CN201116908Y - High and low temperature shock test box - Google Patents
High and low temperature shock test box Download PDFInfo
- Publication number
- CN201116908Y CN201116908Y CNU2007201024121U CN200720102412U CN201116908Y CN 201116908 Y CN201116908 Y CN 201116908Y CN U2007201024121 U CNU2007201024121 U CN U2007201024121U CN 200720102412 U CN200720102412 U CN 200720102412U CN 201116908 Y CN201116908 Y CN 201116908Y
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- heating
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- heating chamber
- cool room
- temperature
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Abstract
The utility model discloses a high-low-temperature concussion test, which provides the experiment environment of a device for space which needs to do a compacting experiment of space temperature environment. The high-low-temperature concussion test comprises a refrigerating room (2), a heating room (4), an infrared heating (5), a moving carrier (6) and a mounting seat (7), wherein the refrigerating room is fixedly connected with the left of the heating room, a heating element is arranged in the heating room, and temperature sensors are respectively arranged on the opening of the refrigerating room, in the heating room and the moving carrier. The left end of the refrigerating room is connected with a self boosting liquid nitrogen bottle (1), the moving carrier (6) horizontal moves between the refrigerating room and the heating room, the infrared heating is arranged on the positive upper portion of the moving carrier in the heating room. The high-low-temperature concussion test has the advantages of simple structure and low cost, which can aim at products with different technique requirements to conveniently adjust cold and hot temperature.
Description
Technical field
The utility model relates to a kind of equipment of simulation space temperature rapidly changing environment, particularly a kind of high low temperature thermal shock test chamber, and this equipment is mainly used in the workpiece that need carry out high low temperature temperature shock environmental experiment.
Background technology
At present, high low temperature temperature shock test mainly relies on compressor cooling to finish, but common compressor is difficult to competent two the very big environment temperatures of the height temperature difference of building, the device that particularly a lot of spaces are used all needs to do the environment of simulation space temperature-170 ℃~120 ℃ and does impulse test, therefore is badly in need of the high low temperature thermal shock test chamber of the fast-changing experimental situation of a kind of simulation space temperature of exploitation.
Summary of the invention
The utility model has solved traditional compressor can not provide-170 ℃~120 ℃ environment to do the technical matters of high low temperature temperature shock test, has realized changing fast from nearly 300 ℃ of temperature of-170 ℃ to+120 ℃ in 5 minutes.
The technical scheme that its technical matters that solves the utility model adopts is:
High low temperature thermal shock test chamber, comprise Programmable Logic Controller 13, the band expansion link cylinder 15 that on the heating chamber 4 that is provided with on the cool room 2 that is provided with on supercharging liquid nitrogen bottle 1, trapezoidal mount pad 7, the low seat, the dais, maximum block, is provided with at mount pad 7, between supercharging liquid nitrogen bottle 1 and cool room 2, be provided with liquid nitrogen delivery pipe 8, liquid nitrogen delivery pipe 8 is provided with low-temperature solenoid valve 9, and this valve is electrically connected and is subjected to it to control with Programmable Logic Controller 13; Be provided with temperature sensor 3 and liquid nitrogen 10 in the described cool room 2, temperature sensor 3 is electrically connected with Programmable Logic Controller 13; Be provided with the heating element 5 and the sensor 12 that are electrically connected with Programmable Logic Controller 13 respectively in the described heating chamber 4, be provided with the passage 11 of a band insertion plate door between the left side of the right side of cool room 2 and heating chamber 4, this passage can be for motion pallet 6 from cool room 2 to heating chamber 4 or 2 move horizontally back and forth from heating chamber 4 to cool room; The hole that the right side of cylinder 15 by heating chamber 4 is provided with puts in heating chamber 4 and is connected with motion pallet 6,15 actions of Programmable Logic Controller 13 control cylinders realize the 6 horizontal move left and right operations of motion pallet are movably set with in motion pallet 6 with Programmable Logic Controller 13 and are electrically connected sensor 14.
Described heating element 5 can be infrared heating element.Described sensor 14 preferably is movably set in by on the test element 16.
The beneficial effects of the utility model are, and are simple in structure, with low cost, and the product that can require at different process is regulated high and low temperature easily and realized high low temperature temperature shock test.
