CN202886209U - High-temperature high-strain rate stretching synchronization experimental apparatus - Google Patents

High-temperature high-strain rate stretching synchronization experimental apparatus Download PDF

Info

Publication number
CN202886209U
CN202886209U CN 201220438121 CN201220438121U CN202886209U CN 202886209 U CN202886209 U CN 202886209U CN 201220438121 CN201220438121 CN 201220438121 CN 201220438121 U CN201220438121 U CN 201220438121U CN 202886209 U CN202886209 U CN 202886209U
Authority
CN
China
Prior art keywords
bar
air chamber
incident
sample
tensile sample
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.)
Withdrawn - After Issue
Application number
CN 201220438121
Other languages
Chinese (zh)
Inventor
郭伟国
朱泽
曾志银
邵小军
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.)
Northwestern Polytechnical University
Original Assignee
Northwestern Polytechnical 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 Northwestern Polytechnical University filed Critical Northwestern Polytechnical University
Priority to CN 201220438121 priority Critical patent/CN202886209U/en
Application granted granted Critical
Publication of CN202886209U publication Critical patent/CN202886209U/en
Anticipated expiration legal-status Critical
Withdrawn - After Issue legal-status Critical Current

Links

Images

Landscapes

  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)

Abstract

The utility model discloses a stretching synchronization experimental apparatus which is used for solving the technical problem that the existing stretching experimental apparatus can not test the high-strain rate stretching performance of a material at high temperature. The technical scheme is as follows: the end of a stretching sample is designed into a convex-edge table form, the end of a pull rod connected with the stretching sample is designed into a wedge slot form, and then high-temperature synchronization is realized under the control of a linkage emission valve group through the cooperation of the two ends. By designing the connection mode between the stretching sample and the pull rod end, arranging a reserved gap and insulating heat between the stretching sample and the pull rod through an insulating material, the direct contact for heat transfer between the stretching sample and the pull rod is avoided when the sample is heated, so that an incident rod and a transmitting rod are always in a normal-temperature state in the experiment process, and the problem that local temperature of the incident rod and the transmitting rod rises at high temperature in the background art is overcome.

