CN205607881U - Wind turbine blades inspection device based on unmanned aerial vehicle - Google Patents

Wind turbine blades inspection device based on unmanned aerial vehicle Download PDF

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Publication number
CN205607881U
CN205607881U CN201620155539.9U CN201620155539U CN205607881U CN 205607881 U CN205607881 U CN 205607881U CN 201620155539 U CN201620155539 U CN 201620155539U CN 205607881 U CN205607881 U CN 205607881U
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CN
China
Prior art keywords
module
information
unmanned plane
aerial vehicle
communication module
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Expired - Fee Related
Application number
CN201620155539.9U
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Chinese (zh)
Inventor
韩斌
赵勇
邓巍
房刚利
高平亮
马振国
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Xian Thermal Power Research Institute Co Ltd
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Thermal Power Research Institute
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Publication date
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Priority to CN201620155539.9U priority Critical patent/CN205607881U/en
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Publication of CN205607881U publication Critical patent/CN205607881U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model provides a wind turbine blades inspection device based on unmanned aerial vehicle, including unmanned helicopter, install in the high -definition camera and the equipment of shooing of unmanned helicopter below, install 360 degrees all -round infrared distance meter with the equipment below of shooing in high -definition camera, the communication module of setting on unmanned helicopter, receiving module with communication module wireless connection, the information display module who is connected with receiving module, information storage module, an information processing module, the closely alarm module who is connected with information processing module, still include and control the handle with communication module wireless connection's unmanned aerial vehicle, through the utility model discloses the device can improve the blade and patrol and examine efficiency, reduces workman intensity of labour, can avoid relevant senior engineer's personnel operation through the unmanned aerial vehicle operation, reduce and patrol and examine the cost, and the used time is shorter, can effectively reduce to shut down and send out power loss, the utility model discloses the device can effectively avoid unmanned aerial vehicle to follow the emergence of wind turbine blades, the tower section of thick bamboo accident of bumping from the 360 degrees all -round infrared distance meter and corresponding automatic control, the alarm device in area.

