CN109193453A - Multi-functional unmanned plane suitable for electric inspection process - Google Patents
Multi-functional unmanned plane suitable for electric inspection process Download PDFInfo
- Publication number
- CN109193453A CN109193453A CN201811150397.7A CN201811150397A CN109193453A CN 109193453 A CN109193453 A CN 109193453A CN 201811150397 A CN201811150397 A CN 201811150397A CN 109193453 A CN109193453 A CN 109193453A
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- China
- Prior art keywords
- unmanned plane
- waterproof
- main body
- upper casing
- signal lamp
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Classifications
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
- H02G1/00—Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines
- H02G1/02—Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines for overhead lines or cables
-
- 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
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- 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
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Manipulator (AREA)
Abstract
The invention discloses a kind of multi-functional unmanned plane suitable for electric inspection process, including unmanned plane main body, it is provided with glove cavity in unmanned plane main body, the side of unmanned plane main body is provided with several rotor flight devices；Unmanned plane main body upper end is provided with a waterproof upper casing, and the first waterproof grommet is provided between waterproof upper casing and unmanned plane main body；An opening up electronic component installation cavity is provided in glove cavity in the middle part of aluminium radiator, the side of waterproof upper casing is arcwall face, the upper surface of waterproof upper casing is plane, waterproof upper casing is made of transparent plastic material, it is fixedly installed on the upper surface of waterproof upper casing and grabs cable machinery hand automatically, thermal infrared imaging instrument, video camera and supersonic detector are fixedly installed in waterproof upper casing.Above-mentioned technical proposal, reasonable in design, structure is simple, assembly and disassembly are easy, waterproof performance is good, longevity of service, easy to use and can work normally under the mal-conditions such as rainy day, night.
Description
Technical field
The present invention relates to air vehicle technique fields, and in particular to the multi-functional unmanned plane suitable for electric inspection process.
Background technique
Unmanned plane is the not manned aircraft using wireless remote control device and process control, in dual-use two big necks
Domain is widely used.Unmanned plane it is many kinds of, extensively take photo by plane, detect, search and rescue, security, resource exploration, agricultural etc.
Aspect use, multi-rotor unmanned aerial vehicle due to its simple and compact mechanical structure, it is more flexible action, landing environmental requirement compared with
It is low, easy to operate, the excellent characteristics such as take off, hover, landing can be realized in small atmosphere, especially paid attention to.Unmanned air vehicle technique is answered
There are many advantages for power-line patrolling field, still, the particularity and complexity of the task as performed by multi-rotor unmanned aerial vehicle,
It determines that it must carry a large amount of sophisticated electronics, while must also be able in face of various severe or even extreme ring
Border.But there is also deficiencies for existing unmanned plane structure: more rotary wind type unmanned plane structure settings are unreasonable, poor waterproof properties, once
After water inlet, internal electronic element part, which will damage, is even submitted an expense account, thus the service life of serious curtailment unmanned plane, and structure is multiple
Miscellaneous, assembly and disassembly operations is difficult, and maintenance is inconvenient, and battery reserve of electricity is few, and unmanned plane generally once can only be flight 0.5-1.5 hours, then
In addition other electrical equipments, faster, the working time is short for power consumption, and inconvenient to use, the practicability is poor.
Summary of the invention
In view of the deficiencies of the prior art, the present invention intends to provide it is a kind of it is reasonable in design, structure is simple,
Assembly and disassembly are easy, waterproof performance is good, longevity of service, easy to use and can be in work normal under the mal-conditions such as rainy day, night
The multi-functional unmanned plane suitable for electric inspection process made.
