CN112357083A - Electric power engineering construction operation continuation of journey type reconnaissance unmanned aerial vehicle - Google Patents
Electric power engineering construction operation continuation of journey type reconnaissance unmanned aerial vehicle Download PDFInfo
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- CN112357083A CN112357083A CN202011230454.XA CN202011230454A CN112357083A CN 112357083 A CN112357083 A CN 112357083A CN 202011230454 A CN202011230454 A CN 202011230454A CN 112357083 A CN112357083 A CN 112357083A
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- 238000010276 construction Methods 0.000 title claims abstract description 46
- 238000004891 communication Methods 0.000 claims abstract description 30
- 230000005540 biological transmission Effects 0.000 claims abstract description 26
- 238000012806 monitoring device Methods 0.000 claims abstract description 12
- 230000017525 heat dissipation Effects 0.000 claims description 10
- 238000013016 damping Methods 0.000 claims description 8
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 6
- 239000000741 silica gel Substances 0.000 claims description 6
- 229910002027 silica gel Inorganic materials 0.000 claims description 6
- 238000000605 extraction Methods 0.000 claims description 4
- 125000003003 spiro group Chemical group 0.000 claims description 3
- 238000000034 method Methods 0.000 abstract description 9
- 230000005611 electricity Effects 0.000 abstract description 4
- 238000010521 absorption reaction Methods 0.000 abstract 1
- 230000035939 shock Effects 0.000 abstract 1
- 238000010586 diagram Methods 0.000 description 3
- 238000013440 design planning Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000007689 inspection Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 230000002035 prolonged effect Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000013439 planning Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
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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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/34—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
- H02J7/35—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering with light sensitive cells
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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
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Power Engineering (AREA)
- Mechanical Engineering (AREA)
- Photovoltaic Devices (AREA)
Abstract
The invention discloses a cruising type exploration unmanned aerial vehicle for construction operation of electric power engineering, which comprises an unmanned aerial vehicle body, a cruising monitoring device and a portable construction tool storage device, wherein the cruising monitoring device comprises a solar cell panel, a fixed storage battery, a second telescopic supporting rod, a communication antenna, a camera, a circuit control panel and a data transmission piece. The invention relates to the technical field of unmanned aerial vehicle equipment, in particular to a portable construction tool storage device which fully utilizes light energy and is provided with a mobile power supply for electricity continuation, increases the duration of the unmanned aerial vehicle body, can transmit a shot picture in real time through a communication antenna in the process of observation and tour, is convenient for a user to observe and monitor construction operation of an electric power project in real time, reduces the output of labor force, can achieve the purpose of long-distance transmission of needed lacked tools, and can prevent the unmanned aerial vehicle body from being damaged due to multiple shock absorption settings.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle equipment, in particular to a cruising type reconnaissance unmanned aerial vehicle for electric power engineering construction operation.
Background
Along with the development of science and technology, the unmanned aerial vehicle technique has matured very much, through installation communication, transmission, processing module on the unmanned aerial vehicle, shoots through the camera and can transmit picture or the specific position of something to the studio, then handles the information of transmission again.
At present, when an electric pole is installed in electric power engineering construction, firstly, an installation position is searched, a design planning sketch is firstly formulated, then, the design planning sketch is compared with a three-dimensional drawing and a satellite drawing, the planning sketch is modified, and a GPS coordinate of the electric pole is determined; then let reconnaissance personnel near the coordinate, utilize unmanned aerial vehicle's advantage, carry out the reconnaissance through the camera to near a plurality of coordinate points to in feeding back the information of gathering to the control room, transmit it for the treater through signal receiver, handle the demonstration on the display through the treater, for the designer carries out final definite design and makes the reference.
However, the existing unmanned aerial vehicle cannot obtain a good solution to the problem of endurance, and the unmanned aerial vehicle is less used in the monitoring of power engineering construction due to the problem of poor endurance.
