CN111998212A - High-stability structure of aircraft hanging panoramic camera - Google Patents
High-stability structure of aircraft hanging panoramic camera Download PDFInfo
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- CN111998212A CN111998212A CN202010709480.4A CN202010709480A CN111998212A CN 111998212 A CN111998212 A CN 111998212A CN 202010709480 A CN202010709480 A CN 202010709480A CN 111998212 A CN111998212 A CN 111998212A
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- hanging
- pressing block
- panoramic camera
- aircraft
- steel wire
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M13/00—Other supports for positioning apparatus or articles; Means for steadying hand-held apparatus or articles
- F16M13/02—Other supports for positioning apparatus or articles; Means for steadying hand-held apparatus or articles for supporting on, or attaching to, an object, e.g. tree, gate, window-frame, cycle
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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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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon Stands for scientific apparatus such as gravitational force meters
- F16M11/02—Heads
- F16M11/04—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand
- F16M11/043—Allowing translations
- F16M11/046—Allowing translations adapted to upward-downward translation movement
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon Stands for scientific apparatus such as gravitational force meters
- F16M11/02—Heads
- F16M11/04—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand
- F16M11/06—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting
- F16M11/08—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting around a vertical axis, e.g. panoramic heads
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon Stands for scientific apparatus such as gravitational force meters
- F16M11/02—Heads
- F16M11/18—Heads with mechanism for moving the apparatus relatively to the stand
Abstract
The invention discloses a high-stability structure of an aircraft hanging panoramic camera, and relates to the technical field of camera equipment. The invention comprises a hanging bracket arranged at the bottom of an unmanned aerial vehicle and a hanging bracket hung at the bottom of the hanging bracket and used for hanging a panoramic camera; the hanger comprises a fixed plate, a hanger rod, a circular hanger plate, a connecting column and a hanging ring; the hanging rack comprises a circular bearing plate, a hanging column and a hanging plate; each first pressing block is elastically connected with the corresponding second pressing block through two groups of four symmetrically arranged steel wire ropes. The panoramic camera has the advantages that the assembly and disassembly among all the parts are efficient, rapid and convenient, the carrying is convenient after the disassembly, the structural rigidity is reliable, the stability is strong, the imaging stability and the high reliability of the panoramic camera are ensured, the problems of flash or unstable pictures caused by the acceleration of an aircraft in the panoramic imaging are solved, the wiring and the whole structure are delicate, and the efficient work and the stable operation of the panoramic camera are ensured.
Description
Technical Field
The invention belongs to the technical field of camera equipment, and particularly relates to a high-stability structure of a hanging panoramic camera of an aircraft.
Background
Panoramic camera can realize panoramic video shooting's camera, because the needs of shooing, regular can involve the shooting of large-scale outdoor activities, need provide the formation of the panoramic scene image of the depression angle of certain height, need hang panoramic camera through unmanned aerial vehicle and carry out high panorama formation of image shooting this time. Due to the structural characteristics and the imaging principle of the panoramic camera, the existing panoramic camera is directly hung at the bottom of the unmanned aerial vehicle, so that the aircraft and the hanging structure of the aircraft are inevitably presented in a panoramic image, and the incompleteness and incompleteness of the panoramic image are caused. Secondly, due to the acceleration generated by the flight of the aircraft, the panoramic camera is unstably shaken when the aircraft ascends and descends and the aircraft moves in an angle deviation manner under the condition of no structural buffer, and the imaging effect and the reliability of the panoramic camera are influenced. Therefore, the high-stability structure of the aircraft hanging panoramic camera is significant.
Disclosure of Invention
The invention provides a high-stability structure of an aircraft hanging panoramic camera, which solves the problems.