Description

A kind of pneumatic equipment blades inspection device based on unmanned plane
Technical field
This utility model belongs to wind power generation field, fault diagnosis field and field of non destructive testing, specifically Relate to a kind of pneumatic equipment blades inspection device based on unmanned plane.
Background technology
For the detection of in-service wind generator set blade, current most common method is for hope by use Remote mirror or utilize hanging basket people to be suspended on blade surface to observe the damage status of blade, the method pair Blade surface damages, has spread over the crackle of blade and has good recognition reaction.
The most on-the-spot blade fault routine inspection mode mainly has by the visual inspection of binoculars, hanging basket Decline visual inspection (spider-man), blade repair platform inspection etc., said method 1) to patrol and examine efficiency low, Labor strength is big;2) work high above the ground, routing inspection cost is high;3) monitoring time is long, shuts down generated energy Loss is big.
The most traditional have shooting, camera function SUAV when on-the-spot blade is patrolled and examined by Impact in fitful wind can not be the nearest close to blade, prevent unmanned plane with sending out that blade crashes Raw (mainly due to consideration of safety), causes some tiny defects of blade surface to be difficult to be found.
Summary of the invention
For the deficiencies in the prior art, the purpose of this utility model is to provide a kind of based on nothing Man-machine pneumatic equipment blades inspection device, can improve blade by this utility model and patrol and examine efficiency, fall Low labor strength, can avoid senior engineer's related personnel operation by unmanned plane operation, and reduction is patrolled and examined Cost, and the time used is shorter, can effectively reduce shutdown generated energy loss;This utility model device is certainly Band 360 degree of all-directional infrared diastimeters and automatically control accordingly, alarm device, can be prevented effectively from The generation that unmanned plane crashes with blade.
For realizing object above, the technical solution adopted in the utility model is:
A kind of pneumatic equipment blades inspection device based on unmanned plane, including for carrying shooting, taking pictures sets The standby depopulated helicopter 1 arriving appointment position, is installed on the acquisition wind energy conversion system below depopulated helicopter 1 The high-definition camera of blade surface information and photographing device 2, be installed on high-definition camera and photographing device 2 times The unmanned plane of monitoring in real time of side and pneumatic equipment blades, 360 degree of all-directional infrared range findings of tower spacing Instrument 3, be arranged on depopulated helicopter 1 passes the image information obtained and range information real-time radio It is passed to ground and receives the communication module 4 of ground-launched control instruction, company wireless with communication module 4 The information receiving module 5 for obtaining the information that communication module 4 transmission comes connect, receives mould with information The information display module 6 of the information that the camera head of display in real time that block 5 connects photographs, connects with information The information storage module 7 of the information that the real-time storage information receiving module that receipts module 5 connects receives, The 360 degree of all-directional infrared diastimeters 3 that process in real time being connected with information receiving module 5 detect unmanned Range information between machine and blade or tower, and the message processing module 8 compared with setting value, Be connected with message processing module 8 detects unmanned plane and blade or tower when all-directional infrared diastimeter 3 Range information between Tong provides alarm less than this module during the value set with sound or alternate manner Short-distance alarm module 9, also include with communication module 4 wireless connections for controlling unmanned plane Flight and launching relevant is taken pictures, the unmanned plane control handle 10 of instruction of recording a video.
The value of described setting determines according to the following rules not less than D, D value: when depopulated helicopter 1 carries More than d+50cm, (wherein d is unmanned to the minimum effectively shooting distance f of high-definition camera and photographing device 2 Machine effective diameter, unit cm), D=f, the high-definition camera carried when depopulated helicopter 1 and photographing device The minimum effectively shooting distance f of 2 is less than d+50cm (wherein d is unmanned plane effective diameter, unit cm), D=d+50cm.
The most relatively, this utility model possesses following advantage:
1, at this utility model device carries 360 degree of all-directional infrared diastimeters and corresponding information Reason module, short-distance alarm module, can be prevented effectively from unmanned plane and touch with pneumatic equipment blades or tower Hit the generation of accident.
2, this utility model device is owing to having carried 360 degree of all-directional infrared diastimeters, can make unmanned Machine is as close as pneumatic equipment blades surface, it is simple to find some tiny defects of blade surface.
The effect that above-mentioned advantage is brought: blade can be improved and patrol and examine efficiency and effectiveness, reduce workman's labor Fatigue resistance, can avoid senior engineer's related personnel operation by unmanned plane operation, reduces routing inspection cost, and Time used is shorter, can effectively reduce shutdown generated energy loss.
Accompanying drawing explanation
Fig. 1 is that this utility model pneumatic equipment blades based on unmanned plane inspection device constitutes block diagram.
Detailed description of the invention
In order to make the purpose of this utility model, technical scheme and advantage more clear and concise, below in conjunction with Drawings and Examples, are further elaborated to this utility model.Should be appreciated that this place is retouched The specific embodiment stated, only in order to explain this utility model, is not used to limit this utility model.
As it is shown in figure 1, a kind of pneumatic equipment blades inspection device based on unmanned plane of this utility model, bag Include for carrying shooting, photographing device arrives the depopulated helicopter 1 specifying position, is installed on unmanned straight Rise the high-definition camera obtaining pneumatic equipment blades surface information below machine 1 and photographing device 2, be installed on The unmanned plane of monitoring in real time below high-definition camera and photographing device 2 and pneumatic equipment blades, tower spacing 360 degree of all-directional infrared diastimeters 3, be arranged on depopulated helicopter 1 will obtain image letter Breath and range information real-time radio are transferred to ground and receive the communication mould of ground-launched control instruction Block 4, with the information for obtaining the information that communication module 4 transmission comes of communication module 4 wireless connections Receiver module 5, the information that the camera head of display in real time being connected with information receiving module 5 photographs Information display module 6, the real-time storage information receiving module being connected with information receiving module 5 receives The information storage module 7 of information, be connected with information receiving module 5 processes 360 degree the most in real time Position infrared range-measurement system 3 detects the range information between unmanned plane and blade or tower, and enters with setting value The message processing module 8 that compares of row, be connected with message processing module 8 when all-directional infrared diastimeter 3 detect that when the range information between unmanned plane and blade or tower is less than the value set, this module is with sound Or alternate manner provides the short-distance alarm module 9 of alarm, also include wireless with communication module 4 Being correlated with for the flight and transmitting controlling unmanned plane of connecting is taken pictures, the unmanned plane manipulation hands of instruction of recording a video Handle 10.
As preferred implementation of the present utility model, the value of described setting is not less than D D, and D value is by such as Lower rule determines: the shooting carried when unmanned plane and the minimum effectively shooting distance f of device are more than D+50cm (wherein d is unmanned plane effective diameter, unit cm), D=f, when the shooting that unmanned plane carries And the minimum effectively shooting distance f of device is less than d+50cm, and (wherein d is unmanned plane effective diameter, single Position cm), D=d+50cm.Make unmanned plane as close as pneumatic equipment blades surface.

Claims (1)

  1. null1. a pneumatic equipment blades inspection device based on unmanned plane,It is characterized in that: include for carrying shooting、Photographing device arrives the depopulated helicopter (1) specifying position,It is installed on the high-definition camera obtaining pneumatic equipment blades surface information and the photographing device (2) of depopulated helicopter (1) lower section,It is installed on monitoring unmanned plane and the pneumatic equipment blades in real time of high-definition camera and photographing device (2) lower section、360 degree of all-directional infrared diastimeters (3) of tower spacing,It is arranged on the image information by acquisition on depopulated helicopter (1) and range information real-time radio is transferred to ground and receives the communication module (4) of ground-launched control instruction,With communication module (4) wireless connections be used for obtain the information receiving module (5) of information that communication module (4) transmission comes,The information display module (6) of the information that the camera head of display in real time being connected with information receiving module (5) photographs,The information storage module (7) of the information that the real-time storage information receiving module being connected with information receiving module (5) receives,The 360 degree of all-directional infrared diastimeters (3) that process in real time being connected with information receiving module (5) detect the range information between unmanned plane and blade or tower,And the message processing module (8) compared with setting value,This module when the range information that all-directional infrared diastimeter (3) detects between unmanned plane and blade or tower is less than the value set being connected with message processing module (8) provides the short-distance alarm module (9) of alarm with sound or alternate manner,Also include the flight being used for controlling unmanned plane to communication module (4) wireless connections and launch relevant taking pictures、The unmanned plane control handle (10) of video recording instruction.
CN201620155539.9U 2016-03-01 2016-03-01 Wind turbine blades inspection device based on unmanned aerial vehicle Expired - Fee Related CN205607881U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620155539.9U CN205607881U (en) 2016-03-01 2016-03-01 Wind turbine blades inspection device based on unmanned aerial vehicle

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Application Number Priority Date Filing Date Title
CN201620155539.9U CN205607881U (en) 2016-03-01 2016-03-01 Wind turbine blades inspection device based on unmanned aerial vehicle

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CN205607881U true CN205607881U (en) 2016-09-28

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106762451A (en) * 2016-12-05 2017-05-31 北京金风科创风电设备有限公司 Fan blade damage detection method, device and system based on unmanned aerial vehicle
CN106841214A (en) * 2017-01-21 2017-06-13 兰州理工大学 A kind of non-contact wind power blade dust storm erosion degree detection method
CN108252872A (en) * 2016-12-29 2018-07-06 财团法人金属工业研究发展中心 Wind turbine blade face view finding method and its unmanned plane, the computer program product of internally stored program and the medium capable of reading record used
CN110471447A (en) * 2019-08-27 2019-11-19 无锡风电设计研究院有限公司 The method for inspecting and system of wind energy conversion system

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106762451A (en) * 2016-12-05 2017-05-31 北京金风科创风电设备有限公司 Fan blade damage detection method, device and system based on unmanned aerial vehicle
CN106762451B (en) * 2016-12-05 2018-10-23 北京金风科创风电设备有限公司 Fan blade damage detection method, device and system based on unmanned aerial vehicle
CN108252872A (en) * 2016-12-29 2018-07-06 财团法人金属工业研究发展中心 Wind turbine blade face view finding method and its unmanned plane, the computer program product of internally stored program and the medium capable of reading record used
CN106841214A (en) * 2017-01-21 2017-06-13 兰州理工大学 A kind of non-contact wind power blade dust storm erosion degree detection method
CN110471447A (en) * 2019-08-27 2019-11-19 无锡风电设计研究院有限公司 The method for inspecting and system of wind energy conversion system

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C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20160928

Termination date: 20170301

CF01 Termination of patent right due to non-payment of annual fee