CN109193453A - Multi-functional unmanned plane suitable for electric inspection process - Google Patents

Multi-functional unmanned plane suitable for electric inspection process Download PDF

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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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CN
China
Prior art keywords
waterproof
main body
drone
stainless steel
sealing ring
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201811150397.7A
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Chinese (zh)
Inventor
陈蕾
徐重酉
潘杰锋
高文婷
袁忠君
刘月娥
王彦波
曹华
朱岩
李峥嵘
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
State Grid Zhejiang Electric Power Co Ltd
Ningbo Power Supply Co of State Grid Zhejiang Electric Power Co Ltd
Electric Power Research Institute of State Grid Beijing Electric Power Co Ltd
Original Assignee
State Grid Zhejiang Electric Power Co Ltd
Ningbo Power Supply Co of State Grid Zhejiang Electric Power Co Ltd
Electric Power Research Institute of State Grid Beijing Electric Power Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by State Grid Zhejiang Electric Power Co Ltd, Ningbo Power Supply Co of State Grid Zhejiang Electric Power Co Ltd, Electric Power Research Institute of State Grid Beijing Electric Power Co Ltd filed Critical State Grid Zhejiang Electric Power Co Ltd
Priority to CN201811150397.7A priority Critical patent/CN109193453A/en
Publication of CN109193453A publication Critical patent/CN109193453A/en
Pending legal-status Critical Current

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Classifications

    • 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

本发明公开了一种适用于电力巡检的多功能无人机，包括无人机主体，无人机主体内设置有置物空腔，无人机主体的侧面设置有若干个旋翼飞行装置；无人机主体上端设置有一个防水上壳，防水上壳与无人机主体之间设置有第一防水密封圈；置物空腔内铝散热器的中部设置有一个开口朝上的电子元件安装腔，防水上壳的侧面为弧形面，防水上壳的上端面为平面，防水上壳由透明的塑料材料制成，防水上壳的上端面上固定设置有自动抓电缆机械手，防水上壳内固定设置有热红外成像仪、摄像机和超声波探伤仪。上述技术方案，结构设计合理、结构简单、装拆容易、防水性能好、工作时间长、使用方便且能够在在雨天、夜间等恶劣条件下正常工作。

The invention discloses a multifunctional unmanned aerial vehicle suitable for electric power inspection. The upper end of the man-machine main body is provided with a waterproof upper casing, and a first waterproof sealing ring is arranged between the waterproof upper casing and the main body of the drone; the middle part of the aluminum radiator in the storage cavity is provided with an electronic component installation cavity with an opening facing upwards. The side surface of the waterproof upper shell is curved surface, the upper end surface of the waterproof upper shell is flat, the waterproof upper shell is made of transparent plastic material, the upper end surface of the waterproof upper shell is fixed with an automatic cable grasping manipulator, and the waterproof upper shell is fixed inside Set up with thermal infrared imager, camera and ultrasonic flaw detector. The above technical solution has the advantages of reasonable structural design, simple structure, easy assembly and disassembly, good waterproof performance, long working time, convenient use, and can work normally in harsh conditions such as rainy days and nights.

