CN209231267U - A kind of test of flaw detection system of turbocompressor blade - Google Patents

A kind of test of flaw detection system of turbocompressor blade Download PDF

Info

Publication number
CN209231267U
CN209231267U CN201821890889.5U CN201821890889U CN209231267U CN 209231267 U CN209231267 U CN 209231267U CN 201821890889 U CN201821890889 U CN 201821890889U CN 209231267 U CN209231267 U CN 209231267U
Authority
CN
China
Prior art keywords
test
flaw detection
detection system
sliding sleeve
turbocompressor
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.)
Active
Application number
CN201821890889.5U
Other languages
Chinese (zh)
Inventor
王小龙
白永贵
赵成
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.)
Sichuan Poly Heavy Industry Co Ltd
Original Assignee
Sichuan Poly Heavy Industry 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 Sichuan Poly Heavy Industry Co Ltd filed Critical Sichuan Poly Heavy Industry Co Ltd
Priority to CN201821890889.5U priority Critical patent/CN209231267U/en
Application granted granted Critical
Publication of CN209231267U publication Critical patent/CN209231267U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Investigating Or Analyzing Materials By The Use Of Ultrasonic Waves (AREA)

Abstract

The utility model discloses a kind of test of flaw detection systems of turbocompressor blade, belong to turbocompressor preparation technical field.By the setting of pedestal, support device, detection device, multi-joint manipulator and calibrating installation etc., the problems such as blade test of flaw detection is limited in the prior art is solved;This test of flaw detection system can be realized to different size model turbocompressor blade in system and In-service testing, guarantee the accessibility and covering comprehensively of detection zone;This test of flaw detection system accuracies are high, easy to operate, applied widely, and labor intensity can be effectively reduced, and improve production efficiency.