Disclosure of Invention
In order to solve the existing problems, the invention provides a portable construction tool storage device which fully utilizes light energy and is provided with a mobile power supply for electricity continuation, the duration of the unmanned aerial vehicle body is prolonged, a camera can transmit a shot picture in real time through a communication antenna in the process of observation and inspection, a user can conveniently observe and monitor construction operation of an electric power project in real time, the output of labor force is reduced, the arrangement of the portable construction tool storage device can achieve the purpose of long-distance transmission of needed tools, and the unmanned aerial vehicle body cannot be damaged due to multiple damping arrangements.
The technical scheme adopted by the invention is as follows: the invention discloses an endurance type exploration unmanned aerial vehicle for electric power engineering construction operation, which comprises an unmanned aerial vehicle body, an endurance monitoring device and a portable construction tool storage device, wherein the endurance monitoring device is connected to the upper part of the unmanned aerial vehicle body, the portable construction tool storage device is connected to the lower part of the unmanned aerial vehicle body, the unmanned aerial vehicle body comprises a rack, a fixed support frame, propellers, a driving motor, a battery placing frame and a communication device connecting frame, the rack is arranged in a rack shape, the fixed support frame is uniformly arranged on the periphery of the rack, a motor base is arranged on one side, away from the rack, of the fixed support frame, the driving motor is arranged on the motor base, the propellers are connected to an output shaft of the driving motor, the battery placing frame is connected to the upper part of the rack, the communication device connecting frame is connected to the lower part of the rack, and the battery, The communication device connecting frame comprises a battery lower supporting plate and a first telescopic supporting rod, wherein the battery lower supporting plate is connected to the center of the frame, the first telescopic supporting rod is uniformly arranged on the battery lower supporting plate, the battery upper supporting plate is connected to the telescopic end of the first telescopic supporting rod and arranged in parallel to the battery lower supporting plate, a heat dissipation through hole is formed in the battery upper supporting plate, the communication device connecting frame comprises a control supporting cavity and a heat dissipation fan, the control supporting cavity is connected to the bottom of the frame, and the heat dissipation fan is rotatably arranged at the bottom of the control supporting cavity; the cruising monitoring device comprises a solar cell panel, a fixed storage battery, second telescopic support rods, a communication antenna, a camera, a circuit control panel and a data transmission piece, wherein the second telescopic support rods are connected and arranged on two sides of a battery upper support plate, the solar cell panel is connected and arranged above the second telescopic support rods on two sides, the circuit control panel is arranged in a control support cavity, the camera is connected and arranged on one side of a battery placing frame, the communication antenna is connected and arranged below the fixed support frame, the fixed storage battery is arranged on a battery lower support plate, the solar cell panel is electrically connected with the fixed storage battery, the data transmission piece is arranged on the fixed storage battery, the camera is connected with the communication antenna and the data transmission piece, a data reading port is arranged on the data transmission piece, and the fixed storage battery is provided with a charging port and a movable connecting port, the mobile connector is characterized in that a mobile power supply is connected to the outside of the mobile connector, a power supply flexible fixing piece is arranged at the bottom of the battery upper supporting plate and is in contact with the mobile power supply, and the circuit control board is connected with the driving motor, the communication antenna, the camera, the data transmission piece and the fixed storage battery.
Further, the portable construction tool storage device comprises a tool box connecting plate, a containing box body, a first fixing bolt, a tension spring, a first closing door and a second closing door, wherein the first fixing bolt is provided with four groups of fixing bolts vertically and uniformly arranged on the tool box connecting plate, two opposite sides of the tool box connecting plate extend downwards to be provided with buckle fixing parts, the buckle fixing parts are provided with buckle fixing holes, the containing box body is provided with a hollow cavity with an opening at the bottom, fixing buckles are symmetrically arranged at the tops of two sides of the containing box body and detachably arranged in the buckle fixing holes, the first closing door is hinged on one side of the opening of the containing box body, the second closing door is hinged on the opposite side of the opening of the containing box body, one side end of the first closing door close to the second closing door is provided with a first electromagnet, one side end of the second closing door close to the first closing door is provided with a second electromagnet, the first electromagnet and the second electromagnet are opposite in polarity and are mutually attracted in a power-on mode, the tension springs are arranged in two groups, the two groups of tension springs are respectively connected to the inner side wall of one side of the first closed door and the containing box body and the inner side wall of the other side of the second closed door and the containing box body, and the first electromagnet and the second electromagnet are electrically connected with the fixed storage battery.