Description

Multi-functional unmanned plane suitable for electric inspection process
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.适用于电力巡检的多功能无人机，包括无人机主体(1)，所述无人机主体(1)内设置有置物空腔(11)，所述无人机主体(1)的侧面设置有若干个旋翼飞行装置(2)；其特征在于：所述无人机主体(1)上端设置有一个防水上壳(3)，所述防水上壳(3)下端与无人机主体(1)上端螺纹连接，且防水上壳(3)与无人机主体(1)之间设置有第一防水密封圈(4)；所述置物空腔(11)内设置有一个铝散热器(8)，所述铝散热器(8)的外表面上一体设置有多片散热片(81)，铝散热器(8)的中部设置有一个开口朝上的电子元件安装腔(82)，所述铝散热器(8)的下端与置物空腔(11)的底面之间通过粘接固定后其连接处构成密封；所述铝散热器(8)的上端伸入防水上壳(3)内；所述防水上壳(3)的侧面为弧形面，防水上壳(3)的上端面为平面，所述防水上壳(3)由透明的塑料材料制成，防水上壳(3)的上端面上固定设置有自动抓电缆机械手(9)，所述防水上壳(3)内固定设置有热红外成像仪(13)、摄像机(14)和超声波探伤仪(15)；所述自动抓电缆机械手(9)包括微型电液推杆装置(91)、竖支撑板(92)和横限位板(93)，所述竖支撑板(92)下端与防水上壳(3)的上端面一体设置，所述微型电液推杆装置(91)的壳体与竖支撑板(92)可拆卸连接，所述微型电液推杆装置(91)的推杆上端一体设置有推板(95)，所述推板(95)的上端面左端一体设置有竖限位板(94)，所述推板(95)、竖限位板(94)、横限位板(93)和竖支撑板(92)之间一起构成一个电缆限位腔(96)。1. A multifunctional drone suitable for electric power inspection, comprising a drone main body (1), wherein a storage cavity (11) is provided in the drone main body (1), and the drone main body (1) is provided with an object storage cavity (11). ) is provided with several rotor flight devices (2); it is characterized in that: the upper end of the drone main body (1) is provided with a waterproof upper shell (3), and the lower end of the waterproof upper shell (3) is connected with the unmanned aerial vehicle. The upper end of the main body (1) is screwed together, and a first waterproof sealing ring (4) is arranged between the waterproof upper casing (3) and the main body (1) of the drone; an aluminum alloy is arranged in the storage cavity (11). A radiator (8), the outer surface of the aluminum radiator (8) is integrally provided with a plurality of fins (81), and the middle of the aluminum radiator (8) is provided with an electronic component mounting cavity (82) with an opening facing upwards ), the lower end of the aluminum radiator (8) and the bottom surface of the storage cavity (11) are fixed by bonding to form a seal; the upper end of the aluminum radiator (8) extends into the waterproof upper shell ( 3) inside; the side surface of the waterproof upper shell (3) is an arc surface, the upper end surface of the waterproof upper shell (3) is a plane, the waterproof upper shell (3) is made of a transparent plastic material, and the waterproof upper shell (3) is made of a transparent plastic material. The upper end surface of (3) is fixedly provided with an automatic cable grasping manipulator (9), and a thermal infrared imager (13), a camera (14) and an ultrasonic flaw detector (15) are fixedly arranged in the waterproof upper casing (3); The automatic cable grasping manipulator (9) includes a miniature electro-hydraulic push rod device (91), a vertical support plate (92) and a horizontal limit plate (93), and the lower end of the vertical support plate (92) is connected to the waterproof upper shell (3). The upper end face of the miniature electro-hydraulic push rod device (91) is detachably connected to the vertical support plate (92), and the upper end of the push rod of the miniature electro-hydraulic push rod device (91) is integrally provided with a A push plate (95), the left end of the upper end face of the push plate (95) is integrally provided with a vertical limit plate (94), the push plate (95), the vertical limit plate (94), the horizontal limit plate (93) ) and the vertical support plate (92) together form a cable limiting cavity (96). 2.根据权利要求1所述的适用于电力巡检的多功能无人机，其特征在于：所述推板(95)的上端面上固定粘接有第一绝缘垫、竖限位板(94)的右端面上固定粘接有第二绝缘垫，所述横限位板(93)的下端面上固定粘接有第三绝缘垫，所述竖支撑板(92)的左端面上端固定粘接有第四绝缘垫。