KR101692824B1 - Test apparatus for altitude simulation and test method therefor - Google Patents
Test apparatus for altitude simulation and test method therefor Download PDFInfo
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- KR101692824B1 KR101692824B1 KR1020150150767A KR20150150767A KR101692824B1 KR 101692824 B1 KR101692824 B1 KR 101692824B1 KR 1020150150767 A KR1020150150767 A KR 1020150150767A KR 20150150767 A KR20150150767 A KR 20150150767A KR 101692824 B1 KR101692824 B1 KR 101692824B1
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- Prior art keywords
- chamber
- specimen
- vacuum pump
- vacuum
- cooling water
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- 238000012360 testing method Methods 0.000 title claims abstract description 48
- 238000004088 simulation Methods 0.000 title claims abstract description 26
- 238000010998 test method Methods 0.000 title claims abstract description 10
- 238000010438 heat treatment Methods 0.000 claims abstract description 59
- 239000000498 cooling water Substances 0.000 claims abstract description 38
- 238000007789 sealing Methods 0.000 claims description 21
- 238000000034 method Methods 0.000 claims description 10
- 230000005855 radiation Effects 0.000 claims description 4
- 230000001276 controlling effect Effects 0.000 description 13
- 238000007599 discharging Methods 0.000 description 3
- 238000001931 thermography Methods 0.000 description 3
- 230000006870 function Effects 0.000 description 2
- 239000010453 quartz Substances 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N silicon dioxide Inorganic materials O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000036632 reaction speed Effects 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 229910001285 shape-memory alloy Inorganic materials 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N25/00—Investigating or analyzing materials by the use of thermal means
- G01N25/18—Investigating or analyzing materials by the use of thermal means by investigating thermal conductivity
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B37/00—Pumps having pertinent characteristics not provided for in, or of interest apart from, groups F04B25/00 - F04B35/00
- F04B37/10—Pumps having pertinent characteristics not provided for in, or of interest apart from, groups F04B25/00 - F04B35/00 for special use
- F04B37/14—Pumps having pertinent characteristics not provided for in, or of interest apart from, groups F04B25/00 - F04B35/00 for special use to obtain high vacuum
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B49/00—Control, e.g. of pump delivery, or pump pressure of, or safety measures for, machines, pumps, or pumping installations, not otherwise provided for, or of interest apart from, groups F04B1/00 - F04B47/00
- F04B49/22—Control, e.g. of pump delivery, or pump pressure of, or safety measures for, machines, pumps, or pumping installations, not otherwise provided for, or of interest apart from, groups F04B1/00 - F04B47/00 by means of valves
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25D—REFRIGERATORS; COLD ROOMS; ICE-BOXES; COOLING OR FREEZING APPARATUS NOT OTHERWISE PROVIDED FOR
- F25D17/00—Arrangements for circulating cooling fluids; Arrangements for circulating gas, e.g. air, within refrigerated spaces
- F25D17/02—Arrangements for circulating cooling fluids; Arrangements for circulating gas, e.g. air, within refrigerated spaces for circulating liquids, e.g. brine
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01J—MEASUREMENT OF INTENSITY, VELOCITY, SPECTRAL CONTENT, POLARISATION, PHASE OR PULSE CHARACTERISTICS OF INFRARED, VISIBLE OR ULTRAVIOLET LIGHT; COLORIMETRY; RADIATION PYROMETRY
- G01J5/00—Radiation pyrometry, e.g. infrared or optical thermometry
- G01J5/48—Thermography; Techniques using wholly visual means
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
- G01K13/00—Thermometers specially adapted for specific purposes
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
- G01L19/00—Details of, or accessories for, apparatus for measuring steady or quasi-steady pressure of a fluent medium insofar as such details or accessories are not special to particular types of pressure gauges
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B3/00—Ohmic-resistance heating
- H05B3/0033—Heating devices using lamps
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B3/00—Ohmic-resistance heating
- H05B3/02—Details
- H05B3/06—Heater elements structurally combined with coupling elements or holders
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- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Biochemistry (AREA)
- Health & Medical Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Analytical Chemistry (AREA)
- Thermal Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Combustion & Propulsion (AREA)
- Immunology (AREA)
- Pathology (AREA)
- Spectroscopy & Molecular Physics (AREA)
- Testing Resistance To Weather, Investigating Materials By Mechanical Methods (AREA)
Abstract
Description
More particularly, the present invention relates to a test apparatus and a test method capable of performing a heat transfer test on the ground by controlling a degree of vacuum and a heating amount in a chamber, and more particularly, The present invention relates to a high-level simulation test apparatus and a test method capable of simulating a rapid change in pressure and a change in a heating amount in an environment where the air is lean according to a heating amount variation profile.
In order to simulate altimetry of real time pressure and heating change in ground test equipment, rapid reaction speed of vacuum pump and heating lamp is required as much as the vacuum degree and heating performance of test equipment. Conventional rapid heat transfer test equipment consisted of an infrared heating lamp made of nickel-chrome hot wire and transparent quartz, a heating lamp controller to control it, and a specimen holder to fix the specimen. Here, the infrared heating lamp satisfies the sufficient heating performance to simulate the heating amount in the actual environment. However, when heating is performed in an open space at atmospheric pressure, convection heat transfer due to the air around the specimen is additionally generated, so that it is difficult to simulate accurate heating amount in an environment where the air is lean.
On the other hand, a vacuum chamber device is used to simulate a pressure change, and a typical vacuum chamber device can be implemented with a vacuum pump to evacuate internal air to create a vacuum condition within the enclosed chamber. At this time, the vacuum pump is required to be capable of reducing pressure from atmospheric pressure to a low vacuum level within a few minutes in order to simulate a rapidly changing real environment. Also, precise control performance is required so that the required pressure level is maintained for a certain period of time. However, when a vacuum pump capable of precise control is used, it is difficult to simulate a rapid pressure change, and it is difficult to precisely control the pressure when using a large-capacity vacuum pump.
It is an object of the present invention to provide a method and apparatus for heating a specimen using an infrared quartz heating lamp so as to simultaneously simulate a rapidly changing pressure and a heating amount in an air- The present invention also provides an apparatus and a method for testing a high-level simulator capable of precisely controlling the pressure inside a vacuum chamber through a large-capacity and precise vacuum pump while simultaneously simulating changes in heating amount through the vacuum chamber.
The apparatus for testing high-level samples according to an embodiment of the present invention includes a
The elevation simulation apparatus includes a moving
The
The high-level simulation testing apparatus includes a
And the second
The vacuum pump (300) includes a large capacity vacuum pump (310) which performs depressurization to a predetermined ratio of the target degree of vacuum; A
The controller (400) includes a heating lamp controller (410) for controlling the amount of heating of the heating lamp (100) with respect to the specimen (1); And a vacuum
The high-level simulation test method according to another embodiment of the present invention is characterized in that a pressure sensor and a temperature sensor are connected to a
The
In the step S600 of starting the altitude simulation test, the large
The step S600 of starting the elevation simulation test is characterized in that the
As described above, according to the present invention, the specimen is heated in a low vacuum (760 to 1 Torr) state in a closed chamber, so that the convection heat transfer can be prevented and the heating amount according to the altitude can be accurately simulated.
Further, according to the present invention, the test data obtained only through the direct test in the air-lean environment can be acquired through the ground test equipment simulating the same environment, thereby reducing the cost of performing the test .
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a view for explaining the entire structure of a high-level simulation test apparatus according to an embodiment of the present invention; FIG.
FIGS. 2 to 4 are a sectional view, a left side view, and a front view of an apparatus for testing an altitude according to an embodiment of the present invention.
5 is a flowchart of an altitude simulation test method according to another embodiment of the present invention.