Further, the bottom in control support chamber is equipped with dead lever and first fixation nut, the dead lever is the shaft-like cavity setting of bottom open-ended cavity, the outer bottom of dead lever is located in the first fixation nut is rotatable, first fixing bolt spiro union is located in first fixation nut and can insert and locate the cavity of dead lever, the height of dead lever is greater than the thickness of heat extraction fan.
Further, the first closing door comprises a supporting layer and a buffer layer which are connected from top to bottom, buffer springs are uniformly connected between the supporting layer and the buffer layer, and the structure of the second closing door is the same as that of the first closing door.
Further, the control support cavity includes supporting fixed plate, second fixing bolt and second fixation nut, supporting fixed plate is equipped with six groups, six groups supporting fixed plate makes up into sealed form cube through second fixing bolt and second fixation nut, the control supports the chamber outer wall and evenly is equipped with the louvre, the last control interface that is equipped with different models of supporting fixed plate, the control interface is connected with circuit control board.
Furthermore, the outer wall of the containing box body is provided with a flashing lamp.
Further, the buckle fixing piece is arranged in an inverted L shape.
Furthermore, four groups of fixed support frames, propellers and driving motors are correspondingly arranged.
Further, a damping spring is arranged below the first fixing nut and arranged outside the first fixing bolt.
Further, the buffer layer is a sponge layer or a silica gel layer, and the power supply flexible fixing piece is a silica gel bulge or a rubber bulge.
Furthermore, the first telescopic supporting rod and the second telescopic supporting rod are telescopic rods.
The invention with the structure has the following beneficial effects: the scheme relates to a cruising type exploration unmanned aerial vehicle for power engineering construction operation, which is characterized in that on the basis of the use of a common unmanned aerial vehicle, a solar cell panel is additionally arranged, the light energy is fully utilized, a mobile power supply can be creatively arranged and disassembled, and is connected with a fixed storage battery through a mobile connector for continuous use, the cruising duration of an unmanned aerial vehicle body is increased, a camera can transmit a shot picture through a communication antenna in real time in the process of observation and tour, a user can conveniently observe and monitor the power engineering construction operation in real time, the output of labor force is reduced, the arrangement of a portable construction tool storage device can achieve the lack of tools needed by remote transmission, on the premise that a transmission tool is resistant to falling, the first electromagnet and the second electromagnet can be controlled to be powered off when the power engineering construction operation is at a certain height from the ground, the tool is transmitted in place, and on the premise that the tool to be transmitted is not resistant to falling, can reach after the ground at the unmanned aerial vehicle body, cutting off the power supply, in addition, first closing door and second closing door include supporting layer, buffer spring and the buffer layer that from the top down is connected, when contacting ground, partial effort is offset to the buffer layer, and buffer spring offsets partial effort afterwards, and the damping spring of first fixation nut's below setting plays absorbing effect once more for the unmanned aerial vehicle body can not receive the damage.
Drawings
Fig. 1 is a schematic overall structure diagram of a cruising type exploration unmanned aerial vehicle for electric power engineering construction operation;
fig. 2 is a partial sectional view of a front view of a cruising type exploration unmanned aerial vehicle for electric power engineering construction work of the present invention;
FIG. 3 is a schematic structural diagram of a portable construction tool storage device of a cruising type exploration unmanned aerial vehicle for power engineering construction work according to the invention;
fig. 4 is a schematic structural diagram of the cruising type unmanned aerial vehicle for electric power engineering construction operation of the present invention.
The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the principles of the invention and not to limit the invention.