2. The multifunctional unmanned aerial vehicle suitable for power inspection according to claim 1, characterized in that: the upper end surface of the push plate (95) is fixedly bonded with a first insulating pad, a vertical limit plate ( A second insulating pad is fixedly adhered to the right end surface of 94), a third insulating pad is fixedly adhered to the lower end surface of the horizontal limit plate (93), and the left end surface of the vertical support plate (92) is fixed to the upper end. A fourth insulating pad is bonded. 3.根据权利要求2所述的适用于电力巡检的多功能无人机，其特征在于：所述无人机主体(1)的底面为平面，所述无人机主体(1)的底面边缘设置有若干个降落支架(5)，所述无人机主体(1)的底面中部可拆卸设置信号灯装置(6)，所述信号灯装置(6)包括信号灯灯座(61)，所述信号灯灯座(61)的下端面上至少设置有一个LED信号灯(62)和一个无线遥控开关(63)，所述每个LED信号灯(62)上均套设有第一透明防水罩(64)，每个无线遥控开关(63)上均套设有第二透明防水罩(65)；所述信号灯灯座(64)与无人机主体(1)的底面上至少设置有一个第二防水密封圈(7)。3. The multifunctional drone suitable for power inspection according to claim 2, wherein the bottom surface of the drone body (1) is a plane, and the bottom surface of the drone body (1) A number of landing brackets (5) are arranged on the edges, and a signal light device (6) is detachably arranged in the middle of the bottom surface of the drone main body (1). At least one LED signal light (62) and a wireless remote control switch (63) are provided on the lower end surface of the lamp holder (61), and a first transparent waterproof cover (64) is sleeved on each LED signal light (62), A second transparent waterproof cover (65) is sleeved on each wireless remote control switch (63); at least one second waterproof sealing ring is provided on the bottom surface of the signal lamp socket (64) and the drone body (1) (7). 4.根据权利要求1或2所述的适用于电力巡检的多功能无人机，其特征在于：所述电子元件安装腔(82)内设置有微处理器、图像采集设备、陀螺仪、气压传感器、无线收发器、卫星定位通信模块、存储器、稳压装置和充电电池，所述充电电池通过导线分别与微处理器、图像采集设备、陀螺仪、气压传感器、无线收发器、卫星定位通信模块、存储器、稳压装置、旋翼飞行装置和信号灯装置连接，并且充电电池给各部件供电，所述微处理器通过导线分别与图像采集设备、陀螺仪、气压传感器、无线收发器、卫星定位通信模块、存储器、稳压装置和旋翼飞行装置连接。4. The multifunctional unmanned aerial vehicle suitable for power inspection according to claim 1 or 2, characterized in that: a microprocessor, an image acquisition device, a gyroscope, a Air pressure sensor, wireless transceiver, satellite positioning communication module, memory, voltage stabilizer and rechargeable battery, the rechargeable battery communicates with microprocessor, image acquisition device, gyroscope, air pressure sensor, wireless transceiver, satellite positioning through wire respectively The module, memory, voltage stabilization device, rotor flight device and signal light device are connected, and the rechargeable battery supplies power to each component, and the microprocessor communicates with image acquisition equipment, gyroscope, air pressure sensor, wireless transceiver and satellite positioning through wires. Modules, memories, voltage regulators, and rotorcraft connections. 5.根据权利要求4所述的适用于电力巡检的多功能无人机，其特征在于：所述旋翼飞行装置(2)包括连接支架、旋翼壳体、电机、电机转速测量仪和旋翼叶片，所述连接支架一端与无人机主体可拆卸连接或固定连接，连接支架另一端与旋翼壳体一体设置，所述电机和电机转速测量仪均设置在旋翼壳体内，所述旋翼叶片套设在电机的主轴上，旋翼叶片与电机的主轴联动。5. The multifunctional unmanned aerial vehicle suitable for power inspection according to claim 4, wherein the rotor flight device (2) comprises a connecting bracket, a rotor housing, a motor, a motor speed measuring instrument and a rotor blade One end of the connecting bracket is detachably connected or fixedly connected to the main body of the UAV, and the other end of the connecting bracket is integrally arranged with the rotor housing, the motor and the motor speed measuring instrument are both arranged in the rotor housing, and the rotor blades are sleeved On the main shaft of the motor, the rotor blades are linked with the main shaft of the motor. 6.根据权利要求5所述的适用于电力巡检的多功能无人机，其特征在于：所述无人机主体(1)的外表面上端设置有第一密封圈安装槽，所述第一防水密封圈(4)套设在第一密封圈安装槽内，所述防水上壳(3)下端与无人机主体(1)上端通过螺纹旋紧时夹紧第一防水密封圈(4)，使得防水上壳(3)与无人机主体(1)的连接处构成密封。