To achieve the above object, the present invention provides the following technical scheme that being suitable for the multi-functional unmanned plane of electric inspection process,
Including unmanned plane main body, glove cavity is provided in the unmanned plane main body, the side of the unmanned plane main body is provided with several
A rotor flight device；Unmanned plane main body upper end is provided with a waterproof upper casing, waterproof upper casing lower end and unmanned plane
The connection of main body threaded upper ends, and the first waterproof grommet is provided between waterproof upper casing and unmanned plane main body；The glove cavity
It is inside provided with an aluminium radiator, has been wholely set multi-disc cooling fin on the outer surface of the aluminium radiator, in aluminium radiator
Portion is provided with an opening up electronic component installation cavity, leads between the lower end of the aluminium radiator and the bottom surface of glove cavity
It crosses its junction after being adhesively fixed and constitutes sealing；The upper end of the aluminium radiator is protruded into waterproof upper casing；The waterproof upper casing
Side is arcwall face, and the upper surface of waterproof upper casing is plane, and the waterproof upper casing is made of transparent plastic material, waterproof upper casing
Upper surface on be fixedly installed and grab cable machinery hand automatically, thermal infrared imaging instrument is fixedly installed in the waterproof upper casing, is taken the photograph
Camera and supersonic detector；Automatically the cable machinery hand of grabbing includes miniature electro-hydraulic push rod device, perpendicular support plate and horizontal limit
Plate, the perpendicular support plate lower end and the upper surface of waterproof upper casing are wholely set, the shell of the miniature electro-hydraulic push rod device and perpendicular
Support plate is detachably connected, and the push rod upper end of the miniature electro-hydraulic push rod device has been wholely set push plate, the upper end of the push plate
Face left end has been wholely set perpendicular limit plate, and the push plate perpendicular constitutes one between limit plate, horizontal limit plate and perpendicular support plate together
Cable limit chamber.
By using above-mentioned technical proposal, by being provided with the first waterproof sealing between waterproof upper casing and unmanned plane main body
Circle, good seal performance, antileaking, assembly and disassembly are easy, easy to maintenance；The side of waterproof upper casing is arcwall face, can be effectively reduced
Windage, so that unmanned plane during flying is reliable；Automatically it is flexible by the push rod of miniature Electrohydraulic push rod to grab cable machinery hand, it can will be existing
Cable be caught in cable limit chamber, to make the suspension setting of entire unmanned plane, rotor flight device is then turned off, to save nothing
Man-machine power consumption extends the working time of unmanned plane；Using thermal infrared imaging instrument, video camera and supersonic detector to line
Road is monitored；Thermal infrared imaging instrument, which can be realized, carries out infrared measurement of temperature to transmission line of electricity, monitors route heat condition；Video camera
It can be realized and the corrosion of transmission pressure, fitting, insulator and steel tower and filthy, line corridor are monitored；Supersonic detector
It can be realized to existing in route and transmission facility and potential crackle detects.Complete machine structure is reasonable in design, structure
Simply, assembly and disassembly are easy, waterproof performance is good, longevity of service, it is easy to use and can energy saving power consumption, practicability is good.
The present invention is further arranged to: fixed bonding has the first felt pad, erects limit plate on the upper surface of the push plate
Fixed bonding has the second felt pad on right side, and fixed bonding has third felt pad on the lower end surface of the horizontal limit plate, described
The left side upper end fixed bonding of perpendicular support plate has the 4th felt pad.By this setting, structure setting is more reasonable, and each component is exhausted
Edge performance is good, so that unmanned plane work is relatively reliable.
The present invention is further arranged to: the bottom surface of the unmanned plane main body is plane, the bottom surface of the unmanned plane main body
Edge is provided with several alighting carriages, detachable setting signal lamp device in the middle part of the bottom surface of the unmanned plane main body, the letter
Signal lamp device includes signal lamp lamp holder, at least provided with a LED signal lamp and one on the lower end surface of the signal lamp lamp holder
Radio remote control switch is arranged with the first transparent watertight cover in each LED signal lamp, covers on each radio remote control switch
Equipped with the second transparent watertight cover；At least provided with a second anti-watertight on the bottom surface of the signal lamp lamp holder and unmanned plane main body
Seal.By this setting, structure setting is more reasonable, and signal lamp device structure is simple, can in dense fog or rainy night
So that LED signal lamp Yellow light-emitting low temperature, yellow light has good penetration capacity, may insure that unmanned plane can work normally in this way,
Fine night makes LED light group emit white light, and is also ensured that unmanned plane works normally；Electronics is arranged in the middle part of aluminium radiator
Existing electronic component is mounted in the electronic component installation cavity of aluminium radiator, not only perfect heat-dissipating by element installation cavity, and
Good water-proof effect is not easy to extend the service life of electronic component into water.