In order to solve the technical problems, the invention is realized by the following technical scheme:
the invention relates to a high-stability structure of an aircraft hanging panoramic camera, which comprises a hanging bracket arranged at the bottom of an unmanned aircraft and a hanging frame hung at the bottom of the hanging bracket and used for hanging the panoramic camera;
the hanging bracket comprises a fixed plate fixedly arranged on a fixed seat at the bottom of the unmanned aerial vehicle, a hanging rod of a long carbon fiber hollow structure vertically arranged at the center of the bottom of the fixed plate, a circular hanging plate arranged at the bottom end of the hanging rod, connecting columns uniformly distributed and vertically arranged at the bottom of the circular hanging plate in a surrounding manner, and hanging rings fixedly arranged at the bottoms of the connecting columns; right-angled trapezoid first connecting blocks are symmetrically arranged on the surface of the hanging ring and between two adjacent connecting columns respectively, and a first pressing block is mounted on the inclined surface of each first connecting block through screws in a locking mode;
the hanging frame comprises a circular bearing plate, hanging columns and a hanging plate, wherein the circular bearing plate is arranged at the bottom of the circular hanging plate and positioned between the connecting columns, the hanging columns are uniformly distributed and vertically arranged at the bottom of the circular bearing plate in a surrounding mode, and the hanging plate is fixedly arranged at the bottom end of each hanging column; right-angled trapezoid second connecting blocks are symmetrically arranged at the bottom of the circular bearing plate and between two adjacent suspension posts respectively, and a second pressing block is locked and installed on the inclined surface of each second connecting block through screws respectively; the second pressing block is opposite to the first pressing block in position, and the surfaces of the second pressing block and the first pressing block are flush and are symmetrically arranged in parallel;
each first pressing block is elastically connected with the corresponding second pressing block through two groups of four symmetrically arranged steel wire ropes.
Furthermore, a first threaded hole is formed in the surface of the first pressing block, two first channels with two openings are symmetrically formed in the two sides of the first threaded hole between the upper side surface and the lower side surface of the first pressing block in a penetrating mode, the two ends of each first channel are respectively connected with one end of each of the two groups of steel wire ropes in an inserting mode, and one ends of the two groups of steel wire ropes are locked after being extruded through screws and the first threaded holes.
Furthermore, a second threaded hole is formed in the surface of the second pressing block, two second channels with two openings are symmetrically formed in the two sides of the second threaded hole between the left side surface and the right side surface of the second pressing block in a penetrating mode, the two ends of each second channel are respectively connected with the other ends of the two groups of steel wire ropes in an inserting mode, and the other ends of the two groups of steel wire ropes are locked after being extruded through screws and the second threaded holes.
Furthermore, the panoramic camera is electrically connected with the electronic device and the power supply module which are arranged on the fixed seat through the hollow cavity wiring in the suspender.
Furthermore, the length of the steel wire rope connected between the first pressing block and the second pressing block is the same, and the bending radians are consistent, so that the hanging rack is stably installed at the bottom of the circular hanging plate and located between the connecting columns.
Compared with the prior art, the invention has the following beneficial effects:
1. the whole body of the invention is formed by fixedly connecting each suspension part and the bottom of the aircraft in sequence, the parts are efficiently, quickly and conveniently assembled and disassembled, the disassembly is convenient and fast to carry, the assembly is convenient during use, and the invention is suitable for long-distance transportation and carrying tasks.
2. The hanging bracket structure can enable the panoramic camera to be removed from the picture of the unmanned aerial vehicle, enables the panoramic camera to be shielded outside the picture, and keeps the imaging integrity and completeness of the panoramic camera.
3. The elastic connection structure formed by the connecting blocks and the pressing blocks and the steel wire ropes is adopted between the hanging bracket and the hanging rack, so that the acceleration caused by much acceleration can be effectively buffered in the process that the aircraft drives the panoramic camera to lift and turn, the panoramic camera keeps relative stable motion, the imaging stability and high reliability of the panoramic camera are ensured, and the problems of flash or unstable pictures caused by the acceleration of the aircraft in panoramic imaging are solved.
4 the wiring and the whole structure of the full-view camera are delicate, the full-view camera is arranged at the bottom, the aircraft, the hanging bracket and the hanging bracket can be peeled off to the outside of a full-view picture, and the control and power supply of the full-view camera are realized by the way that the wiring at the top of the full-view camera penetrates through a hollow cavity in the hanging rod to be electrically connected with an electronic device at the top and a power supply module for control and power supply, so that the high-efficiency work and the stable operation of the full-view.
Of course, it is not necessary for any product in which the invention is practiced to achieve all of the above-described advantages at the same time.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings used in the description of the embodiments will be briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art that other drawings can be obtained according to the drawings without creative efforts.
FIG. 1 is a schematic diagram of the overall structure of the high stability structure of the aircraft hanging panoramic camera and the installation of the unmanned aircraft;
FIG. 2 is a front view of the structure of FIG. 1;
FIG. 3 is an enlarged view of a portion of FIG. 2 at position A;
FIG. 4 is a schematic view of the hanger of the present invention;
FIG. 5 is a schematic view of the structure at view B in FIG. 4;
FIG. 6 is a schematic structural view of a hanger according to the present invention;
FIG. 7 is a front view of the structure of FIG. 6;
FIG. 8 is a schematic structural view of a second compact of the present invention;
FIG. 9 is a cross-sectional view showing the lateral structure of a first compact of the present invention;
FIG. 10 is a schematic structural diagram of a first connecting block according to the present invention;
in the drawings, the components represented by the respective reference numerals are listed below:
1-unmanned aerial vehicle, 101-fixed seat, 2-hanger, 201-hanger rod, 202-fixed plate, 2021-fixed mounting hole, 203-circular hanger plate, 2031-hollow cavity, 204-connecting column, 205-hanging ring, 206-first connecting block, 207-first pressing block, 2071-first threaded hole, 2072-first channel, 3-hanger, 301-circular bearing plate, 302-hanger plate, 303-hanging column, 304-second connecting block, 305-second pressing block, 3051-second threaded hole, 3052-second channel, 4-panoramic camera and 5-steel wire rope.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
In the description of the present invention, it is to be understood that the terms "bottom", "vertical", "bottom", "surface", "bevel", "two sides", etc., indicate an orientation or positional relationship only for the convenience of describing the present invention and for simplicity of description, and do not indicate or imply that the referenced components or elements must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention.
Referring to fig. 1-10, the high stability structure of the aircraft hanging panoramic camera of the present invention includes a hanging bracket 2 mounted at the bottom of an unmanned aircraft 1, and a hanging rack 3 hung at the bottom of the hanging bracket 2 for hanging a panoramic camera 4;
the hanger 2 comprises a fixed plate 202 fixedly arranged on a fixed seat 101 at the bottom of the unmanned aerial vehicle 1, a hanger rod 201 of a long carbon fiber hollow structure vertically arranged at the center of the bottom of the fixed plate 202, a circular hanger plate 203 arranged at the bottom end of the hanger rod 201, connecting columns 204 uniformly distributed and vertically arranged at the bottom of the circular hanger plate 203 in a surrounding manner, and hanging rings 205 fixedly arranged at the bottoms of the connecting columns 204; right-angled trapezoid-shaped first connecting blocks 206 are symmetrically arranged on the surface of the hanging ring 205 and between two adjacent connecting columns 204, and a first pressing block 207 is locked and installed on the inclined surface of each first connecting block 206 through a screw;
the hanger 3 comprises a circular bearing plate 301 arranged at the bottom of the circular hanging plate 203 and positioned between the connecting columns 204, hanging columns 303 uniformly distributed and vertically arranged at the bottom of the circular bearing plate 301 in a surrounding manner, and hanging plates 302 fixedly arranged at the bottom ends of the hanging columns 303; right-angled trapezoid second connecting blocks 304 are symmetrically arranged at the bottom of the circular bearing plate 301 and between two adjacent suspension posts 303, and a second pressing block 305 is locked and mounted on the inclined surface of each second connecting block 304 through screws; the second pressing block 305 is opposite to the first pressing block 207, the surfaces of the second pressing block 305 are flush and are symmetrically arranged in parallel, the number of the first connecting block 206 and the number of the second connecting block 304 are four, and the number of the first pressing block 207 and the number of the second pressing block 305 are also four;
each first pressing block 207 is elastically connected with the corresponding second pressing block 305 through two groups of four symmetrically arranged steel wire ropes 5, the steel wire ropes 5 are elastic steel wire ropes with the diameter of 5mm, the steel wire ropes 5 are composite structures twisted and connected with the first pressing block 207 and the second pressing block 305 to bear the bearing stress, the composite structures are formed by twisting five thin steel wire ropes with the diameter of 1mm, the deviation force generated by the vertical inclination and the horizontal inclination of the hanging panoramic camera 4 can be buffered, the hanging stability of the panoramic camera 4 is kept, and the hanging rack 3 for hanging the panoramic camera 4 at the bottom can be hung stably.
Wherein, first screw hole 2071 has been seted up on first briquetting 20 surface, lies in first screw hole 2071 bilateral symmetry between the side from top to bottom and runs through and set up two open-ended first channels 2072, and the one end of two sets of wire rope 5 is pegged graft respectively at the both ends of first channel 2072 to carry out the locking to two sets of wire rope 5 one end after the extrusion through screw and first screw hole 2071.
Wherein, second screw hole 3051 has been seted up on the surface of second briquetting 305, lies in second screw hole 3051 bilateral symmetry between the side about it and runs through and seted up two open-ended second channel 3052, and two sets of wire rope 5's the other end is pegged graft respectively at the both ends of second channel 3052 to extrude the back through screw and second screw hole 3051 and lock two sets of wire rope 5 other ends.
The panoramic camera 4 is electrically connected to the electronic device and the power supply module mounted on the fixing base 101 through the hollow cavity 2031 in the suspension rod 201.
The length of the steel wire rope 5 connecting the first pressing block 207 and the second pressing block 305 is the same, and the curvature is consistent, so that the hanger 3 is stably installed at the bottom of the circular hanging plate 203 and between the connecting columns 204. The fixing plate 202 is fixedly connected to the fixing base 101 through a fixing hole 2021 formed in the surface of the fixing plate 202 and a bolt.
The working method of the invention is as follows:
through assembling according to the above description, aircraft control personnel control aircraft 1 to take off, this in-process is hung the stores pylon 3 that the bottom installed panoramic camera 4 by gallows 2 and is taken panoramic camera 4 to rise, panoramic camera 4's power supply and control are walked to the electron device on fixing base 101 and power module electric connection by hollow chamber 2031 in jib 201 and are controlled and the power supply, this in-process because first connecting block 206, second connecting block 304, first briquetting 207, the position and the angle of second briquetting 305 are set for and the elastic mode's of wire rope 5 connected mode is set for, shake or vibrations that can effectual buffering aircraft 1 brings, keep panoramic camera 4 effective buffering and steady turn to and take off and land to keep the stability of camera lens formation of image. The length of boom 201 on boom 2 is set to enable the aircraft 1 to be out of the resulting imaging frame when the panoramic camera 4 is imaging to maintain the integrity and completeness of panoramic imaging.
The beneficial effects of the invention compared with the prior art comprise:
1. the whole body of the invention is formed by fixedly connecting each suspension part and the bottom of the aircraft in sequence, the parts are efficiently, quickly and conveniently assembled and disassembled, the disassembly is convenient and fast to carry, the assembly is convenient during use, and the invention is suitable for long-distance transportation and carrying tasks.
2. The hanging bracket structure can enable the panoramic camera to be removed from the picture of the unmanned aerial vehicle, enables the panoramic camera to be shielded outside the picture, and keeps the imaging integrity and completeness of the panoramic camera.
3. The elastic connection structure formed by the connecting blocks and the pressing blocks and the steel wire ropes is adopted between the hanging bracket and the hanging rack, so that the acceleration caused by much acceleration can be effectively buffered in the process that the aircraft drives the panoramic camera to lift and turn, the panoramic camera keeps relative stable motion, the imaging stability and high reliability of the panoramic camera are ensured, and the problems of flash or unstable pictures caused by the acceleration of the aircraft in panoramic imaging are solved.
4. The wiring and the whole structure of the panoramic camera are delicate, the aircraft, the hanging bracket and the hanging bracket can be peeled off from the panoramic picture by arranging the panoramic camera at the bottom, and the control and power supply of the panoramic camera are realized by electrically connecting the wiring at the top of the panoramic camera, which penetrates through a hollow cavity in the hanging bracket, with an electronic device at the top and a power supply module, so that the high-efficiency work and the stable operation of the panoramic camera are ensured.
The preferred embodiments of the invention disclosed above are intended to be illustrative only. The preferred embodiments are not intended to be exhaustive or to limit the invention to the precise embodiments disclosed. Obviously, many modifications and variations are possible in light of the above teaching. The embodiments were chosen and described in order to best explain the principles of the invention and the practical application, to thereby enable others skilled in the art to best utilize the invention. The invention is limited only by the claims and their full scope and equivalents.