Wherein, 1, unmanned aerial vehicle body, 2, continuation of journey monitoring device, 3, portable construction tool storage device, 4, frame, 5, fixed support frame, 6, screw, 7, driving motor, 8, battery rack, 9, communication device link, 10, motor cabinet, 11, battery upper support plate, 12, battery lower support plate, 13, first telescopic supporting rod, 14, control supporting cavity, 15, heat extraction fan, 16, solar cell panel, 17, fixed storage battery, 18, second telescopic supporting rod, 19, communication antenna, 20, camera, 21, circuit control panel, 22, data transmission piece, 23, data reading port, 24, charging port, 25, mobile connector, 26, power flexible fixing piece, 27, toolbox connecting plate, 28, containing box, 29, first fixing bolt, 30, tension spring, 31, first closing door, 32, second closing door, 33. the fixing device comprises a buckle fixing piece, 34, a fixing buckle, 35, a fixing rod, 36, a first fixing nut, 37, a supporting layer, 38, a buffer layer, 39, a buffer spring, 40, a supporting and fixing plate, 41, a second fixing bolt, 42, a second fixing nut, 43, a heat dissipation hole, 44, a control interface, 45, a flashing lamp, 46, a damping spring, 47, a first electromagnet, 48 and a second electromagnet.
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.
As shown in fig. 1-4, the cruising type reconnaissance unmanned aerial vehicle for electric power engineering construction operation of the invention comprises an unmanned aerial vehicle body 1, a cruising monitoring device 2 and a portable construction tool storage device 3, wherein the cruising monitoring device 2 is connected above the unmanned aerial vehicle body 1, the portable construction tool storage device 3 is connected below the unmanned aerial vehicle body 1, the unmanned aerial vehicle body 1 comprises a frame 4, a fixed support frame 5, a propeller 6, a driving motor 7, a battery placing frame 8 and a communication device connecting frame 9, the frame 4 is arranged in a frame shape, the fixed support frame 5 is uniformly arranged at the periphery of the frame 4, a motor base 10 is arranged at one side of the fixed support frame 5, which is far away from the frame 4, the driving motor 7 is arranged on the motor base 10, the propeller 6 is connected on an output shaft of the driving motor 7, and the battery placing frame 8 is connected above the frame 4, the communication device connecting frame 9 is connected below the rack 4, the battery placing frame 8 comprises a battery upper supporting plate 11, a battery lower supporting plate 12 and a first telescopic supporting rod 13, the battery lower supporting plate 12 is connected to the center of the rack 4, the first telescopic supporting rod 13 is uniformly arranged on the battery lower supporting plate 12, the battery upper supporting plate 11 is connected to the telescopic end of the first telescopic supporting rod 13, the battery upper supporting plate 11 is arranged in parallel with the battery lower supporting plate 12, a heat dissipation through hole is formed in the battery upper supporting plate 11, the communication device connecting frame 9 comprises a control supporting cavity 14 and a heat dissipation fan 15, the control supporting cavity 14 is connected to the bottom of the rack 4, and the heat dissipation fan 15 is rotatably arranged at the bottom of the control supporting cavity 14; the cruising monitoring device 2 comprises a solar cell panel 16, a fixed storage battery 17, a second telescopic supporting rod 18, a communication antenna 19, a camera 20, a circuit control panel 21 and a data transmission piece 22, wherein the second telescopic supporting rod 18 is connected and arranged on two sides of a battery upper supporting plate 11, the solar cell panel 16 is connected and arranged above the second telescopic supporting rods 18 on two sides, the circuit control panel 21 is arranged in a control supporting cavity 14, the camera 20 is connected and arranged on one side of a battery placing frame 8, the communication antenna 19 is connected and arranged below a fixed supporting frame 5, the fixed storage battery 17 is arranged on a battery lower supporting plate 12, the solar cell panel 16 is electrically connected with the fixed storage battery 17, the data transmission piece 22 is arranged on the fixed storage battery 17, the camera 20 is connected with the communication antenna 19 and the data transmission piece 22, and the data transmission piece 22 is provided with a data reading port 23, the fixed storage battery 17 is provided with a charging port 24 and a movable connecting port 25, a mobile power supply is connected to the outside of the movable connecting port 25, a power supply flexible fixing part 26 is arranged at the bottom of the battery upper supporting plate 11, the power supply flexible fixing part 26 is in contact with the mobile power supply, and the circuit control board 21 is connected with the driving motor 7, the communication antenna 19, the camera 20, the data transmission part 22 and the fixed storage battery 17.
