip a12, the rubber scraping strip a12 is favorable for scraping with the surface of an outer cover under the cooperation of the inner cavity a11 and the pressure seat a13, and meanwhile, jacking and depressurization are made through the cooperation of an inner structure, so that the problem that water drops on the outer cover are not cleaned and the outer cover are avoided.
The wind guide block b11 comprises a guide pipe C1, an air inlet C2 and an outflow cavity C3, wherein the top end of the guide pipe C1 is fixedly connected with the outer side of the air inlet C2 in a embedding mode, the lower end of the air inlet C2 is in clearance fit with the outer side of the outflow cavity C3, two sides of the top of the outflow cavity C3 are fixedly connected with the tail end of the guide pipe C1 in a embedding mode, the top end of the guide pipe C1 is fixedly connected with the outer side surface of the air inlet C2 in a C-shaped return pipe, the tail end of the guide pipe is fixedly connected with the side wall of the outflow cavity C3 in a embedding mode, the air inlet C2 is beneficial to enabling tiny wind to enter the guide pipe C1 through a necking design, the guide pipe C3 is led into the inside, and the problem of internal fog of an internal shield caused by high air humidity in a sea area is mainly avoided, and meanwhile small air inlet quantity and large flow speed is internal heat for guiding.
The specific working principle is as follows:
the invention is fixed at the tail end of the rotating rod 13 by the partition cover 121 under the assistance of the fixed frame 122, and the inner ring machine 123 and the camera 124 in the inner ring machine are protected in a variable manner, so that the camera 124 performs three-dimensional image acquisition on the aerial image through the high-definition transparent plate b3 at the lower end of the flow strip b1, the anti-moving fixed b2 is fixed on the fixed frame 122 through bolts, and the diffused wind can be blown in from the inner end of the inner expanding groove b14 of the wind guide block b11 clamped and fixed by the limiting block b13 in the groove body b12 due to the fact that the wind is diffused when the unmanned aerial vehicle flies forwards, the wind direction enters from the reduced air inlet C2 and is transmitted to the outer flow cavity C3 in cooperation with the C-shaped flow guide pipe C1, the common outer expanding groove b14 dissipates the heat generated by the inner ring machine 123, the inner air inlet is reduced, so that the problem of internal fog of an inner shield caused by high humidity of air in sea areas is mainly avoided, meanwhile, the air is guided by taking small air inlet quantity and large flow rate as internal heat, and meanwhile, the cooling effect is achieved.
The technical features of the above-described embodiments may be arbitrarily combined, and all possible combinations of the technical features in the above-described embodiments are not described for brevity of description, however, as long as there is no contradiction between the combinations of the technical features, they should be considered as the scope of the description.
The present embodiments are, therefore, to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein; any reference sign in a claim should not be construed as limiting the claim concerned.
Claims (1)
1. A three-dimensional low altitude map inspection device for unmanned aerial vehicle inspection, its structure includes inspection probe (1), scroll press (2), slides wing (3), unmanned aerial vehicle body (4), inspection probe (1) top and unmanned aerial vehicle body (4) front side lower extreme nest connection, unmanned aerial vehicle body (4) both sides and slide wing (3) top welded connection, slide wing (3) lower surface and scroll press (2) top bolt fastening, scroll press (2) inboard and unmanned aerial vehicle body (4) whole clearance fit, its characterized in that:
the inspection probe (1) comprises a wiper (11), a panoramic camera (12), a rotating rod (13) and a conducting wire (14), wherein the inner wall of the wiper (11) is in movable fit with the surface of the panoramic camera (12), the top of the panoramic camera (12) is fixedly embedded with the tail end of the rotating rod (13), the inside of the rotating rod (13) is integrally and fixedly embedded with the conducting wire (14), and the top of the conducting wire (14) is fixedly embedded with the inside of the panoramic camera (12);