Description of drawings
Fig. 1 is vertical section structure figure of the present utility model
Fig. 2 is support holder structure figure of the present utility model
Fig. 3 is a PLC flow chart of the present utility model
Embodiment
Below in conjunction with accompanying drawing the utility model is described:
On low, the high mount pad of mount pad 7, place cool room 2 and heating chamber 4 respectively, passage 11 by a band insertion plate door in the middle of cool room 2 and the heating chamber 4 is communicated with, and Programmable Logic Controller drives motion pallet 6 by control cylinder 15 actions and moves between cool room 2 and heating chamber 4.When motion pallet 6 is being with measured workpiece 16 to enter cool room 2, the signal that Programmable Logic Controller reception temperature sensor 3,14 transmits makes the liquid nitrogen in supercharging liquid nitrogen bottle 1 be pressed into from cool room 2 left ends by control low-temperature solenoid valve 9, thereby change the liquid level of the liquid nitrogen 10 in the cool room 2, and then the indoor temperature of change cool room 2, promptly can realize the temperature of measured workpieces in the pallet 6 is controlled by liquid surface height controlling.In the time of in motion pallet 6 enters heating chamber 4, can improve pallets 6 interior temperature rapidly by control infrared heating element 5 all over the signal that range controller 13 reception temperature sensors 12,14 transmit.Change fast by motion pallet 6 height that to realize the measured workpiece temperature in the pallet 6 that between cool room 2 and heating chamber 4, moves around like this, thereby realize temperature shock.At first set attack time, temperature, number of times after Programmable Logic Controller 13 energisings, the program that brings into operation is then opened liquid nitrogen 10 with low-temperature solenoid valve 9 and is entered cool room, heating element 5 begins heating, motion this moment pallet 6 enters cool room 2, after temperature in the motion pallet 6 arrives design temperature, entering hot room 4 from cool room 2 by passage 11 behind the motion pallet 6 stop certain hours heats, after temperature in the motion pallet 6 arrives the heating-up temperature of setting, entering cool room 2 coolings, circulation reaches EOP (end of program) behind the set point number like this, finishes whole impact process.
Claims (3)
1, a kind of high low temperature thermal shock test chamber, comprise Programmable Logic Controller (13), from supercharging liquid nitrogen bottle (1), trapezoidal mount pad (7), low seat at mount pad (7) is gone up the cool room (2) that is provided with, the heating chamber that is provided with on the dais (4), the cylinder (15) of the band expansion link that the horizontal pressure pin with motion pallet (6) that is provided with on the maximum block is fixedlyed connected, it is characterized in that, between supercharging liquid nitrogen bottle (1) and cool room (2), be provided with liquid nitrogen delivery pipe (8), liquid nitrogen delivery pipe (8) is provided with low-temperature solenoid valve (9), and this valve is electrically connected and is subjected to it to control with Programmable Logic Controller (13); Be provided with temperature sensor (3) and liquid nitrogen (10) in the described cool room (2), temperature sensor (3) is electrically connected with Programmable Logic Controller (13); Be provided with the heating element (5) and the sensor (12) that are electrically connected with Programmable Logic Controller (13) respectively in the described heating chamber (4), be provided with the passage (11) of a band insertion plate door between the left side of the right side of cool room (2) and heating chamber (4), this passage can move horizontally to cool room (2) from cool room (2) to heating chamber (4) or from heating chamber (4) back and forth for motion pallet (6); Right side at motion pallet (6) fixedly installs horizontal pressure pin, this pressure pin stretches out heating chamber (4) by the hole of the right side setting of heating chamber (4) and is connected with the expansion link of described cylinder (15), Programmable Logic Controller (13) control cylinder (15) is realized the horizontal move left and right to the motion pallet, is movably set with the sensor (14) that is electrically connected with Programmable Logic Controller (13) in motion pallet (6).
2, a kind of high low temperature thermal shock test chamber according to claim 1 is characterized in that described heating element (5) is an infrared heating element.