The present invention is further arranged to: be provided in the electronic component installation cavity microprocessor, image capture device,
Gyroscope, baroceptor, wireless transceiver, satellite positioning communication module, memory, stable-pressure device and rechargeable battery, it is described
Rechargeable battery by conducting wire respectively with microprocessor, image capture device, gyroscope, baroceptor, wireless transceiver, satellite
Positioning and communicating module, memory, stable-pressure device, rotor flight device are connected with signal lamp device, and rechargeable battery gives each portion
Part power supply, the microprocessor by conducting wire respectively with image capture device, gyroscope, baroceptor, wireless transceiver, defend
Star positioning and communicating module, memory, stable-pressure device are connected with rotor flight device.
The present invention is further arranged to: the rotor flight device includes connecting bracket, rotor shell, motor, motor
Tachometer of measuring and rotor blade, described connecting bracket one end are detachably connected or are fixedly connected with unmanned plane main body, connection branch
The frame other end is wholely set with rotor shell, and the motor and motor speed measurement instrument are arranged in rotor shell, the rotation
Wing blade is set on the main shaft of motor, the main shaft linkage of rotor blade and motor.
The present invention is further arranged to: the outer surface upper end of the unmanned plane main body is provided with the installation of the first sealing ring
Slot, first waterproof grommet are set in the first sealing ring mounting groove, on waterproof upper casing lower end and unmanned plane main body
End clamps the first waterproof grommet when screwing by screw thread, seals so that the junction of waterproof upper casing and unmanned plane main body is constituted.
The present invention is further arranged to: the bottom side alignment signal lamp lamp holder position of the unmanned plane main body is provided with second
Sealing ring mounting groove, second waterproof grommet are mounted in the second sealing ring mounting groove, the signal lamp lamp holder and nobody
The underrun screw of owner's body is connected and fixed, and the upper surface of signal lamp lamp holder compresses the second waterproof grommet, so that signal
The bottom surface junction of lamp lamp holder and unmanned plane main body, which is constituted, to be sealed.
The present invention is further arranged to: the lower end of the LED signal lamp and radio remote control switch with signal lamp lamp holder
Face is connected by screw to fixation, and the first transparent watertight cover and the second transparent watertight cover pass through glass cement and signal lamp lamp holder
Lower end surface be adhesively fixed.
The present invention is further arranged to: the alighting carriage includes that stainless steel nut, stainless steel connecting rod, stainless steel are slow
Spring and stainless steel plate are rushed, the upper surface of the stainless steel nut and the bottom surface of unmanned plane main body are wholely set or weld solid
It is fixed；Stainless steel connecting rod upper end is threadedly coupled with the nut bore of stainless steel nut, and the stainless steel buffer spring is set in
In stainless steel connecting rod, and the upper end of stainless steel buffer spring is welded and fixed with stainless steel connecting rod, the stainless steel buffering elastic
The lower end of spring and the upper surface of stainless steel plate are welded and fixed.
The present invention is further arranged to: several connection screwed pipes, the connection are provided on the side of unmanned plane main body
Bracket is connected through a screw thread fixation close to unmanned plane bulk end and the connection screwed pipe of alignment.
The invention has the advantages that compared with prior art, structure of the invention setting rationally, passes through waterproof upper casing and unmanned plane
The first waterproof grommet is provided between main body, good seal performance, antileaking, assembly and disassembly are easy, easy to maintenance；Signal lamp device
Structure is simple, can make LED signal lamp Yellow light-emitting low temperature in dense fog or rainy night, and yellow light has good penetration capacity,
It may insure that unmanned plane can work normally in this way, so that LED light group is emitted white light at fine night, nobody is also ensured
Machine works normally；Electronic component installation cavity is arranged in the middle part of aluminium radiator, and existing electronic component is mounted on aluminium radiator
In electronic component installation cavity, not only perfect heat-dissipating, and good water-proof effect is not easy to extend the service life of electronic component into water；
The side of waterproof upper casing is arcwall face, windage can be effectively reduced, so that unmanned plane during flying is reliable；Automatically cable is grabbed
Manipulator is flexible by the push rod of miniature Electrohydraulic push rod, existing cable can be caught in cable limit chamber, to make entire nothing
Man-machine suspension setting, is then turned off rotor flight device, to save unmanned plane power consumption, extends the working time of unmanned plane；
Route is monitored using thermal infrared imaging instrument, video camera and supersonic detector；Thermal infrared imaging instrument can be realized pair
Transmission line of electricity carries out infrared measurement of temperature, monitors route heat condition；Video camera can be realized to transmission pressure, fitting, insulator and
Steel tower corrosion and filthy, line corridor are monitored；Supersonic detector can be realized to existing in route and transmission facility and
Potential crackle is detected.