the wiper (11) comprises a wiper strip (111), a connecting frame (112) and a fixed sleeve ring (113), wherein the top of the wiper strip (111) is hinged with the tail end of the connecting frame (112), the top end of the connecting frame (112) is welded with the outer surface of the fixed sleeve ring (113), and the lower end of the fixed sleeve ring (113) is in clearance fit with the wiper strip (111) integrally;
the scraping strip (111) comprises a strip body (a 1), an anti-falling cap (a 2), a movable bolt (a 3) and a spring strip (a 4), wherein the top of the strip body (a 1) is integrally connected with the movable bolt (a 3) in a nested manner, the outer end of the movable bolt (a 3) is integrally movably matched with the spring strip (a 4), and the top end of the spring strip (a 4) is integrally clamped and connected with the anti-falling cap (a 2);
the strip body (a 1) comprises an inner cavity (a 11), a rubber scraping strip (a 12) and a pressure seat (a 13), wherein the inner wall of the inner cavity (a 11) is fixedly connected with the tail end of the pressure seat (a 13), the surface of the pressure seat (a 13) is in clearance fit with the inner wall of the rubber scraping strip (a 12), and the inner side of the rubber scraping strip (a 12) is in clearance fit with the inner cavity (a 11);
the panoramic camera (12) comprises a partition cover (121), a fixing frame (122), an inner ring machine (123) and a photographic head (124), wherein the inside of the partition cover (121) is fixed with two ends of the fixing frame (122) through bolts, the lower end of the fixing frame (122) is integrally clamped and connected with the inner ring machine (123), and the inside of the inner ring machine (123) is integrally movably matched with the photographic head (124);
the partition cover (121) comprises a circulation strip (b 1), an anti-moving fixing plate (b 2) and a high-definition transparent plate (b 3), wherein the bottom of the circulation strip (b 1) is fixedly connected with the top end of the high-definition transparent plate (b 3) in a embedding way, the inner side of the high-definition transparent plate (b 3) is in integral clearance fit with the anti-moving fixing plate (b 2), and the inner wall of the anti-moving fixing plate (b 2) is connected with the inner wall of the circulation strip (b 1) in a welding way;
the circulation strip (b 1) comprises a wind guide block (b 11), a groove body (b 12), a limiting block (b 13) and an outward expansion groove (b 14), wherein the inner side of the wind guide block (b 11) is in integral movable fit with the outward expansion groove (b 14), two sides of the outward expansion groove (b 14) are integrally clamped and connected with the limiting block (b 13), the inner wall of the limiting block (b 13) is fixedly embedded and connected with the inside of the groove body (b 12), and the inside of the groove body (b 12) is integrally clamped and connected with the wind guide block (b 11);
the wind guide block (b 11) comprises a guide pipe (c 1), an air inlet (c 2) and an outflow cavity (c 3), the top end of the guide pipe (c 1) is fixedly connected with the outer side of the air inlet (c 2), the lower end of the air inlet (c 2) is in integral clearance fit with the outflow cavity (c 3), and two sides of the top of the outflow cavity (c 3) are fixedly connected with the tail end of the guide pipe (c 1);
the unmanned aerial vehicle body (4) is driven to fly through the vortex press (2), the unmanned aerial vehicle body flies to a specified aerial line under the cooperation of the sliding wings (3) to carry out inspection, then the inspection probe (1) carries out three-dimensional image acquisition, the image of the panoramic camera (12) is transmitted to a terminal through the cooperation transmission line (14), the sea level temperature of the panoramic camera is increased due to refraction of sunlight when flying on a sea area, a factor of high humidity is added, water mist appears on the partition cover (121) at the outer end of the panoramic camera (12), in order to ensure the high-definition performance of three-dimensional image acquisition, the wiper (11) nested and fixed on the rotating rod (13) is attached to the surface of the partition cover (121), the rotating rod (13) is matched with the lower end wiper strip (111) of the connecting frame (112) welded at the outer end of the inner fixed sleeve ring (113) of the auxiliary panoramic camera (12), the movable bolt (a 3) at the inner side of the anti-release cap (a 2) is matched with the spring strip (a 4), the wiper strip (1) is matched with the surface of the wiper strip (121) to form a clearance fit with the upper wiper strip (13) to