Wherein, the portable construction tool storage device 3 comprises a tool box connecting plate 27, a containing box body 28, a first fixing bolt 29, a tension spring 30, a first closing door 31 and a second closing door 32, the first fixing bolt 29 is provided with four groups which are vertically and uniformly arranged on the tool box connecting plate 27, two opposite sides of the tool box connecting plate 27 extend downwards to be provided with buckle fixing parts 33, the buckle fixing parts 33 are provided with buckle fixing holes, the containing box body 28 is arranged in a hollow cavity with an opening at the bottom, fixing buckles 34 are symmetrically arranged at the tops of two sides of the containing box body 28, the fixing buckles 34 are detachably arranged in the buckle fixing holes, the first closing door 31 is hinged on one side of the opening of the containing box body 28, the second closing door 32 is hinged on the opposite side of the opening of the containing box body 28, one side end of the first closing door 31 close to the second closing door 32 is provided with a first electromagnet 47, the second closed door 32 is close to one side end of first closed door 31 and is equipped with second electro-magnet 48, first electro- magnet 47 and 48 opposite polarity of second electro-magnet and circular telegram are inhaled mutually and are closed, tension spring 30 is equipped with two sets ofly, and two sets of tension spring 30 are connected respectively and are located first closed door 31 and hold on the inside wall of one side of box 28 and on second closed door 32 and the opposite side inside wall that holds box 28, first electro-magnet and second electro-magnet are connected with fixed battery 17 electricity.
The bottom in control support cavity 14 is equipped with dead lever 35 and first fixation nut 36, dead lever 35 is the shaft-like cavity setting of bottom open-ended cavity, the outer bottom of dead lever 35 is located in first fixation nut 36 is rotatable, first fixation bolt 29 spiro union is located in first fixation nut 36 and can insert and locate the cavity of dead lever 35, the height of dead lever 35 is greater than the thickness of heat extraction fan 15.
The first closing door 31 comprises a supporting layer 37 and a buffer layer 38 which are connected from top to bottom, buffer springs 39 are uniformly connected between the supporting layer 37 and the buffer layer 38, and the structure of the second closing door 32 is the same as that of the first closing door 31.
The control support cavity 14 includes support fixed plate 40, second fixing bolt 41 and second fixing nut 42, support fixed plate 40 is equipped with six groups, six groups support fixed plate 40 makes up into sealed form cube through second fixing bolt 41 and second fixing nut 42, the control supports the outer wall in cavity 14 and evenly is equipped with louvre 43, be equipped with the control interface 44 of different models on support fixed plate 40, control interface 44 is connected with circuit control board 21.
The outer wall of the containing box body 28 is provided with a flashing lamp 45.
The snap fastener 33 is disposed in an inverted L shape.
Four groups of the fixed support frame 5, the propellers 6 and the driving motors 7 are correspondingly arranged.
A damping spring 46 is arranged below the first fixing nut 36, and the damping spring 46 is arranged outside the first fixing bolt 29.
The buffer layer 38 is a sponge layer or a silica gel layer, and the power flexible fixing member 26 is a silica gel protrusion or a rubber protrusion.
The first telescopic supporting rod 13 and the second telescopic supporting rod 18 are telescopic rods.
When the portable construction tool storage device is used, on the basis of the use of a common unmanned aerial vehicle, the solar cell panel 16 is additionally arranged, the light energy is fully utilized, the portable power supply can be creatively arranged and disassembled, and is connected with the fixed storage battery 17 through the movable connecting port 25 for electricity continuation use, the duration of the unmanned aerial vehicle body 1 is prolonged, the camera 20 can transmit a shot picture in real time through the communication antenna 19 in the process of observation and inspection, a user can conveniently observe and monitor the construction operation of the electric power engineering in real time, the output of labor force is reduced, the arrangement of the portable construction tool storage device 3 can achieve the lack of tools needed by remote transmission, on the premise that the transmission tool is anti-falling, the first electromagnet and the second electromagnet can be controlled to be powered off when the transmission tool is at a certain height from the ground, the tools are transmitted in place, and on the premise that the tools to be transmitted are not anti, can reach behind the ground at unmanned aerial vehicle body 1, cutting off the power supply, in addition, first closing door 31 and second closing door 32 include from the top down the supporting layer 37 of connecting, buffer spring 39 and buffer layer 38, when contacting ground, buffer layer 38 offsets partial effort, buffer spring 39 then offsets partial effort, and the damping spring 46 of the below setting of first fixation nut 36 plays absorbing effect again for unmanned aerial vehicle body 1 can not receive the damage.