6. The multifunctional drone suitable for power inspection according to claim 5, characterized in that: the outer surface of the drone main body (1) is provided with a first sealing ring installation groove, and the A waterproof sealing ring (4) is sleeved in the first sealing ring installation groove, and the first waterproof sealing ring (4) is clamped when the lower end of the waterproof upper shell (3) and the upper end of the drone main body (1) are screwed together by threads ), so that the connection between the waterproof upper casing (3) and the drone body (1) forms a seal. 7.根据权利要求6所述的适用于电力巡检的多功能无人机，其特征在于：所述无人机主体(1)的底面对准信号灯灯座(61)位置设置有第二密封圈安装槽，所述第二防水密封圈(7)安装在第二密封圈安装槽内，所述信号灯灯座(61)与无人机主体(1)的底面通过螺钉连接固定，且信号灯灯座(61)的上端面压紧第二防水密封圈(7)，使得信号灯灯座(61)与无人机主体(1)的底面连接处构成密封。7. The multifunctional drone suitable for power inspection according to claim 6, wherein the bottom surface of the drone main body (1) is aligned with the signal lamp socket (61) and is provided with a second A sealing ring installation groove, the second waterproof sealing ring (7) is installed in the second sealing ring installation groove, the signal lamp socket (61) is fixed with the bottom surface of the drone main body (1) by screws, and the signal lamp The upper end surface of the lamp holder (61) presses the second waterproof sealing ring (7), so that the connection between the signal lamp lamp holder (61) and the bottom surface of the drone main body (1) forms a seal. 8.根据权利要求7所述的适用于电力巡检的多功能无人机，其特征在于：所述LED信号灯(62)和无线遥控开关(63)均与信号灯灯座(61)的下端面通过螺钉连接固定，所述第一透明防水罩(64)和第二透明防水罩(65)均通过玻璃胶与信号灯灯座(65)的下端面粘接固定。8 . The multifunctional drone suitable for power inspection according to claim 7 , wherein the LED signal light ( 62 ) and the wireless remote control switch ( 63 ) are connected to the lower end surface of the signal light socket ( 61 ). 9 . The first transparent waterproof cover (64) and the second transparent waterproof cover (65) are both bonded and fixed to the lower end surface of the signal lamp socket (65) through glass glue. 9.根据权利要求1所述的适用于电力巡检的多功能无人机，其特征在于：所述降落支架(5)包括不锈钢螺母(51)、不锈钢连接杆(52)、不锈钢缓冲弹簧(53)和不锈钢底板(54)，所述不锈钢螺母(51)的上端面与无人机主体(1)的底面一体设置或焊接固定；所述不锈钢连接杆(52)上端与不锈钢螺母(51)的螺母孔螺纹连接，所述不锈钢缓冲弹簧(53)套设在不锈钢连接杆(52)上，且不锈钢缓冲弹簧(53)的上端与不锈钢连接杆(52)焊接固定，所述不锈钢缓冲弹簧(53)的下端与不锈钢底板(54)的上端面焊接固定。9. The multifunctional drone suitable for power inspection according to claim 1, wherein the landing bracket (5) comprises a stainless steel nut (51), a stainless steel connecting rod (52), a stainless steel buffer spring ( 53) and a stainless steel bottom plate (54), the upper end surface of the stainless steel nut (51) is integrally arranged with the bottom surface of the drone main body (1) or fixed by welding; the upper end of the stainless steel connecting rod (52) is connected to the stainless steel nut (51) The stainless steel buffer spring (53) is sleeved on the stainless steel connecting rod (52), and the upper end of the stainless steel buffer spring (53) is welded and fixed with the stainless steel connecting rod (52). The lower end of 53) is fixed by welding with the upper end surface of the stainless steel bottom plate (54). 10.根据权利要求5所述的适用于电力巡检的多功能无人机，其特征在于：无人机主体(1)的侧面上设置有若干根连接螺管(12)，所述连接支架靠近无人机主体(1))端与对准的连接螺管(12)通过螺纹连接固定。10. The multifunctional drone suitable for electric power inspection according to claim 5, characterized in that: a plurality of connecting solenoids (12) are provided on the side of the drone main body (1), and the connecting brackets The end close to the main body (1)) of the drone is fixed with the aligned connecting solenoid (12) through screw connection.
CN201811150397.7A 2018-09-29 2018-09-29 Multi-functional unmanned plane suitable for electric inspection process Pending CN109193453A (en)

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