prevent the water mist from being attached to the surface of the wiper strip (13) through the pressure release cover (13 a) so as to realize the fit between the upper wiper strip and the upper wiper strip (11) and the surface (13) and the pressure release cover (11) and the pressure-release cover, in the process of collecting panoramic three-dimensional images of the panoramic camera (12) by the rotating rod (13), the rubber scraping strip (a 12) matched with the inner wall of the strip body (a 1) scrapes the water mist on the partition cover (121) under the assistance of rotation, so that the problem of unclear three-dimensional image collection caused by the fact that the probe is shielded by the water mist is effectively avoided; the partition cover (121) is fixed at the tail end of the rotating rod (13) under the assistance of the fixing frame (122), and the inner ring machine (123) and the camera (124) in the inner ring machine are protected in a variable phase mode, so that the camera (124) performs three-dimensional image acquisition on a navigation chart through a high-definition transparent plate (b 3) at the lower end of a flow-through strip (b 1), the anti-moving fixing plate (b 2) is fixed on the fixing frame (122) through bolts, the air guide is diffused to two sides when the unmanned aerial vehicle flies forwards, the diffused air can be blown in from the inner side of a groove body (b 12) through a limiting block (b 13) to the inner end of an inner expanding groove (b 14) so that the air direction enters from a reduced air inlet (C2), the inner expanding groove (b 14) is matched with a 'C' -shaped flow guide pipe (C1), heat generated by the inner ring machine (123) is prevented from being reduced by the inner expanding groove, the inner air inlet is mainly reduced, the inner side of the inner ring machine is mainly prevented from being polluted by the sea area, the humidity, the inner ring machine is simultaneously reduced, the air inlet is cooled down through the air inlet (b 2) and the inner expanding groove (b) is reduced, and simultaneously, the air flow of the inner ring machine (2) is cooled down through the inner expanding groove (b) is reduced, and the inner air flow is cooled down through the air inlet (2) is reduced, and the inner air is cooled down, the draft tube (C1) matched with the shape of C conveys the wind from the outer expansion groove (b 14) to the inside for cooling and heat dissipation, meanwhile, the small air intake and the large flow rate are used for guiding the heat in the inside, and meanwhile, the cooling effect is achieved, and the problem of fog in the shield is also avoided.
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| CN113865934A (en) * | 2021-09-08 | 2021-12-31 | 刘国明 | A water intaking ware for environmental monitoring unmanned aerial vehicle |
| CN215436974U (en) * | 2021-07-24 | 2022-01-07 | 青岛雷震子科技有限公司 | Survey and drawing is patrolled and examined fixed wing VTOL unmanned aerial vehicle |
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| KR102548228B1 (en) * | 2016-08-09 | 2023-06-28 | 삼성전자주식회사 | Unmanned aerial vehicle having camera |
| KR20180133190A (en) * | 2017-06-05 | 2018-12-13 | 김재윤 | Unmaned aerial vehicle for washing insulator |
| NL2020695B1 (en) * | 2018-03-30 | 2019-10-07 | Ronik Inspectioneering B V | Method for inspecting and/or manipulating a beam using an unmanned aerial vehicle |
| CN110769728A (en) * | 2018-10-27 | 2020-02-07 | 深圳市赫兹科技有限公司 | Cleaning method and system based on unmanned aerial vehicle |
| CN110920918B (en) * | 2019-12-05 | 2020-09-11 | 南京林业大学 | Unmanned aerial vehicle aerial photography hangs cloud platform |
| CN212580161U (en) * | 2020-07-09 | 2021-02-23 | 正元地球物理有限责任公司 | Based on antifog structure of camera for unmanned aerial vehicle exploration device |
| CN213921526U (en) * | 2020-12-16 | 2021-08-10 | 天津博思启慧科技发展有限责任公司 | Unmanned aerial vehicle image acquisition device |
| CN213768970U (en) * | 2020-12-22 | 2021-07-23 | 武汉理工大学 | Air traffic route reconnaissance unmanned aerial vehicle |
| CN215826996U (en) * | 2021-09-24 | 2022-02-15 | 武汉赛飞智特科技有限公司 | Auxiliary support tool for inspection operation of unmanned aerial vehicle for power line |
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| CN215436974U (en) * | 2021-07-24 | 2022-01-07 | 青岛雷震子科技有限公司 | Survey and drawing is patrolled and examined fixed wing VTOL unmanned aerial vehicle |
| CN113865934A (en) * | 2021-09-08 | 2021-12-31 | 刘国明 | A water intaking ware for environmental monitoring unmanned aerial vehicle |
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