CN201434817Y - High temperature damping tester - Google Patents
High temperature damping tester Download PDFInfo
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- CN201434817Y CN201434817Y CN2009200334736U CN200920033473U CN201434817Y CN 201434817 Y CN201434817 Y CN 201434817Y CN 2009200334736 U CN2009200334736 U CN 2009200334736U CN 200920033473 U CN200920033473 U CN 200920033473U CN 201434817 Y CN201434817 Y CN 201434817Y
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- furnace body
- pintongs
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Abstract
A high temperature damping tester adopts a double-layer chamber structure and comprises a high temperature vacuum chamber and an ambient temperature vacuum chamber. The high temperature vacuum chamberis used for heating the tested member (7). The ambient temperature vacuum chamber is provided below the high temperature vacuum chamber and is communicated with the high temperature vacuum chamber through an annular water cooling jacket (6). An excitation mechanism is provided in the ambient temperature vacuum chamber. Heating member (8) and thermoelectric couples (9) are arranged in the upper heat insulation layer (13) and is communicated with an electric furnace control cabinet (29). A data analysis system (24) and a data collection system (25) are respectively connected with a displacementsensor (28) and an accelerometer (17) through data wires. A double lug cantilever beam testing component (7) is adopted. The contact damping effect brought by direct excitation and error caused by the rotation of central rigid block of tested member are prevented. According to the utility model, the test temperature of the tested member is changed, and the effect of air damping is removed. The insulation between an electromagnetic exciter and the high temperature environment is realized effectively. The high temperature damping tester has the characteristics of simple structure, convenient use, accurate and reliable test result.
Description
One, affiliated field:
The invention belongs to the material mechanical performance field tests, specifically is a kind of high-temperature material damping test device.
Two, background technology:
Material damping is one of key factor of decision structural system dynamics, all necessary material damping of considering but structural vibrations, noise analysis and noise abatement are shaken.But the inherent mechanism of material damping is very complicated, relevant with multiple factor, not only relevant with the internal organizational structure of material, with strain amplitude, temperature and vibration frequency substantial connection is arranged also.Therefore the accurate test request test macro that carries out material damping can satisfy conditions such as environment temperature is controlled, strain amplitude is constant, test frequency is adjustable, system's additional damping (comprising air damping) influence is little simultaneously.For the material damping test of (＜400 ℃) under the lower temperature environments, the also more or less freely realization of above compbined test condition has had the issue of corresponding standard method of testing at present both at home and abroad.Traditional material damping testing device as: rock instrument, DMTA dynamic thermomechanical analysis apparatus etc.Rocking instrument groundwork part is made up of sample, chuck and coasting body (balance stem adds balance bob), according to free Attenuation Method and force the subresonance method to measure, but increased a coasting body owing to rock the working portion of instrument, so caused many discussion about the measuring accuracy problem of rocking instrument.DMTA dynamic thermomechanical analysis apparatus sample two ends are connected with driver, strain gauge and displacement detector respectively through anchor clamps, connecting rod, be to force subresonance type dynamic mechanical surveying instrument, but, be difficult to theoretically the test findings under the different mode different condition be converted because it is a lot of to influence dynamic test result's factor.For the material of working under the high temperature high frequency environment, as blade of aviation engine etc., working temperature is greater than 1000 ℃ even higher, and traditional material damping testing device is no longer suitable.Main difficulty shows the following aspects: one, conventional exciting and method of testing can't directly be used under the hot conditions, must adopt special excitation and vibration measuring mode; Two, the influence of additional dampings such as air damping, contact damping and test macro damping is difficult to eliminate; Three, be difficult to stable control test specimen temperature and keep constant under the high temperature high frequency condition than large amplitude.
Three, summary of the invention
For the influence that overcomes the additional damping that exists in the prior art is difficult to eliminate, be difficult to stable control test specimen temperature under the high temperature high frequency condition and can't keep constant deficiency than large amplitude, the present invention proposes a kind of high-temperature material damping test device.