It is to be understood that the words or words used in the present specification and claims are not to be construed in a conventional or dictionary sense and that the inventor can properly define the concept of a term to describe its invention in the best way And should be construed in accordance with the meaning and concept consistent with the technical idea of the present invention. Therefore, the embodiments described in the present specification and the configurations shown in the drawings are merely the most preferred embodiments of the present invention and are not intended to represent all of the technical ideas of the present invention. Therefore, various equivalents It should be understood that water and variations may be present. In the following description, well-known functions or constructions are not described in detail since they would obscure the invention in unnecessary detail. Hereinafter, preferred embodiments of the present invention will be described in detail with reference to the accompanying drawings.
FIG. 1 is a view for explaining the overall structure of an apparatus for testing an altimeter according to an embodiment of the present invention, and FIGS. 2 to 4 are a sectional view, a left side view, and a front view, respectively, of an apparatus for testing an altimeter according to an embodiment of the present invention . Referring to FIGS. 1 to 5, an apparatus for testing an elevation profile according to an embodiment of the present invention includes a
The elevation simulation apparatus includes a moving
The
The high-level simulation testing apparatus includes a
That is, the sealing
And the second
The vacuum pump (300) includes a large capacity vacuum pump (310) which performs depressurization to a predetermined ratio of the target degree of vacuum; A
The controller (400) includes a heating lamp controller (410) for controlling the amount of heating of the heating lamp (100) with respect to the specimen (1); And a vacuum
5 is a flowchart of an altitude simulation test method according to another embodiment of the present invention. Referring to FIG. 5, an elevation simulation test method according to another embodiment of the present invention includes connecting a pressure sensor and a temperature sensor to the
In the step S600 of starting the altitude simulation test, the large-
The step S600 of starting the elevation simulation test is characterized in that the
It is to be understood that both the foregoing general description and the following detailed description of the present invention are exemplary and explanatory only and are not restrictive of the invention, as claimed, and will be fully understood by those of ordinary skill in the art. The present invention is not limited thereto. It will be apparent to those skilled in the art that various substitutions, modifications and variations are possible within the scope of the present invention, and it is obvious that those parts easily changeable by those skilled in the art are included in the scope of the present invention .
1 The Psalms
100 heating lamp
110 moving rails
200 chamber
210 Specimen mounting hole
220 Infrared Thermal Camera
230 Observation Window
240 Specimen plate
250 sealing member
261 First cooling water pipe
262 Second cooling water pipe
263 flap
270 clamp
280 Cover
290 vent valve
300 vacuum pump
310 Large capacity vacuum pump
320 Precision Vacuum Pump
330 euros
340 Vacuum control valve
400 controller
410 heating lamp controller
420 Vacuum Regulating Valve Controller
500 cooler
Claims (10)
A chamber 200 in which a test environment of the specimen 1 can be formed in a vacuum state;
A vacuum pump 300 for changing the pressure inside the chamber 200;
A controller 400 for controlling the heating lamp 100 and the vacuum pump 300; And
And a cooler (500) for supplying the cooled cooling water to the chamber (200) and recovering the heated cooling water in the chamber (200)
The chamber 200 includes a specimen mounting hole 210 formed at a front central portion thereof; And
And an observation window (230) formed on the rear surface so as to observe the temperature distribution of the specimen (1) by using the infrared ray camera (220)
A specimen fixing plate 240 for fixing the specimen 1 inside the specimen mounting hole 210;
A sealing member 250 surrounding the specimen mounting hole 210 and interposed between the inner surface of the specimen fixing plate 240 and the chamber 200;
A first cooling water conduit 261 formed to communicate with upper and lower surfaces of both sides of the chamber 200 to cool the chamber 200;
A second cooling water conduit 262 formed on the outer surface of the specimen fixing plate 240 along the sealing member 250 to prevent the sealing member 250 from being deteriorated;
A cover 280 for fixing the specimen fixing plate 240 and the second cooling water conduit 262 to the chamber 200 by a plurality of clamps 270; And
A vent valve (290) formed at the lower rear of the chamber (200) to discharge air inside the chamber (200) to the outside of the chamber (200) when the inside of the chamber (200) is in an overpressure state;
Wherein the apparatus further comprises:
A moving rail 110 attached to a lower end of the heating lamp 100 and capable of adjusting a distance from the chamber 200 to the heating lamp 100;
Wherein the apparatus further comprises:
The second cooling water conduit 262 has a flap 263 opened at a predetermined temperature or higher;
Wherein the apparatus further comprises:
The vacuum pump (300)
A large capacity vacuum pump 310 for reducing the pressure to a predetermined ratio of the target vacuum degree;
A precision vacuum pump 320 for reducing pressure to the target degree of vacuum after depressurization by the large capacity vacuum pump 310; And
The flow path 330 communicates the chamber 200, the large capacity vacuum pump 310 and the precision vacuum pump 320 so that the large capacity vacuum pump 310 and the precision vacuum pump 320 can be selectively used. A vacuum control valve 340 for opening and closing the vacuum control valve 340;
Wherein the apparatus further comprises:
The controller (400)
A heating lamp controller 410 for controlling the heating amount of the heating lamp 100 with respect to the specimen 1; And
A vacuum control valve controller 420 for controlling the degree of vacuum in the chamber 200 by opening and closing the vacuum control valve 340;
Wherein the apparatus further comprises:
Connecting a pressure sensor and a temperature sensor to the specimen 1 and fixing the specimen 1 to a chamber 200 capable of forming a test environment of the specimen 1 in a vacuum state S100;
A controller 400 for controlling a vacuum pump 300 for controlling a heating lamp 100 for heating the specimen 1 and a pressure inside the chamber 200, (S200);
Confirming whether the temperature and pressure inside the chamber 200 are controlled according to the pressure profile and the temperature profile (S300);
Disposing the infrared radiographic camera 220 of the chamber 200 to start observation of the specimen (S400);
(S500) operating the cooler (500) to supply the cooling water to the chamber (200) and recover the heated cooling water in the chamber (200);
(S600) of controlling the temperature and pressure inside the chamber (200) in accordance with a pressure profile and a temperature profile to initiate an elevation simulation test for the specimen (1); And
(S700) of logging real-time pressure and temperature data after the end of the test,
The chamber 200 includes a specimen mounting hole 210 formed at a front central portion thereof; And
And an observation window (230) formed on the rear surface so as to observe the temperature distribution of the specimen (1) by using the infrared ray camera (220)
A specimen fixing plate 240 for fixing the specimen 1 inside the specimen mounting hole 210;
A sealing member 250 surrounding the specimen mounting hole 210 and interposed between the inner surface of the specimen fixing plate 240 and the chamber 200;
A first cooling water conduit 261 formed to communicate with upper and lower surfaces of both sides of the chamber 200 to cool the chamber 200;
A second cooling water conduit 262 formed on the outer surface of the specimen fixing plate 240 along the sealing member 250 to prevent the sealing member 250 from being deteriorated;
A cover 280 for fixing the specimen fixing plate 240 and the second cooling water conduit 262 to the chamber 200 by a plurality of clamps 270; And
A vent valve (290) formed at the lower rear of the chamber (200) to discharge air inside the chamber (200) to the outside of the chamber (200) when the inside of the chamber (200) is in an overpressure state;
Wherein the high altitude simulation test method comprises the steps of:
In the step S600 of starting the altitude simulation test, the vacuum pump 300 is depressurized to a predetermined ratio of the target degree of vacuum using the large capacity vacuum pump 310, (300) is selectively depressurized to a target degree of vacuum.
Wherein the step (S600) of starting the elevation simulation test is to heat the specimen (1) by any one of the heating method of radiation or convection according to the inputted pressure profile and temperature profile.
Priority Applications (1)
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KR1020150150767A KR101692824B1 (en) | 2015-10-29 | 2015-10-29 | Test apparatus for altitude simulation and test method therefor |
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KR1020150150767A KR101692824B1 (en) | 2015-10-29 | 2015-10-29 | Test apparatus for altitude simulation and test method therefor |
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Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20190073712A (en) * | 2017-12-19 | 2019-06-27 | 주식회사 우창이엔씨 | Apparatus for measuring coefficient of heat transmission for heat insulation material |
CN111678942A (en) * | 2020-05-08 | 2020-09-18 | 江苏禹治流域管理技术研究院有限公司 | Testing device and testing method for wet expansion coefficient of fiber composite material |
CN113899576A (en) * | 2021-10-11 | 2022-01-07 | 江南造船(集团)有限责任公司 | Measuring device and measuring method for measuring convective heat transfer coefficient of ship cabin |
CN115783319A (en) * | 2022-12-30 | 2023-03-14 | 中国科学院地质与地球物理研究所 | Ultrahigh vacuum low-temperature sample transfer operation experiment system |
WO2023070779A1 (en) * | 2021-10-27 | 2023-05-04 | 中国南方电网有限责任公司超高压输电公司检修试验中心 | Vacuum arc-extinguishing chamber test system for transformer on-load tap-changer and method therefor |
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JPH09138205A (en) * | 1995-11-15 | 1997-05-27 | Agency Of Ind Science & Technol | Detection method for flaw of material by infrared thermography |
JP2002107317A (en) * | 2000-10-02 | 2002-04-10 | Sanyo Seiko Kk | Device for observing high-temperature |
KR20090055431A (en) * | 2007-11-28 | 2009-06-02 | 한국원자력연구원 | Vacuum system and operating method thereof |
KR101218092B1 (en) | 2010-11-29 | 2013-01-03 | 국방과학연구소 | Temperature and pressure test apparatus |
KR101304980B1 (en) * | 2012-05-02 | 2013-09-06 | 주식회사 썬앤라이트 | U-value and g-value measuring apparatus |
-
2015
- 2015-10-29 KR KR1020150150767A patent/KR101692824B1/en active IP Right Grant
Patent Citations (5)
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JPH09138205A (en) * | 1995-11-15 | 1997-05-27 | Agency Of Ind Science & Technol | Detection method for flaw of material by infrared thermography |
JP2002107317A (en) * | 2000-10-02 | 2002-04-10 | Sanyo Seiko Kk | Device for observing high-temperature |
KR20090055431A (en) * | 2007-11-28 | 2009-06-02 | 한국원자력연구원 | Vacuum system and operating method thereof |
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Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20190073712A (en) * | 2017-12-19 | 2019-06-27 | 주식회사 우창이엔씨 | Apparatus for measuring coefficient of heat transmission for heat insulation material |
KR102019661B1 (en) * | 2017-12-19 | 2019-09-09 | 주식회사 우창이엔씨 | Apparatus for measuring coefficient of heat transmission for heat insulation material |
CN111678942A (en) * | 2020-05-08 | 2020-09-18 | 江苏禹治流域管理技术研究院有限公司 | Testing device and testing method for wet expansion coefficient of fiber composite material |
CN113899576A (en) * | 2021-10-11 | 2022-01-07 | 江南造船(集团)有限责任公司 | Measuring device and measuring method for measuring convective heat transfer coefficient of ship cabin |
WO2023070779A1 (en) * | 2021-10-27 | 2023-05-04 | 中国南方电网有限责任公司超高压输电公司检修试验中心 | Vacuum arc-extinguishing chamber test system for transformer on-load tap-changer and method therefor |
CN115783319A (en) * | 2022-12-30 | 2023-03-14 | 中国科学院地质与地球物理研究所 | Ultrahigh vacuum low-temperature sample transfer operation experiment system |
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