Complete machine structure design is rationally, structure is simple, assembly and disassembly are easy, waterproof performance is good, easy to use, easy to maintenance and can
It is worked normally under the mal-conditions such as rainy day, night, function is more, and practicability is good.
The invention will be further described with specific embodiment with reference to the accompanying drawings of the specification.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the embodiment of the present invention；
Fig. 2 is the enlarged diagram in the portion I in Fig. 1；
Fig. 3 is the enlarged diagram in the portion II in Fig. 1；
Fig. 4 is the structural schematic diagram of internal circuit of the embodiment of the present invention.
Specific embodiment
In the description of the present embodiment, it should be noted that such as occur term " center ", "upper", "lower", "left", "right",
"vertical", "horizontal", "inner", "outside", "front", "rear" etc., indicated by orientation or positional relationship be it is based on the figure
Orientation or positional relationship is merely for convenience of description of the present invention and simplification of the description, rather than the device of indication or suggestion meaning or
Element must have a particular orientation, be constructed and operated in a specific orientation, it is thus impossible to be interpreted as limitation of the present invention.
In addition, such as there is term " first ", " second ", " third " are used for description purposes only, be not understood to indicate or imply opposite
Importance.
Referring to Fig. 1, Fig. 2, Fig. 3 and Fig. 4, the multi-functional unmanned plane disclosed by the invention suitable for electric inspection process, including nothing
Man-machine main body 1 is provided with glove cavity 11 in the unmanned plane main body 1, and the side of the unmanned plane main body 1 is provided with several
Rotor flight device 2；1 upper end of unmanned plane main body is provided with a waterproof upper casing 3,3 lower end of waterproof upper casing and nobody
The connection of 1 threaded upper ends of owner's body, and the first waterproof grommet 4 is provided between waterproof upper casing 3 and unmanned plane main body 1；It is described to set
It is provided with an aluminium radiator 8 in object cavity 11, has been wholely set multi-disc cooling fin 81 on the outer surface of the aluminium radiator 8,
The middle part of aluminium radiator 8 is provided with an opening up electronic component installation cavity 82, the lower end of the aluminium radiator 8 with set
Sealing is constituted by its junction after being adhesively fixed between the bottom surface of object cavity 11；Waterproof is protruded into the upper end of the aluminium radiator 8
In upper casing 3；The side of the waterproof upper casing 3 is arcwall face, and the upper surface of waterproof upper casing 3 is plane, and the waterproof upper casing 3 is by saturating
Bright plastic material is made, and is fixedly installed on the upper surface of waterproof upper casing 3 and grabs cable machinery hand 9, the waterproof upper casing 3 automatically
Inside it is fixedly installed thermal infrared imaging instrument 13, video camera 14 and supersonic detector 15；It is described to grab cable machinery hand 9 automatically and include
Miniature electro-hydraulic push rod device 91, perpendicular support plate 92 and horizontal limit plate 93, perpendicular 92 lower end of support plate are upper with waterproof upper casing 3
End face is wholely set, and the shell of the miniature electro-hydraulic push rod device 91 is detachably connected with perpendicular support plate 92, described miniature electro-hydraulic
The push rod upper end of push rod device 91 has been wholely set push plate 95, and the upper surface left end of the push plate 95 has been wholely set perpendicular limit plate
96, the push plate 95 perpendicular constitutes a cable limit chamber 96 together between limit plate 94, horizontal limit plate 93 and perpendicular support plate 92.