3, a kind of high low temperature thermal shock test chamber according to claim 1 and 2 is characterized in that, described sensor (14) is movably set in by on the test element (16).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNU2007201024121U CN201116908Y (en) | 2007-08-29 | 2007-08-29 | High and low temperature shock test box |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNU2007201024121U CN201116908Y (en) | 2007-08-29 | 2007-08-29 | High and low temperature shock test box |
Publications (1)
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CN201116908Y true CN201116908Y (en) | 2008-09-17 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CNU2007201024121U Expired - Fee Related CN201116908Y (en) | 2007-08-29 | 2007-08-29 | High and low temperature shock test box |
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CN (1) | CN201116908Y (en) |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102331436A (en) * | 2011-07-06 | 2012-01-25 | 上海林频仪器股份有限公司 | Two-box type temperature impact test box |
CN102331435A (en) * | 2011-07-06 | 2012-01-25 | 上海林频仪器股份有限公司 | Three-box type temperature impact test box |
CN102353529A (en) * | 2011-06-15 | 2012-02-15 | 卓旦春 | Testing apparatus for temperature strength of thermostatic control valve |
CN102435523A (en) * | 2011-09-13 | 2012-05-02 | 芜湖宇舸瑞汽车电子有限公司 | Temperature impact test equipment for fuel pump core |
CN102614944A (en) * | 2012-02-27 | 2012-08-01 | 华中科技大学 | Multifunctional environmental test box and environmental test method and use thereof |
CN103543079A (en) * | 2013-10-29 | 2014-01-29 | 苏州市职业大学 | Alternation cooling thermal fatigue test bench |
CN104792642A (en) * | 2015-05-06 | 2015-07-22 | 重庆超力高科技股份有限公司 | Endurance test device for temperature valve |
CN105699039A (en) * | 2016-03-16 | 2016-06-22 | 中国直升机设计研究所 | High and low temperature environment test device for landing gear drop test |
CN106525633A (en) * | 2016-11-25 | 2017-03-22 | 防城港市质量技术监督局 | High-low-temperature experiment device with fire extinguishment function |
CN107991091A (en) * | 2017-11-07 | 2018-05-04 | 芜湖赛宝机器人产业技术研究院有限公司 | A kind of split type industrial robot gear reducer high-low temperature tester |
CN108132200A (en) * | 2018-01-30 | 2018-06-08 | 重庆大学 | A kind of two-box type thermal shock experiment device for superhigh temperature ceramics |
CN108132199A (en) * | 2018-01-30 | 2018-06-08 | 重庆大学 | A kind of hyperthermal material batch thermal shock test device |
CN110646315A (en) * | 2019-10-08 | 2020-01-03 | 北京卫星环境工程研究所 | Wide-temperature-zone rapid temperature impact test system for product based on liquid nitrogen immersion deep space detection |
CN113933200A (en) * | 2021-10-15 | 2022-01-14 | 贵州航天计量测试技术研究所 | Electronic component temperature impact test device and test method |
-
2007
- 2007-08-29 CN CNU2007201024121U patent/CN201116908Y/en not_active Expired - Fee Related
Cited By (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102353529A (en) * | 2011-06-15 | 2012-02-15 | 卓旦春 | Testing apparatus for temperature strength of thermostatic control valve |
CN102331436A (en) * | 2011-07-06 | 2012-01-25 | 上海林频仪器股份有限公司 | Two-box type temperature impact test box |
CN102331435A (en) * | 2011-07-06 | 2012-01-25 | 上海林频仪器股份有限公司 | Three-box type temperature impact test box |
CN102435523A (en) * | 2011-09-13 | 2012-05-02 | 芜湖宇舸瑞汽车电子有限公司 | Temperature impact test equipment for fuel pump core |
CN102614944A (en) * | 2012-02-27 | 2012-08-01 | 华中科技大学 | Multifunctional environmental test box and environmental test method and use thereof |
CN102614944B (en) * | 2012-02-27 | 2014-03-12 | 华中科技大学 | Multifunctional environmental test box and environmental test method and use thereof |
CN103543079A (en) * | 2013-10-29 | 2014-01-29 | 苏州市职业大学 | Alternation cooling thermal fatigue test bench |
CN104792642A (en) * | 2015-05-06 | 2015-07-22 | 重庆超力高科技股份有限公司 | Endurance test device for temperature valve |
CN105699039A (en) * | 2016-03-16 | 2016-06-22 | 中国直升机设计研究所 | High and low temperature environment test device for landing gear drop test |
CN105699039B (en) * | 2016-03-16 | 2019-02-26 | 中国直升机设计研究所 | A kind of high-low-temperature environmental testing device for landing gear drop test |
CN106525633A (en) * | 2016-11-25 | 2017-03-22 | 防城港市质量技术监督局 | High-low-temperature experiment device with fire extinguishment function |
CN107991091A (en) * | 2017-11-07 | 2018-05-04 | 芜湖赛宝机器人产业技术研究院有限公司 | A kind of split type industrial robot gear reducer high-low temperature tester |
CN108132200A (en) * | 2018-01-30 | 2018-06-08 | 重庆大学 | A kind of two-box type thermal shock experiment device for superhigh temperature ceramics |
CN108132199A (en) * | 2018-01-30 | 2018-06-08 | 重庆大学 | A kind of hyperthermal material batch thermal shock test device |
CN108132199B (en) * | 2018-01-30 | 2020-08-07 | 重庆大学 | Batch thermal shock testing device for ultra-high temperature materials |
CN110646315A (en) * | 2019-10-08 | 2020-01-03 | 北京卫星环境工程研究所 | Wide-temperature-zone rapid temperature impact test system for product based on liquid nitrogen immersion deep space detection |
CN113933200A (en) * | 2021-10-15 | 2022-01-14 | 贵州航天计量测试技术研究所 | Electronic component temperature impact test device and test method |
CN113933200B (en) * | 2021-10-15 | 2024-02-06 | 贵州航天计量测试技术研究所 | Electronic component temperature impact test device and test method |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C17 | Cessation of patent right | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20080917 Termination date: 20100829 |