CN201716228U - High-temperature Hopkinson pressure bar experiment system with atmosphere protecting device - Google Patents

High-temperature Hopkinson pressure bar experiment system with atmosphere protecting device Download PDF

Info

Publication number
CN201716228U
CN201716228U CN2010202634564U CN201020263456U CN201716228U CN 201716228 U CN201716228 U CN 201716228U CN 2010202634564 U CN2010202634564 U CN 2010202634564U CN 201020263456 U CN201020263456 U CN 201020263456U CN 201716228 U CN201716228 U CN 201716228U
Authority
CN
China
Prior art keywords
guard box
temperature
kit
pressure bar
heating
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.)
Expired - Lifetime
Application number
CN2010202634564U
Other languages
Chinese (zh)
Inventor
谢若泽
胡文军
何鹏
张方举
吴庆海
王薇
徐艾民
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.)
General Engineering Research Institute China Academy of Engineering Physics
Original Assignee
General Engineering Research Institute China Academy of Engineering Physics
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 General Engineering Research Institute China Academy of Engineering Physics filed Critical General Engineering Research Institute China Academy of Engineering Physics
Priority to CN2010202634564U priority Critical patent/CN201716228U/en
Application granted granted Critical
Publication of CN201716228U publication Critical patent/CN201716228U/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Abstract

The utility model discloses a high-temperature Hopkinson pressure bar experiment system with an atmosphere protecting device, which wholly comprises the atmosphere protecting device, a heating system and a loading system, wherein the atmosphere protecting device comprises a protecting box, an exhaust discharging pipeline and an exhaust filtering device, the protecting box is provided with a gas protecting inlet, an exhaust discharging port and a cooling gas inlet, and a sealing kit is installed between the protecting box and a wave guide rod; and the heating system comprises a heating furnace, a sheathed thermocouple used for monitoring fire box temperature, and a thermocouple wire which is in spot welding on the kit and used for measuring the temperature of the kit. The whole heating furnace, the kit and the end parts of the two wave guide rods are arranged in the protecting box. Two experiment modes that the kit is heated singly and firstly, and then the assembly of the kit and the wave guide rods is completed, or the heating of the kit and the wave guide rods are heated simultaneously are adopted. The high-temperature Hopkinson pressure bar experiment system with the atmosphere protecting device not only can conveniently conduct high-temperature dynamic experiment on special materials under protecting atmosphere, but also can be used for the high-temperature dynamic experiment in normal air.