Preferably, six, and six 2 rings of rotor flight device are arranged in described 2 the present embodiment of rotor flight device altogether
Shape is uniformly distributed；The lower end of the aluminium radiator 8 and the existing glass cement of underrun of glove cavity 11 are adhesively fixed.It is described
The shell of miniature electro-hydraulic push rod device 91 is connected and fixed with perpendicular support plate 92 by existing screw.The thermal infrared imaging instrument
13, video camera 14 and supersonic detector 15 are connected and fixed with the inner wall of waterproof upper casing 3 by existing screw, and each spiral shell
Follow closely interconnecting piece sealed set；The thermal infrared imaging instrument 13, video camera 14, supersonic detector 15 and miniature electro-hydraulic push rod device
9 be existing product, the prior art that structure, working principle and connection type are well known to the skilled person, sheet
Embodiment is just no longer described.
To keep structure of the invention setting more reasonable, preferably, solid on the upper surface of push plate 95 described in the present embodiment
Surely being bonded with fixed bonding on the right side of the first felt pad, perpendicular limit plate 94 has the second felt pad, the horizontal limit plate 93
Fixed bonding has third felt pad on lower end surface, and the left side upper end fixed bonding of the perpendicular support plate 92 has the 4th felt pad.
The bottom surface of the unmanned plane main body 1 is plane, and the bottom edge of the unmanned plane main body 1 is provided with several landing
Bracket 5, the detachable setting signal lamp device 6 in bottom surface middle part of the unmanned plane main body 1, the signal lamp device 6 includes signal
Lamp lamp holder 61 is opened at least provided with a LED signal lamp 62 and a wireless remote control on the lower end surface of the signal lamp lamp holder 61
63 are closed, the first transparent watertight cover 64 is arranged in each LED signal lamp 62, is arranged on each radio remote control switch 63
There is the second transparent watertight cover 65；The signal lamp lamp holder 61 is prevented on the bottom surface of unmanned plane main body 1 at least provided with one second
Waterstop ring 7.
Be provided in the electronic component installation cavity 82 microprocessor, image capture device, gyroscope, baroceptor,
Wireless transceiver, satellite positioning communication module, memory, stable-pressure device and rechargeable battery, the rechargeable battery pass through conducting wire point
Not with microprocessor, image capture device, gyroscope, baroceptor, wireless transceiver, satellite positioning communication module, storage
Device, stable-pressure device, rotor flight device are connected with signal lamp device, and rechargeable battery is powered to each component, the micro process
Device by conducting wire respectively with image capture device, gyroscope, baroceptor, wireless transceiver, satellite positioning communication module, deposit
Reservoir, stable-pressure device are connected with rotor flight device.
The rotor flight device 2 includes connecting bracket, rotor shell, motor, motor speed measurement instrument and rotor blade,
Described connecting bracket one end is detachably connected or is fixedly connected with unmanned plane main body 1, the connecting bracket other end and rotor shell one
Body setting, the motor and motor speed measurement instrument are arranged in rotor shell, and the rotor blade is set in the master of motor
On axis, the main shaft of rotor blade and motor links.The rotor flight device 2 is existing product, and structure and working principle are all
It is the prior art.
The outer surface upper end of the unmanned plane main body 1 is provided with the first sealing ring mounting groove, first waterproof grommet 4
It is set in the first sealing ring mounting groove, clamping when 3 lower end of waterproof upper casing and 1 upper end of unmanned plane main body are screwed by screw thread
First waterproof grommet 4 seals so that the junction of waterproof upper casing 3 and unmanned plane main body 1 is constituted.
61 position of bottom side alignment signal lamp lamp holder of the unmanned plane main body 1 is provided with the second sealing ring mounting groove, described
Second waterproof grommet 7 is mounted in the second sealing ring mounting groove, and the signal lamp lamp holder 61 and the bottom surface of unmanned plane main body 1 are logical
It crosses screw to be connected and fixed, and the upper surface of signal lamp lamp holder 61 compresses the second waterproof grommet 7, so that signal lamp lamp holder 61 and nothing
The bottom surface junction of man-machine main body 1 constitutes sealing.
