CN106643789A - Control method of acceleration-temperature combination and calibration equipment - Google Patents

Control method of acceleration-temperature combination and calibration equipment Download PDF

Info

Publication number
CN106643789A
CN106643789A CN201610829996.6A CN201610829996A CN106643789A CN 106643789 A CN106643789 A CN 106643789A CN 201610829996 A CN201610829996 A CN 201610829996A CN 106643789 A CN106643789 A CN 106643789A
Authority
CN
China
Prior art keywords
temperature
acceleration
attemperating unit
accurate
unit
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.)
Granted
Application number
CN201610829996.6A
Other languages
Chinese (zh)
Other versions
CN106643789B (en
Inventor
董雪明
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.)
Beijing Changcheng Institute of Metrology and Measurement AVIC
Original Assignee
Beijing Changcheng Institute of Metrology and Measurement AVIC
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 Beijing Changcheng Institute of Metrology and Measurement AVIC filed Critical Beijing Changcheng Institute of Metrology and Measurement AVIC
Priority to CN201610829996.6A priority Critical patent/CN106643789B/en
Publication of CN106643789A publication Critical patent/CN106643789A/en
Application granted granted Critical
Publication of CN106643789B publication Critical patent/CN106643789B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C25/00Manufacturing, calibrating, cleaning, or repairing instruments or devices referred to in the other groups of this subclass
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P21/00Testing or calibrating of apparatus or devices covered by the preceding groups

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Manufacturing & Machinery (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Centrifugal Separators (AREA)

Abstract

The invention provides a control method of acceleration-temperature combination and a piece of calibration equipment for executing the method. The calibration equipment is used for producing thermal environment with stable acceleration, high precision and wide region. The method comprises the following steps: when a precise centrifuge is stationary, temperature of a precise temperature control apparatus is controlled to be increased or decreased to a target temperature, when the precise centrifuge rotates, the temperature of the precise temperature control apparatus is kept to the temperature when the precise centrifuge is stationary, and acceleration of the precise temperature control apparatus is controlled to a target accelerated speed. Metering calibration requirements of inertial components in a thermal environment complex condition with stable acceleration, high precision and wide region are satisfied, and controlled acceleration and temperature have large ranges and high precision.