The present invention and its embodiments have been described above, and the description is not intended to be limiting, and the drawings are only one embodiment of the present invention, and the actual structure is not limited thereto. In summary, those skilled in the art should appreciate that they can readily use the disclosed conception and specific embodiments as a basis for designing or modifying other structures for carrying out the same purposes of the present invention without departing from the spirit and scope of the invention as defined by the appended claims.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Claims (10)
1. The utility model provides an electric power engineering construction operation continuation of journey type reconnaissance unmanned aerial vehicle which characterized in that: the unmanned aerial vehicle comprises an unmanned aerial vehicle body, a cruising monitoring device and a portable construction tool storage device, wherein the cruising monitoring device is connected above the unmanned aerial vehicle body, the portable construction tool storage device is connected below the unmanned aerial vehicle body, the unmanned aerial vehicle body comprises a rack, a fixed support frame, a propeller, a driving motor, a battery placing frame and a communication device connecting frame, the rack is arranged in a frame shape, the fixed support frame is uniformly arranged at the periphery of the rack, a motor base is arranged on one side of the fixed support frame, which is far away from the rack, the driving motor is arranged on the motor base, the propeller is connected on an output shaft of the driving motor, the battery placing frame is connected above the rack, the communication device connecting frame is connected below the rack, and the battery placing frame comprises a battery upper support plate, a battery lower support plate and a first telescopic support rod, the battery lower support plate is connected to the center of the rack, the first telescopic support rods are uniformly arranged on the battery lower support plate, the battery upper support plate is connected to the telescopic end of the first telescopic support rod and arranged parallel to the battery lower support plate, the battery upper support plate is provided with a heat dissipation through hole, the communication device connecting frame comprises a control support cavity and a heat dissipation fan, the control support cavity is connected to the bottom of the rack, and the heat dissipation fan is rotatably arranged at the bottom of the control support cavity; the cruising monitoring device comprises a solar cell panel, a fixed storage battery, second telescopic support rods, a communication antenna, a camera, a circuit control panel and a data transmission piece, wherein the second telescopic support rods are connected and arranged on two sides of a battery upper support plate, the solar cell panel is connected and arranged above the second telescopic support rods on two sides, the circuit control panel is arranged in a control support cavity, the camera is connected and arranged on one side of a battery placing frame, the communication antenna is connected and arranged below the fixed support frame, the fixed storage battery is arranged on a battery lower support plate, the solar cell panel is electrically connected with the fixed storage battery, the data transmission piece is arranged on the fixed storage battery, the camera is connected with the communication antenna and the data transmission piece, a data reading port is arranged on the data transmission piece, and the fixed storage battery is provided with a charging port and a movable connecting port, the mobile connector is characterized in that a mobile power supply is connected to the outside of the mobile connector, a power supply flexible fixing piece is arranged at the bottom of the battery upper supporting plate and is in contact with the mobile power supply, and the circuit control board is connected with the driving motor, the communication antenna, the camera, the data transmission piece and the fixed storage battery.