Claims (5)
1. A high-stability structure of an aircraft hanging panoramic camera is characterized by comprising a hanging bracket (2) arranged at the bottom of an unmanned aircraft (1) and a hanging rack (3) hung at the bottom of the hanging bracket (2) and used for hanging a panoramic camera (4);
the lifting frame (2) comprises a fixed plate (202) fixedly arranged on a fixed seat (101) at the bottom of the unmanned aerial vehicle (1), a lifting rod (201) which is vertically arranged at the center of the bottom of the fixed plate (202) and has a long carbon fiber hollow structure, a circular lifting plate (203) arranged at the bottom end of the lifting rod (201), connecting columns (204) uniformly distributed and vertically arranged at the bottom of the circular lifting plate (203) in a surrounding manner, and lifting rings (205) fixedly arranged at the bottoms of the connecting columns (204); right-angled trapezoid first connecting blocks (206) are symmetrically arranged on the surface of the hanging ring (205) and between two adjacent connecting columns (204), and a first pressing block (207) is mounted on the inclined surface of each first connecting block (206) through screws in a locking mode;
the hanger (3) comprises circular bearing plates (301) which are arranged at the bottoms of the circular hanging plates (203) and located between the connecting columns (204), hanging columns (303) which are uniformly distributed and vertically arranged at the bottoms of the circular bearing plates (301) in a surrounding mode, and hanging plates (302) which are fixedly arranged at the bottom ends of the hanging columns (303); right-angled trapezoid second connecting blocks (304) are symmetrically arranged at the bottom of the circular bearing plate (301) and between two adjacent suspension posts (303), and a second pressing block (305) is locked and mounted on the inclined surface of each second connecting block (304) through screws; the second pressing block (305) is opposite to the first pressing block (207), and the surfaces of the second pressing block and the first pressing block are flush and are symmetrically arranged in parallel;
each first pressing block (207) is elastically connected with the corresponding second pressing block (305) through two groups of four symmetrically arranged steel wire ropes (5).
2. The high-stability structure of the aircraft hanging panoramic camera according to claim 1, characterized in that a first threaded hole (2071) is formed in the surface of the first pressing block (207), two first channels (2072) with two openings are symmetrically formed through the first threaded hole (2071) between the upper and lower side surfaces of the first pressing block, one ends of two groups of steel wire ropes (5) are respectively inserted into two ends of each first channel (2072), and one ends of the two groups of steel wire ropes (5) are locked after being extruded with the first threaded hole (2071) through screws.
3. The high-stability structure of the aircraft hanging panoramic camera according to claim 1, characterized in that a second threaded hole (3051) is formed in the surface of the second pressing block (305), two second channels (3052) with two openings are symmetrically formed in the two sides of the second threaded hole (3051) between the left side and the right side of the second pressing block, the two ends of each second channel (3052) are respectively inserted with the other ends of two sets of steel wire ropes (5), and the other ends of the two sets of steel wire ropes (5) are locked after being extruded with the second threaded hole (3051) through screws.
4. The high-stability structure of the aircraft hanging panoramic camera according to claim 1, wherein the panoramic camera (4) is electrically connected with the electronic device and the power supply module installed on the fixed base (101) through routing of a hollow cavity (2031) in the suspension rod (201).
5. The high-stability structure of an aircraft hanging panoramic camera is characterized in that the steel wire ropes (5) connecting the first pressing block (207) and the second pressing block (305) are identical in structural size and length and consistent in bending radian, so that the hanging rack (3) is stably installed at the bottom of the circular hanging plate (203) and located between the connecting columns (204).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN202010709480.4A CN111998212A (en) | 2020-07-22 | 2020-07-22 | High-stability structure of aircraft hanging panoramic camera |
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| CN202010709480.4A CN111998212A (en) | 2020-07-22 | 2020-07-22 | High-stability structure of aircraft hanging panoramic camera |
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| CN107956837A (en) * | 2017-11-15 | 2018-04-24 | 深圳市科比特航空科技有限公司 | Unmanned machine head damping device |
| CN209064373U (en) * | 2018-11-05 | 2019-07-05 | 广东工业大学 | A kind of damping holder for aerial photographing with reflecting mirror |
| CN211001834U (en) * | 2019-10-21 | 2020-07-14 | 广西电网有限责任公司 | Unmanned aerial vehicle laser radar nacelle and unmanned aerial vehicle |
| CN111169650A (en) * | 2020-02-11 | 2020-05-19 | 广东电网有限责任公司电力科学研究院 | Lightweight electric power corridor data acquisition equipment and unmanned aerial vehicle |
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