CN101694584A - Aero-engine labyrinth disc hot list processing thickness information extraction system - Google Patents

Aero-engine labyrinth disc hot list processing thickness information extraction system Download PDF

Info

Publication number
CN101694584A
CN101694584A CN200910188043A CN200910188043A CN101694584A CN 101694584 A CN101694584 A CN 101694584A CN 200910188043 A CN200910188043 A CN 200910188043A CN 200910188043 A CN200910188043 A CN 200910188043A CN 101694584 A CN101694584 A CN 101694584A
Authority
CN
China
Prior art keywords
data
aero
industrial robot
hot list
labyrinth disc
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
CN200910188043A
Other languages
Chinese (zh)
Inventor
马孜
胡英
黄进
吴翔
王文标
汪洋
张旭
吴德烽
李爱国
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.)
Dalian Maritime University
Original Assignee
Dalian Maritime University
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 Dalian Maritime University filed Critical Dalian Maritime University
Priority to CN200910188043A priority Critical patent/CN101694584A/en
Publication of CN101694584A publication Critical patent/CN101694584A/en
Pending legal-status Critical Current

Links

Images

Classifications

    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P90/00Enabling technologies with a potential contribution to greenhouse gas [GHG] emissions mitigation
    • Y02P90/02Total factory control, e.g. smart factories, flexible manufacturing systems [FMS] or integrated manufacturing systems [IMS]

Abstract

The invention relates to an aero-engine labyrinth disc hot list processing thickness information extraction system which consists of an industrial robot, a laser scanning head and an automatic control positioner, wherein the non-contact laser scanning head is connected with the industrial robot by a data cable for transmitting scanning data, and is connected with a control cabinet by a communication cable so as to transfer the scanning data when receiving a motion command; the control cabinet is connected with a computer through a network port and is used for transferring a control command and the scanning data; the computer mainly completes the core tasks such as motion scan path planning, data processing and coating thickness and the like; and the high accuracy automatic control positioner and the industrial robot are connected with the main control computer by data lines, and receive the control command sent out by the main control computer to finish the spraying operation until a spraying aero-engine labyrinth disc is fixed on the positioner. The system can automatically and efficiently acquire comprehensive aero-engine labyrinth disc hot list processing thickness information distribution data, so as to be applicable to the spraying occasion of the aero-engine labyrinth disc hot list processing.

Description

The aero-engine labyrinth disc hot list processing thickness information extracting system
Technical field
The invention belongs to the detection technique field, the definite aero-engine labyrinth disc hot list processing thickness information extracting system of saying so.
Background technology
The spraying of aeromotor labyrinth is a kind of common hotlist process technology, and each large aerospace engine processing enterprise all is equipped with special painting workshop.Because spraying coating process, there is certain uncertainty in coating thickness, must detect coating thickness.
Existing labyrinth coating thickness measurement method mainly contains: the wedge cutting method, light cuts method, electrolytic process, thickness difference mensuration, weight method, x-ray fluorescence method, β ray backscattering method, capacitance method, ultrasonic method and eddy current measurement method etc.The first five kind is to diminish detection in these methods, and measurement means is loaded down with trivial details, and speed is slow, is applicable to pick test more.X ray and β rays method are contactless nondestructive measurements, but the device complex and expensive, measurement range is less.Capacitance method, ultrasonic method and eddy current measurement method have strict requirement to coated substrate material and coating material, need use corresponding probe at different substrates and coating.In addition, existing characterization processes all is to detect or the method for local detection, can't finish fast detecting and assessment to whole labyrinth coating surface fast, occurs the zone of omission easily and causes product to have hidden danger of quality.
The present invention proposes a kind of aero-engine labyrinth disc hot list processing thickness information extracting method of novel holographic robotization, realized labyrinth surface coating thickness complete, efficiently, the measurement of robotization, solved the problem that existing method exists effectively.
Summary of the invention
The purpose of this invention is to provide a novel aeromotor labyrinth coating thickness information extraction mode, realized aeromotor labyrinth surface coating thickness complete, efficiently, the measurement of robotization.
Principle of the present invention is, cooperate industrial robot, utilize the non-contact laser measuring technique with the high precision in control positioner, before spraying and afterwards, the spraying area of aeromotor labyrinth is carried out three-dimensional surface measurement respectively, operation with the data of twice measurement are subtracted each other along the spraying direction can draw spraying area complete coating thickness distributed intelligence comprehensively.
Technical solution of the present invention is: system is made up of industrial robot 1, non-contact laser scanner head 2, high precision in control positioner 3 and aeromotor labyrinth 4 to be sprayed, as shown in Figure 1.Wherein non-contact laser scanner head 2 is connected with industrial robot 1 by data cable, the transmission scan-data, industrial robot 2 links to each other with switch board by communication cable, accept movement instruction transmission scan data simultaneously, switch board links to each other with main control computer by network interface, transmit steering order and scan-data, main control computer is mainly finished core missions such as motion planning parameters of scanning paths, data presentation, data processing, coating thickness calculating.High precision in control positioner 3, industrial robot 1 link to each other with main control computer by data line, accept the steering order that main control computer sends, and finish spraying operation.Aeromotor labyrinth 4 to be sprayed is fixed on the positioner.
The groundwork flow process of system is as follows: the user imports the basic parameters such as range of size of part to be sprayed by main control computer, and system at first carries out planning parameters of scanning paths, and control robot, positioner and laser feeler carry out surface scan.Scan-data carries out real-time three-dimensional and shows, until the measuring task of finishing whole work-piece.Next spray robot is finished spraying operation according to the technological requirement of spraying.Scan robot then and once more spraying area is carried out surface scan.Final system along spraying the operation that direction is subtracted each other, draws spraying area coating thickness data to twice scan-data, and requires to compare with spraying, provides survey report.
Because native system adopts six degree of freedom industrial robot and non-contact laser scanner head, detection efficiency is higher than the conventional coatings detecting thickness device based on a detection far away.Can finish surface three dimension scanning fast, and serve as according to the control program that generates spraying process fast, greatly improve the work efficiency that aeromotor labyrinth thickness information is extracted with the three-dimensional data of piece surface.In addition, native system can be realized the automatic planning in coat thickness detection path, has overcome problems such as manually getting efficient that point detecting method exists and technical requirement.This cover detection system volume is little, can be placed on the spraying scene, is connected with paint finishing, accomplishes the survey of limit spraying frontier inspection, forms closed-loop system, improves the precision of coating.
The beneficial effect that the present invention reached is: the present invention creatively combines laser surface scanning and industrial robot spraying, has solved the problem of aeromotor labyrinth coating thickness information extraction robotization.The present invention can obtain comprehensive aeromotor labyrinth coating thickness distributed data, has eliminated existing mode and has relied on the various hidden danger that artificial partial check exists.The present invention provides the brand-new technology means for the quality control of aeromotor labyrinth spraying coating process.To greatly improve the efficient of aeromotor labyrinth coat thickness detection by this project implementation, promote labyrinth spraying coating process precision, reduce staff's labour intensity, bring considerable economic and social benefit.In addition, simultaneously, this project assorted software systems can file, add up, analyze testing result, thereby set up a cover complete coating quality monitoring, analytic system, help enterprise to pinpoint the problems and find the root place of problem.At present domestic also do not have similar equipment to occur, and the research of this project has originality, will fill up the blank in domestic air mail engine labyrinth fluted disc coating thickness information extraction field.
Description of drawings
The present invention is further described below in conjunction with the drawings and specific embodiments.
Fig. 1 is a system schematic of the present invention.
Fig. 2 is a concrete implementing procedure of the present invention.
Fig. 3 is the registration report of embodiment.
Fig. 4 is labyrinth thickness information distribution report.
Embodiment
The present invention mainly comprises following three parts:
(1) utilizes industrial robot and non-contact laser scanner head, aeromotor labyrinth to be sprayed is carried out three-dimensional surface scanning.
(2) labyrinth after the spraying is scanned once more
(3) operation that twice scan-data subtracted each other along the spraying direction draws spraying area coating thickness information data.
Below in conjunction with above-mentioned two parts, the coat thickness detection process of a typical labyrinth is described in detail:
Step 1: the basic parameter of input labyrinth
Size: 30 * 20 * 12cm 3,
Material: carbon steel
Surfaceness :≤0.5%.
Step 2: the surface scan before the spraying
Industrial robot drives laser scanning head labyrinth to be sprayed is carried out three-dimensional surface scanning, generates the preceding three-dimensional data of spraying.
Step 3: spraying
Require to finish the surface spraying of labyrinth according to spraying coating process
Step 4: the surface scan after the spraying
Industrial robot drives laser feeler once more labyrinth to be sprayed is carried out three-dimensional surface scanning, generates spraying back three-dimensional data.
Step 5: coating thickness calculates
System software along spraying the operation that direction is subtracted each other, draws spraying area coating thickness data to twice scan-data.
Operation result: Fig. 3 is the registration report of example.Fig. 4 is labyrinth thickness information distribution report.

Claims (3)

1. aero-engine labyrinth disc hot list processing thickness information extracting system, by industrial robot, the non-contact laser scanner head, the high precision in control positioner is formed, it is characterized in that: non-contact laser scanner head (2) is connected with industrial robot (1) by data cable, the transmission scan-data, industrial robot (1) links to each other with switch board by communication cable, accept movement instruction transmission scan data simultaneously, switch board links to each other with main control computer by network interface, transmit steering order and scan-data, main control computer is mainly finished the motion planning parameters of scanning paths, data presentation, data processing, coating thickness calculates core missions, high precision in control positioner (3), industrial robot (1) links to each other with main control computer by data line, accept the steering order that main control computer sends, finish spraying operation, aeromotor labyrinth 4 to be sprayed is fixed on the positioner.
2. aero-engine labyrinth disc hot list processing thickness information extracting system according to claim 1, it is characterized in that: non-contact laser scanner head (2) is to send line-structured light, is fixed on industrial robot (1) end aero-engine labyrinth disc hot list two-dimensional signal before and after treatment is provided.
3. aero-engine labyrinth disc hot list processing thickness information extracting system according to claim 1 is characterized in that: industrial robot (1) provides aero-engine labyrinth disc hot list third dimension information before and after treatment.
CN200910188043A 2009-10-23 2009-10-23 Aero-engine labyrinth disc hot list processing thickness information extraction system Pending CN101694584A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN200910188043A CN101694584A (en) 2009-10-23 2009-10-23 Aero-engine labyrinth disc hot list processing thickness information extraction system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN200910188043A CN101694584A (en) 2009-10-23 2009-10-23 Aero-engine labyrinth disc hot list processing thickness information extraction system

Publications (1)

Publication Number Publication Date
CN101694584A true CN101694584A (en) 2010-04-14

Family

ID=42093558

Family Applications (1)

Application Number Title Priority Date Filing Date
CN200910188043A Pending CN101694584A (en) 2009-10-23 2009-10-23 Aero-engine labyrinth disc hot list processing thickness information extraction system

Country Status (1)

Country Link
CN (1) CN101694584A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107130100A (en) * 2016-02-26 2017-09-05 斗山重工业株式会社 The control method of laser peening device
CN108151661A (en) * 2016-12-02 2018-06-12 上海Abb工程有限公司 A kind of membrane thickness measuring system
CN108838513A (en) * 2018-06-20 2018-11-20 中国民航大学 A kind of laser processing localization method
CN109579760A (en) * 2018-11-22 2019-04-05 北京航天计量测试技术研究所 A kind of measurement method of shaped face heat shield molding thickness
CN109590139A (en) * 2018-12-19 2019-04-09 航天材料及工艺研究所 The multi-shaft interlocked spray equipment of special-shaped structure piece surface heat barrier coating and spraying method
CN113856938A (en) * 2021-11-29 2021-12-31 单县多米石墨烯科技有限公司 Spraying uniformity detection method and system for graphene anticorrosive paint

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107130100A (en) * 2016-02-26 2017-09-05 斗山重工业株式会社 The control method of laser peening device
CN108151661A (en) * 2016-12-02 2018-06-12 上海Abb工程有限公司 A kind of membrane thickness measuring system
CN108838513A (en) * 2018-06-20 2018-11-20 中国民航大学 A kind of laser processing localization method
CN109579760A (en) * 2018-11-22 2019-04-05 北京航天计量测试技术研究所 A kind of measurement method of shaped face heat shield molding thickness
CN109590139A (en) * 2018-12-19 2019-04-09 航天材料及工艺研究所 The multi-shaft interlocked spray equipment of special-shaped structure piece surface heat barrier coating and spraying method
CN113856938A (en) * 2021-11-29 2021-12-31 单县多米石墨烯科技有限公司 Spraying uniformity detection method and system for graphene anticorrosive paint
CN113856938B (en) * 2021-11-29 2022-03-04 单县多米石墨烯科技有限公司 Spraying uniformity detection method and system for graphene anticorrosive paint

Similar Documents

Publication Publication Date Title
CN110654571B (en) Nondestructive testing robot system and method for surface defects of aircraft skin
CN109489580B (en) On-machine point cloud detection and compensation method for surface processing of aero-engine blade
CN109623656B (en) Mobile double-robot cooperative polishing device and method based on thickness online detection
CN101694584A (en) Aero-engine labyrinth disc hot list processing thickness information extraction system
US20180326591A1 (en) Automatic detection and robot-assisted machining of surface defects
CN108931961B (en) Integral end mill wear damage detection method based on machine vision
CN211055414U (en) Nondestructive testing robot system for surface defects of aircraft skin
CN107315391B (en) A kind of pretravel error compensating method of numerically-controlled machine tool on-line checking
CN106600681A (en) A method for polishing a curved surface having obstacles
CN101890638A (en) Assembling system of complex structural member
CN1730248A (en) Reverse engineering robot system
CN104502456A (en) Single-manipulator ultrasonic non-destructive testing device and single-manipulator ultrasonic non-destructive testing method
CN107037130B (en) Monocular vision three-D ultrasonic nondestructive detection system and detection method
CN104535577B (en) A kind of workpiece quality loss detection method
CN109341532A (en) A kind of part coordinate scaling method based on structure feature towards automatic assembling
CN113848182B (en) Composite material layering quality online detection system and detection method
CN103884775A (en) Water immersion ultrasonic automatic flaw detection system used for swing bolster or side frame of railway wagon
CN104833325B (en) Intelligent workpiece metering and detecting unit and using method thereof
CN110281152A (en) A kind of robot constant force polishing paths planning method and system based on online examination touching
CN1987344A (en) Flexible three dimension holographic measuring system
Tang et al. Research on edge detection algorithm based on line laser scanning
CN109055930B (en) Rapid repair method for workpiece surface damage
CN110405259A (en) Free form surface class part system of processing based on multi-sensor integral measuring
CN115717868A (en) Real-time online three-dimensional automatic scanning measurement system
Zhao et al. On-machine measurement of thermal influence of the long-span crossbeam of gantry machine tools using a 3D laser profiler

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Open date: 20100414