CN108341074A - 2600M thermoregulator testers - Google Patents
2600M thermoregulator testers Download PDFInfo
- Publication number
- CN108341074A CN108341074A CN201810427317.1A CN201810427317A CN108341074A CN 108341074 A CN108341074 A CN 108341074A CN 201810427317 A CN201810427317 A CN 201810427317A CN 108341074 A CN108341074 A CN 108341074A
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- thermoregulator
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- 238000012360 testing method Methods 0.000 claims description 43
- 238000010438 heat treatment Methods 0.000 claims description 20
- 238000001816 cooling Methods 0.000 claims description 9
- 238000000034 method Methods 0.000 claims description 6
- 230000005611 electricity Effects 0.000 claims 2
- 238000013461 design Methods 0.000 abstract description 3
- 238000009434 installation Methods 0.000 abstract 1
- 238000010586 diagram Methods 0.000 description 3
- 238000012545 processing Methods 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000003638 chemical reducing agent Substances 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012795 verification Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/60—Testing or inspecting aircraft components or systems
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
- G01K15/00—Testing or calibrating of thermometers
- G01K15/005—Calibration
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D23/00—Control of temperature
- G05D23/19—Control of temperature characterised by the use of electric means
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- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Control Of Temperature (AREA)
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
Abstract
The invention discloses a kind of 2600M thermoregulators testers, by realizing the installation of tester circuit design, tester panel and the design of babinet and layout, each component of tester from no equipment, without means to thering are reliable apparatus and corresponding means to check first, the functional of B-mode thermoregulator, tester is easy to carry, can work at any time and any place.
Description
Technical field
The present invention relates to a kind of 2600M thermoregulators testers, and 2600M thermoregulators tester is (hereinafter referred to as:School
Test instrument) be examination and maintenance first, B-mode thermoregulator important equipment, whether first, B-mode thermoregulator work normally shadow
Ring aircraft safety.A type thermoregulator major function is to control to adjust the temperature in certain type helicopter equipment cabin, and aircraft is made to set
It is standby to run well under complicated weather conditions;B-mode thermoregulator reaches highest with Mr. Yu's type helicopter reducer oil temperature
It sends warning signal when temperature, to enable aircraft to work normally, ensures flight safety.
Background technology
Currently, being examined whether normal operation to the function of first, B-mode thermoregulator without technological means and special equipment
It looks into.
Invention content
The present invention is to solve above-mentioned technical problem and the technical solution adopted is that provide a kind of 2600M thermoregulators verification
Instrument, wherein specific technical solution is:
Including Щ Х -36 types aviation plug, ganged switch, solid-state relay, potentiometer, diode, signal lamp;Institute
Щ Х -36 type aviation plugs connection ganged switch is stated, the ganged switch connection diode 1 and 5 signal lamps of Л, the duplex are opened
Close relay P1 in parallel, 1 signal lamps of relay P1 connections Л, 3 signal lamps of Л and diode 2, the ganged switch parallel connection
Relay P2,2 signal lamps of relay P2 connections Л, 4 signal lamps of Л and diode 3;The ganged switch, which is also connected with, tests oneself
It tries mouth;Further include tester panel, test interface, indicator light and change-over switch are set on tester panel.
Using the method for calibration of the 2600M thermoregulator testers, including:1) A type thermoregulator hand is checked
Dynamic temperature adjustment function:By adjusting " cabin heating " change-over switch on certain type helicopter second navigator's instrument board manually, make conversion
Switch is placed in " heating " or " cooling " position, and A type thermoregulator exports 27V d. c. voltage signals to tester, makes tester
Corresponding signal lamp ignites, to realize the manual temperature function check to A type thermoregulator;2) first, B-mode is checked
Thermoregulator automatic temperature-adjusting function:Temperature sensor signal on certain type machine is simulated by the rheostat of tester, is input to temperature
Adjuster, output 27V d. c. voltage signals make the corresponding signal of tester refer to 2 testers after thermoregulator receives signal
Show that lamp ignites, to realize that the automatic temperature-adjusting function to first, second thermoregulator verifies.
The method of calibration of the 2600M thermoregulator testers, specially:
1) test interface T5 (+)/T6 (-)
(1) even under machine working condition, when test temperature adjuster is powered, voltage is measured according to T5 (+)/T6 (-) program, is had
Direct current 27V voltage outputs, No. 3, No. 1 terminals output voltage of Щ Х -36 type plugs;
(2) under off working state, according to T5 (+)/T6 (-) program input direct-current 27V voltages, working power letter can be simulated
Number, check 5 working conditions of Л.
2) test interface T1 (+)/T6 (-), T5 (+)/T6 (-)
(1) even under machine working condition, when test temperature adjuster " heating ", according to T1 (+)/T6 (-), T5 (+)/T6 (-)
Program measures voltage, there is a direct current 27V voltage outputs, No. 5 of Щ Х -36 type plugs, No. 1 terminals output voltage it is normal;
(2) it under off working state, according to T1 (+)/T6 (-), T5 (+)/T6 (-) program input direct-current 27V voltages, can simulate
Thermoregulator signal checks Л 3,5 all lights of Л, working properly.
3) test interface T3 (+)/T6 (-), T5 (+)/T6 (-)
(1) even under machine working condition, when test temperature adjuster " cooling ", according to T3 (+)/T6 (-), T5 (+)/T6 (-)
Program measures voltage, there is direct current 27V voltage outputs, No. 6, No. 1 terminals output voltage of Щ Х -36 type plugs;
(2) it under off working state, according to T3 (+)/T6 (-), T5 (+)/T6 (-) program input direct-current 27V voltages, can simulate
Thermoregulator signal checks Л 4,5 all lights of Л, working properly.
4) test interface T4 (+)/T6 (-), T5 (+)/T1 (-)
(1) even under machine working condition, when testing closed throttle, according to T4 (+)/T6 (-), T5 (+)/T1 (-) program is surveyed
Measure voltage, there is a direct current 27V voltage outputs, No. 3 of Щ Х -36 type plugs, No. 5 terminals output voltages it is normal;
(2) it under off working state, can be simulated according to T4 (+)/T6 (-), T5 (+)/T1 (-) program input direct-current 27V voltages
Throttle signal checks Л 1, Л 4,5 all lights of Л, working properly.
5) test interface T2 (+)/T6 (-), T5 (+)/T4 (-)
(1) even under machine working condition, when test air throttle is opened, according to T2 (+)/T6 (-), T5 (+)/T4 (-) program is surveyed
Measure voltage, there is a direct current 27V voltage outputs, No. 3 of Щ Х -36 type plugs, No. 6 terminals output voltages it is normal;
(2) it under off working state, can be simulated according to T2 (+)/T6 (-), T5 (+)/T4 (-) program input direct-current 27V voltages
Throttle signal checks Л 2, Л 3,5 all lights of Л, working properly.
The present invention has the advantages that compared with the existing technology:
When being verified to airborne thermoregulator, this tester is inserted by Щ Х -36 types aviation plugs with airborne
Head connection, is closed ganged switch, is connected to airborne 27V DC power supplies.For adjusting cabin temperature, this tester utilizes solid-state relay
A series of actions of the correlation component such as device, airborne thermoregulator is simulated by the light on and off of one group of signal lamp to cabin
The state of a control of temperature, to realize the checking function to airborne thermoregulator and its line related.Meanwhile this tester is set
In respect of self-test interface, even when machine work, can measure under airborne thermoregulator different working condition, 27V DC power supplies it is defeated
Artificial situation;Or when off line, 27V DC power supplies are inputted by self-test interface, realize the self-test to this tester.
First, B-mode thermoregulator are to realize the tune to temperature in cabin by controlling the folding of air throttle in aircraft cabin
Section:When air throttle is opened, engine hot gas enters cabin, realizes heating;When air throttle is closed, engine hot gas cannot be into
Enter cabin, realizes cooling.
Tester is to realize to check first, the functional of B-mode thermoregulator, can be used for scene and directly judges first, second
Whether type thermoregulator works normally, and whether air throttle normally opens and closes, and is important the setting for ensureing certain type helicopter flight safety
It is standby.
Description of the drawings
Fig. 1 is the schematic diagram of each component connection structure of tester.
Fig. 2 is the schematic diagram of tester panel.
Fig. 3 is the schematic diagram of tester circuit.
Specific implementation mode
The present invention provides a kind of 2600M thermoregulators tester;
1 design principle
1.1 check A type thermoregulator manual temperature function
By adjusting " cabin heating " change-over switch on certain type helicopter second navigator's instrument board manually, make change-over switch
It is placed in " heating " or " cooling " position, A type thermoregulator exports 27V d. c. voltage signals and verified to 2600M thermoregulators
Instrument makes the corresponding signal lamp of 2600M thermoregulator testers ignite by processing, to realize to A type temperature tune
Save the manual temperature function check of device.
1.2 check first, B-mode thermoregulator automatic temperature-adjusting function
Temperature sensor signal on certain type machine is simulated by the rheostat of tester and is input to thermoregulator, thermoregulator
Output 27V d. c. voltage signals make the corresponding signal lamp of tester ignite to tester by processing after receiving signal,
To realize that the automatic temperature-adjusting function to thermoregulator verifies.
2 the key technical indexes
2.1 test event:Check the manual work performance of A type thermoregulator
(1) closed throttle, indicator light Л 1 are bright
No. 3, No. 5 terminals output voltage DC27 (1 ± 10%) V of Щ Х -36 type plugs
(2) air throttle is opened, and indicator light Л 2 is bright
No. 3, No. 6 terminals output voltage DC27 (1 ± 10%) V of Щ Х -36 type plugs
(3) " cabin heating " change-over switch is placed in " heating " position, and indicator light Л 3 is bright
No. 5, No. 1 terminals output voltage DC27 (1 ± 10%) V of Щ Х -36 type plugs
(4) " cabin heating " change-over switch is placed in " cooling " position, and indicator light Л 4 is bright
No. 6, No. 1 terminals output voltage DC27 (1 ± 10%) V of Щ Х -36 type plugs
(5) thermoregulator is powered on, and indicator light Л 5 is bright
No. 3, No. 1 terminals output voltage DC27 (1 ± 10%) V of Щ Х -36 type plugs
2.2 test event:Check the automatic work performance of thermoregulator
(1) closed throttle, indicator light Л 1 are bright
No. 3, No. 5 terminals output voltage DC27 (1 ± 10%) V of Щ Х -36 type plugs
(2) air throttle is opened, and indicator light Л 2 is bright
No. 3, No. 6 terminals output voltage DC27 (1 ± 10%) V of Щ Х -36 type plugs
(3) 2714A types manipulation device starts heating function, and indicator light Л 3 is bright
No. 5, No. 1 terminals output voltage DC27 (1 ± 10%) V of Щ Х -36 type plugs
(4) 2714A types manipulation device starts refrigerating function, and indicator light Л 4 is bright
No. 6, No. 1 terminals output voltage DC27 (1 ± 10%) V of Щ Х -36 type plugs
(5) thermoregulator is powered on, and indicator light Л 5 is bright
No. 3, No. 1 terminals output voltage DC27 (1 ± 10%) V of Щ Х -36 type plugs
2.3 test event:Check the alarm performance of B-mode thermoregulator
(1) air throttle manipulation device starts refrigerating function, and indicator light Л 4 is bright
No. 6, No. 1 terminals output voltage DC27 (1 ± 10%) V of Щ Х -37 type plugs
(2) thermoregulator is powered on, and indicator light Л 5 is bright
No. 3, No. 1 terminals output voltage DC27 (1 ± 10%) V of Щ Х -37 type plugs
2.4 operating ambient temperature:(- 10~50) DEG C.
3 specific technical solutions
Including Щ Х -36 types aviation plug, ganged switch, solid-state relay, potentiometer, diode, signal lamp;Institute
Щ Х -36 type aviation plugs connection ganged switch is stated, the ganged switch connection diode 1 and 5 signal lamps of Л, the duplex are opened
Close relay P1 in parallel, 1 signal lamps of relay P1 connections Л, 3 signal lamps of Л and diode 2, the ganged switch parallel connection
Relay P2,2 signal lamps of relay P2 connections Л, 4 signal lamps of Л and diode 3;The ganged switch, which is also connected with, tests oneself
It tries mouth;Further include tester panel, test interface, indicator light and change-over switch are set on tester panel.
Using the method for calibration of 2600M thermoregulator testers, including:1) A type thermoregulator manual temperature is checked
Function:By adjusting " cabin heating " change-over switch on certain type helicopter second navigator's instrument board manually, change-over switch is made to set
In " heating " or " cooling " position, A type thermoregulator exports 27V d. c. voltage signals to tester, keeps tester corresponding
Signal lamp ignites, to realize the manual temperature function check to A type thermoregulator;2) first, B-mode temperature tune are checked
Save device automatic temperature-adjusting function:Temperature sensor signal on certain type machine is simulated by the rheostat of tester, is input to thermoregulator,
Output 27V d. c. voltage signals make the corresponding signal lamp combustion of tester to 2 testers after thermoregulator receives signal
It is bright, to realize that the automatic temperature-adjusting function to first, second thermoregulator verifies.
Using the method for calibration of 2600M thermoregulator testers, specially:
1) test interface T5 (+)/T6 (-)
(1) even under machine working condition, when test temperature adjuster is powered, voltage is measured according to T5 (+)/T6 (-) program, is had
Direct current 27V voltage outputs, No. 3, No. 1 terminals output voltage of Щ Х -36 type plugs;
(2) under off working state, according to T5 (+)/T6 (-) program input direct-current 27V voltages, working power letter can be simulated
Number, check 5 working conditions of Л.
2) test interface T1 (+)/T6 (-), T5 (+)/T6 (-)
(1) even under machine working condition, when test temperature adjuster " heating ", according to T1 (+)/T6 (-), T5 (+)/T6 (-)
Program measures voltage, there is a direct current 27V voltage outputs, No. 5 of Щ Х -36 type plugs, No. 1 terminals output voltage it is normal;
(2) it under off working state, according to T1 (+)/T6 (-), T5 (+)/T6 (-) program input direct-current 27V voltages, can simulate
Thermoregulator signal checks Л 3,5 all lights of Л, working properly.
3) test interface T3 (+)/T6 (-), T5 (+)/T6 (-)
(1) even under machine working condition, when test temperature adjuster " cooling ", according to T3 (+)/T6 (-), T5 (+)/T6 (-)
Program measures voltage, there is direct current 27V voltage outputs, No. 6, No. 1 terminals output voltage of Щ Х -36 type plugs;
(2) it under off working state, according to T3 (+)/T6 (-), T5 (+)/T6 (-) program input direct-current 27V voltages, can simulate
Thermoregulator signal checks Л 4,5 all lights of Л, working properly.
4) test interface T4 (+)/T6 (-), T5 (+)/T1 (-)
(1) even under machine working condition, when testing closed throttle, according to T4 (+)/T6 (-),
T5 (+)/T1 (-) program measures voltage, there is direct current 27V voltage outputs, No. 3, No. 5 wiring of Щ Х -36 type plugs
Hold output voltage normal;
(2) it under off working state, can be simulated according to T4 (+)/T6 (-), T5 (+)/T1 (-) program input direct-current 27V voltages
Throttle signal checks Л 1, Л 4,5 all lights of Л, working properly.
5) test interface T2 (+)/T6 (-), T5 (+)/T4 (-)
(1) even under machine working condition, when test air throttle is opened, according to T2 (+)/T6 (-), T5 (+)/T4 (-) program is surveyed
Measure voltage, there is a direct current 27V voltage outputs, No. 3 of Щ Х -36 type plugs, No. 6 terminals output voltages it is normal;
(2) it under off working state, can be simulated according to T2 (+)/T6 (-), T5 (+)/T4 (-) program input direct-current 27V voltages
Throttle signal checks Л 2, Л 3,5 all lights of Л, working properly.
Embodiment 1:
1, A type thermoregulator manual temperature function is checked
(1) certain type helicopter closed throttle, No. 3, No. 5 terminals of the Щ Х -36 type plugs of A type thermoregulator
Output voltage DC27 (1 ± 10%) V, indicator light Л 1 is bright;
(2) air throttle is opened, No. 3, No. 6 terminals output voltage DC27 (1 ± 10%) V of Щ Х -36 type plugs, instruction
Lamp Л 2 is bright;
(3) " cabin heating " change-over switch is placed in " heat " position, No. 5, No. 1 terminals output voltage of Щ Х -36 type plugs
DC27 (1 ± 10%) V, indicator light Л 3 is bright;
(4) " cabin heating " change-over switch is placed in " cold " position, No. 6, No. 1 terminals output voltage of Щ Х -36 type plugs
DC27 (1 ± 10%) V, indicator light Л 4 is bright;
(5) thermoregulator is powered on, No. 3 of Щ Х -36 type plugs, No. 1 terminals output voltage DC27 (1 ±
10%) V, indicator light Л 5 are bright.
2:Check first, B-mode thermoregulator automatic temperature-adjusting function
(1) certain type helicopter closed throttle, No. 3, No. 5 terminals outputs of the Щ Х -36 type plugs of thermoregulator
Voltage DC27 (1 ± 10%) V, indicator light Л 1 is bright;
(2) air throttle is opened, No. 3, No. 6 terminals output voltage DC27 (1 ± 10%) V of Щ Х -36 type plugs, instruction
Lamp Л 2 is bright;
(3) 2714A types manipulation device starts heating function, No. 5, No. 1 terminals output voltage of Щ Х -36 type plugs
DC27 (1 ± 10%) V, indicator light Л 3 is bright;
(4) 2714A types manipulation device starts heating function, No. 6, No. 1 terminals output voltage of Щ Х -36 type plugs
DC27 (1 ± 10%) V, indicator light Л 4 is bright;
(5) thermoregulator is powered on, No. 3 of Щ Х -36 type plugs, No. 1 terminals output voltage DC27 (1 ±
10%) V, indicator light Л 5 are bright.
Although the present invention is disclosed as above with preferred embodiment, however, it is not to limit the invention, any this field skill
Art personnel, without departing from the spirit and scope of the present invention, when can make a little modification and it is perfect, therefore the present invention protection model
It encloses to work as and is subject to what claims were defined.
Claims (3)
1. a kind of 2600M thermoregulators tester, it is characterised in that:
Including Щ Х -36 types aviation plug, ganged switch, solid-state relay, potentiometer, diode, signal lamp;The Щ
Х -36 type aviation plugs connect ganged switch, the ganged switch connection diode 1 and 5 signal lamps of Л, and the ganged switch is simultaneously
Join relay P1,1 signal lamps of relay P1 connections Л, 3 signal lamps of Л and diode 2, the ganged switch parallel connection relay
Device P2,2 signal lamps of relay P2 connections Л, 4 signal lamps of Л and diode 3;The ganged switch is also connected with to test oneself and try
Mouthful;Further include tester panel, test interface, indicator light and change-over switch are set on tester panel.
2. a kind of method of calibration of application 2600M thermoregulators tester as described in claim 1, it is characterised in that:1)
Check A type thermoregulator manual temperature function:By adjusting " the cabin on certain type helicopter second navigator's instrument board manually
Heating " change-over switch, makes change-over switch be placed in " heating " or " cooling " position, and A type thermoregulator exports 27V DC voltages
Signal makes the corresponding signal lamp of tester ignite to tester, to realize the manual temperature to A type thermoregulator
Function check;2) first, B-mode thermoregulator automatic temperature-adjusting function are checked:Temperature on certain type machine is simulated by the rheostat of tester
Sensor signal, is input to thermoregulator, and thermoregulator receives after signal output 27V d. c. voltage signals to 2 testers,
The corresponding signal lamp of tester is set to ignite, to realize that the automatic temperature-adjusting function to first, second thermoregulator verifies.
3. the method for calibration of 2600M thermoregulators tester as claimed in claim 2, it is characterised in that:
1) test interface T5 (+)/T6 (-)
(1) even under machine working condition, when test temperature adjuster is powered, voltage is measured according to T5 (+)/T6 (-) program, there is direct current
27V voltage outputs, No. 3, No. 1 terminals output voltage of Щ Х -36 type plugs;
(2) under off working state, according to T5 (+)/T6 (-) program input direct-current 27V voltages, working power signal can be simulated, is examined
Look into 5 working conditions of Л.
2) test interface T1 (+)/T6 (-), T5 (+)/T6 (-)
(1) even under machine working condition, when test temperature adjuster " heating ", according to T1 (+)/T6 (-), T5 (+)/T6 (-) program
Measure voltage, there is a direct current 27V voltage outputs, No. 5 of Щ Х -36 type plugs, No. 1 terminals output voltage it is normal;
It (2), can analog temperature according to T1 (+)/T6 (-), T5 (+)/T6 (-) program input direct-current 27V voltages under off working state
Regulator signal checks Л 3,5 all lights of Л, working properly.
3) test interface T3 (+)/T6 (-), T5 (+)/T6 (-)
(1) even under machine working condition, when test temperature adjuster " cooling ", according to T3 (+)/T6 (-), T5 (+)/T6 (-) program
Voltage is measured, there is direct current 27V voltage outputs, No. 6, No. 1 terminals output voltage of Щ Х -36 type plugs;
It (2), can analog temperature according to T3 (+)/T6 (-), T5 (+)/T6 (-) program input direct-current 27V voltages under off working state
Regulator signal checks Л 4,5 all lights of Л, working properly.
4) test interface T4 (+)/T6 (-), T5 (+)/T1 (-)
(1) even under machine working condition, when testing closed throttle, according to T4 (+)/T6 (-), T5 (+)/T1 (-) program measures electricity
Pressure, there is a direct current 27V voltage outputs, No. 3 of Щ Х -36 type plugs, No. 5 terminals output voltages it is normal;
(2) under off working state, solar term can be simulated according to T4 (+)/T6 (-), T5 (+)/T1 (-) program input direct-current 27V voltages
Gate signal checks Л 1, Л 4,5 all lights of Л, working properly.
5) test interface T2 (+)/T6 (-), T5 (+)/T4 (-)
(1) even under machine working condition, when test air throttle is opened, according to T2 (+)/T6 (-), T5 (+)/T4 (-) program measures electricity
Pressure, there is a direct current 27V voltage outputs, No. 3 of Щ Х -36 type plugs, No. 6 terminals output voltages it is normal;
(2) under off working state, solar term can be simulated according to T2 (+)/T6 (-), T5 (+)/T4 (-) program input direct-current 27V voltages
Gate signal checks Л 2, Л 3,5 all lights of Л, working properly.
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CN103674327A (en) * | 2013-12-09 | 2014-03-26 | 张金木 | Automatic thermal resistance temperature calibration instrument |
CN203519788U (en) * | 2013-09-16 | 2014-04-02 | 国家电网公司 | Main transformer temperature relay verifying device |
CN104502000A (en) * | 2014-12-26 | 2015-04-08 | 上海市计量测试技术研究院 | Shallow-type micro temperature calibration furnace and calibration method |
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2018
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CN2113496U (en) * | 1991-07-21 | 1992-08-19 | 苏州供电局 | Relay checking box |
US20030028345A1 (en) * | 1999-12-20 | 2003-02-06 | Watkins Arthur D. | Device for self-verifying temperature measurement and control |
CN200946760Y (en) * | 2006-08-31 | 2007-09-12 | 上海宝钢设备检修有限公司 | Pneumatic calibration equipment |
CN103135012A (en) * | 2012-12-21 | 2013-06-05 | 中国飞行试验研究院 | Airplane direct current appliance function detector |
CN103162901A (en) * | 2013-03-28 | 2013-06-19 | 北京国浩传感器技术研究院(普通合伙) | Nonlinear calibrating method for multiple temperature points of pressure sensor |
CN203519788U (en) * | 2013-09-16 | 2014-04-02 | 国家电网公司 | Main transformer temperature relay verifying device |
CN103674327A (en) * | 2013-12-09 | 2014-03-26 | 张金木 | Automatic thermal resistance temperature calibration instrument |
CN104502000A (en) * | 2014-12-26 | 2015-04-08 | 上海市计量测试技术研究院 | Shallow-type micro temperature calibration furnace and calibration method |
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Address after: No. 3127, Changzhong Road, Jing'an District, Shanghai 200436 Patentee after: SHANGHAI HAIYING MACHINERY PLANT Address before: No. 3127, Changzhong Road, Hongkou District, Shanghai, 200080 Patentee before: SHANGHAI HAIYING MACHINERY PLANT |