2. The electric power engineering construction operation continuation of journey type reconnaissance unmanned aerial vehicle of claim 1, characterized in that: the portable construction tool storage device comprises a tool box connecting plate, a containing box body, a first fixing bolt, a tension spring, a first closing door and a second closing door, wherein the first fixing bolt is provided with four groups of fixing bolts which are vertically and uniformly arranged on the tool box connecting plate, the two opposite sides of the tool box connecting plate extend downwards to be provided with buckle fixing parts, the buckle fixing parts are provided with buckle fixing holes, the containing box body is provided with a hollow cavity with an opening at the bottom, the tops of the two sides of the containing box body are symmetrically provided with fixing buckles, the fixing buckles are detachably arranged in the buckle fixing holes, the first closing door is hinged on one side of the opening of the containing box body, the second closing door is hinged on the opposite side of the opening of the containing box body, one side end of the first closing door close to the second closing door is provided with a first electromagnet, one side end of the second closing door close to the first closing door is provided with a second electromagnet, the first electromagnet and the second electromagnet are opposite in polarity and are mutually attracted in a power-on mode, the tension springs are arranged in two groups, the two groups of tension springs are respectively connected to the inner side wall of one side of the first closed door and the containing box body and the inner side wall of the other side of the second closed door and the containing box body, and the first electromagnet and the second electromagnet are electrically connected with the fixed storage battery.
3. The electric power engineering construction operation continuation of journey type reconnaissance unmanned aerial vehicle of claim 2, characterized in that: the bottom in control support chamber is equipped with dead lever and first fixation nut, the dead lever is the shaft-like cavity setting of bottom open-ended cavity, but first fixation nut rotary locate the outer bottom of dead lever, first fixation bolt spiro union is located in first fixation nut and can insert and establish in the cavity of dead lever, the thickness that highly is greater than the heat extraction fan of dead lever.
4. The electric power engineering construction operation continuation of journey type reconnaissance unmanned aerial vehicle of claim 2, characterized in that: the first closing door comprises a supporting layer and a buffer layer which are connected from top to bottom, buffer springs are uniformly connected between the supporting layer and the buffer layer, and the structure of the second closing door is the same as that of the first closing door.
5. The electric power engineering construction operation continuation of journey type reconnaissance unmanned aerial vehicle of claim 1, characterized in that: the control support cavity includes supporting fixed plate, second fixing bolt and second fixation nut, supporting fixed plate is equipped with six groups, six groups supporting fixed plate makes up into sealed form cube through second fixing bolt and second fixation nut, the control supports the chamber outer wall and evenly is equipped with the louvre, the last control interface that is equipped with different models of supporting fixed plate, control interface is connected with circuit control board.
6. The electric power engineering construction operation continuation of journey type reconnaissance unmanned aerial vehicle of claim 2, characterized in that: the outer wall of the containing box body is provided with a flashing lamp; the buckle fixing piece is arranged in an inverted L shape.
7. The electric power engineering construction operation continuation of journey type reconnaissance unmanned aerial vehicle of claim 1, characterized in that: four groups of the fixed support frame, the propellers and the driving motors are correspondingly arranged.
8. The electric power engineering construction operation continuation of journey type reconnaissance unmanned aerial vehicle of claim 3, characterized in that: and a damping spring is arranged below the first fixing nut and is arranged outside the first fixing bolt.
9. The electric power engineering construction operation continuation of journey type reconnaissance unmanned aerial vehicle of claim 4, characterized in that: the buffer layer is a sponge layer or a silica gel layer, and the power supply flexible fixing piece is a silica gel bulge or a rubber bulge.
10. The electric power engineering construction operation continuation of journey type reconnaissance unmanned aerial vehicle of claim 1, characterized in that: the first telescopic supporting rod and the second telescopic supporting rod are telescopic rods.
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| CN202011230454.XA CN112357083A (en) | 2020-11-06 | 2020-11-06 | Electric power engineering construction operation continuation of journey type reconnaissance unmanned aerial vehicle |
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| CN202011230454.XA CN112357083A (en) | 2020-11-06 | 2020-11-06 | Electric power engineering construction operation continuation of journey type reconnaissance unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113075939A (en) * | 2021-03-29 | 2021-07-06 | 浙江中能工程设计有限公司 | Real-time monitoring device for electric power engineering |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113075939A (en) * | 2021-03-29 | 2021-07-06 | 浙江中能工程设计有限公司 | Real-time monitoring device for electric power engineering |
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