Description

A kind of test of flaw detection system of turbocompressor blade
Technical field
The utility model relates to a kind of test of flaw detection systems, especially be related to a kind of test of flaw detection of turbocompressor blade System belongs to turbocompressor preparation technical field.
Background technique
Turbocompressor is for improving gas pressure and conveying the machinery of gas, is to have moving for high-speed rotating impeller Power formula compressor improves gas pressure by the interaction force between rotary blade and air-flow, while generates air-flow and adding Speed and obtain kinetic energy, then air-flow slows down in diffuser, converts kinetic energy into pressure energy, further increases pressure, is pressing Gas flowing is continuous in compression process.It, which is widely used in various technical process, conveys air and various gases, and improves it Pressure, while gas temperature also correspondinglys increase.By multistage-combination, also there are intercooled multistage combination or even multi-cylinder combination Compression obtains final pressure required for gas.Impeller in turbocompressor is the mostly important component of whole equipment, works as pressure When contracting machine is run under design conditions, air-flow flowed in runner it is smooth, with geometric dimension no-float, airflow direction and blade Geometry established angle it is consistent, the work coordinations at different levels of compressor at this moment, overall efficiency is high.And when blade exists and damages, meeting Making compressor, air-flow flowing is abnormal in the process of running, causes compressor performance can be greatly reduced, there is also pressure when serious Contracting machine rotor and stator are subjected to alternate stress effect and are broken, and keep interstage pressure not normal and cause judder.Cause sealing and Damage of thrust pad;So that motor element and stationary element is collided, causes major accident.
Blade is also easy to produce fracture and crackle equivalent damage problem under high speed rotation in turbocompressor.In turbocompressor In actual use, since turbocompressor blade inlet port is impacted by impurity and root of blade is corroded etc. draws It plays material surface and generates microdefect, eventually lead to blade and generate fatigue fracture under the action of reversed torsion power.As a result, in order to Guarantee turbocompressor stable operation, needs accurately to obtain crop leaf measuring data.
Currently, when carrying out test of flaw detection to blade ultrasound examination, consumption need to be carried out to rotor by manually mode Take a large amount of man power and material, this not only large labor intensity, detection cycle is longer, and for the rotor that blade assembly is completed When In-service testing, manual detection mode can not then be implemented.
A kind of publication number CN204925043U is disclosed on December 30th, 2015, patent name is " flaw detection robot " Utility model patent, the flaw detection robot include robot, scanning frame, mould group, electric control system, ultrasound detection host, rolling Wheel carrier and operation machine, robot includes robot body, robot control cabinet and robot demonstrator, realizes flaw detection data The label of record and spatial coordinate location.It is visited since the structure can not detect the surface layout to be checked of blade in turbocompressor Head, and it is unable to complete the covering detection of detection faces, therefore it is not suitable for the workpiece configurations and specification of blade in turbocompressor.
A kind of publication number CN106662553A was disclosed on May 10th, 2017, patent name is " turbine rotor disc The utility model patent of the defect detection on ultrasonic basis and device of blade groove portion ", the device disclose ultrasonic examination, phased array The components such as probe, probe supporting arrangement, elastic component, height adjusting part, arm and trolley, can change the depth of examination scope. The patent checks the fixed blade groove portion of the turbo blade for that will be set on the rotor disk of turbine, probe using phase array method Only phased array probe has some limitations when in use, and application range is relatively narrow.
Utility model content
The utility model overcomes the shortcomings of the prior art, and proposes a kind of test of flaw detection of turbocompressor blade System.This test of flaw detection system passes through the setting of pedestal, support device, detection device, multi-joint manipulator and calibrating installation etc., Solve the problems such as blade test of flaw detection is limited in the prior art;This test of flaw detection system can be realized to different size model turbine pressure Contracting machine blade in system and In-service testing, guarantee the accessibility and covering comprehensively of detection zone;This test of flaw detection system accuracies Height, it is easy to operate, it is applied widely, and labor intensity can be effectively reduced, improve production efficiency.
In order to achieve the above technical purposes, the following technical solution is proposed:
A kind of test of flaw detection system of turbocompressor blade, including pedestal and the support device and inspection that are set on the base Device is surveyed, pedestal includes multiple base units, is connected between base unit for pin-connected panel;
Support device includes that vertically arranged strut, sliding sleeve and hydraulically extensible part, strut are fixed on by removably On base unit, strut top is equipped with upper limit position block, and lower part is equipped with lower position block, and sliding sleeve is set in upper limit position block and lower position block Between;Sliding sleeve includes sliding sleeve I and sliding sleeve II, and sliding sleeve I is arranged above sliding sleeve II, and sliding sleeve I passes through connecting rod and hydraulically extensible part Connection, the hydraulically extensible part other end are connect with sliding sleeve II, and hydraulically extensible part is equipped with gate gurgle valve;
Detection device includes detection probe and distance measuring sensor, and code-disc is equipped with above detection probe, and code-disc is connected by flexible Fitting is connect with detection probe;Distance measuring sensor setting in detection probe two sides, and distance measuring sensor by be telescopically connected to part with Detection probe connection;Detection probe is connect by multi-joint manipulator with sliding sleeve I, and detection probe is arranged at multi-joint manipulator end Portion, and be equipped between detection probe and multi-joint manipulator and be telescopically connected to part;
Calibrating installation is additionally provided on base unit, calibrating installation includes multi-joint manipulator and is arranged in multi-joint manipulator The color mark sensor of end, color mark sensor are connect by being telescopically connected to part with multi-joint manipulator.
Further, the bottom of the pedestal is equipped with sliding equipment.
Further, the sliding equipment includes guide rail, and guide rail is connected with driving device.
Further, the driving device is motor, and retarder is equipped between driving device and pedestal.
Further, the sliding equipment includes pulley, and pulley is cardan wheel with brake.
Further, the removably includes being bolted and snapping connection.
Further, the detection probe is ultrasonic phase array probe.
Further, the distance measuring sensor is ultraviolet distance measuring sensor or laser range sensor.
Further, the multi-joint manipulator is the robot of four-degree-of-freedom or the robot of six degree of freedom, according to saturating The robot of different size difference freedom degrees may be selected in flat compressor assembly product and space requirement, multi-joint manipulator.
Further, the strut, upper limit position block and lower position block are integrally formed setting.
The test of flaw detection system further includes signal receiver, analysis center and remote controllers, signal receiver and inspection Probing head, distance measuring sensor, code-disc and color mark sensor connection, signal receiver connect with analysis center, analysis center with far Range controller connection;And analysis center is connected with display screen and alarm.Reception, processing and the feedback of test of flaw detection signal, and Long-range control etc., is the test of flaw detection signal working process technology in existing mature technology.
Using the technical program, bring advantageous effects are as follows:
1) in the present invention, test of flaw detection system passes through pedestal, support device, detection device, multi-joint manipulator And the setting of calibrating installation, solve the problems such as blade test of flaw detection is limited in the prior art;This test of flaw detection system can be realized pair Different size model turbocompressor blade in system and In-service testing, guarantee the accessibility and covering comprehensively of detection zone;This Test of flaw detection system accuracies are high, easy to operate, applied widely, and labor intensity can be effectively reduced, and improve production efficiency.
2) in the present invention, the setting of pin-connected panel pedestal, convenient for transport, installation and the receipts of a whole set of test of flaw detection system It the assembling such as picks up, and facilitates support device, detection device, and then expand the detection range to blade;
3) in the support device of the utility model, the setting of strut, sliding sleeve and hydraulically extensible part etc. guarantees multi-joint machine Tool hand can stablize, it is controllable move up and down, and then improve the efficiency and quality of blade test of flaw detection process;
4) in the detection device of the utility model, it is telescopically connected to the setting of part, guarantees that detection probe, code-disc, ranging pass Sensor and color mark sensor are with the freedom degree with elastic telescopic, when guaranteeing that multi-joint manipulator expands in place, multi-joint machine The face flexible contact to be checked of tool hand end and blade to be checked, and the pressure limit of adaptation is progressivelyed reach, to realize detection probe It is bonded Deng ideal between face to be checked, meanwhile, the elastic telescopic freedom degree for being telescopically connected to part can also reduce multi-joint manipulator exhibition To the kinematic accuracy requirement of freedom degree when opening.Detection probe two sides are equipped with distance measuring sensor, are surveyed according to the distance of distance measuring sensor Examination is accurately completed multi-joint manipulator expansion and is withdrawn, and then carries out the movement of detection probe, and the stabilization of characterization processes is improved Property;
5) in the present invention, calibrating installation includes multi-joint manipulator and the color that multi-joint manipulator end is arranged in Sensor is marked, color mark sensor marks corresponding position on detection blade, using mark position as detection circumferential direction zero point, and to code Disk feedback position information corrects mutually and synthesizes accurately circumferentially opposed scanning position.Wherein, code-disc record subdivision angle, school Standard apparatus effect is that blade to be checked often rotates a circle, then to subdivision angle zero;
6) in the present invention, the setting of sliding equipment improves the accessibility of multi-joint manipulator, is convenient for detection probe Comprehensive covering;
7) in the present invention, multi-joint manipulator be four-degree-of-freedom robot or six degree of freedom robot, just In driving detection probe, code-disc, distance measuring sensor and color mark sensor, the reachable ranges such as detection probe are improved, and then promote The accuracy of test of flaw detection system results and comprehensive.
Detailed description of the invention
FIG. 1 is a schematic structural view of the utility model
Fig. 2 is structure of the detecting device schematic diagram in the utility model
Fig. 3 is that test of flaw detection signal transmits logical connection schematic diagram in the utility model
In figure, 1, pedestal, 11, base unit;2, support device, 21, strut, 22, sliding sleeve I, 23, sliding sleeve II, 24, hydraulic Extensible member, 25, upper limit position block, 26, lower position block, 27, connecting rod, 28, gate gurgle valve;3, detection device, 31, detection probe, 32, Distance measuring sensor, 33, code-disc, 34, be telescopically connected to part;4, multi-joint manipulator;5, calibrating installation, 51, color mark sensor;6, sliding Motivation structure, 7, signal receiver, 8, analysis center, 9, remote controllers, 10, display screen, 11, alarm.
Specific embodiment
Below by the technical scheme in the utility model embodiment is clearly and completely described, it is clear that described Embodiment be only the utility model a part of the embodiment, instead of all the embodiments.Based on the reality in the utility model Example is applied, all other embodiment obtained by those of ordinary skill in the art without making creative efforts all belongs to In the range of the utility model protection.
Embodiment 1
It is as shown in Figs. 1-2: a kind of test of flaw detection system of turbocompressor blade, including pedestal 1 and setting are on pedestal 1 Support device 2 and detection device 3, pedestal 1 includes multiple base units 11, is connected between base unit 11 for pin-connected panel;
Support device 2 includes vertically arranged strut 21, sliding sleeve and hydraulically extensible part 24, and strut 21 passes through removably It is fixed on base unit 11,21 top of strut is equipped with upper limit position block 25, and lower part is equipped with lower position block 26, and sliding sleeve is set in the upper limit Between position block 25 and lower position block 26;Sliding sleeve includes sliding sleeve I 22 and sliding sleeve II 23, and sliding sleeve I 22 is arranged above sliding sleeve II 23, sliding It covers I 22 to connect by connecting rod 27 with hydraulically extensible part 24,24 other end of hydraulically extensible part is connect with sliding sleeve II 23, hydraulically extensible Part 24 is equipped with gate gurgle valve 28;
Detection device 3 includes detection probe 31 and distance measuring sensor 32, is equipped with code-disc 33, code-disc 33 above detection probe 31 It is connect by being telescopically connected to part 34 with detection probe 31;The setting of distance measuring sensor 32 is in 31 two sides of detection probe, and ranging senses Device 32 is connect by being telescopically connected to part 34 with detection probe 31;Detection probe 31 is connected by multi-joint manipulator 4 and sliding sleeve I 22 It connects, detection probe 31 is arranged in 4 end of multi-joint manipulator, and is equipped between detection probe 31 and multi-joint manipulator 4 flexible Connector 34;
Calibrating installation 5 is additionally provided on base unit 11, calibrating installation 5 includes multi-joint manipulator 4 and is arranged in multi-joint The color mark sensor 51 of 4 end of manipulator, color mark sensor 51 are connect by being telescopically connected to part 34 with multi-joint manipulator 4.
Embodiment 2
On the basis of embodiment 1, further:
The bottom of the pedestal 1 is equipped with sliding equipment 6.
The sliding equipment 6 includes guide rail, and guide rail is connected with driving device.
The driving device is motor, and retarder is equipped between driving device and pedestal 1.
Embodiment 3
On the basis of embodiment 2, the present embodiment difference is:
The sliding equipment 6 includes pulley, and pulley is cardan wheel with brake.
Embodiment 4
It is further on the basis of embodiment 2-3:
The removably is to be bolted.
Embodiment 5
It is further on the basis of embodiment 4:
The detection probe 31 is ultrasonic phase array probe.
The distance measuring sensor 32 is laser range sensor 32.
The multi-joint manipulator 4 is the robot of four-degree-of-freedom, assembles product and space requirement according to turbocompressor, The robot of different size difference freedom degrees may be selected in multi-joint manipulator 4.
Embodiment 6
On the basis of embodiment 5, the present embodiment difference is:
The detection probe 31 is ultrasonic phase array probe.
The distance measuring sensor 32 is laser range sensor 32.
The multi-joint manipulator 4 is the robot of six degree of freedom, assembles product and space requirement according to turbocompressor, The robot of different size difference freedom degrees may be selected in multi-joint manipulator 4.
The strut 21, upper limit position block 25 and lower position block 26 are integrally formed setting.
Embodiment 7
On the basis of embodiment 1, further:
As shown in Figure 3: the test of flaw detection system further includes signal receiver 7, analysis center 8 and remote controllers 9, letter Number receiver 7 is connect with detection probe 31, distance measuring sensor 32, code-disc 33 and color mark sensor 51, signal receiver 7 and analysis Center 8 connects, and analysis center 8 connect with remote controllers 9;And analysis center 8 is connected with display screen 10 and alarm 11.Flaw detection is surveyed Reception, processing and feedback of trial signal, and long-range control etc., are at the test of flaw detection signal processing in existing mature technology Reason technology.

Claims (10)

1. a kind of test of flaw detection system of turbocompressor blade, it is characterised in that: including pedestal (1) and be arranged in pedestal (1) On support device (2) and detection device (3), pedestal (1) includes multiple base units (11), is spelled between base unit (11) The connection of dress formula;
Support device (2) includes vertically arranged strut (21), sliding sleeve and hydraulically extensible part (24), and strut (21) passes through detachable Mode is fixed on base unit (11), and strut (21) top is equipped with upper limit position block (25), and lower part is equipped with lower position block (26), sliding It is set between upper limit position block (25) and lower position block (26);Sliding sleeve includes sliding sleeve I (22) and sliding sleeve II (23), sliding sleeve I (22) setting is above sliding sleeve II (23), and sliding sleeve I (22) is connect by connecting rod (27) with hydraulically extensible part (24), hydraulically extensible Part (24) other end is connect with sliding sleeve II (23), and hydraulically extensible part (24) is equipped with gate gurgle valve (28);
Detection device (3) includes detection probe (31) and distance measuring sensor (32), is equipped with code-disc (33) above detection probe (31), Code-disc (33) is connect by being telescopically connected to part (34) with detection probe (31);Distance measuring sensor (32) is arranged in detection probe (31) Two sides, and distance measuring sensor (32) is connect by being telescopically connected to part (34) with detection probe (31);Detection probe (31) passes through more Joint Manipulator (4) is connect with sliding sleeve I (22), and detection probe (31) is arranged in multi-joint manipulator (4) end, and detection probe (31) it is equipped between multi-joint manipulator (4) and is telescopically connected to part (34);
It is additionally provided on base unit (11) calibrating installation (5), calibrating installation (5) includes multi-joint manipulator (4) and is arranged more The color mark sensor (51) of joint Manipulator (4) end, color mark sensor (51) is by being telescopically connected to part (34) and multi-joint machine Tool hand (4) connection.
2. the test of flaw detection system of turbocompressor blade according to claim 1, it is characterised in that: the pedestal (1) Bottom be equipped with sliding equipment (6).
3. the test of flaw detection system of turbocompressor blade according to claim 2, it is characterised in that: the sliding equipment It (6) include guide rail, guide rail is connected with driving device.
4. the test of flaw detection system of turbocompressor blade according to claim 3, it is characterised in that: the driving device For motor, and retarder is equipped between driving device and pedestal (1).
5. the test of flaw detection system of turbocompressor blade according to claim 2, it is characterised in that: the sliding equipment It (6) include pulley, pulley is cardan wheel with brake.
6. the test of flaw detection system of turbocompressor blade according to claim 1, it is characterised in that: the detachable side Formula includes being bolted and snapping connection.
7. the test of flaw detection system of turbocompressor blade according to claim 1, it is characterised in that: the detection probe (31) it pops one's head in for ultrasonic phase array.
8. the test of flaw detection system of turbocompressor blade according to claim 1, it is characterised in that: the ranging sensing Device (32) is ultraviolet distance measuring sensor (32) or laser range sensor (32).
9. the test of flaw detection system of turbocompressor blade according to claim 1, it is characterised in that: the multi-joint machine Tool hand (4) is the robot of four-degree-of-freedom or the robot of six degree of freedom.
10. the test of flaw detection system of turbocompressor blade according to claim 1, it is characterised in that: the strut (21), upper limit position block (25) and lower position block (26) are integrally formed setting.
CN201821890889.5U 2018-11-16 2018-11-16 A kind of test of flaw detection system of turbocompressor blade Active CN209231267U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201821890889.5U CN209231267U (en) 2018-11-16 2018-11-16 A kind of test of flaw detection system of turbocompressor blade

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201821890889.5U CN209231267U (en) 2018-11-16 2018-11-16 A kind of test of flaw detection system of turbocompressor blade

Publications (1)

Publication Number Publication Date
CN209231267U true CN209231267U (en) 2019-08-09

Family

ID=67503305

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201821890889.5U Active CN209231267U (en) 2018-11-16 2018-11-16 A kind of test of flaw detection system of turbocompressor blade

Country Status (1)

Country Link
CN (1) CN209231267U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109358114A (en) * 2018-11-16 2019-02-19 四川聚亿重工有限公司 A kind of test of flaw detection system of turbocompressor blade

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109358114A (en) * 2018-11-16 2019-02-19 四川聚亿重工有限公司 A kind of test of flaw detection system of turbocompressor blade

Similar Documents

Publication Publication Date Title
CN207764168U (en) Steam turbine welded disc turbine rotor automatized ultrasound flaw detection system
CN103790647B (en) Hydraulic pressure based on inductance sensing grabs cassette aeroengine rotor assembly apparatus
CN106342170B (en) Hollow turbine vane wall thickness method for automatic measurement
CN103899367B (en) The stacking assembly method of aeroengine rotor and device
CN209231267U (en) A kind of test of flaw detection system of turbocompressor blade
CN105004462A (en) Fault-identification-based fan energy consumption monitoring system
CN106482694A (en) Tip clearance measurement sensor dynamic calibration apparatus under hot environment
CN103806958B (en) Hydraulic pressure based on inductosyn grabs cassette aeroengine rotor assembly apparatus
CN108686982A (en) A kind of detection device and detection method of wheel hub blank outer margin deformation amount
CN104515490A (en) Automatic turnover online outer diameter measuring device
CN103791815A (en) Aero-engine rotor air floatation assembling method and device based on inductance measurement
CN109358114A (en) A kind of test of flaw detection system of turbocompressor blade
CN106813818A (en) A kind of mechanical seal ring friction measurement device and measuring method
CN103790652B (en) Based on the aeroengine rotor air supporting assembly apparatus of photoelectric encoder angle measurement
CN210173321U (en) Compact active high-precision force and position compensation device
CN103790653A (en) Method and device for assembling gantry type aero-engine rotors based on gas and magnetism combined support
CN104389777B (en) Lubricating oil pump test device
CN104019785A (en) Measuring instrument for measuring circularity of large-size bearing assembly
CN103790649A (en) Assembling method and device for aero-engine rotors of movable double-stand-column structure
CN217236974U (en) Cutter abnormal vibration static detection test device
CN205374039U (en) High -speed testboard of engine phase place speed sensor
CN203610916U (en) Mounting device for front windshield of bullet train
CN202133550U (en) Testing stand of air cycle machine of airplane
CN206095187U (en) Opening detection mechanism and opening detection device
CN103790648A (en) Aircraft engine rotor assembling method and device based on multi-component concentricity optimizing

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant