CN106840562A - With the split type shielding fixture and method in tenon blade high-temperature vibrating fatigue test in a kind of turbomachine - Google Patents

With the split type shielding fixture and method in tenon blade high-temperature vibrating fatigue test in a kind of turbomachine Download PDF

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Publication number
CN106840562A
CN106840562A CN201710012508.7A CN201710012508A CN106840562A CN 106840562 A CN106840562 A CN 106840562A CN 201710012508 A CN201710012508 A CN 201710012508A CN 106840562 A CN106840562 A CN 106840562A
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water
tongue
cooling
groove seat
fixture
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CN201710012508.7A
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CN106840562B (en
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胡殿印
曲震
曹福良
张龙
王荣桥
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Beihang University
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Beihang University
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M7/00Vibration-testing of structures; Shock-testing of structures
    • G01M7/02Vibration-testing by means of a shake table
    • G01M7/027Specimen mounting arrangements, e.g. table head adapters

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)

Abstract

The present invention relates in a kind of turbomachine with the split type shielding fixture and method in tenon blade high-temperature vibrating fatigue test.The test fixture mainly includes two large divisions:Water-cooling base and tongue-and-groove holder part, its middle tenon groove holder part include tongue-and-groove seat and two tongue-and-groove seat limited blocks, additionally including the heat-insulated asbestos pad between shake table and water-cooling base.Water-cooling chassis interior is provided with cooling-water duct, and vibration mechine is fixed on by four bolts, between the two plus asbestos pad, in order to strengthen effect of heat insulation, four heat dams is milled out on the upper and lower surface of heat dissipation base, reduces transmission of heat by contact area;Tongue-and-groove seat is connected by four bolts with water-cooling base, and bolt is connected to vibration table through tongue-and-groove seat and water-cooling base, and the limited block of both sides is fixed on tongue-and-groove seat both sides, prevents blade tenon from breakking away by cross bolts.The fixture can efficiently transmit the vibration of shake table, and can at utmost reduce heat to shake table conduction.

Description

In a kind of turbomachine with tenon blade high-temperature vibrating fatigue test in it is split type every Hot fixture and method
Technical field
The invention belongs to impeller machinery technical field, band tenon blade high-temperature vibrating in more particularly to a kind of turbomachine Split type shielding fixture and method in fatigue test.
Background technology
Turbo blade is one of very important parts in turbomachine, and high-temperature vibrating wear-out failure is its common mistake Effect pattern, it is therefore desirable to carry out high-temperature vibrating fatigue test for the type blade to determine its safe operating life.In order to incite somebody to action The vibration of shake table is efficiently delivered to blade, and at utmost reduces experiment Leaf heat to shake table conduction, it is necessary to set A kind of efficient biography of meter is shaken, heat-insulated vibration test fixture.
In laboratory conditions, vibration test is typically carried out on a vibration table.The size of vibration table surface is limited, platform The specification and quantity of the fixing screwed hole (Fig. 3) on face are also limited, therefore are all by fixture clamping to shake table by test specimen On table top.Due to connecting shake table and test specimen using fixture, the vibration of shake table and energy can not be transmitted directly Onto test specimen, but first pass on fixture, then be delivered on test specimen by fixture, thus the biography performance of shaking of fixture is straight Connect influence test effect;Blade vibration experimental condition is usually 700-800 DEG C, and the safe working temperature of shake table is generally 80 Below DEG C, the heat of blade is also first to be transmitted to fixture, then is transmitted to shake table, in order to ensure the safe and reliable of shake table, must Design on thermal insulation must be carried out on fixture.Therefore the jig Design of vibration test is a ring critically important in entirely testing, and is also included The manufacture and installation of fixture.
The content of the invention
The technical problem to be solved in the present invention is:For high-temperature vibrating experiment, for the energy efficient for providing shake table is passed Testpieces is delivered to, and can well step up testpieces, prevent loosening occur in process of the test;To prevent shake table overtemperature, it is right to need Shake table is thermally shielded, and temperature is down to below safe temperature during by shaketalle test;Different leaves vibration test needs different Fixture is, it is necessary to repeatedly process integral clamp, split-type design reduces the workload of fixture processing.
The present invention solve above-mentioned technical problem use technical scheme be:Band tenon blade high temperature shakes in a kind of turbomachine Split type shielding fixture in dynamic fatigue test, including:Tongue-and-groove seat, water-cooling base, the first limited block, the second limited block and Asbestos pad;Wherein, 4 bolts on water-cooling base are connected with shake table, and four bolts on tongue-and-groove seat dissipate through water-cooled Hot base is connected with shake table, and water-cooling base and tongue-and-groove seat are all fixed on vibration mechine, and blade tenon is installed To after tongue-and-groove seat, the limited block of both sides is fixed with two stay bolts through tongue-and-groove seat.
Wherein, the material of the water-cooling base be aluminium alloy, limited block and tongue-and-groove seat material be stainless steel.
Wherein, four sides of water-cooling base are respectively provided with 3 cooling water holes, and cooling-water duct is by heat dissipation base Opened hole is formed, and unwanted cooling water hole in experiment is clogged with waterproof plug;The upper and lower surface of water-cooling seat respectively mills out 4 Rectangle heat dam:Heat transfer contact area is reduced, radiating can be assisted to air blast in groove when radiating is not enough.
Wherein, heat-insulated asbestos pad is added between water-cooling base and shake table, if necessary in tongue-and-groove seat and water-cooling seat Between add heat-insulated asbestos pad.
Wherein, all bolts should all install spring shim additional in fixture, bolt looseness when preventing vibration test;It is non-complete on screw rod Screw thread, screw rod be polished rod through fixture and fixture intersection, be threaded rod with shake table coupling part.
In addition, a kind of carry out the side with tenon blade high-temperature vibrating fatigue test in turbomachine using above-mentioned fixture Method, the method comprises the following steps:
Water-cooling base is fixed on shake table, shake table and water-cooled by step (1) with 4 bolts with spring washer Install heat-insulated asbestos pad between seat additional, choose manhole appendix of the suitable cooling water hole as cooling water, remaining hole is clogged with waterproof plug;
With 4 bolts with spring washer be fixed on shake table tongue-and-groove seat through water-cooling base by step (2), And pilot blade is installed;
Limited block is installed to tongue-and-groove seat both sides by step (3) with the bolt with spring washer;
Step (4) is passed through cooling water, and blade is heated with electromagnetic induction coil, is vibrated according to test load spectrum Fatigue test;
After step (5) off-test, induction coil and shake table power supply are cut off, unload lower position block and tongue-and-groove seat, changed not Follow-up test is carried out to other blades with tongue-and-groove seat.
Principle of the invention is:
Shaken to ensure that shake table is efficiently passed, using specific stiffness (elastic modulus E of material and density of material ρ during design fixture Ratio) big material, material requirements " light and hard ", tongue-and-groove seat and limited block part use stainless steel material, and blade is constrained respectively The displacement of vertical table-board and the displacement of parallel table top, while taking into account radiating effect, heat dissipation base uses aluminium alloy;Heat dissipation base In be provided with cooling water channel, heat is taken away by cooling water in experiment, in order to further enhance effect of heat insulation, in water-cooling base One layer of heat-insulated asbestos are clamped and shake table between, and radiating rectangular channel is milled out respectively in water-cooling base upper and lower surface;Using Split-type design, wherein water-cooling base and limited block can be reused, and the blade for different tenon forms is tried When testing, tongue-and-groove seat need to be only re-worked.
The present invention has advantages below compared with prior art:
(1) fixture light weight, specific stiffness is big, and vibration transmission efficiency is high;
(2) using water-cooling is heat-insulated, asbestos 5 and the heat-insulated mode of the physics of heat dam 19 between shake table and testpieces to entering Row is heat-insulated, enhances effect of heat insulation;
(3) fixture uses split-type design, with wider applicability, greatly reduces test fixture manufacture processed The workload of journey, helps speed up test process.
Brief description of the drawings
Fig. 1 is with the split type shielding fixture in tenon blade high-temperature vibrating fatigue test in a kind of turbomachine of the invention Dimensional structure diagram;
Fig. 2 be water-cooling base and cooling water channel schematic diagram, wherein, Fig. 2 (a) be water-cooling base schematic diagram, Fig. 2 B () is cooling water channel schematic diagram;
Fig. 3 is vibration table bolthole circle;
Fig. 4 is with the split type shielding fixture in tenon blade high-temperature vibrating fatigue test in a kind of turbomachine of the invention Front view;
Fig. 5 is with the split type shielding fixture in tenon blade high-temperature vibrating fatigue test in a kind of turbomachine of the invention Top view;
Fig. 6 is with the split type heat insulation clamps in tenon blade high-temperature vibrating fatigue test in a kind of turbomachine of the invention Tool;
Symbol description is as follows in figure:
1:Tongue-and-groove seat 11:Second tongue-and-groove seat bolt hole
2:Water-cooling subbase 12:3rd tongue-and-groove seat bolt hole
3:First limited block 13:4th tongue-and-groove seat bolt hole
4:Second limited block 14:First limited block bolt hole
5:Asbestos pad 15:Second limited block bolt hole
6:First water-cooling subbase bolt hole 16:First cooling water hole
7:Second water-cooling subbase bolt hole 17:Second cooling water hole
8:3rd water-cooling subbase bolt hole 18:3rd cooling water hole
9:4th water-cooling subbase bolt hole 19:Heat dam
10:First tongue-and-groove seat bolt hole
Specific embodiment
Below in conjunction with the accompanying drawings and specific embodiment further illustrates the present invention.
1. clamp structure is designed and performance verification
As shown in figure 1, in a kind of turbomachine of the invention with tenon blade high-temperature vibrating fatigue test in it is split type every Hot fixture, including tongue-and-groove seat 1, water-cooling subbase 2, the first limited block 3, the second limited block 4 and asbestos pad 5.4 bolts pass through water-cooled Heat dissipation base is by the first water-cooling subbase bolt hole 6, the second water-cooling subbase bolt hole 7, the 3rd water-cooling subbase bolt at corner Hole 8, the 4th water-cooling subbase bolt hole 9 are connected with shake table, 4 bolts through the first tongue-and-groove seat bolt hole 10 on tongue-and-groove seat, It is then passed through water-cooling subbase 2 and shakes after second tongue-and-groove seat bolt hole 11, the 3rd tongue-and-groove seat bolt hole 12, the 4th tongue-and-groove seat bolt hole 13 Dynamic platform is connected, and two cross bolts are connected two limited blocks through the bolt hole 14,15 on limited block and tongue-and-groove seat with nut It is fixed on tongue-and-groove seat both sides:Blade tenon is inserted sideways in tongue-and-groove seat, and limited block prevents it from breakking away.Water-cooling base four Respectively there are three cooling water holes individual side, such as positive first cooling water hole 16, the second cooling water hole 17, the 3rd cooling water hole 18, according to actual tests room situation determine cooling water into and out of water hole.The upper and lower surface of water-cooling base mills out two respectively Horizontal two indulge four heat dams 19, and purpose is reduction transmission of heat by contact area.
With reference to the quantity of the position of experiment table top (Fig. 3) upper bolt hole of vibration test, selection is near shake table central part The a number of bolt hole of position fixes required bolt hole as fixture, and present clip have chosen positioned at shake table center Fixation and positioning bolt hole of 8 bolts hole as fixture (square is indicated in Fig. 3).Computer simulation fixture is carried out afterwards to set Meter, for the fixture that design is completed, the test of fixture is carried out using Finite Element:Model analysis is carried out by fixture, is obtained To its first natural frequency, its vibration carry-over factor is analyzed according to material property, be that the adjustment of shake table power is carried in process of the test For reference, shaken effect with reaching satisfied biography.
2. fixture processing and test
For the fixture for having machined, before shaketalle test is carried out, fixture need to be placed in resistant to elevated temperatures The enterprising trip temperature test in face, water-cooling subbase is passed through cooling water, blade to be measured is installed on fixture and is incited somebody to action with electromagnetic induction coil Whether blade is heated to test temperature, and high temperature resistant table top temperature is measured after a period of time, met with the effect of heat insulation for verifying fixture Shake table safety test demand.
3. vibration test is carried out
(1) fixed water-cooling base
The bolt with spring washer that fixed water-cooling base is used, is sequentially inserted into four fixations on water-cooling subbase In hole 6,7,8,9, screw rod is polished rod with base intersection, and thread segment is screwed into shake table.Using diagonal peace when bolt is fixed The order of dress installs four bolts successively, again successively tightens bolt reinforcing by diagonal order after bolt is screwed into successively.
(2) fixed tongue-and-groove seat
Fixed tongue-and-groove seat is sequentially inserted into tongue-and-groove upper 4 fixing holes 10,11,12,13 of seat using the bolt with spring washer In, screw rod is polished rod with fixture intersection, and thread segment is screwed into shake table.Bolt is screwed into and reinforcing order and the spiral shell of water-cooling subbase Bolt is identical.Can again add one layer of heat-insulated asbestos between effect of heat insulation, then tongue-and-groove seat and heat dissipation base according to demand to strengthen.
(3) blade is installed
Blade is inserted along tongue-and-groove seat upper tenon groove orientation.Electromagnetic induction heating coil is installed additional the position of heating is needed.
(4) limited block on tongue-and-groove seat is installed
Using the bolt with spring washer, it is sequentially inserted into the fixing hole 14,15 of limited block and tongue-and-groove seat, screw rod and tenon Groove seat and limited block intersection are polished rod, and limited block opposite side is fixed with nut, successively twist nut reinforcing after nut of screwing on Fasten.In order to prevent nut from being loosened in vibration test, insurance is played after nut screwing clamping.
(5) access cooling water pipe and be passed through cooling water
Appropriate cooling water hole is selected as the import and export of cooling water according to test site and cooling water pipeline is accessed, with not To cooling water hole clogged with stopper;Cooling water pipe joint axis direction should be consistent with the vibration displacement direction of shake table, if Cooling water pipe is long, should be coiled into spring shape, prevents the pipe joint for cooling water occur during vibration test from loosening leak.
(6) shake table parameter is set and starts vibration test
(7) off-test
Shake table is first closed in off-test, disconnects electromagnetic induction coil, is first unloaded on lower position block after fixture is cooled down completely Bolt, remove blade, unloaded if it need to carry out the vibration test of next blade tongue-and-groove seat on 4 bolts, more renew Tongue-and-groove seat, repeats above-mentioned test operation.
Non-elaborated part of the present invention belongs to techniques well known.
The above, part specific embodiment only of the present invention, but protection scope of the present invention is not limited thereto, and appoints What those skilled in the art the invention discloses technical scope in, the change or replacement that can be readily occurred in should all be covered Within protection scope of the present invention.

Claims (6)

1. with the split type shielding fixture in tenon blade high-temperature vibrating fatigue test in a kind of turbomachine, it is characterised in that Including:Tongue-and-groove seat (1), water-cooling base (2), the first limited block (3), the second limited block (4) and asbestos pad (5);Wherein, water 4 bolts on cold heat dissipation base are connected with shake table, and four bolts on tongue-and-groove seat pass through water-cooling base and shake table It is connected, water-cooling base and tongue-and-groove seat is all fixed on vibration mechine, blade tenon is installed to after tongue-and-groove seat, will The limited block of both sides is fixed with two stay bolts through tongue-and-groove seat.
2. in a kind of turbomachine according to claim 1 with tenon blade high-temperature vibrating fatigue test it is split type every Hot fixture, it is characterised in that:The material of the water-cooling base is aluminium alloy, and the material of limited block and tongue-and-groove seat is for stainless Steel.
3. in a kind of turbomachine according to claim 1 with tenon blade high-temperature vibrating fatigue test it is split type every Hot fixture, it is characterised in that:Four sides of water-cooling base are respectively provided with 3 cooling water holes, and cooling-water duct is by radiating Opened hole is formed in base, and unwanted cooling water hole in experiment is clogged with waterproof plug;The upper and lower surface of water-cooling seat is each Mill out 4 rectangle heat dams:Heat transfer contact area is reduced, radiating can be assisted to air blast in groove when radiating is not enough.
4. in a kind of turbomachine according to claim 1 with tenon blade high-temperature vibrating fatigue test it is split type every Hot fixture, it is characterised in that:Add heat-insulated asbestos pad between water-cooling base and shake table, dissipated in tongue-and-groove seat and water-cooled if necessary Heat-insulated asbestos pad is added between hot seat.
5. in a kind of turbomachine according to claim 1 with tenon blade high-temperature vibrating fatigue test it is split type every Hot fixture, it is characterised in that:All bolts should all install spring shim additional in fixture, bolt looseness when preventing vibration test;Screw rod Upper non-full thread, screw rod be polished rod through fixture and fixture intersection, be threaded rod with shake table coupling part.
6. a kind of fixture using described in claim 1 carries out the side with tenon blade high-temperature vibrating fatigue test in turbomachine Method, it is characterised in that the method comprises the following steps:
Water-cooling base is fixed on shake table by step (1) with 4 bolts with spring washer, shake table and Water-cooling seat it Between install heat-insulated asbestos pad additional, choose manhole appendix of the suitable cooling water hole as cooling water, remaining hole is clogged with waterproof plug;
With 4 bolts with spring washer be fixed on shake table tongue-and-groove seat through water-cooling base by step (2), and is pacified Dress pilot blade;
Limited block is installed to tongue-and-groove seat both sides by step (3) with the bolt with spring washer;
Step (4) is passed through cooling water, and blade is heated with electromagnetic induction coil, and vibrating fatigue is carried out according to test load spectrum Experiment;
After step (5) off-test, induction coil and shake table power supply are cut off, unload lower position block and tongue-and-groove seat, change different tenons Groove seat carries out follow-up test to other blades.
CN201710012508.7A 2017-01-09 2017-01-09 With the split type shielding fixture and method in tenon blade high-temperature vibrating fatigue test in a kind of turbomachine Active CN106840562B (en)

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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107314932A (en) * 2017-06-16 2017-11-03 河海大学 Modularization fatigue test place and corollary apparatus, fatigue test method
CN108393818A (en) * 2018-01-16 2018-08-14 中国航发贵州黎阳航空动力有限公司 A kind of compressor arc tooth vibration of rotor blades fatigue test clamper
CN108519225A (en) * 2018-03-19 2018-09-11 江苏大学 A kind of detection device and method of blade of aviation engine high-temperature vibrating fatigue properties
CN109827735A (en) * 2019-04-02 2019-05-31 湘潭大学 A kind of high-temperature vibrating analog machine
CN110530590A (en) * 2019-07-02 2019-12-03 东北大学 A kind of turbine blade vibration test experimental bed considering more contact conditions
CN111024349A (en) * 2019-12-23 2020-04-17 北京工业大学 High-temperature multi-axis vibration fatigue test method
CN114720170A (en) * 2022-06-10 2022-07-08 中国飞机强度研究所 Temperature control device and method for clamp for vibration test of aircraft component in high-temperature environment
CN114791347A (en) * 2022-06-23 2022-07-26 中国飞机强度研究所 Response control method based on mapping correction in high-temperature vibration fatigue test of airplane

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101167184A (en) * 2005-04-21 2008-04-23 日本轻金属株式会社 Liquid-cooled jacket
EP2351631A1 (en) * 2010-01-27 2011-08-03 Rolls-Royce PLC Apparatus for generating vibrations in a component
CN102539135A (en) * 2011-12-31 2012-07-04 北京航空航天大学 Thermal mechanical fatigue test system for hollow air-cooled turbine blade
CN203993613U (en) * 2014-07-21 2014-12-10 北京强度环境研究所 A kind of water-cooling type high temperature vibration test fixture
CN104535438A (en) * 2014-12-31 2015-04-22 北京航空航天大学 High-temperature high-low cycle complex fatigue crack propagation testing system and measuring method for test article
CN205483460U (en) * 2015-12-11 2016-08-17 天津航天瑞莱科技有限公司 High temperature is heat -proof device for vibration test
CN205799150U (en) * 2016-06-22 2016-12-14 中国航空工业集团公司沈阳发动机设计研究所 A kind of positioner for grinding blade tip

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101167184A (en) * 2005-04-21 2008-04-23 日本轻金属株式会社 Liquid-cooled jacket
EP2351631A1 (en) * 2010-01-27 2011-08-03 Rolls-Royce PLC Apparatus for generating vibrations in a component
CN102539135A (en) * 2011-12-31 2012-07-04 北京航空航天大学 Thermal mechanical fatigue test system for hollow air-cooled turbine blade
CN203993613U (en) * 2014-07-21 2014-12-10 北京强度环境研究所 A kind of water-cooling type high temperature vibration test fixture
CN104535438A (en) * 2014-12-31 2015-04-22 北京航空航天大学 High-temperature high-low cycle complex fatigue crack propagation testing system and measuring method for test article
CN205483460U (en) * 2015-12-11 2016-08-17 天津航天瑞莱科技有限公司 High temperature is heat -proof device for vibration test
CN205799150U (en) * 2016-06-22 2016-12-14 中国航空工业集团公司沈阳发动机设计研究所 A kind of positioner for grinding blade tip

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107314932A (en) * 2017-06-16 2017-11-03 河海大学 Modularization fatigue test place and corollary apparatus, fatigue test method
CN107314932B (en) * 2017-06-16 2024-04-12 河海大学 Modularized fatigue test field, matched device and fatigue test method
CN108393818A (en) * 2018-01-16 2018-08-14 中国航发贵州黎阳航空动力有限公司 A kind of compressor arc tooth vibration of rotor blades fatigue test clamper
CN108519225A (en) * 2018-03-19 2018-09-11 江苏大学 A kind of detection device and method of blade of aviation engine high-temperature vibrating fatigue properties
CN109827735A (en) * 2019-04-02 2019-05-31 湘潭大学 A kind of high-temperature vibrating analog machine
CN109827735B (en) * 2019-04-02 2020-11-06 湘潭大学 High-temperature vibration simulation equipment
CN110530590A (en) * 2019-07-02 2019-12-03 东北大学 A kind of turbine blade vibration test experimental bed considering more contact conditions
CN111024349A (en) * 2019-12-23 2020-04-17 北京工业大学 High-temperature multi-axis vibration fatigue test method
CN114720170A (en) * 2022-06-10 2022-07-08 中国飞机强度研究所 Temperature control device and method for clamp for vibration test of aircraft component in high-temperature environment
CN114791347A (en) * 2022-06-23 2022-07-26 中国飞机强度研究所 Response control method based on mapping correction in high-temperature vibration fatigue test of airplane
CN114791347B (en) * 2022-06-23 2022-09-02 中国飞机强度研究所 Response control method based on mapping correction in high-temperature vibration fatigue test of airplane

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