The present invention includes the high-temperature vacuum chamber, normal temperature vacuum chamber and exciting agency.The high-temperature vacuum chamber is used to heat test block.The normal temperature vacuum chamber is positioned at the below of high-temperature vacuum chamber, is communicated with by annular water collar between the two.Exciting agency is positioned at the normal temperature internal vacuum chamber.Corrugated tube is communicated with upper furnace body and lower furnace body respectively.Be distributed with the via hole of the terminal of vacuum meter, thermopair and heater on the housing of upper furnace body; Be distributed with the via hole of accelerometer signal line and the sealed wiring post of electromagnetic exciter on the housing of lower furnace body.Data analysis system is connected by data line with accelerometer with laser displacement sensor with data acquisition system (DAS).
The high-temperature vacuum chamber comprises bell, upper furnace body, heater, insulation cover, heat-insulation layer, heat shield and test window.There is the mounting hole of water collar at upper furnace body base plate center, in the both sides of water collar mounting hole test window is arranged.The center of last bell is equipped with leading screw.Last bell and upper furnace body fix.
Heat-insulation layer comprises heat-insulation layer and following heat-insulation layer, all is positioned at upper furnace body; Insulation cover is positioned at the heat-insulation layer top.In the inner chamber of last heat-insulation layer heater is arranged, the test block that is positioned at heat-insulation layer is heated by heater.Following heat-insulation layer is between upper thermal-insulation layer and upper furnace body base plate; Have the test block of double cantilever beam structure and the water collar of central block all to be positioned at heat-insulation layer down, and the double cantilever beam of test block central block both sides passes heat shield and be positioned among the high-temperature burner hearth, heated by heater.
Heat shield is positioned at the top of double cantilever beam test block central block, and the central block and the heater of symmetric double semi-girder test block separated, and is too high with the temperature that prevents central block.Be symmetrically distributed with four connecting holes on the heat insulation, there is the fixed orifice of exciting rod at the center of heat insulation.The accelerometer mounting hole site is on the line of symmetry between any two connecting holes, and the center of circle of the distance of center circle heat insulation of the center of circle of accelerometer mounting hole and each connecting hole is equidistant.Heat insulation is positioned at below, the water collar of test block, and an end face of heat insulation and the applying of test block one end face; The central block of test block is by being positioned at the upper surface that connecting hole on the heat insulation is fixed on heat insulation.Accelerometer is positioned on the other end of heat insulation, picks up the acceleration of test block central block, and the acceleration signal that picks up passes to data acquisition system (DAS) by the via hole on the lower furnace body.Test window is positioned at the upper furnace body bottom, and laser displacement sensor is installed in the below of test window, with the vibration signal of collecting test spare semi-girder end.
The normal temperature vacuum chamber comprises lower furnace body and lower furnace door, is used to install electromagnetic exciter.Electromagnetic exciter is positioned at the lower furnace body center, is fixed on the base plate of lower furnace body; One end of exciting rod is connected with the electromagnetic exciter that is positioned at lower furnace body by adapter sleeve, and the other end passes water collar, is connected with the heat insulation that is positioned at upper furnace body.The end cap of lower furnace body upper end is connected by bolt with the end cap of water collar lower end.
The present invention is power with the vacuum pump, by corrugated tube vacuum pump is connected on the bleeding point of high-temperature vacuum chamber and normal temperature vacuum chamber, and passes through the pressure of the vacuum meter real-time monitored high-temperature vacuum damping test furnace interior on the high-temperature vacuum chamber.Vacuum meter, vacuum pump and electric furnace switch board constitute control loop simultaneously, control the indoor vacuum tightness of high-temperature vacuum automatically.
The present invention as heater, monitors furnace temperature by two thermopairs that are distributed in the rectangular inner cavity by the electric furnace heating wire in the rectangular inner cavity that is distributed in upper thermal-insulation layer; The signal of heater and thermopair is connected on the electric furnace switch board by the sealed wiring post, forms control loop control fire box temperature.
The double-deck chamber structure that the present invention adopts has been realized the change of test specimen probe temperature, eliminate air-damped influence simultaneously, effectively realized the isolation of electromagnetic exciter and hot environment, the part of being taked cooling and Design on thermal insulation can guarantee the safety of acceleration transducer.The double cantilever beam test block that the present invention adopts had both effectively been avoided because the contact damping influence that direct-drive brings also prevents to rotate the error of bringing because test specimen left and right sides semi-girder vibrates asymmetric caused center rigidity piece.The present invention has simple in structure, and is easy to use, and test result is accurate, reliable characteristics.
Four, description of drawings
Accompanying drawing 1 is the principal section view of high-temperature vacuum damping test stove
Accompanying drawing 2 is upper furnace body cross section views of high-temperature vacuum damping test stove
Accompanying drawing 3 is high-temperature vacuum damping test systems
Accompanying drawing 4 is A-A cross section views of high-temperature vacuum damping test stove
Accompanying drawing 5 is lower furnace body cross section views of high-temperature vacuum damping test stove
Accompanying drawing 6 is B-B cross section views of high-temperature vacuum damping test stove
Accompanying drawing 7 is cross section views of adapter sleeve
Accompanying drawing 8 is cross section views of the fastening of adapter sleeve
Accompanying drawing 9 is side views of the fastening of adapter sleeve
Accompanying drawing 10 is that the section of the pintongs joint of adapter sleeve is attempted
Accompanying drawing 11 is side views of the pintongs joint of adapter sleeve
Accompanying drawing 12 is that the section of the vibrator top cap of adapter sleeve is attempted
Accompanying drawing 13 is side views of the vibrator top cap of adapter sleeve
Accompanying drawing 14 is vertical views of heat insulation
Accompanying drawing 15 is A-A cut-open views of heat insulation
1. go up bell 2. upper furnace bodies 3. lower furnace doors 4. electromagnetic exciters 5. lower furnace bodies
6. water collar 7. test blocks 8. heaters 9. thermopairs 10. packing washers
11. heat-insulation layer 14. testing windows 15. sealed windows on corrugated tube 12. insulation covers 13.
16. heat insulation 17. accelerometers 18. vacuum meters 19. heat shields 20. water inlet pipes
21. vacuum pump 22. power amplifiers 23. signal generators 24. data analysis systems 25. data acquisition system (DAS)s
26. column 27. rising pipes 28. displacement transducers 29. electric furnace switch boards 30. exciting rods
31. 34. times heat-insulation layer 35. adapter sleeves of fastening 32. pintongs joints, 33. vibrator top caps
Five, embodiment:
Present embodiment is a kind of high-temperature material damping test device, comprises the high-temperature vacuum chamber, normal temperature vacuum chamber and exciting agency, as shown in Figure 1.The high-temperature vacuum chamber is used to heat test block.The normal temperature vacuum chamber is positioned at the below of high-temperature vacuum chamber, is communicated with by annular water collar 6 between the two.Exciting agency is positioned at the normal temperature internal vacuum chamber, is connected with power amplifier 22 by the sealed wiring post, after the signal amplification of power amplifier 22 with signal generator 23, drives electromagnetic exciter 4, for test block 7 provides basic excitation.Corrugated tube 11 is communicated with upper furnace body 2 and lower furnace body 5 respectively.Be distributed with the via hole of the terminal of vacuum meter 18, thermopair 9 and heater 8 on the housing of upper furnace body 2; Be distributed with the via hole of accelerometer signal line and the sealed wiring post of electromagnetic exciter 4 on the housing of lower furnace body 5.Data analysis system 24 and data acquisition system (DAS) 25 and laser displacement sensor 28 and accelerometer 17 are connected by data line.
In the present embodiment:
Shown in Fig. 2～4, the high-temperature vacuum chamber comprises bell 1, upper furnace body 2, heater 8, insulation cover 12, heat-insulation layer, heat shield 19 and test window 14.Upper furnace body 2 is the circular cavity structure, and base plate is arranged at its bottom.There is the mounting hole of water collar 6 at the base plate center of upper furnace body 2, in the both sides of water collar mounting hole test window 14 is arranged.On the skirtboard of base plate connecting hole is arranged,, upper furnace body is linked to each other with pillar 26, be used to support upper furnace body by this connecting hole; On the excircle at upper furnace body 2 tops skirtboard is arranged, on this skirtboard connecting hole is arranged.Last bell 1 is the ball crown type structure, and the internal diameter of spherical crown bottom is with the internal diameter of upper furnace body 2.The center of last bell 1 is equipped with leading screw, by the rotation of leading screw, and the open and close of bell 1 in the realization.On the last bell 1 bottom excircle skirtboard is arranged, the position that this skirtboard is corresponding with the connecting hole of upper furnace body 2 top skirtboards also is distributed with connecting hole, and will go up bell 1 with bolt and link to each other with upper furnace body 2.
Heat-insulation layer comprises heat-insulation layer 13 and following heat-insulation layer 15, all is positioned at upper furnace body.The inner chamber of last heat-insulation layer 13 is a rectangle, and adds a cover insulation cover 12 above last heat-insulation layer 13; Be surrounded with the heater of making of electric furnace heating wire 8 in the rectangular inner cavity of last heat-insulation layer 13, the test block 7 that is positioned at heat-insulation layer by 8 pairs of heaters heats.Following heat-insulation layer 15 is between upper thermal-insulation layer 13 and upper furnace body base plate; Test window 14 corresponding positions on following heat-insulation layer 15 and the base plate have and connect the viewport of heat-insulation layer 15 down.The endoporus at following heat-insulation layer 15 centers is stepped; Wherein, heat-insulation layer 15 is laid test block 7 with the minor diameter endoporus of last heat-insulation layer 13 abutting ends under being arranged in, and water collar 6 is arranged in the large diameter hole of heat-insulation layer 15 down.
As Figure 14 and shown in Figure 15, the heat insulation 16 that pottery is made highly satisfies heat insulation requirement for cylindrical.Be symmetrically distributed with four connecting holes on the heat insulation 16, this connecting hole is parallel to the axis of heat insulation 16, and connects heat insulation.The center of heat insulation 16 is useful on the fixedly stepped hole of exciting rod 30.The accelerometer mounting hole site is on the line of symmetry between any two connecting holes.The center of circle of the distance of center circle heat insulation 16 of the center of circle of accelerometer mounting hole and each connecting hole is equidistant.Heat insulation 16 is fixed in the below, water collar 6 of test block 7 by connecting hole, and an end face of heat insulation 16 and test block 7 one end faces are fitted.The central block of test block 7 is by being positioned at the upper surface that connecting hole on the heat insulation 16 is fixed on heat insulation 16.Accelerometer 17 is fixed on the other end of heat insulation 16, picks up the acceleration of test block central block, and the acceleration signal that picks up passes to data acquisition system (DAS) 25 by the via hole on the lower furnace body 5.
The test window 14 of upper furnace body bottom is made up of a block length square high temperature resistant quartz glass and rectangular backing metal; The cushion block middle part has viewport; Periphery at cushion block has connecting hole, by this connecting hole high temperature resistant quartz glass is fixed on the cushion block.By bolt test window 14 is fixed on bottom of furnace body.Laser displacement sensor 28 is installed in the below of test window 14, with the vibration signal of collecting test spare 7 semi-girder ends.
As shown in Figure 5, the normal temperature vacuum chamber comprises lower furnace body 5 and lower furnace door 3, is used to install electromagnetic exciter 4.
Exciting agency comprises electromagnetic exciter 4, exciting rod 30, adapter sleeve 34, heat insulation 16, is used for test block 7 is carried out direct-drive.Electromagnetic exciter 4 is positioned at lower furnace body 5 centers, and by bolt to the base plate of lower furnace body 5.Exciting rod 30 is the female rod member of an end, and its length is the distance of heat insulation to adapter sleeve.The female end of exciting rod 30 links to each other with heat insulation 16; The other end links to each other with electromagnetic exciter 4 by adapter sleeve 34.
Adapter sleeve 34 is made of fastening 31, pintongs joint 32, vibrator top cap 33.
As shown in Figure 10 and Figure 11, pintongs joint 32 is a thin cylinder shape.One end outer wall of pintongs joint 32 is taper; On the outer wall of pintongs joint 32, be evenly distributed with four distortion grooves that connect pintongs joint 32 thin-walleds; This distortion groove, extended to more than pintongs joint 32 middle parts along the axis direction of pintongs joint 32 from the tapering point beginning of pintongs joint 32.The internal diameter of pintongs joint 32 is with the external diameter of exciting rod 30.
As Figure 12 and shown in Figure 13, vibrator top cap 33 is a thin cylinder shape, and two outer round surface of this thin cylinder symmetry are the plane.Cap 33 1 sections outer walls in vibrator top have external thread, and internal diameter is with the external diameter of pintongs joint 32; Cap 33 another section outer walls in vibrator top are step-like, have formed limited step on the outer wall of vibrator top cap 33; And the inner hole wall of this section has the internal thread that cooperates with the driving head of electromagnetic exciter 4.The different aperture of cap 33 endoporus, vibrator top makes vibrator top cap 33 endoporus be step-like, has also formed limited step.
As Fig. 8 and shown in Figure 9, fastening 31 also is a thin cylinder shape.One end of fastening 31 is isometrical thin cylinder, and this end has the internal thread that cooperates with external thread on cap 33 outer walls of vibrator top; The other end of fastening 31 is the thin cylinder that endoporus and outer wall are taper, and the tapering of the taper of fastening 31 is with the taper tapering of pintongs joint 32 outer walls.
As shown in Figure 7, during the assembling adapter sleeve, vibrator top cap 33 is tightened on the driving head of electromagnetic exciter 4 by internal thread; Pintongs joint 32 is nested in the fastening 31, and the taper of taper on pintongs joint 32 outer walls and fastening 31 inwalls is fitted; The endoporus that exciting rod 30 is passed pintongs joint 32 inserts in the vibrator top cap 33, and the internal thread of fastening 31 and the external thread of vibrator top cap 33 are screwed, can be with exciting rod 30 lockings, thus exciting rod 30 is connected on the electromagnetic exciter 4.
Present embodiment adopts vacuum pump 21 as power, by corrugated tube 11 vacuum pump 21 is connected on the bleeding point of high-temperature vacuum chamber and normal temperature vacuum chamber, and passes through the pressure of the vacuum meter 18 real-time monitored high-temperature vacuum damping test furnace interiors on the high-temperature vacuum chamber.Vacuum meter 18, vacuum pump 21 and electric furnace switch board 29 constitute control loop simultaneously, control the indoor vacuum tightness of high-temperature vacuum automatically.
Present embodiment as heater 8, is monitored furnace temperature by two thermopairs 9 that are distributed in the rectangular inner cavity by the electric furnace heating wire in the rectangular inner cavity that is distributed in upper thermal-insulation layer; The signal of heater 8 and thermopair 9 is connected on the electric furnace switch board 29 by the sealed wiring post, forms control loop control fire box temperature.
During assembling,
1. encapsulation process must be carried out in each detachable interface.As above bell 1 is provided with rubber gasket 10 with the faying face of upper furnace body 2, and is same, the faying face of lower furnace body 5 and lower furnace door 3, and water collar 6 all is provided with rubber gasket with the faying face of lower furnace body 5.Non-dismountable parts on other body of heater all connect to guarantee sealing with welding manner.
2. electromagnetic exciter 4 is moved into by lower furnace door 3, and be fixed on the base plate of lower furnace body.Successively test block 7, ceramic insulation piece 16, high temperature resistant accelerometer 17, exciting rod 30 are assembled into a subassembly outside body of heater, enter by last bell 1 then, exciting rod 30 is fixed on the driving head of electromagnetic exciter 4 by adapter sleeve.Again heat shield 19 is buckled in the top of test block 7 central blocks.
3. all associated tracks all pass through special-purpose enclosed electrode and are connected with body of heater joint outward in the stove.
Claims (10)
1. a high-temperature material damping test device is characterized in that test macro comprises high-temperature vacuum chamber, normal temperature vacuum chamber, exciting agency, corrugated tube (11), data analysis system (24), data acquisition system (DAS) (25), accelerometer (17), vacuum meter (18), thermocouple (9) and displacement transducer (28); Wherein: the normal temperature vacuum chamber is positioned at the below of high-temperature vacuum chamber, is communicated with by water collar (6) between the two; Exciting agency is positioned at the normal temperature internal vacuum chamber; Heater (8) is positioned in the inner chamber of heat-insulation layer (13); Have the test block (7) of double cantilever beam structure and the water collar (6) of central block all to be positioned at heat-insulation layer (15) down, and the double cantilever beam of test block (7) central block both sides pass heat shield (19) and is positioned among the high-temperature vacuum chamber; Heat shield (19) is positioned at the top of double cantilever beam test block (7) central block; Heat insulation (16) is positioned at below, the water collar (6) of test block (7); The central block of test block (7) is fixed on the upper surface of heat insulation (16); Accelerometer (17) is positioned on the other end of heat insulation (16); Exciting rod (30) passes the through hole that is positioned at lower furnace body 5 end cap centers, is fixed on the base plate of lower furnace body (5); One end of exciting rod (30) is connected with the electromagnetic exciter that is positioned at lower furnace body (4) by adapter sleeve (34), and the other end passes water collar (6), is connected with the heat insulation that is positioned at upper furnace body; Laser displacement sensor (28) is installed in the below of test window (14).
2. high-temperature material damping test device according to claim 1 is characterized in that the high-temperature vacuum chamber comprises bell (1), upper furnace body (2), heater (8), insulation cover (12), heat-insulation layer, heat shield (19) and test window (14); The normal temperature vacuum chamber comprises lower furnace body (5) and lower furnace door (3).
3. high-temperature material damping test device according to claim 1 is characterized in that the water collar 6 of described high-temperature vacuum chamber is positioned at upper furnace body (2) base plate center, and test window (14) is arranged in the both sides of water collar; Last heat-insulation layer (13), following heat-insulation layer (15) and insulation cover (12) all are positioned at upper furnace body; Insulation cover (12) is positioned at heat-insulation layer (13) top; Following heat-insulation layer (15) is positioned between upper thermal-insulation layer (13) and the upper furnace body base plate; The center of last bell 1 is equipped with leading screw; Last bell (1) fixes with upper furnace body 2.
4. high-temperature material damping test device according to claim 1, there is the fixed orifice of exciting rod (30) at the center that it is characterized in that described heat insulation (16); The accelerometer mounting hole site is on the line of symmetry between any two connecting holes, and the center of circle of the distance of center circle heat insulation (16) of the center of circle of accelerometer mounting hole and each connecting hole is equidistant.
5. high-temperature material damping test device according to claim 1 is characterized in that having in the barrel of described water collar (6) circulation path of chilled water; There is end cap water collar (6) lower end; The external diameter of water collar (6) is with the internal diameter of lower floor's heat-insulation layer, and the internal diameter of water collar (6) is a bit larger tham the diameter of heat insulation (16).
6. a kind of according to claim 1 high-temperature material damping test device is characterized in that described exciting agency comprises that electromagnetic exciter (4), an end have internal thread exciting rod (30), adapter sleeve (34), heat insulation (16); Electromagnetic exciter (4) is fixed on the center of lower furnace body (5) base plate; Adapter sleeve (34) is made up of fastening (31), pintongs joint (32) and vibrator top cap (33), and vibrator top cap (33) is installed on the driving head of electromagnetic exciter (4); Pintongs joint (32) is nested in the fastening (31), and the taper of taper on pintongs joint (32) outer wall and fastening (31) inwall is fitted; The endoporus that exciting rod (30) passes pintongs joint (32) inserts in the vibrator top cap (33); Fastening (31) is connected with vibrator top cap (33).