Description

High temperature high strain rate tensile synchronous experimental facility
Technical field
The utility model relates to a kind of experimental provision, particularly relates to a kind of high temperature high strain rate tensile synchronous experimental facility.
Background technology
With reference to Fig. 1, Fig. 2, document " S.Nemat-Nasser; J.B.Isaacs; and J.E.Starrett; Hopkinson Techniques for DynamicRecovery Experiments; Proc.R.Soc. (London) A[J]; 435 (1991) 371-391 " and " S.Nemat-Nasser, Recovery Hopkinson Bar Techniques, Mechanical Test and Evaluation, Vol.8ASM Handbook, American Society for Metals, 2000, P.1068-1073 " a kind of tensile test device of material being realized the high strain rate tensile performance test is disclosed.This device comprises that energy absorber 1, energy transmit bar 2, loading flange 3, impact tube 4, emission valve 5, impact air chamber 6, incident bar 7, tensile sample 8 and transmission bar 9.Wherein energy absorber 1, energy transmission bar 2, impact air chamber 6, incident bar 7 and transmission bar 9 all are placed on the platform.Emission valve 5 is connected by tracheae with impact air chamber 6; Energy transmission bar 2, incident bar 7, transmission bar 9 are cylindrical bar; Impact tube 4 is the tubulose quarter butt, is enclosed within on the incident bar 7, and can be free to slide along incident bar 7, and whole incident bar 7 runs through impact air chamber 6; Incident bar 7 is designed to load flange 3 with impact tube 4 colliding parts; Energy transmits bar 2 and all has aperture at axis part with loading flange 3, places one and be about the straight thin iron staff of 3cm in aperture, makes the two coaxial; Energy transmits bar 2, load flange 3, impact tube 4, incident bar 7 and transmission bar 9 is to process (as all being 18Ni or all being Ti) by same material.Tensile sample 8 two ends are threaded, and are threaded connection with incident bar 7 and transmission bar 9.Impact tube 4 is enclosed within on the incident bar 7, and can be free to slide along incident bar 7, and whole incident bar 7 runs through impact air chamber 6.
When carrying out stretching experiment, first tensile sample 8 and incident bar 7 and transmission bar 9 are threaded connection, impact tube 4 are pushed impact air chamber 6 again.Be added to predetermined pressure by impact air chamber 6, at this moment open emission valve 5, impact tube 4 can be pushed at a high speed load to flange 3, load flange 3 by bump and in incident bar 7, produce a tensile strain ripple, this ripple is delivered to tensile sample 8 by incident bar 7 and tensile sample 8 is loaded, calculate by the strain wave pulse to incident bar 7 and transmission bar 9, can obtain the dynamic stress strain curve of tensile sample 8.
The disclosed device of document can carry out the dynamic performance testing of material under the normal temperature (room temperature), but can not carry out the dynamic performance testing of material under the high temperature.Reason is: (1) is if directly increase temperature sample, since tensile sample 8 by screw thread directly and incident bar 7 and transmission bar 9 be connected, the local temperature of the incident bar 7 that is connected with sample and transmission bar 9 is raise, cause the hydraulic performance declines such as the elastic modulus of incident bar 7 and transmission bar 9 and intensity, and velocity of wave changes in the bar, can't accurately calculate tensile sample 8 dynamic stress strain curves by the strain wave pulse of incident bar 7 and transmission bar 9; (2) if select resistant to elevated temperatures incident bar 7 and transmission bar 9, because tensile sample 8 directly is connected with incident bar 7 and transmission bar 9 by screw thread, specimen temperature is very fast along the pole transmission, also very difficult sample is increased temperature; (3) no matter select incident bar 7 and the transmission bar 9 of which kind of metal, its elastic modulus can descend rapidly after temperature surpasses about 250 ° of C.
Summary of the invention
For overcome existing tensile test device can not test material the problem of high-strain-rate tensile property at high temperature, the utility model provides a kind of high temperature high strain rate tensile synchronous experimental facility.This device is designed to convex edge platform form with the termination of tensile sample, the termination of the pull bar that is connected with tensile sample is designed to the wedge-shaped slot form, realize that high temperature is synchronous under the control that is engaged in interlock emission valve group by both, can realize the high rate of strain performance test of material at high temperature.
The technical scheme that its technical matters that solves the utility model adopts is: a kind of high temperature high strain rate tensile synchronous experimental facility, comprise energy absorber 1, energy transmission bar 2, load flange 3, impact tube 4, emission valve 5, impact air chamber 6, incident bar 7, tensile sample 8 and transmission bar 9, energy absorber 1, energy transmit bar 2, impact air chamber 6, incident bar 7 and transmission bar 9 and all are placed on the platform.Emission valve 5 is connected by tracheae with impact air chamber 6; Energy transmission bar 2, incident bar 7, transmission bar 9 are cylindrical bar; Impact tube 4 is the tubulose quarter butt, is enclosed within on the incident bar 7, and can be free to slide along incident bar 7, and whole incident bar 7 runs through impact air chamber 6; Incident bar 7 is designed to load flange 3 with impact tube 4 colliding parts; Energy transmits bar 2 and all designs an aperture at axis part with loading flange 3, places straight thin iron staff in aperture, makes the two coaxial.Be characterized in also comprising synchronous air chamber 10, piston 11, tracheae 12, high temperature furnace 13, draft cylinder 14, thermocouple wire 15, thermal insulation material 16.Emission valve 5 is comprised of emission valve, impact air chamber valve and draft cylinder valve, and air chamber 10 is connected by tracheae 12 through emission valve 5 with draft cylinder 14 synchronously, and the piston 11 in the draft cylinder 14 is threaded connection transmission bar 9.Incident bar 7 is connected the termination that connects tensile sample and is designed a wedge-shaped slot with transmission bar; Tensile sample 8 two ends are designed to convex edge platform shape, remove crescent along diametric(al); Effective gauge length section is cylindrical in the middle of the two convex edge you heads.Both sides, tensile sample termination and wedge-shaped slot inwall are thermal insulation materials 16, and thermocouple wire 15 is strapped in the gauge length section of tensile sample 8, effective bringing-up section of high temperature furnace 13 be fixed on tensile sample 8 gauge length sections around.
The beneficial effects of the utility model are: by design tensile sample and pull bar termination type of attachment, preset clearance is set, and by thermal insulation material that tensile sample and pull bar is heat insulation, so that when sample is heated, avoided the direct contact heat transfer of tensile sample and pull bar, thereby in experimentation, so that incident bar and transmission bar are in the normal temperature state all the time, overcome in the background technology problem that the local temperature of incident bar and transmission bar at high temperature can raise.
Below in conjunction with embodiment the utility model is elaborated.
Description of drawings
Fig. 1 is the schematic diagram of background technology tensile test device.
Fig. 2 is the partial enlarged drawing of A part among Fig. 1.
Fig. 3 is the schematic diagram of the utility model high temperature high strain rate tensile synchronous experimental facility.
Fig. 4 is the partial enlarged drawing of A part among Fig. 3.
Fig. 5 is the partial enlarged drawing of B part among Fig. 3.
Fig. 6 is the front view of tensile sample among Fig. 4.
Fig. 7 is the vertical view of tensile sample among Fig. 4.
Fig. 8 is the axonometric drawing of tensile sample among Fig. 4.
Among the figure, 1-energy absorber, 2-energy transmit bar, 3-loads flange, 4-impact tube, 5-emission valve, 6-impact air chamber, 7-incident bar, 8-tensile sample, 9-transmission bar, the synchronous air chamber of 10-, 11-piston, 12-tracheae, 13-high temperature furnace, 14-synchro-draw cylinder, 15-thermocouple wire, 16-thermal insulation material, 17-gauge length section.
Embodiment
With reference to Fig. 3~8, the utility model high temperature high strain rate tensile synchronous experimental facility comprises energy absorber 1, energy transmission bar 2, loads flange 3, impact tube 4, links and launch valve 5, impact air chamber 6, incident bar 7, tensile sample 8, transmission bar 9, synchronous air chamber 10, piston 11, tracheae 12, high temperature furnace 13, draft cylinder 14, thermocouple wire 15, thermal insulation material 16.Energy absorber 1, energy transmit bar 2, impact air chamber 6, incident bar 7 and transmission bar 9 and all are placed on the platform.Energy transmission bar 2, incident bar 7, transmission bar 9 are cylindrical bar; Impact tube 4 is the tubulose quarter butt, is enclosed within on the incident bar 7, and can be free to slide along incident bar 7, and whole incident bar 7 runs through impact air chamber 6; Incident bar 7 is designed to load flange 3 with impact tube 4 colliding parts; Energy transmits bar 2 and all has aperture at axis part with loading flange 3, places one and be about the straight thin iron staff of 3cm in aperture, makes the two coaxial; Energy transmits bar 2, load flange 3, impact tube 4, incident bar 7 and transmission bar 9 is to process (as all being 18Ni or all being Ti) by same material.Emission valve 5 impacts the air chamber valve by the emission valve, and three valves of draft cylinder valve form, and emission valve and impact air chamber 6 are connected by tracheae; Can realize impact air chamber 6 and synchronous air chamber 10 independent pressurising and synchronized transmissions; Synchronously air chamber 10 is connected ventilation with draft cylinder 14 by interlock emission valve 5 process tracheaes 12, spurs the piston rod in the draft cylinder 14, and then the transmission bar 9 that is connected with piston rod thread of pulling.Incident bar 7 is connected the termination that connects sample and is designed a wedge-shaped slot with transmission bar; Tensile sample 8 terminations are designed to convex edge platform shape, remove crescent along diametric(al); Effective gauge length section 17 is cylindrical in the middle of the two convex edge you heads.The physical dimension of convex edge platform is less than the physical dimension of wedge-shaped slot, thereby 2mm easily be put into and be left in the sample termination can to the gap of 3mm along wedge-shaped slot, makes its integral body just remain cylindrical; Add 2mm to the thermal insulation material 16 of 3mm in both sides, sample termination and wedge-shaped slot inwall, completely cut off on the one hand the transmission of heat by contact of the two, the sample termination is fixed in the wedge-shaped slot.
During work: at first impact tube 4 is pushed and impact air chamber 6, with tensile sample 8 two ends convex edge platform and incident bar 7 and the assembling of transmission bar 9 wedge-shaped slot rod ends.Separate in diametric(al) with the inwall of thermal insulation material 16 with tensile sample 8 two ends sidewalls and wedge-shaped slot rod end during assembling, make it can not transmission of heat by contact, tensile sample 8 two ends convex edge platform and wedge-shaped slot rod end stay approximately 3mm gap vertically, guarantee that tensile sample 8 does not directly contact with transmission bar 9 with incident bar 7, then thermocouple wire 15 is bound to tensile sample 8 gauge length sections 17, mobile high temperature furnace 13 makes the effective bringing-up section of stove at gauge length section 17 positions of tensile sample 8.At this moment, impact air chamber 6 is stamped into the pressure 0.2Mpa that experiment needs, synchronous air chamber 10 is pressurized to lucky gap-closing under the predefined pressure 0.06Mpa, when thermocouple wire 15 given temperature reach the temperature 1000K of experiment needs, open interlock emission valve 5 so that the high pressure gas of impacting in the air chamber 6 promotes impact tube 4 to loading flange 3 motions, the air pressure of air chamber 10 enters into draft cylinder 14 along tracheae 12 synchronously simultaneously, make fast pulling transmission bar 9 of piston 11, and then make tensile sample 8 two ends convex edge platform and incident bar 7 and transmission bar 9 rod end wedge-shaped slot close contacts, at this moment, load the stretching ripple and just in time arrive tensile sample 8, tensile sample 8 is loaded, by incident bar 7 and transmission bar 9 strain waves are calculated, can obtain the stress-strain diagram of tensile sample 8.This device has guaranteed incident bar 7 and transmission bar 9 at low temperatures, only tensile sample is applied high temperature, accurately and reliably material is carried out the high rate of strain coupling performance test of high temperature.

Claims (1)

1. high temperature high strain rate tensile synchronous experimental facility, comprise energy absorber (1), energy transmission bar (2), load flange (3), impact tube (4), emission valve (5), impact air chamber (6), incident bar (7), tensile sample (8) and transmission bar (9), energy absorber (1), energy transmit bar (2), impact air chamber (6), incident bar (7) and transmission bar (9) and all are placed on the platform; Emission valve (5) is connected by tracheae with impact air chamber (6); Energy transmission bar (2), incident bar (7), transmission bar (9) are cylindrical bar; Impact tube (4) is the tubulose quarter butt, is enclosed within on the incident bar (7), and can be free to slide along incident bar (7), and whole incident bar (7) runs through impact air chamber (6); Incident bar (7) is fixed with loading flange (3) with an end of impact tube (4) collision; Energy transmits bar (2) and all designs an aperture at axis part with loading flange (3), places straight thin iron staff in aperture, makes the two coaxial; It is characterized in that: also comprise synchronous air chamber (10), piston (11), tracheae (12), high temperature furnace (13), draft cylinder (14), thermocouple wire (15), thermal insulation material (16); Emission valve (5) is comprised of emission valve, impact air chamber valve and draft cylinder valve, air chamber (10) is connected by tracheae (12) through emission valve (5) with draft cylinder (14) synchronously, and the piston (11) in the draft cylinder (14) is threaded connection transmission bar (9); Incident bar (7) is connected 9 with transmission bar) termination that connects tensile sample designs a wedge-shaped slot; Tensile sample (8) two ends is designed to convex edge platform shape, removes crescent along diametric(al); Effective gauge length section (17) is cylindrical in the middle of the two convex edge you heads; Both sides, tensile sample termination and wedge-shaped slot inwall are thermal insulation material (16), and thermocouple wire (15) is strapped in the gauge length section (17) of tensile sample (8), effective bringing-up section of high temperature furnace (13) be fixed on tensile sample (8) gauge length section (17) around.
CN 201220438121 2011-12-18 2012-08-30 High-temperature high-strain rate stretching synchronization experimental apparatus Withdrawn - After Issue CN202886209U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201220438121 CN202886209U (en) 2011-12-18 2012-08-30 High-temperature high-strain rate stretching synchronization experimental apparatus

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
CN201120558310.7 2011-12-18
CN201120558310 2011-12-18
CN 201220438121 CN202886209U (en) 2011-12-18 2012-08-30 High-temperature high-strain rate stretching synchronization experimental apparatus

Publications (1)

Publication Number Publication Date
CN202886209U true CN202886209U (en) 2013-04-17

Family

ID=48077623

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201220438121 Withdrawn - After Issue CN202886209U (en) 2011-12-18 2012-08-30 High-temperature high-strain rate stretching synchronization experimental apparatus

Country Status (1)

Country Link
CN (1) CN202886209U (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102830019A (en) * 2011-12-18 2012-12-19 西北工业大学 Tensile synchronous experiment device
CN104089810A (en) * 2014-07-08 2014-10-08 天津大学 Device for testing thermal buckling of thin-wall pipeline under different embedding conditions
CN110470551A (en) * 2019-09-04 2019-11-19 湖北文理学院 A kind of SHPB experimental rig and its emitter and control method
CN113237775A (en) * 2021-05-11 2021-08-10 中国科学技术大学 Device for testing dynamic tensile mechanical properties of fiber monofilaments at high temperature

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102830019A (en) * 2011-12-18 2012-12-19 西北工业大学 Tensile synchronous experiment device
CN104089810A (en) * 2014-07-08 2014-10-08 天津大学 Device for testing thermal buckling of thin-wall pipeline under different embedding conditions
CN110470551A (en) * 2019-09-04 2019-11-19 湖北文理学院 A kind of SHPB experimental rig and its emitter and control method
CN113237775A (en) * 2021-05-11 2021-08-10 中国科学技术大学 Device for testing dynamic tensile mechanical properties of fiber monofilaments at high temperature

Similar Documents

Publication Publication Date Title
CN102830019B (en) Tensile synchronous experiment device
CN202886209U (en) High-temperature high-strain rate stretching synchronization experimental apparatus
CN103674738B (en) Under hot conditions, SHPB is automatically to bar impact loading experiment device
CN101480689A (en) Near-isothermal forging method of two-phase titanium alloy disk-type forgeable piece
CN100393447C (en) Electromagnetically heating airplane riveting device
CN102513440B (en) Method and device for forming magnesium alloy formed parts with excellent high-temperature mechanical property
CN110196198A (en) Can accurate quantification Electromagnetic Control high temperature Hopkinson bar tensile test apparatus and method
CN104826969A (en) Method for forging 500-Kg-level GH3230 high-temperature alloy
EP2177715A3 (en) Airfoil with cooling passage providing variable heat transfer rate
CN202862225U (en) Mechanical arm used for workpiece clamping
CN204789174U (en) Warm shake bending test appearance of height
CN201785457U (en) Clamping device for discharging furnace door of heating furnace
CN203937179U (en) Plastic tube building mortion
CN208124876U (en) A kind of pusher-type furnace furnace ribbed tube bracing means
CN106475510B (en) A kind of rivet hot holder and apply the holder hot-riveting mobile device
CN204486737U (en) A kind of continuous casting billet end heat preservation device
CN2923103Y (en) Plane-rivet electromagnetic-heating riveting device
CN106424517B (en) U-shaped hot riveting machine
CN102205375A (en) Method for pressing press pipe joint of steel inhaul cable
CN102941306B (en) Isothermal Hot molding forging press attemperator
CN202398757U (en) Automatic hot-forging control device for large-specification wind power bolts
CN205414757U (en) High -frequency induction welder retaining device that links
CN203336872U (en) Fixing structure of heating pipe and casing pipe
CN205393436U (en) A hawkbill for forging factory presss from both sides and burns red iron plate
CN203445532U (en) Power transmission line tension current-guide plate bolt fastener

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
AV01 Patent right actively abandoned

Granted publication date: 20130417

Effective date of abandoning: 20141015

RGAV Abandon patent right to avoid regrant