The LED signal lamp 62 and radio remote control switch 63 are connected by screw to the lower end surface of signal lamp lamp holder 61 solid
Fixed, the first transparent watertight cover 64 and the second transparent watertight cover 65 are viscous by the lower end surface of glass cement and signal lamp lamp holder 61
Connect fixation.
The alighting carriage 5 includes stainless steel nut 51, stainless steel connecting rod 52, stainless steel buffer spring 53 and stainless
Steel sole plate 54, the upper surface of the stainless steel nut 51 and the bottom surface of unmanned plane main body 1 are wholely set or are welded and fixed；It is described not
Rust 52 upper end of steel connecting rod is threadedly coupled with the nut bore of stainless steel nut 52, and the stainless steel buffer spring 53 is set in stainless
In steel connecting rod 52, and the upper end of stainless steel buffer spring 53 is welded and fixed with stainless steel connecting rod 52, the stainless steel buffering
The lower end of spring 53 and the upper surface of stainless steel plate 54 are welded and fixed.By this setting, the alighting carriage 5 is at least arranged
Two.
Several connection screwed pipes 12 are provided on the side of the unmanned plane main body 1, the connecting bracket is close to unmanned plane
The connection screwed pipe 12 of 1 end of main body and alignment is connected through a screw thread fixation.
LED signal lamp 62, radio remote control switch 63 described in the present embodiment, the first transparent watertight cover 64, the second transparent watertight
Cover 65, microprocessor, image capture device, gyroscope, baroceptor, wireless transceiver, satellite positioning communication module, storage
Device, stable-pressure device and the equal existing product of rechargeable battery, structure, connection relationship and working principle are those skilled in the art institute
The well known prior art, the present embodiment are just no longer subject to burden and describe.
When practical application, by being provided with the first waterproof grommet, sealing performance between waterproof upper casing and unmanned plane main body
Good, antileaking, assembly and disassembly are easy, easy to maintenance；Signal lamp device structure is simple, can make in dense fog or rainy night
LED signal lamp Yellow light-emitting low temperature, yellow light have good penetration capacity, may insure that unmanned plane can work normally in this way, in weather
Sunny night makes LED light group emit white light, and is also ensured that unmanned plane works normally；Electronic component is arranged in the middle part of aluminium radiator
Existing electronic component is mounted in the electronic component installation cavity of aluminium radiator, not only perfect heat-dissipating by installation cavity, and waterproof
Effect is good, is not easy to extend the service life of electronic component into water；
The side of waterproof upper casing is arcwall face, windage can be effectively reduced, so that unmanned plane during flying is reliable；Automatically cable is grabbed
Manipulator is flexible by the push rod of miniature Electrohydraulic push rod, existing cable can be caught in cable limit chamber, to make entire nothing
Man-machine suspension setting, is then turned off rotor flight device, to save unmanned plane power consumption, extends the working time of unmanned plane；
Route is monitored using thermal infrared imaging instrument, video camera and supersonic detector；Thermal infrared imaging instrument can be realized pair
Transmission line of electricity carries out infrared measurement of temperature, monitors route heat condition；Video camera can be realized to transmission pressure, fitting, insulator and
Steel tower corrosion and filthy, line corridor are monitored；Supersonic detector can be realized to existing in route and transmission facility and
Potential crackle is detected.
Complete machine structure design is rationally, structure is simple, assembly and disassembly are easy, waterproof performance is good, easy to use, easy to maintenance and can
It is worked normally under the mal-conditions such as rainy day, night, function is more, and practicability is good.
Above-described embodiment is served only for that invention is further explained to specific descriptions of the invention, should not be understood as
Limiting the scope of the present invention, the technician of this field make the present invention according to the content of foregoing invention some non-
The modifications and adaptations of essence are fallen within the scope of protection of the present invention.
Claims (10)
1. being suitable for the multi-functional unmanned plane of electric inspection process, including unmanned plane main body (1), setting in the unmanned plane main body (1)
Have glove cavity (11), the side of the unmanned plane main body (1) is provided with several rotor flight devices (2)；It is characterized by:
Unmanned plane main body (1) upper end is provided with a waterproof upper casing (3), waterproof upper casing (3) lower end and unmanned plane main body (1)
Threaded upper ends connection, and the first waterproof grommet (4) are provided between waterproof upper casing (3) and unmanned plane main body (1)；The glove
It is provided with an aluminium radiator (8) in cavity (11), has been wholely set multi-disc cooling fin on the outer surface of the aluminium radiator (8)
(81), an opening up electronic component installation cavity (82), the aluminium radiator (8) are provided in the middle part of aluminium radiator (8)
Lower end and glove cavity (11) bottom surface between pass through after being adhesively fixed its junction constitute seal；The aluminium radiator (8)
Upper end protrude into waterproof upper casing (3)；The side of the waterproof upper casing (3) is arcwall face, and the upper surface of waterproof upper casing (3) is flat
Face, the waterproof upper casing (3) are made of transparent plastic material, are fixedly installed on the upper surface of waterproof upper casing (3) and grab automatically
Cable machinery hand (9), the waterproof upper casing (3) is interior to be fixedly installed thermal infrared imaging instrument (13), video camera (14) and ultrasonic wave
Defectoscope (15)；Automatically the cable machinery hand (9) of grabbing includes miniature electro-hydraulic push rod device (91), perpendicular support plate (92) and horizontal limit
Position plate (93), perpendicular support plate (92) lower end and the upper surface of waterproof upper casing (3) are wholely set, the miniature Electrohydraulic push rod dress
The shell and perpendicular support plate (92) for setting (91) are detachably connected, and the push rod upper end of the miniature electro-hydraulic push rod device (91) is integrally set
It is equipped with push plate (95), the upper surface left end of the push plate (95) has been wholely set perpendicular limit plate (94), the push plate (95), perpendicular limit
A cable limit chamber (96) is constituted together between position plate (94), horizontal limit plate (93) and perpendicular support plate (92).
2. the multi-functional unmanned plane according to claim 1 suitable for electric inspection process, it is characterised in that: the push plate (95)
Upper surface on fixed bonding have the first felt pad, perpendicular limit plate (94) right side on fixed bonding have the second felt pad, institute
Stating fixed bonding on the lower end surface of horizontal limit plate (93) has third felt pad, and the left side upper end of the perpendicular support plate (92) is fixed
It is bonded with the 4th felt pad.
3. the multi-functional unmanned plane according to claim 2 suitable for electric inspection process, it is characterised in that: the unmanned owner
The bottom surface of body (1) is plane, and the bottom edge of the unmanned plane main body (1) is provided with several alighting carriages (5), it is described nobody
Detachable setting signal lamp device (6) in the middle part of the bottom surface of owner's body (1), the signal lamp device (6) includes signal lamp lamp holder
(61), it is opened on the lower end surface of the signal lamp lamp holder (61) at least provided with a LED signal lamp (62) and a wireless remote control
It closes (63), is arranged with the first transparent watertight cover (64), each radio remote control switch (63) on each LED signal lamp (62)
On be arranged with the second transparent watertight cover (65)；It is at least set on the signal lamp lamp holder (64) and the bottom surface of unmanned plane main body (1)
It is equipped with second waterproof grommet (7).
4. the multi-functional unmanned plane according to claim 1 or 2 suitable for electric inspection process, it is characterised in that: the electronics
Microprocessor, image capture device, gyroscope, baroceptor, wireless transceiver, satellite are provided in element installation cavity (82)
Positioning and communicating module, memory, stable-pressure device and rechargeable battery, the rechargeable battery by conducting wire respectively with microprocessor, figure
As acquisition equipment, gyroscope, baroceptor, wireless transceiver, satellite positioning communication module, memory, stable-pressure device, rotor
Flight instruments are connected with signal lamp device, and rechargeable battery give each component power supply, the microprocessor by conducting wire respectively with
Image capture device, gyroscope, baroceptor, wireless transceiver, satellite positioning communication module, memory, stable-pressure device and
Rotor flight device connection.
5. the multi-functional unmanned plane according to claim 4 suitable for electric inspection process, it is characterised in that: the rotor flying
Device (2) includes connecting bracket, rotor shell, motor, motor speed measurement instrument and rotor blade, described connecting bracket one end with
Unmanned plane main body is detachably connected or is fixedly connected, and the connecting bracket other end is wholely set with rotor shell, the motor and electricity
Machine tachometer of measuring is arranged in rotor shell, and the rotor blade is set on the main shaft of motor, rotor blade and motor
Main shaft linkage.
6. the multi-functional unmanned plane according to claim 5 suitable for electric inspection process, it is characterised in that: the unmanned owner
The outer surface upper end of body (1) is provided with the first sealing ring mounting groove, and first waterproof grommet (4) is set in the first sealing ring
In mounting groove, waterproof upper casing (3) lower end and unmanned plane main body (1) upper end clamp the first waterproof sealing when screwing by screw thread
It encloses (4), is sealed so that the junction of waterproof upper casing (3) and unmanned plane main body (1) is constituted.
7. the multi-functional unmanned plane according to claim 6 suitable for electric inspection process, it is characterised in that: the unmanned owner
Bottom side alignment signal lamp lamp holder (61) position of body (1) is provided with the second sealing ring mounting groove, second waterproof grommet (7)
It is mounted in the second sealing ring mounting groove, the signal lamp lamp holder (61) connect with the underrun screw of unmanned plane main body (1)
It is fixed, and the upper surface of signal lamp lamp holder (61) compresses the second waterproof grommet (7), so that signal lamp lamp holder (61) and unmanned plane
The bottom surface junction of main body (1) constitutes sealing.
8. the multi-functional unmanned plane according to claim 7 suitable for electric inspection process, it is characterised in that: the LED signal
Lamp (62) and radio remote control switch (63) are connected by screw to fixation with the lower end surface of signal lamp lamp holder (61), and described first thoroughly
Bright waterproof cover (64) and the second transparent watertight cover (65) are adhesively fixed by the lower end surface of glass cement and signal lamp lamp holder (65).
9. the multi-functional unmanned plane according to claim 1 suitable for electric inspection process, it is characterised in that: the alighting carriage
It (5) include stainless steel nut (51), stainless steel connecting rod (52), stainless steel buffer spring (53) and stainless steel plate (54), institute
The bottom surface of the upper surface and unmanned plane main body (1) of stating stainless steel nut (51) is wholely set or is welded and fixed；The stainless steel connects
Extension bar (52) upper end is threadedly coupled with the nut bore of stainless steel nut (51), and the stainless steel buffer spring (53) is set in stainless
In steel connecting rod (52), and the upper end of stainless steel buffer spring (53) is welded and fixed with stainless steel connecting rod (52), described stainless
The lower end of steel buffer spring (53) and the upper surface of stainless steel plate (54) are welded and fixed.
10. the multi-functional unmanned plane according to claim 5 suitable for electric inspection process, it is characterised in that: unmanned plane main body
(1) several connection screwed pipes (12) are provided on side, the connecting bracket is close to unmanned plane main body (1)) end be aligned
Connection screwed pipe (12) is connected through a screw thread fixation.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811150397.7A CN109193453A (en) | 2018-09-29 | 2018-09-29 | Multi-functional unmanned plane suitable for electric inspection process |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811150397.7A CN109193453A (en) | 2018-09-29 | 2018-09-29 | Multi-functional unmanned plane suitable for electric inspection process |
Publications (1)
| Publication Number | Publication Date |
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| CN109193453A true CN109193453A (en) | 2019-01-11 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811150397.7A Pending CN109193453A (en) | 2018-09-29 | 2018-09-29 | Multi-functional unmanned plane suitable for electric inspection process |
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| Country | Link |
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| CN (1) | CN109193453A (en) |
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| CN112382975A (en) * | 2020-11-17 | 2021-02-19 | 国网冀北电力有限公司张家口供电公司 | Rotor wing mixed type line patrol device |
| CN112564285A (en) * | 2020-07-17 | 2021-03-26 | 国网浙江省电力有限公司宁波供电公司 | Regional system diagram management system of transformer substation |
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