Description

A kind of compound control method of acceleration-temperature and calibrator (-ter) unit
Technical field
The present invention relates to a kind of compound control method of acceleration-temperature and its calibrator (-ter) unit, more particularly to one kind is used Property the compound calibrator (-ter) unit of device configuration stable state acceleration and target temperature and its control method, belong to inertia device measurement and calibration Technical field.
Background technology
The continuous development of inertial technology proposes higher and higher requirement to inertia measurement and calibration technology.Past is in single standard Carrying out the work of measurement and calibration under input condition to inertia type instrument can not meet under complicated applications environment to inertia type instrument output The magnitude tracing of amount.And, inertia device quantum property is compound with acceleration and thermal environment in the case of single acceleration effect Under operative condition is different, i.e. the single acceleration or heat effect rule that can not pass through single obtains accurately acceleration The rule of degree and thermal environment compound action.Therefore, the calibration that a kind of precision centrifuge and accurate attemperating unit are composited is developed Equipment is very necessary.
In the research of compound calibrator (-ter) unit, focus predominantly stays in combined environment testing aspect, mainly including combinational environment The testing equipment and test method of test.As combined low temperature low air pressure testing chamber, temperature low pressure vibration (sine) combined test chamber with Temperature low pressure vibration (random) combined test chamber etc., is all the equipment about combined environment testing, it is of interest that reliability is tried Test and functional test, and cannot be used for the measurement and calibration field of high accuracy inertia device, and these equipment complexes be all Ground handling, it is impossible to for the centrifuge of high speed rotation output high acceleration.Rarely has the control of disclosed acceleration-temperature at present The document of method processed and calibrator (-ter) unit.
The present invention controls the temperature of accurate attemperating unit when precision centrifuge is static and rises or be down to target temperature, Yi Ji When precision centrifuge rotates, temperature when keeping the temperature of accurate attemperating unit to be in static, and control accurate attemperating unit Acceleration is to aimed acceleration.So that being calibrated the common activation that inertia device is directly subject to high acceleration and heat, complete to be used to The gamut temperature control of property device high order term coefficient or the calibration of temperature coefficient and acceleration.
The content of the invention
The invention discloses a kind of acceleration-temperature-controlled process and its calibrator (-ter) unit.By the method and calibrator (-ter) unit, The compound condition of stable state acceleration and thermal environment can be constructed such that it is able to inertia device in acceleration and the compound work of thermal environment Quantum property with carries out measurement and calibration with analysis.
The present invention is achieved by the following technical solutions:
The compound calibrator (-ter) unit of a kind of acceleration-temperature, it is characterised in that include:Precision centrifuge, accurate temperature control dress Put, ground temperature control box, liquid nitrogen control system and pipeline;It is calibrated inertia device to be placed in accurate attemperating unit;Precision centrifugation Machine is connected with accurate attemperating unit flange, there is provided required acceleration;Between ground temperature control box and accurate attemperating unit, liquid nitrogen control Connected by pipeline between system processed and accurate attemperating unit;Institute when ground temperature control box provides static for accurate attemperating unit The temperature for needing, temperature of the liquid nitrogen control system needed for for when accurate attemperating unit provides rotation.
The compound control method of a kind of acceleration-temperature, when precision centrifuge is static:By ground temperature control box control essence The temperature of close attemperating unit is risen or fallen to target temperature, and when precision centrifuge rotates:By liquid nitrogen control system Temperature when keeping the temperature of accurate attemperating unit to be in static, and fill accurate temperature control by controlling the rotating speed of precision centrifuge The acceleration put is to aimed acceleration.
Specifically, when precision centrifuge is static, the temperature that accurate attemperating unit is controlled by ground temperature control box rise or Target temperature is dropped to, step includes:
S1, connection ground temperature control box are connected with the heat exchange medium turnover of accurate attemperating unit, in making ground temperature control box Heat exchange medium Jing pipelines and accurate attemperating unit form closed circuit;
S2, by control ground temperature control box in heat exchange medium temperature rise or decline, make to be followed in the temperature control box of ground The dynamic heat exchange medium of circulation carries out heat exchange Jing after S1 with the air in accurate attemperating unit;
S3, when the air in accurate attemperating unit or it is calibrated the temperature of inertia device and rises or drop to target temperature When, the connection of the ground temperature control box described in S1 and accurate attemperating unit is disconnected, stop hot described in circulation and S2 described in S1 friendship Change.
Specifically, when precision centrifuge rotates, the temperature of accurate attemperating unit is kept to be in by liquid nitrogen control system Temperature when static, and by controlling the rotating speed of precision centrifuge the acceleration of accurate attemperating unit is made to aimed acceleration, step Suddenly include:
S4, the connection connected between liquid nitrogen control system and accurate attemperating unit;
S5, the influx of control liquid nitrogen make to be calibrated inertia in accurate attemperating unit to keep or micro adjusting box body temperature The temperature of device be in precision centrifuge it is static when temperature value;