7. high-temperature material damping test device according to claim 1 is characterized in that described vacuum meter (18), vacuum pump (21) and electric furnace switch board (29) constitute the control loop of vacuum tightness; Heater (8), electroheat pair (9) and electric furnace switch board (29) constitute temperature control loop.
8. as high-temperature material damping test device as described in the claim 6, it is characterized in that described pintongs joint (32) is thin cylinder shape, an end outer wall is taper; On the outer wall of pintongs joint (32), be evenly distributed with four distortion grooves that connect pintongs joint (32) thin-walled; The external diameter of the same exciting rod of internal diameter (30) of pintongs joint (32).
9. as high-temperature material damping test device as described in the claim 6, it is characterized in that described vibrator top cap (33) is thin cylinder shape, and two outer round surface of this thin cylinder symmetry are the plane; Cap (33) one sections outer walls in vibrator top have external thread, and internal diameter is with the external diameter of pintongs joint (32); The outer wall of another section of vibrator top cap (33) is step-like, has formed limited step on the outer wall of vibrator top cap (33); And the inner hole wall of this section has the internal thread that cooperates with the driving head of electromagnetic exciter (4); Vibrator top cap (33) endoporus has limited step.
10. as high-temperature material damping test device as described in the claim 6, an end that it is characterized in that described fastening (31) is isometrical thin cylinder, and this end has the internal thread that cooperates with external thread on vibrator top cap (33) outer wall; The other end of fastening (31) is the thin cylinder that endoporus and outer wall are taper, and the tapering of the taper of fastening (31) is with the taper tapering of pintongs joint (32) outer wall.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009200334736U CN201434817Y (en) | 2009-06-09 | 2009-06-09 | High temperature damping tester |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009200334736U CN201434817Y (en) | 2009-06-09 | 2009-06-09 | High temperature damping tester |
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| CN201434817Y true CN201434817Y (en) | 2010-03-31 |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101571476B (en) * | 2009-06-09 | 2011-08-17 | 西北工业大学 | Test system for testing damping performance of high-temperature material |
| CN103954798A (en) * | 2014-05-06 | 2014-07-30 | 中国工程物理研究院总体工程研究所 | Testing apparatus for high temperature acceleration sensor |
| CN108279174A (en) * | 2018-02-06 | 2018-07-13 | 沈阳航空航天大学 | A kind of detection method and device of the failure by shear temperature of material |
| CN112284749A (en) * | 2020-09-07 | 2021-01-29 | 武汉理工大学 | Comprehensive experiment platform for testing high-temperature components |
| CN113740013A (en) * | 2021-09-06 | 2021-12-03 | 青海大学 | High-temperature resistant device for powder metallurgy damping experiment |
| CN113739852A (en) * | 2021-09-06 | 2021-12-03 | 青海大学 | Magnesium matrix alloy damping detection device |
-
2009
- 2009-06-09 CN CN2009200334736U patent/CN201434817Y/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101571476B (en) * | 2009-06-09 | 2011-08-17 | 西北工业大学 | Test system for testing damping performance of high-temperature material |
| CN103954798A (en) * | 2014-05-06 | 2014-07-30 | 中国工程物理研究院总体工程研究所 | Testing apparatus for high temperature acceleration sensor |
| CN108279174A (en) * | 2018-02-06 | 2018-07-13 | 沈阳航空航天大学 | A kind of detection method and device of the failure by shear temperature of material |
| CN112284749A (en) * | 2020-09-07 | 2021-01-29 | 武汉理工大学 | Comprehensive experiment platform for testing high-temperature components |
| CN113740013A (en) * | 2021-09-06 | 2021-12-03 | 青海大学 | High-temperature resistant device for powder metallurgy damping experiment |
| CN113739852A (en) * | 2021-09-06 | 2021-12-03 | 青海大学 | Magnesium matrix alloy damping detection device |
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