Description

The high-temperature Hopkinson pressure bar experimental system that has atmosphere protection device
Technical field
The utility model belongs to material at high temperature dynamic mechanical experimental technique field, is specifically related to a kind of high-temperature Hopkinson pressure bar experimental system that has atmosphere protection device.
Background technology
Utilize Hopkinson (Hopkinson) depression bar carry out the material at high temperature Research of dynamic mechanical commonly used two kinds of methods are arranged.A kind of is to keep waveguide rod and test specimen to be in released state before the experiment, and heating is only carried out test specimen, finishes the assembling of test specimen and waveguide rod then before impact.This method since when heating bar separate with test specimen, reduced the thermograde in the bar, data processing is simple relatively.Name is called the patent of invention (patent No.: ZL200610021096.5) describe this method in detail of " double-air path bidirectional automatic assembling device that is used for high-temperature Hopkinson pressure bar experiment ", a kind of double-air path bidirectional automatic assembling device that is used for high-temperature Hopkinson pressure bar experiment is disclosed, this device can guarantee that the stability of assembling and assembling and stress wave arrive the synchronism of test specimen, and avoids test specimen to lower the temperature rapidly because of leaving thermal source.Another kind method is that waveguide rod and test specimen are heated simultaneously, when data processing waveguide rod thermograde influence is revised then.
The high temperature experiment of part material has specific requirement to experimental situation; in air, carry out the high temperature experiment as most of metals and all will produce more serious oxidation; material property after the oxidation and original material have bigger difference; and some material oxidation at high temperature even can produce toxic gas; experimenter and environment are caused than major injury, so this class experiment has clear and definite demand to atmosphere protection.But present high-temperature Hopkinson pressure bar experimental system can not provide the experiment that meets particular requirement atmosphere, and relevant experiment atmosphere generator does not appear in the newspapers.
Summary of the invention
Can not provide the experimental situation that meets particular requirement in order to overcome when the high temperature depression bar is tested in the prior art; cause the deficiency of experiment material generation high-temperature oxydation even release toxic gas, the utility model provides a kind of high-temperature Hopkinson pressure bar experimental system that has atmosphere protection device.Experimental system of the present utility model not only can be carried out the high temperature dynamic experiment of the special material under the protective atmosphere easily, also can be used for conventional airborne high temperature dynamic experiment.
The high-temperature Hopkinson pressure bar experimental system that has atmosphere protection device of the present utility model, comprise loading system, heating system, be characterized in, also comprise a cover atmosphere protection device, described atmosphere protection device contains guard box, exhaust emission pipe and waste gas filter, guard box links to each other with waste gas filter by exhaust emission pipe, the guard box bottom is provided with the blanket gas air intake opening, the top is provided with Waste gas outlet, the middle part is provided with the refrigerating gas air intake opening, waveguide rod in the loading system stretches in the guard box by the hole of guard box both sides, between guard box and the waveguide rod Seal Kit is housed; The heating furnace of heating system is arranged in the guard box, is provided with armoured thermocouple, thermocouple wire in the heating furnace, and armoured thermocouple places in the burner hearth by the hole of furnace wall, heating furnace end, and the head of thermocouple wire is fixedlyed connected with the test specimen that occupy the burner hearth center.
When adopting heating, the utility model keep waveguide rod to separate with test specimen, heating is only carried out test specimen, when before impact, finishing the experiment method of assembling of test specimen and waveguide rod, loading system comprises incident bar, transmission bar, be separately positioned on two promotion bearings and gas circuit on incident bar and the transmission bar, and total valve is by air bubble percussion gas circuit and promote gas circuit and can control the air bubble percussion simultaneously and promote support movement.
During experiment method that adopt the utility model test specimen and waveguide rod heat simultaneously, loading system comprises incident bar, transmission bar, common bearing.
The utility model places guard box with whole heating furnace, test specimen and subwave guide rod, and guard box is welded to form rectangular configuration by sheet metal, and the guard box top cover is dismountable cover plate, to make things convenient for experimental implementation.The guard box top cover can adopt bolt to connect with being connected of protection casing, and other connected modes such as also can adopt that hinge is buckled separate with the high-temperature resistant rubber pad between guard box top cover and the protection casing, can play the effect of sealing effectively.Heating furnace and guard box base plate are integrally welded, and the protection casing adopts bolt to be connected with the guard box base plate equally, seals by the high-temperature resistant rubber pad.
The utility model is provided with an air intake opening in the bottom of guard box, the top is provided with a Waste gas outlet, and the blanket gas density of employing should be greater than atmospheric density.Blanket gas density is during less than atmospheric density, and then the top with guard box is the input port, and the guard box bottom is a Waste gas outlet.Waste gas outlet links to each other with pipeline, and waste gas is directed into the safety zone, enters filtration unit and filters and absorb.Blanket gas in the guard box has reduced the possibility that test specimen reacts with oxygen when high temperature, even have the oxygen of small amount of residual to contact with test specimen simultaneously, react the generation toxic gas, also can discharge from Waste gas outlet.
The utility model is provided with another blanket gas input port at protection casing middle part, after experiment finishes, is blown into blanket gas in heating furnace, accelerates the cooling velocity of burner hearth, accelerates the experiment process.
Two cover temperature thermocouples are set in heating furnace, wherein a cover is thermocouple wire, adopts the mode of spot welding to be welded on the test specimen periphery, is used to measure the transient temperature of test specimen, and as the input temp of heating system switch board, with accurate control heating process and test specimen temperature.Another set of is armoured thermocouple, places burner hearth, on the one hand compares monitoring with thermocouple wire, on the other hand, when experiment is finished, behind the welding breaking of thermocouple wire and test specimen, continuation is monitored the burner hearth temperature-fall period.
When the utility model adopts the experiment method of the independent heating of test specimen; because waveguide rod at first is in beyond the heating region in the experimentation; waveguide rod will move to test specimen under the promotion of package system after being heated to assigned temperature; finish and the docking of test specimen; require waveguide rod move left and right freely; therefore the sealing that should guarantee gas that is connected of waveguide rod and guard box can not have moving freely of big friction force obstruction waveguide rod again.The utility model adopts the mode that is flexible coupling, and adopts heat-resisting soft material such as rubber etc. to make teleflex, and an end is fixedly connected on the flange of guard box wallboard through hole, and the other end is fixedly connected on the waveguide rod.Adopt being connected of teleflex and flange and waveguide rod and tie up silk or adhesive tape is tied up.
During experiment method that adopt the utility model test specimen and waveguide rod heat simultaneously, waveguide rod need not to move, and the connecting portion of waveguide rod and guard box can adopt O-ring seal to seal, and cancels teleflex.
To other parts that may leak gas,, adopt the shutoff of refractory seals glue as power supply lead wire hole, thermocouple jack, bolt hole etc.
Experimental system of the present utility model not only can be carried out conventional airborne high temperature dynamic experiment easily; protective atmosphere can also be provided; satisfy the requirement of special material to experimental situation atmosphere; reduce and avoid the oxidation and the release toxic gas of test specimen; make experimental result more meet truth, reduce injury experimenter and environment.
Description of drawings
The utility model is described in further detail below in conjunction with accompanying drawing.
Fig. 1 is the embodiment 1 general structure synoptic diagram of the high-temperature Hopkinson pressure bar experimental system of band atmosphere protection device of the present utility model.
Fig. 2 is the embodiment 2 general structure synoptic diagram of the high-temperature Hopkinson pressure bar experimental system of band atmosphere protection device of the present utility model.
Fig. 3 is the syndeton synoptic diagram of the waveguide rod among the embodiment 1 of the high-temperature Hopkinson pressure bar experimental system of band atmosphere protection device with the protection casing.
Fig. 4 is the syndeton synoptic diagram of the waveguide rod among the embodiment 2 of the high-temperature Hopkinson pressure bar experimental system of band atmosphere protection device with the protection casing.
Among the figure: 1. incident bar 2. transmission bars 3. promote bearing I 4. common bearing I 5. common bearing II 6. common bearing III 7. common bearing IV 8. test specimens 9. heating furnaces 10. total valves 11. air bubbles percussion gas circuits 12. and promote gas circuits 13. air inlets 14. Waste gas outlets 15. exhaust emission pipes 16. filters 17. protection casings 18. guard box top covers 19. guard box base plates 20. refrigerating gas air inlets 21. armoured thermocouples 22. thermocouple wires 23. and promote bearing II 24. heating furnace power lines 31. flanges 32. sealing teleflexs 33. and tie up an I 34. and tie up an II 41. sealing rings 50. heating system switch boards.
Embodiment
Below in conjunction with drawings and Examples the utility model is further described.
Embodiment 1
Keep waveguide rod to separate with test specimen when the experiment method of present embodiment adopts heating, heating is only carried out test specimen, finishes the mode of the assembling of test specimen and waveguide rod before impact, has disposed double-air path bidirectional automatic assembling device.
Fig. 1 is the embodiment 1 general structure synoptic diagram of the high-temperature Hopkinson pressure bar experimental system of band atmosphere protection device of the present utility model, and Fig. 3 is the syndeton synoptic diagram of the waveguide rod among the embodiment 1 of the high-temperature Hopkinson pressure bar experimental system of band atmosphere protection device with the protection casing.From Fig. 1, Fig. 3, can find out, the one-piece construction that has the high-temperature Hopkinson pressure bar experimental system of atmosphere protection device of the present utility model, total system comprises atmosphere protection device, heating system and loading system.Atmosphere protection device contains guard box, exhaust emission pipe 15 and waste gas filter 16; guard box contains protection casing 17, guard box top cover 18 and guard box base plate 19; guard box links to each other by exhaust emission pipe 15 with waste gas filter 16, and guard box bottom is provided with that blanket gas air intake opening 13, top are provided with Waste gas outlet 14, the middle part is provided with between refrigerating gas air intake opening 20, guard box and the waveguide rod Seal Kit is housed.Heating system comprises the armoured thermocouple 21 of heating furnace 9, monitoring fire box temperature, the thermocouple wire 22 of measurement test specimen temperature, heating furnace power supply 24.Heating furnace power supply 24 links to each other with the output terminal of heating system switch board 50, and armoured thermocouple 21 places in the burner hearth by the hole of furnace wall, heating furnace end, and the head point of thermocouple wire 22 is welded on the test specimen 8.Loading system comprises incident bar 1, transmission bar 2, is separately positioned on promotion bearing I 3, promotion bearing II 23, total valve 10, the air bubble percussion gas circuit 11 on incident bar 1 and the transmission bar 2 and promotes gas circuit 12 that total valve can be controlled the air bubble percussion simultaneously and promote support movement by air bubble percussion gas circuit 11 and promotion gas circuit 12.
Present embodiment is placed in the boom end of whole heating furnace 9, test specimen 8 and waveguide rod in the guard box, and guard box top cover 18 is detachable.Guard box top cover 18 adopts bolt to be connected with protection casing 17, and separates by the high-temperature resistant rubber pad.Heating furnace 9 is integrally welded with guard box base plate 19, and protection casing 17 is connected with the guard box base plate 19 same bolts that adopt, and seals by the high-temperature resistant rubber pad.
Present embodiment is provided with an air intake opening 13 in the bottom of protection casing 17, and guard box top cover 18 is provided with a Waste gas outlet 14, and Waste gas outlet 14 links to each other with pipeline 15, and waste gas is directed into the safety zone, enters filtration unit 16 and filters and absorb.The blanket gas density that adopts should be greater than atmospheric density.
Among Fig. 1, another refrigerating gas air intake opening is set, after experiment finishes, in heating furnace 9 thoraxes, is blown into blanket gas, accelerate the cooling velocity of burner hearth at protection casing middle part.
Two cover temperature thermocouples are set in heating furnace 9, wherein a cover is thermocouple wire 22, the head of thermocouple wire 22 adopts spot welding to be connected with the test specimen 8 that occupy the burner hearth center, the other end of thermocouple wire 22 is connected with heating system switch board 50, with the test specimen transient temperature input heating system switch board of measuring 50.Another set of is armoured thermocouple 21, and its test lead places burner hearth, and fire box temperature is monitored, and the other end is connected with heating system switch board 50.
When adopting heating, present embodiment keep waveguide rod to separate with test specimen 8; heating is only carried out test specimen 8; before impact, finish the experiment method of the assembling of test specimen and waveguide rod; require waveguide rod move left and right freely; therefore waveguide rod and the sealing that should guarantee gas that is connected of protecting casing 17 can not have big friction force to hinder moving freely of waveguide rod again.Among Fig. 3, the sealing teleflex 32 that the utility model adopts high-temperature resistant rubber to make is flexible coupling, and an end of sealing teleflex 32 is fixed on the flange 31 of guard box wallboard through hole, and the other end is fixed on the incident bar 1.Adopt being connected of sealing teleflex 32 and flange 31 and tie up an II 34 and tie up, the employing that is connected of sealing teleflex 32 and incident bar 1 is tied up an I 33 and is tied up, and wherein ties up an II 34 and ties up an I 33 and can replace with adhesive tape.The same mode that is flexible coupling that adopts that is tightly connected between transmission bar 2 and the protection casing 17.
The workflow of the high-temperature Hopkinson pressure bar experimental system of the band atmosphere protection device of present embodiment is: the accurate position of waveguide rod and carry out mark when determining that according to the size of heating furnace 9 and the cylinder stroke that promotes bearing waveguide rod places outside the heating region in advance; test specimen 8, thermocouple wire 22 etc. are installed then; according in advance mark waveguide rod is placed corresponding position; adopt the mode that is flexible coupling to be tightly connected to waveguide rod and protection casing 17, cover guard box top cover 18 and sealing.Guard box is inflated, and check sealing situation then reexamines perfectly if any revealing, and guarantees sealing.Close refrigerating gas air intake opening 20, open blanket gas air intake opening 13, guard box is charged into blanket gas, observe exhausting waste gas pipeline 15 and filtration unit 16, guarantee that air drains.Give heating furnace 9 energisings, test specimen 8 is heated.When temperature reaches preset value, be incubated the enough time.Open total valve 10, finish the automatic assembling of waveguide rod, pull the trigger the gas big gun simultaneously, test specimen 8 is loaded, finish experiment.Continuation is inflated guard box, and waveguide rod is pulled out heating region.Open refrigerating gas air intake opening 20, accelerate fire box temperature and descend, open guard box top cover 18 when temperature to be monitored is enough low, take out test specimen 8, prepare experiment next time.
Embodiment 2
The experiment method that the experiment method of present embodiment adopts test specimen and waveguide rod to heat simultaneously, waveguide rod need not to move.
Fig. 2 is a general structure synoptic diagram among the embodiment 2 of high-temperature Hopkinson pressure bar experimental system of band atmosphere protection device of the present utility model, and Fig. 4 is the waveguide rod of the embodiment 2 of the high-temperature Hopkinson pressure bar experimental system of band atmosphere protection device and the syndeton synoptic diagram of protection casing.From Fig. 2, Fig. 4 as can be seen, the one-piece construction that has the high-temperature Hopkinson pressure bar experimental system of atmosphere protection device of the present utility model, total system comprises atmosphere protection device, heating system and loading system.Atmosphere protection device contains guard box, exhaust emission pipe 15 and waste gas filter 16; guard box contains protection casing 17, guard box top cover 18 and guard box base plate 19; guard box links to each other by exhaust emission pipe 15 with waste gas filter 16, and guard box bottom is provided with that blanket gas air intake opening 13, top are provided with Waste gas outlet 14, the middle part is provided with between refrigerating gas air intake opening 20, guard box and the waveguide rod Seal Kit is housed.Heating system comprises the armoured thermocouple 21 of heating furnace 9, monitoring fire box temperature, the thermocouple wire 22 of measurement test specimen temperature, heating furnace power supply 24.Heating furnace power supply 24 links to each other with the output terminal of heating system switch board 50, and armoured thermocouple 21 places in the burner hearth by the hole of furnace wall, heating furnace end, and the head point of thermocouple wire 22 is welded on the test specimen 8.Loading system comprises incident bar 1, transmission bar 2, also comprises the common bearing I 4 and the common bearing II 5 that are arranged on incident bar 1, is arranged on common bearing III 6 and common bearing IV 7 on the transmission bar 2.
The mode that adopts waveguide rod and test specimen 8 to heat simultaneously, waveguide rod needn't move left and right.Among Fig. 4, adopt O-ring seal 41 to be tightly connected between incident bar 1 and the protection casing 17, the same O-ring seal that adopts is tightly connected between transmission bar 2 and the protection casing 17.
The workflow of the high-temperature Hopkinson pressure bar experimental system of the band atmosphere protection device of present embodiment is: test specimen 8, thermocouple wire 22 etc. are installed in size and position according to heating furnace 9, cover guard box top cover 18 and sealing.Guard box is inflated, and check sealing situation then reexamines perfectly if any revealing, and guarantees sealing.Close refrigerating gas air intake opening 20, open the air intake opening 13 of blanket gas, guard box is charged into blanket gas, observe exhausting waste gas pipeline 15 and filtration unit 16, guarantee that air drains.Give heating furnace 9 energisings, test specimen 8 is heated.When temperature reaches preset value, be incubated the enough time.Open total valve 10, percussion gas big gun loads test specimen 8, finishes experiment.Continuation is inflated guard box, and waveguide rod is pulled out heating region.Open refrigerating gas air intake opening 20, accelerate fire box temperature and descend, open top cover when temperature to be monitored is enough low, take out test specimen 8, prepare experiment next time.
Described blanket gas adopts argon gas.

Claims (4)

1. high-temperature Hopkinson pressure bar experimental system that has atmosphere protection device, comprise loading system, heating system, it is characterized in that: also comprise a cover atmosphere protection device, described atmosphere protection device contains guard box, exhaust emission pipe (15) and waste gas filter (16), guard box links to each other with waste gas filter (16) by exhaust emission pipe (15), the guard box bottom is provided with blanket gas air intake opening (13), the top is provided with Waste gas outlet (14), the middle part is provided with refrigerating gas air intake opening (20), waveguide rod in the loading system stretches in the guard box by the hole of guard box both sides, between guard box and the waveguide rod Seal Kit is housed; Heating furnace in the heating system (9) is arranged in the guard box; be provided with armoured thermocouple (21), thermocouple wire (22) in the heating furnace (9); armoured thermocouple (21) places in the burner hearth by the hole of heating furnace (9) furnace wall, end, and the head of thermocouple wire (22) is fixedlyed connected with the test specimen that occupy the burner hearth center (8).
2. the high-temperature Hopkinson pressure bar experimental system of band atmosphere protection device according to claim 1 is characterized in that: the Seal Kit between described guard box and the waveguide rod is the sealing teleflex.
3. the high-temperature Hopkinson pressure bar experimental system of band atmosphere protection device according to claim 1 is characterized in that: the Seal Kit between described guard box and the waveguide rod is an O-ring seal.
4. the high-temperature Hopkinson pressure bar experimental system of band atmosphere protection device according to claim 1 is characterized in that: described blanket gas is an argon gas.
CN2010202634564U 2010-07-20 2010-07-20 High-temperature Hopkinson pressure bar experiment system with atmosphere protecting device Expired - Lifetime CN201716228U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2010202634564U CN201716228U (en) 2010-07-20 2010-07-20 High-temperature Hopkinson pressure bar experiment system with atmosphere protecting device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2010202634564U CN201716228U (en) 2010-07-20 2010-07-20 High-temperature Hopkinson pressure bar experiment system with atmosphere protecting device

Publications (1)

Publication Number Publication Date
CN201716228U true CN201716228U (en) 2011-01-19

Family

ID=43462233

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2010202634564U Expired - Lifetime CN201716228U (en) 2010-07-20 2010-07-20 High-temperature Hopkinson pressure bar experiment system with atmosphere protecting device

Country Status (1)

Country Link
CN (1) CN201716228U (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101893531A (en) * 2010-07-20 2010-11-24 中国工程物理研究院总体工程研究所 High-temperature Hopkinson pressure bar experimental system with atmosphere protection device
CN102830019A (en) * 2011-12-18 2012-12-19 西北工业大学 Tensile synchronous experiment device
CN103411697A (en) * 2013-07-11 2013-11-27 青岛新力通工业有限责任公司 Armored thermocouple temperature measuring device of material high temperature mechanical testing machine
CN105424893A (en) * 2015-12-24 2016-03-23 浙江工业大学 Air renewing system used for small-size sealing chamber and air renewing method therefor
CN107121330A (en) * 2017-06-09 2017-09-01 北京工业大学 The high temperature test specimen tested for Hopkinson bar cools rapidly rod-pulling type device

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101893531A (en) * 2010-07-20 2010-11-24 中国工程物理研究院总体工程研究所 High-temperature Hopkinson pressure bar experimental system with atmosphere protection device
CN102830019A (en) * 2011-12-18 2012-12-19 西北工业大学 Tensile synchronous experiment device
CN102830019B (en) * 2011-12-18 2014-10-15 西北工业大学 Tensile synchronous experiment device
CN103411697A (en) * 2013-07-11 2013-11-27 青岛新力通工业有限责任公司 Armored thermocouple temperature measuring device of material high temperature mechanical testing machine
CN103411697B (en) * 2013-07-11 2016-04-27 青岛新力通工业有限责任公司 The armoured thermocouple temperature measuring equipment of material at high temperature mechanics machine
CN105424893A (en) * 2015-12-24 2016-03-23 浙江工业大学 Air renewing system used for small-size sealing chamber and air renewing method therefor
CN107121330A (en) * 2017-06-09 2017-09-01 北京工业大学 The high temperature test specimen tested for Hopkinson bar cools rapidly rod-pulling type device
CN107121330B (en) * 2017-06-09 2019-06-28 北京工业大学 High temperature test specimen for Hopkinson bar experiment cools down rapidly rod-pulling type device

Similar Documents

Publication Publication Date Title
CN101893531A (en) High-temperature Hopkinson pressure bar experimental system with atmosphere protection device
CN201716228U (en) High-temperature Hopkinson pressure bar experiment system with atmosphere protecting device
Cao et al. Pressure release characteristics of premixed hydrogen-air mixtures in an explosion venting device with a duct
CN103091189B (en) Tester for simulating service environment of thermal barrier coating and detecting failure of thermal barrier coating in real time
CN104596863A (en) Metallic material tensile experiment system of multifunctional integration structure
CN106769822A (en) A kind of high-temperature corrosion testing system
CN105372146A (en) Testing device and method for high temperature oxidation properties of material under stress action
CN103091237B (en) Spray gun device for simulating high-temperature erosive corrosive service environment of thermal barrier coating
CN102928465A (en) Full-automatic Koenen test system
CN210269493U (en) Thermal cycle life test system for thermal barrier coating
CN109357956A (en) A kind of high-temperature fuel gas corrosion fatigue testing system
JP4546482B2 (en) Gas turbine equipment, low calorie gas supply equipment, and method for suppressing calorie rise of the gas
CN102493954A (en) On-line environment high-temperature test chamber for aviation kerosene hydraulic pump
KR101585762B1 (en) Heating furnace for experimenting skid rail
CN212253637U (en) Chamber type gas heating furnace
CN209926894U (en) Novel exhaust mechanism
KR20150136905A (en) Apparatus for igniting exhaust coke oven gas
US20080050689A1 (en) Method of stabilising a refractory inner wall of a hot blast generating device and use thereof in a hot repair method
CN108106433B (en) A kind of heating and heat-insulating device of heat fatigue simulator stand
CN102062719A (en) Method for detecting air permeability of sintering mixture and sintering device
Belford et al. Development, installation, and operation of a full-copper, deep-cooled slag tap-block for a six-in-line copper slag-cleaning electric furnace
JPH0988631A (en) Gas fuel burning gas turbine misfire preventing method
CN214248349U (en) Smelting furnace with explosion-proof structure
CN212841508U (en) Explosion-proof door device for emergency explosion-proof drainage of furnace top of nonferrous smelting waste heat boiler
CN103217340A (en) High-temperature high-pressure part damage and failure process experimental device

Legal Events

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

Granted publication date: 20110119

Effective date of abandoning: 20150401

AV01 Patent right actively abandoned

Granted publication date: 20110119

Effective date of abandoning: 20150401

RGAV Abandon patent right to avoid regrant