S6, start precision centrifuge (1), control precision centrifuge rotating speed, make in accurate attemperating unit be calibrated it is used Property device reaches aimed acceleration.
A kind of calibrator (-ter) unit, the calibrator (-ter) unit is when precision centrifuge is static:Accurate temperature control is controlled by ground temperature control box The temperature of device is risen or fallen to target temperature, and when precision centrifuge rotates:Essence is kept by liquid nitrogen control system The temperature when temperature of close attemperating unit is in static, and make adding for accurate attemperating unit by controlling the rotating speed of precision centrifuge Speed is to aimed acceleration.
The step of a kind of compound calibrator (-ter) unit of acceleration-temperature, equipment execution above-mentioned S1~S3;A kind of acceleration- The compound calibrator (-ter) unit of temperature, the step of the equipment also performs above-mentioned S4~S6.
The present invention can obtain following beneficial effect:
Can be the combinational environment for being calibrated inertia device construction stable state acceleration and target temperature, that is, be calibrated inertia device Part by precision centrifuge while accurate acceleration is obtained, moreover it is possible to obtain accurate temperature strip by accurate attemperating unit Part such that it is able to which the quantum property to inertia device under acceleration and thermal environment compound action carries out measurement and calibration with analysis;
Meet the stable state acceleration of standard and thermal environment composition is calibrated the requirement that inertia device is combined calibration.Control Acceleration and temperature range are big, high precision.
Description of the drawings
Fig. 1 shows the structural representation of calibrator (-ter) unit of the present invention.
Fig. 2 shows the acceleration-temperature-controlled process flow chart of the present invention.
Specific embodiment
Below in conjunction with the accompanying drawings the present invention will be further described.
Fig. 1 shows the structural representation of calibrator (-ter) unit of the present invention.A kind of compound calibrator (-ter) unit of acceleration-temperature, bag Include:Precision centrifuge 1, accurate attemperating unit 2, ground temperature control box 3, liquid nitrogen control system 4, liquid nitrogen control system 4 and pipeline 5. It is calibrated inertia device 6 to be placed in accurate attemperating unit 2.Precision centrifuge 1 is connected with the accurate flange of attemperating unit 2, there is provided Required acceleration;Between ground temperature control box 3 and accurate attemperating unit 2, between liquid nitrogen control system 4 and accurate attemperating unit 2 Connected by pipeline 5;Temperature of the ground temperature control box 3 needed for for when accurate attemperating unit 2 provides static, liquid nitrogen control system 4 temperature needed for for when accurate attemperating unit 2 provides rotation.
Fig. 2 shows the compound control method flow chart of the acceleration-temperature of the present invention.Inertia device is calibrated in order to give The combinational environment sheet of stable state acceleration and target temperature is constructed, the thinking of the acceleration-temperature-controlled process of invention is:In precision When centrifuge 1 is static, the temperature for controlling accurate attemperating unit 2 by ground temperature control box 3 is risen or fallen to target temperature;And When precision centrifuge 1 rotates, temperature when keeping the temperature of accurate attemperating unit 2 to be in static by liquid nitrogen control system 4, And by controlling the rotating speed of precision centrifuge 1 acceleration of accurate attemperating unit 2 is made to aimed acceleration.So as to realize to precision Quantum property of the inertia device 6 under acceleration and thermal environment compound action that be calibrated in attemperating unit 2 carries out measurement and calibration With analysis.
When precision centrifuge 1 is static, i.e. in the T1 of Fig. 2, the temperature of accurate attemperating unit 2 is controlled by ground temperature control box 3 Degree is risen or fallen to target temperature, and step includes:
S1, connection ground temperature control box 3 are connected with the heat exchange medium turnover of accurate attemperating unit 2, in making ground temperature control box 3 Heat exchange medium Jing pipelines 5 and accurate attemperating unit 2 form closed circuit;
S2, by control ground temperature control box 3 in heat exchange medium temperature rise or decline, in making ground temperature control box 3 The heat exchange medium for circulating carries out heat exchange Jing after S1 with the air in accurate attemperating unit 2;
S3, when the air in accurate attemperating unit 2 or it is calibrated the temperature of inertia device 6 and rises or drop to target temperature When spending, the connection of the ground temperature control box 3 described in S1 and accurate attemperating unit 2 is disconnected, stopped described in circulation and the S2 described in S1 Heat exchange.
When precision centrifuge 1 rotates, i.e. in the T2 of Fig. 2, accurate attemperating unit 2 is kept by liquid nitrogen control system 4 Temperature when temperature is in static, and by controlling the rotating speed of precision centrifuge 1 acceleration of accurate attemperating unit 2 is made to target Acceleration, step includes:
S4, the connection connected between liquid nitrogen control system 4 and accurate attemperating unit 2;
S5, the influx of control liquid nitrogen make to be calibrated inertia in accurate attemperating unit 2 to keep or micro adjusting box body temperature The temperature of device 6 be in precision centrifuge it is static when temperature value;
S6, start precision centrifuge 1, control precision centrifuge 1 rotating speed, make in accurate attemperating unit 2 be calibrated it is used Property device 6 reaches aimed acceleration.
The compound calibrator (-ter) unit of above acceleration-temperature, under combining case, the 0~390m/ of scope of stable state acceleration s2, acceleration analysis uncertainty 2.5 × 10-5;- 60 DEG C of temperature measurement range~85 DEG C, temperature deviation is better than 0.2 DEG C.

Claims (8)

1. the calibrator (-ter) unit that a kind of acceleration-temperature is combined, it is characterised in that include:Precision centrifuge (1), accurate temperature control dress Put (2), ground temperature control box (3), liquid nitrogen control system (4) and pipeline (5);It is calibrated inertia device (6) and is placed in accurate temperature control In device (2);Precision centrifuge (1) is connected with accurate attemperating unit (2) flange, there is provided required acceleration;Ground temperature control box (3) and accurate attemperating unit (2) between, between liquid nitrogen control system (4) and accurate attemperating unit (2) by pipeline (5) company Connect;Temperature of the ground temperature control box (3) needed for for when accurate attemperating unit (2) provides static, liquid nitrogen control system (4) is precision Attemperating unit (2) provides required temperature during rotation.
2. the control method that a kind of acceleration-temperature is combined, it is characterised in that when precision centrifuge (1) is static:By ground The temperature of the accurate attemperating unit (2) of temperature control box (3) control is risen or fallen to target temperature, and in precision centrifuge (1) rotation When turning:Temperature when keeping the temperature of accurate attemperating unit (2) to be in static by liquid nitrogen control system (4), and by control The rotating speed of precision centrifuge (1) makes the acceleration of accurate attemperating unit (2) to aimed acceleration.
3. the control method that temperature-acceleration according to claim 2 is combined, it is characterised in that in precision centrifuge (1) When static, the temperature for controlling accurate attemperating unit (2) by ground temperature control box (3) is risen or fallen to target temperature, step bag Include:
S1, connection ground temperature control box (3) are connected with the heat exchange medium turnover of accurate attemperating unit (2), make ground temperature control box (3) In heat exchange medium Jing pipelines (5) and accurate attemperating unit (2) form closed circuit;
S2, by controlling ground temperature control box (3) in heat exchange medium temperature rise or decline, in making ground temperature control box (3) The heat exchange medium for circulating carries out heat exchange Jing after S1 with the air in accurate attemperating unit (2);
S3, when the air in accurate attemperating unit (2) or it is calibrated the temperature of inertia device (6) and rises or drop to target temperature When spending, the ground temperature control box (3) described in S1 and the connection of accurate attemperating unit (2) are disconnected, stop the circulation described in S1 and S2 The heat exchange.
4. the control method that temperature-acceleration according to claim 2 is combined, it is characterised in that in precision centrifuge (1) During rotation, temperature when keeping the temperature of accurate attemperating unit (2) to be in static by liquid nitrogen control system (4), and by control The rotating speed of precision centrifuge (1) processed makes the acceleration of accurate attemperating unit (2) to aimed acceleration, and step includes:
S4, the connection connected between liquid nitrogen control system (4) and accurate attemperating unit (2);
S5, the influx of control liquid nitrogen make to be calibrated inertia device in accurate attemperating unit (2) to keep or micro adjusting box body temperature The temperature of part (6) be in precision centrifuge it is static when temperature value;
S6, startup precision centrifuge (1), control the rotating speed of precision centrifuge (1), make being calibrated in accurate attemperating unit (2) Inertia device (6) reaches aimed acceleration.
5. the calibrator (-ter) unit that a kind of acceleration-temperature is combined, it is characterised in that the calibrator (-ter) unit is static in precision centrifuge (1) When:The temperature for controlling accurate attemperating unit (2) by ground temperature control box (3) is risen or fallen to target temperature, and in precision When centrifuge (1) rotates:Temperature when keeping the temperature of accurate attemperating unit (2) to be in static by liquid nitrogen control system (4), And by controlling the rotating speed of precision centrifuge (1) acceleration of accurate attemperating unit (2) is made to aimed acceleration.
6. the calibrator (-ter) unit that a kind of acceleration-temperature according to claim 5 is combined, it is characterised in that perform such as right Step in requiring 4.
7. the calibrator (-ter) unit that a kind of acceleration-temperature according to claim 5 is combined, it is characterised in that perform such as right Step in requiring 5.
8. the compound calibrator (-ter) unit of acceleration-temperature according to any claim in claim 1,5,6,7, its feature It is, under combining case, the 0~390m/s of scope of stable state acceleration2, acceleration analysis uncertainty 2.5 × 10-5;Temperature - 60 DEG C of measurement range~85 DEG C, temperature deviation is better than 0.2 DEG C.
CN201610829996.6A 2016-09-18 2016-09-18 A kind of control method and calibrator (-ter) unit that acceleration-temperature is compound Active CN106643789B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610829996.6A CN106643789B (en) 2016-09-18 2016-09-18 A kind of control method and calibrator (-ter) unit that acceleration-temperature is compound

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610829996.6A CN106643789B (en) 2016-09-18 2016-09-18 A kind of control method and calibrator (-ter) unit that acceleration-temperature is compound

Publications (2)

Publication Number Publication Date
CN106643789A true CN106643789A (en) 2017-05-10
CN106643789B CN106643789B (en) 2018-10-02

Family

ID=58852301

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610829996.6A Active CN106643789B (en) 2016-09-18 2016-09-18 A kind of control method and calibrator (-ter) unit that acceleration-temperature is compound

Country Status (1)

Country Link
CN (1) CN106643789B (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108168810A (en) * 2017-11-29 2018-06-15 中国航空工业集团公司沈阳飞机设计研究所 Vibration characteristics tests system under a kind of hyperthermal environments
CN108827294A (en) * 2018-07-12 2018-11-16 湖南科众兄弟科技有限公司 The temperature-compensation method of inertial navigation system
CN110308309A (en) * 2019-08-13 2019-10-08 中北大学 A kind of high temperature resistant capacitive accelerometer and its wireless test verification platform
CN111895945A (en) * 2020-07-21 2020-11-06 苏州久涛传感科技有限公司 Displacement sensor with high temperature resistant shockproof structure

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5321638A (en) * 1990-04-30 1994-06-14 Witney Keith C Calibrated sensor systems and methods of manufacturing same
CN101639488A (en) * 2009-08-22 2010-02-03 中北大学 Test method of micro-accelerometer reliability intensifying test
CN103777039A (en) * 2014-01-10 2014-05-07 北京航空航天大学 Centrifugal-temperature composite test box
CN103791917A (en) * 2014-01-10 2014-05-14 浙江大学 Device and method for testing vibration-temperature crosslinking coupling degree of fiber optic gyroscope

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5321638A (en) * 1990-04-30 1994-06-14 Witney Keith C Calibrated sensor systems and methods of manufacturing same
CN101639488A (en) * 2009-08-22 2010-02-03 中北大学 Test method of micro-accelerometer reliability intensifying test
CN103777039A (en) * 2014-01-10 2014-05-07 北京航空航天大学 Centrifugal-temperature composite test box
CN103791917A (en) * 2014-01-10 2014-05-14 浙江大学 Device and method for testing vibration-temperature crosslinking coupling degree of fiber optic gyroscope

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
李颖奇 等: "《离心-温度复合试验箱温度精密控制方法》", 《计测技术》 *
董雪明 等: "《加速度计校准技术综述》", 《计测技术》 *
董雪明 等: "《大g值条件下加速度计温度系数校准装置研制》", 《计测技术》 *

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108168810A (en) * 2017-11-29 2018-06-15 中国航空工业集团公司沈阳飞机设计研究所 Vibration characteristics tests system under a kind of hyperthermal environments
CN108827294A (en) * 2018-07-12 2018-11-16 湖南科众兄弟科技有限公司 The temperature-compensation method of inertial navigation system
CN110308309A (en) * 2019-08-13 2019-10-08 中北大学 A kind of high temperature resistant capacitive accelerometer and its wireless test verification platform
CN110308309B (en) * 2019-08-13 2021-06-22 中北大学 High-temperature-resistant capacitive accelerometer and wireless test verification platform thereof
CN111895945A (en) * 2020-07-21 2020-11-06 苏州久涛传感科技有限公司 Displacement sensor with high temperature resistant shockproof structure

Also Published As

Publication number Publication date
CN106643789B (en) 2018-10-02

Similar Documents

Publication Publication Date Title
CN106643789A (en) Control method of acceleration-temperature combination and calibration equipment
CN103398835B (en) Based on gaseous film control transient heat flow test macro and the method for hypersonic gun wind tunnel
CN104729017B (en) The constant air capacity control of air conditioner, control device
CN105911091A (en) Test device and method for research of temperature field distribution characteristics under temperature-acceleration environment
CN109590631B (en) Weldability detection method
Luo et al. Thermal transient test based thermal structure function analysis of IGBT package
Hubble et al. A hybrid method for measuring heat flux
CN109073474A (en) Temperature determining device and its calibration and the method for determining medium temperature
CN109063404A (en) A kind of dynamic prediction method of Aerostatic thrust bearing rigidity
Tan et al. Thermal error prediction of machine tool spindle using segment fusion LSSVM
Christensen et al. Infrared temperature measurements of the blade tip for a turbine operating at corrected engine conditions
CN107659241B (en) Servo motor control unit and method, computer-readable storage medium
Haldeman et al. Fully cooled single stage HP transonic turbine—Part I: Influence of cooling mass flow variations and inlet temperature profiles on blade internal and external aerodynamics
Hirano et al. Accurate and fast creep test for viscoelastic fluids using disk-probe-type and quadrupole-arrangement-type electromagnetically spinning systems
CN107884094A (en) A kind of special-shaped high temperature sensor and calibration method
Wang et al. A multicomponent distributed parameter model for spray drying: model development and validation with experiments
CN105258677B (en) A kind of high-precision inclinometer and intelligent temperature complement system
Lian et al. Influence of Operating Temperature on the Static Characteristics of an Externally Pressurized Thrust Bearing Lubricated with Refrigerant Gas
CN203455299U (en) Heat-flux-type differential scanning calorimeter
CN108225667B (en) Pixel-level shear-sensitive liquid crystal calibration method and device
CN114961889B (en) Turbine rotating static disc cavity airflow swirl ratio measuring method
Cuadrado et al. Methodology to Correct the Magnetic Field Effect on Thin Film Measurements
Manjhi et al. Conduction-Based Standardization of K-Type Coaxial Thermocouple for Short-Duration Transient Heat Flux Measurement
Nichols et al. Rotor damped natural frequencies and stability under reduced oil supply flow rates to tilting-pad journal bearings
Weiner et al. Extension of the Freiberg layer model by means of solidification for roll casting

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant