CN114646663A - High-efficiency measurement system and method for thermal radiation characteristics of materials with different thicknesses of high-temperature infrared hood - Google Patents

High-efficiency measurement system and method for thermal radiation characteristics of materials with different thicknesses of high-temperature infrared hood Download PDF

Info

Publication number
CN114646663A
CN114646663A CN202210324793.7A CN202210324793A CN114646663A CN 114646663 A CN114646663 A CN 114646663A CN 202210324793 A CN202210324793 A CN 202210324793A CN 114646663 A CN114646663 A CN 114646663A
Authority
CN
China
Prior art keywords
infrared
radiation
hood
temperature
sample material
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.)
Pending
Application number
CN202210324793.7A
Other languages
Chinese (zh)
Inventor
齐宏
朱泽宇
赵颖
任亚涛
何明键
高包海
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.)
Harbin Institute of Technology
Original Assignee
Harbin Institute of Technology
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 Harbin Institute of Technology filed Critical Harbin Institute of Technology
Priority to CN202210324793.7A priority Critical patent/CN114646663A/en
Publication of CN114646663A publication Critical patent/CN114646663A/en
Pending legal-status Critical Current

Links

Images

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N25/00Investigating or analyzing materials by the use of thermal means
    • G01N25/20Investigating or analyzing materials by the use of thermal means by investigating the development of heat, i.e. calorimetry, e.g. by measuring specific heat, by measuring thermal conductivity

Landscapes

  • Physics & Mathematics (AREA)
  • Health & Medical Sciences (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Chemical & Material Sciences (AREA)
  • Analytical Chemistry (AREA)
  • Biochemistry (AREA)
  • General Health & Medical Sciences (AREA)
  • General Physics & Mathematics (AREA)
  • Immunology (AREA)
  • Pathology (AREA)
  • Length Measuring Devices By Optical Means (AREA)
  • Radiation Pyrometers (AREA)

Abstract

A high-efficiency measurement system and method for thermal radiation characteristics of materials with different thicknesses of a high-temperature infrared hood belong to the technical field of thermal radiation measurement. The method aims to solve the problem that reconstruction result precision is crossed due to the fact that the existing numerical simulation method is greatly influenced by the thickness of a material to be measured and measurement errors. According to the invention, an infrared hood test piece is equally divided along the radiation transfer direction, and the total radiation penetrating through the 1 st layer, the 1 st-2 nd layer, the … … and the 1-n th layer of the hood material is sequentially obtained according to the radiation transmission principle and the energy conservation relation; an algebraic relationship is then derived based on an energy method that is satisfied between the transmittance and self-irradiance of the infrared hood material having a thickness Δ and a temperature T and the transmittance and self-irradiance of the entire infrared detection hood. The transmittance of the infrared hood with the thickness x, the self-radiation characteristic and other heat radiation characteristics are measured through experiments, and the heat radiation characteristic data of the material with the unit thickness are calculated based on an algebraic relation. The infrared hood is mainly used for obtaining the heat radiation characteristic of the infrared hood.

Description

High-efficiency measurement system and method for thermal radiation characteristics of materials with different thicknesses of high-temperature infrared hood
Technical Field
The invention belongs to the technical field of thermal radiation measurement, and particularly relates to a method for measuring thermal radiation characteristics of materials with different thicknesses of a high-temperature infrared hood.
Background
When the aircraft flies in the atmosphere at ultrahigh speed, the high-temperature infrared hood quickly becomes a main factor of the aerodynamic heat radiation effect of the infrared detection system. The high temperature increases the self thermal radiation of the infrared hood, the radiation on the surface of the infrared hood is mainly concentrated on an infrared band, the high-temperature shock wave gas and the infrared hood generate strong pneumatic thermal radiation effect to form radiation interference on a detector and form interference on an infrared signal of a target, the background brightness of the detector is increased, the detection signal-to-noise ratio of the target is reduced, the detection and tracking capacity of the system on the target is reduced, even the infrared detector is saturated and cannot accurately distinguish the signal from the target, the target detection, tracking and identification capacity is weakened, and the imaging quality of the infrared detection system is reduced.
At present, measurement and research on infrared hood materials mostly focus on physical and chemical properties such as strength, hardness, melting point, refractive index, thermal conductivity and corrosion resistance, the research on thermal radiation transmission characteristics such as transmittance and attenuation coefficient is less, data in a high-temperature state is less, the development of the research on the aerodynamic thermal radiation effect of a high-temperature infrared optical window is influenced or even restricted, and the application of an infrared detection system in the field of hypersonic aircrafts is hindered.
The traditional method for testing the radiation characteristic of the infrared hood aims at the same material, one or even a plurality of repeated experiments are required to be carried out when the thickness of the material is changed, the environmental working conditions such as the temperature and the like of each experiment cannot be guaranteed to be completely consistent, the error between the radiation characteristic measured value and the true value of the infrared hood material is large, and extra experiment cost waste is caused. The traditional idea is to simulate the actual situation by adopting a numerical simulation method including a discrete coordinate method, a finite volume method and the like, and inversely reconstruct the radiation characteristic field in the medium, such as an absorption coefficient field, a refractive index field and the like, by combining the measurement results of the apparent radiation intensities at different angles. The reconstruction process is greatly affected by measurement errors and the like, and the reconstruction accuracy decreases as the thickness of the medium increases. Therefore, a method for realizing one-time measurement of thermal radiation characteristics of infrared hood materials with different thicknesses in a high-temperature state is urgently needed, and a high-temperature infrared hood transmission characteristic quantification model is established more efficiently.
Disclosure of Invention
The invention aims to solve the problem of cross-precision of the reconstruction result caused by the fact that the existing numerical simulation method is greatly influenced by the thickness of a material to be measured and measurement errors.
A high-efficiency measurement system for heat radiation characteristics of materials with different thicknesses of a high-temperature infrared hood comprises a Fourier transform infrared spectrometer, a heating furnace, a black body furnace, a temperature control patrol instrument and a data acquisition and processing system;
during measurement, the center of a detection lens of the Fourier infrared spectrometer, the center of the heating furnace and the center of the black body furnace cavity are arranged on the same horizontal line;
a blackbody furnace for emitting blackbody infrared radiation; in the measuring process, adjusting the blackbody furnace to change the temperature of the blackbody so as to emit infrared radiation at different blackbody temperatures;
the heating furnace is used for heating the infrared hood sample; in the measuring process, the temperature of the heating furnace is adjusted to provide different temperatures for the infrared hood sample material;
the temperature control polling instrument is used for detecting and controlling the temperature in the heating furnace;
the Fourier infrared spectrometer is used for acquiring black body infrared radiation penetrating through the infrared hood;
and the data acquisition and processing system is used for acquiring data of the Fourier infrared spectrometer and the temperature control patrol instrument, and calculating the normal phase spectrum apparent radiation intensity of the material at the temperature displayed by the temperature control patrol instrument by using the signals obtained by the Fourier infrared spectrometer.
A high-efficiency measurement method for the thermal radiation characteristics of materials with different thicknesses of a high-temperature infrared hood comprises the following steps:
firstly, building a high-efficiency measuring system for the heat radiation characteristics of materials with different thicknesses of a high-temperature infrared hood according to claim 1;
step two, initial stage, without starting the heating furnace, the heating furnaceStarting the black body furnace without placing a sample therein, and setting the temperature of the black body furnace to be TbObtaining the infrared radiation L of the black body by using a Fourier infrared spectrometerobj
Thirdly, placing the infrared hood sample in a high-temperature heating furnace for heating until the temperature of the infrared hood sample material reaches the specified temperature TwinAfter the infrared radiation L is uniformly distributed, the infrared radiation L penetrating through the infrared hood sample material is obtained by an infrared detectortot
Step four, controlling the temperature of the sample material to keep the temperature of the sample material at TwinChanging the black body temperature T without changebIn the state, repeating the second step and the third step to obtain a plurality of groups of blackbody temperatures Tb,iInfrared radiation L in the stateobj,iAnd Ltot,i(ii) a Wherein the subscript i represents the ith measurement;
step five, when the temperature of the material is not changed, the radiation characteristic parameter is a fixed value, and through statistics of the test result, a least square method is utilized to fit a plurality of groups of blackbody temperatures Tb,iInfrared radiation L in the stateobj,iAnd Ltot,iAnd then the temperature T is obtainedwinTransmittance tau of uniformly distributed infrared hood sample materialT,winAnd self-radiation LT,win
Step six, equally dividing the infrared hood sample into n layers along the thickness direction, and obtaining the apparent spectral transmittance of the infrared hood sample material with unit thickness delta according to the energy conservation relation
Figure BDA0003572945700000021
Self-radiation
Figure BDA0003572945700000022
And based on
Figure BDA0003572945700000023
Obtaining apparent normal spectral emissivity
Figure BDA0003572945700000024
Step seven, solving algorithm according to radiation transmission inverse problem, assuming infrared headThe refractive index of the mask sample material is
Figure BDA0003572945700000025
Absorption coefficient of
Figure BDA0003572945700000026
Calculating to obtain the apparent spectral radiation intensity of any angle on the emergent interface of the infrared hood sample material by solving a radiation transmission equation
Figure BDA0003572945700000031
Apparent normal spectral emissivity estimation
Figure BDA0003572945700000032
And an apparent spectral transmittance estimate
Figure BDA0003572945700000033
Step eight, the apparent normal spectral emissivity of the infrared hood sample material obtained in the step six
Figure BDA0003572945700000034
And apparent spectral transmittance
Figure BDA0003572945700000035
And seventhly, obtaining the estimated value of the apparent normal emissivity of the infrared hood sample material
Figure BDA0003572945700000036
And an apparent spectral transmittance estimate
Figure BDA0003572945700000037
Substituting the obtained target function value into the following target function calculation formula to obtain a target function value Fobj
Figure BDA0003572945700000038
Step nine, judging the objective function value F in the step eightobjWhether or not it is smaller than a set threshold value xi,
if yes, the refractive index of the infrared hood sample material assumed in the step eight
Figure BDA0003572945700000039
Coefficient of absorption
Figure BDA00035729457000000310
The real refractive index and the absorption coefficient of the infrared hood sample material are obtained;
if not, returning to the seventh step, and updating the refractive index of the infrared hood sample material according to the inverse problem algorithm
Figure BDA00035729457000000311
Coefficient of absorption
Figure BDA00035729457000000312
Resetting the refractive index and absorption coefficient of the infrared hood sample material and recalculating until the objective function value F in the step eightobjIs less than a set threshold xi to obtain the real refractive index of the infrared hood sample material
Figure BDA00035729457000000313
Coefficient of absorption
Figure BDA00035729457000000314
In combination with step six, a temperature T is now obtainedwinSelf-irradiation of the sample material
Figure BDA00035729457000000315
Refractive index
Figure BDA00035729457000000316
Coefficient of absorption
Figure BDA00035729457000000317
Step ten, changing the temperature T of the sample materialwinRepeating the second step toStep nine, to obtain different temperatures Twin,jRefractive index of infrared hood sample Material
Figure BDA00035729457000000318
Coefficient of absorption
Figure BDA00035729457000000319
With self-radiation
Figure BDA00035729457000000320
Wherein the subscript j represents the jth set of measurements;
calculating to obtain self-radiation of infrared hood sample material with unit thickness delta in different directions
Figure BDA00035729457000000321
By different temperatures Twin,jRefractive index of sample material
Figure BDA00035729457000000322
Coefficient of absorption
Figure BDA00035729457000000323
And self-radiation
Figure BDA00035729457000000324
Establishing a radiation physical property database of infrared hood materials with different temperature unit thicknesses delta;
step eleven, uniformly dividing the infrared hood to be detected into m thin layers with the thickness of delta by using a physical dispersion idea; measuring by using a thermal infrared imager, and recording the temperature of each infrared hood thin layer as T under the working condition to be measuredwin,kWherein the subscript k ═ 1,2, …, m, denotes the kth thin layer; establishing a temperature field of the infrared hood according to the measurement result, and inquiring a radiation physical property database of the infrared hood materials with different temperature unit thicknesses delta established in the step ten to obtain the refractive index, the absorption coefficient, the self radiation distribution field and the radiation distribution fields in different directions of each infrared hood thin layer; thereby obtaining the refractive indexes of different positions in the infrared hoodAnd the absorption coefficient is obtained by superposing along the thickness direction, and the directional radiation intensity and the directional emissivity of the infrared hood to be detected are obtained.
Has the advantages that:
the traditional calculation method is used for dispersing the infrared optical window to be measured on a model level, but the traditional calculation method is influenced by the thickness of the material to be measured and measurement errors. Therefore, the invention develops a new method, the material is dispersed on the physical level, the material to be measured is divided into a plurality of thin layers with smaller thickness, the transmittance and the self radiation of the thin layers are measured, and a radiation transmission inverse problem calculation method is introduced to perform inversion reconstruction on the radiation characteristics of the material, such as the absorption coefficient and the refractive index. At the moment, the thickness of the model for inversion reconstruction is small, so that the reconstruction result can be ensured to have high precision.
Meanwhile, the invention also provides a method for measuring the transmittance and self-radiation and other thermal radiation characteristics of the infrared hood with different material thicknesses without repeated experiments according to a target characteristic transmission mechanism of the infrared hood, namely, when an infrared hood transmission characteristic quantification model is established in the previous period, the transmittance and self-radiation and other thermal radiation characteristics of the infrared hood with different material thicknesses can be obtained without repeated experiments after a radiometric property database of the infrared hood material with unit thickness is established on the basis of the refractive index, the absorption coefficient and the self-radiation of the sample material with different temperatures. Therefore, key data support is provided for evaluating the influence of the missile-borne condition on the infrared detection image and information processing, a more vivid infrared detection simulation image is formed, and the design and optimization of the hypersonic flight infrared detection system are promoted.
Drawings
FIG. 1 is a schematic view of a high-efficiency measurement system for thermal radiation characteristics of materials with different thicknesses of a high-temperature infrared hood.
Detailed Description
The operation of the present invention will be described in further detail with reference to the accompanying drawings.
The first embodiment is as follows: the present embodiment is described in connection with figure 1,
the embodiment is a high-efficiency measurement system for the heat radiation characteristics of materials with different thicknesses of a high-temperature infrared hood, which comprises a Fourier transform infrared spectrometer 1, a heating furnace 2, a black body furnace 3, a temperature control patrol instrument 4 and a data acquisition and processing system 5;
when the device works, the center of a detection lens of the Fourier infrared spectrometer, the center of a heating furnace and the center of a black body furnace cavity are arranged on the same horizontal line;
a blackbody furnace for emitting blackbody infrared radiation; during the measurement work process, the blackbody furnace is adjusted to change the temperature of the blackbody so as to emit infrared radiation at different blackbody temperatures.
The heating furnace is used for heating the infrared hood sample; in the measuring process, the temperature of the heating furnace is adjusted to provide different temperatures for the infrared hood sample material;
the temperature control polling instrument is used for detecting and controlling the temperature in the heating furnace;
the Fourier infrared spectrometer is used for acquiring black body infrared radiation penetrating through the infrared hood;
and the data acquisition and processing system is used for acquiring data of the Fourier infrared spectrometer and the temperature control patrol instrument, and calculating the normal phase spectrum apparent radiation intensity of the material at the temperature displayed by the temperature control patrol instrument by using the signals obtained by the Fourier infrared spectrometer.
In the present embodiment, it is preferred that,
the Fourier transform infrared spectrometer is an FTIR-6100 Fourier transform infrared spectrometer, and the main indexes are as follows: (1) the highest spectral resolution is 0.022 nm; (2) the scanning spectrum range is 1.25-25; (3) the scanning frequency is 20 Hz; (4) the signal to noise ratio is 50000/1.
The heating furnace is an SGM.M6/14AE type heating furnace which is a double-door heating furnace, and the depth, width and height (mm) of a hearth are 230 multiplied by 180 multiplied by 150. Heating power: 4KW, the heating element is a silicon-molybdenum rod. Maximum temperature: 1700 ℃, the temperature stability is +/-1 ℃, the temperature uniformity is +/-6 ℃, and 45-50 minutes are required for heating from room temperature to 1400 ℃.
The black body furnace is an RT1500 type black body furnace, and the main index parameters are as follows: the maximum temperature is 1450 ℃, the effective emissivity is 0.99, the radiation aperture phi is 50, and the temperature range is as follows: the temperature is arbitrarily set within the range of 0-1450 ℃, the temperature control precision is +/-0.5 ℃, the stability is 1 ℃/3min, and the temperature rise time is as follows: room temperature to 1450 deg.c for not more than 1 hr.
The second embodiment is as follows:
the embodiment is a high-efficiency measuring method for the heat radiation characteristics of materials with different thicknesses of a high-temperature infrared hood, which comprises the following steps:
step one, building a high-efficiency measuring system for the heat radiation characteristics of materials with different thicknesses of the high-temperature infrared hood.
Step two, in the initial stage, the heating furnace is not started, the sample is not placed in the heating furnace, the black body furnace is started, and the temperature of the black body furnace is set to be TbObtaining the infrared radiation L of the black body by using a Fourier infrared spectrometerobj
Thirdly, placing the infrared hood sample in a high-temperature heating furnace for heating until the temperature of the infrared hood sample material reaches the specified temperature TwinAfter the infrared radiation L is uniformly distributed, the infrared radiation L penetrating through the infrared hood sample material is obtained by an infrared detectortot
Infrared hood materials, namely infrared optical window materials;
step four, controlling the temperature of the sample material to keep the temperature of the sample material at TwinChanging the black body temperature T without changebIn the state, repeating the second step and the third step to obtain a plurality of groups of blackbody temperatures Tb,iInfrared radiation L in stateobj,iAnd Ltot,i(ii) a Where the index i indicates the ith measurement.
Step five, when the temperature of the material is not changed, the radiation characteristic parameter is a fixed value, so that a plurality of groups of blackbody temperatures T can be fitted by utilizing a least square method through statistics of test resultsb,iInfrared radiation L in the stateobj,iAnd Ltot,iAnd then the temperature T is obtainedwinTransmittance tau of uniformly distributed infrared hood sample materialT,winAnd self-radiation LT,win
Step six, equally dividing the infrared hood sample into n layers along the thickness direction, and obtaining the apparent spectral transmittance of the infrared hood sample material with unit thickness delta according to the energy conservation relation
Figure BDA0003572945700000051
Self-radiation
Figure BDA0003572945700000052
And based on
Figure BDA0003572945700000053
Obtaining apparent normal spectral emissivity
Figure BDA0003572945700000061
The apparent normal spectral emissivity can be calculated by the following formula
Figure BDA0003572945700000062
In the formula, LT,bIndicating that the temperature is the same as the temperature of the sample material per unit thickness, i.e. the temperature is TwinThe black body radiation intensity of (a).
Step seven, solving an algorithm according to the radiation transmission inverse problem, and assuming that the refractive index of the infrared hood sample material is
Figure BDA0003572945700000063
Absorption coefficient of
Figure BDA0003572945700000064
Calculating to obtain the apparent spectral radiation intensity of any angle on the emergent interface of the infrared hood sample material by solving a radiation transmission equation
Figure BDA0003572945700000065
Apparent normal spectral emissivity estimation
Figure BDA0003572945700000066
And an apparent spectral transmittance estimate
Figure BDA0003572945700000067
Step eight, red obtained in the step sixApparent normal spectral emissivity of outer hood sample material
Figure BDA0003572945700000068
And apparent spectral transmittance
Figure BDA0003572945700000069
And seventhly, obtaining the estimated value of the apparent normal emissivity of the infrared hood sample material
Figure BDA00035729457000000610
And an apparent spectral transmittance estimate
Figure BDA00035729457000000611
Substituting the obtained target function value into the following target function calculation formula to obtain a target function value Fobj
Figure BDA00035729457000000612
Step nine, judging the objective function value F in the step eightobjWhether or not it is smaller than a set threshold value xi,
if yes, the refractive index of the infrared hood sample material assumed in the step eight
Figure BDA00035729457000000613
Coefficient of absorption
Figure BDA00035729457000000614
The real refractive index and the absorption coefficient of the infrared hood sample material are obtained;
if not, returning to the seventh step, and updating the refractive index of the infrared hood sample material according to the inverse problem algorithm
Figure BDA00035729457000000615
Coefficient of absorption
Figure BDA00035729457000000616
Resetting refractive index and absorption coefficient of infrared hood sample materialThe value is recalculated until the value of the objective function F in step eightobjIs less than a set threshold xi to obtain the real refractive index of the infrared hood sample material
Figure BDA00035729457000000617
Coefficient of absorption
Figure BDA00035729457000000618
In combination with step six, a temperature T is now obtainedwinSelf-irradiation of the sample material
Figure BDA00035729457000000619
Refractive index
Figure BDA00035729457000000620
Coefficient of absorption
Figure BDA00035729457000000621
Step ten, changing the temperature T of the sample materialwinRepeating the second to the ninth steps to obtain different temperatures Twin,jRefractive index of infrared hood sample Material
Figure BDA00035729457000000622
Coefficient of absorption
Figure BDA00035729457000000623
And self-radiation
Figure BDA00035729457000000624
Where the index j indicates the jth set of measurements.
The self-radiation of the infrared hood sample material with unit thickness delta in different directions can be obtained by calculation
Figure BDA00035729457000000625
(the intensities of radiation in different directions introduced here are calculated from the refractive index and absorption coefficient and are not measured). By different temperatures Twin,jFold of sample Material underRefractive index
Figure BDA0003572945700000071
Coefficient of absorption
Figure BDA0003572945700000072
And self-radiation
Figure BDA0003572945700000073
And establishing a radiation physical property database of infrared hood materials with different temperature unit thicknesses delta.
And step eleven, uniformly dividing the infrared hood to be measured into m thin layers with the thickness delta by using a physical discrete idea. Measuring by using a thermal infrared imager, and recording the temperature of each infrared hood thin layer as T under the working condition to be measuredwin,kWhere the subscript k ═ 1,2, …, m, denotes the kth layer. And (4) establishing a temperature field of the infrared hood according to the measurement result, and inquiring a radiation physical property database of the infrared hood materials with different temperature unit thicknesses delta established in the step ten to obtain the refractive index, the absorption coefficient, the self radiation distribution field and the radiation distribution fields in different directions of each infrared hood thin layer. And then can obtain the refractive index and the absorption coefficient of different positions department in the infrared hood, can acquire the direction radiation intensity and the direction emissivity of infrared hood that awaits measuring through stacking along thickness direction.
The third concrete implementation mode:
the embodiment is a high-efficiency measurement method for the thermal radiation characteristics of materials with different thicknesses of a high-temperature infrared hood, and the apparent spectral transmittance of an infrared hood sample material with unit thickness delta is obtained in the sixth step
Figure BDA0003572945700000074
Self-radiation
Figure BDA0003572945700000075
Comprises the following steps:
infrared radiation L of infrared hood material measured by infrared detection system (system in Fourier transform infrared spectrometer)totIs the radiance L of the inner surface of the materialλ(s) fromTarget infrared radiation L reaching outer surface of infrared hood sampleobjAnd infrared head cover self-radiation LwinProduced by a combined action, i.e.
Ltot=Lobjτwin+Lwin (3)
In the formula, τwinIs the transmittance of an infrared optical window.
Describing the transmission process of target radiation energy transmitting through an infrared hood test piece by using a radiation transmission equation, equally dividing an infrared hood material into n layers along the radiation transmission direction, and deducing a fixed algebraic relation between the transmittance and self-radiation of the infrared hood material with unit thickness and the transmittance and self-radiation of the whole infrared hood; according to the obtained algebraic relation, the heat radiation characteristic data such as transmittance, attenuation coefficient and the like of the infrared hood materials with different thicknesses under the working conditions such as the same temperature and the like can be directly calculated.
In order to realize the purpose, the invention adopts the technical scheme that: the infrared hood sample was equally divided into n layers in the thickness direction, assuming uniform temperature T distribution of the infrared optical window and apparent spectral transmittance of each layer
Figure BDA0003572945700000076
And self-radiation
Figure BDA0003572945700000077
Isotropy, the total radiation transmitted through the 1 st layer of the infrared hood material can be obtained according to the radiation transmission principle and the energy conservation relation
Figure BDA0003572945700000078
The infrared radiation transmitted through the 1 st to 2 nd layers is
Figure BDA0003572945700000081
Similarly, the total radiation transmitted through the 1 st to n th layers, i.e., the total radiation transmitted through the entire infrared hood, is
Figure BDA0003572945700000082
Furthermore, the apparent spectral transmittance of the infrared hood material having a thickness of Δ and a temperature of T can be estimated by the energy method
Figure BDA0003572945700000083
And self-radiation
Figure BDA0003572945700000084
Transmittance tau of whole infrared detection infrared hoodT,winAnd self-radiation LT,winAn algebraic relation satisfied between them is
Figure BDA0003572945700000085
Figure BDA0003572945700000086
By measuring the transmittance and the infrared radiation characteristic of the infrared hood with the thickness of x, the data of the apparent spectral transmittance, the self radiation and other thermal radiation characteristics of the infrared optical window material with the unit thickness delta are obtained.
Therefore, the thermal radiation characteristic data of the infrared optical window materials with different thicknesses under the same temperature and other environment working conditions can be directly calculated according to the obtained algebraic relation without repeated experiments for many times, and a transmission characteristic quantification model of the infrared hood is established.
The fourth concrete implementation mode:
the embodiment is a high-efficiency measurement method for the thermal radiation characteristics of materials with different thicknesses of a high-temperature infrared hood, and in the seventh step, the apparent spectral radiation intensity of any angle on the emergent interface of the sample material of the infrared hood is calculated and obtained by solving a radiation transmission equation
Figure BDA0003572945700000087
Apparent normal spectral emissivity estimation
Figure BDA0003572945700000088
And an apparent spectral transmittance estimate
Figure BDA0003572945700000089
Comprises the following steps:
assuming an isotropic medium temperature of
Figure BDA00035729457000000810
Refractive index of
Figure BDA00035729457000000811
Absorption coefficient of
Figure BDA00035729457000000812
A reflectivity of
Figure BDA00035729457000000813
The thickness of the medium is delta; under one-dimensional conditions, when the medium is in steady state conditions and medium scattering is not considered, the radiation transfer equation can be reduced to:
Figure BDA00035729457000000814
solving the radiation transfer equation yields:
Figure BDA00035729457000000815
Figure BDA0003572945700000091
wherein,
Figure BDA0003572945700000092
which means the radiation in the forward direction,
Figure BDA0003572945700000093
representing backward radiation; theta is an included angle between the forward radiation and the normal line of the surface and an included angle between the backward radiation and the normal line of the surface;
at the inner boundary x-0, the intensity of the radiation propagating in the positive direction includes a portion that reflects the intensity of the radiation incident on the interface, and therefore:
Figure BDA0003572945700000094
similarly, at the inner boundary x ═ L, the intensity of the radiation propagating in the negative direction also includes the portion that reflects the intensity of the radiation incident on the interface, i.e.:
Figure BDA0003572945700000095
combining the radiation transfer equation in the medium along the positive direction and the negative direction, and two boundary conditions, the method can be simplified to obtain:
Figure BDA0003572945700000096
wherein,
Figure BDA0003572945700000097
and then the apparent spectral radiation intensity of any angle on the emergent interface is as follows:
Figure BDA0003572945700000098
the apparent normal spectral emissivity is:
Figure BDA0003572945700000099
in the formula, LT,bIs the black body radiation intensity corresponding to a temperature T and a wavelength λ;
apparent spectral transmittance
Figure BDA00035729457000000910
From bell's law:
Figure BDA00035729457000000911
due to the temperature of the isotropic medium
Figure BDA0003572945700000101
Refractive index
Figure BDA0003572945700000102
Coefficient of absorption
Figure BDA0003572945700000103
A reflectivity of
Figure BDA0003572945700000104
Is an assumed value and thus corresponds to the resulting apparent normal spectral emissivity
Figure BDA0003572945700000105
Apparent spectral transmittance
Figure BDA0003572945700000106
Namely the estimated value of the apparent spectral emissivity
Figure BDA0003572945700000107
Apparent spectral transmittance estimate
Figure BDA0003572945700000108
According to the infrared hood transmission quantitative model establishing method, the corresponding radiation characteristic of the infrared hood material with unit thickness is calculated by measuring the heat radiation transmission characteristic of the infrared hood material with one thickness, and then the heat radiation characteristic data such as the transmittance of the infrared hood material with different thicknesses under the same temperature working condition is calculated, so that the establishment of the infrared hood transmission quantitative model is realized.
The present invention is capable of other embodiments and its several details are capable of modifications in various obvious respects, all without departing from the spirit and scope of the present invention.

Claims (10)

1. A high-efficiency measurement system for heat radiation characteristics of materials with different thicknesses of a high-temperature infrared hood is characterized by comprising a Fourier transform infrared spectrometer, a heating furnace, a black body furnace, a temperature control polling instrument and a data acquisition and processing system;
during measurement, the center of a detection lens of the Fourier infrared spectrometer, the center of the heating furnace and the center of the black body furnace cavity are arranged on the same horizontal line;
a blackbody furnace for emitting blackbody infrared radiation; in the measuring process, adjusting the blackbody furnace to change the temperature of the blackbody so as to emit infrared radiation at different blackbody temperatures;
the heating furnace is used for heating the infrared hood sample; in the measuring process, the temperature of the heating furnace is adjusted to provide different temperatures for the infrared hood sample material;
the temperature control polling instrument is used for detecting and controlling the temperature in the heating furnace;
the Fourier infrared spectrometer is used for acquiring black body infrared radiation penetrating through the infrared hood;
and the data acquisition and processing system is used for acquiring data of the Fourier infrared spectrometer and the temperature control patrol instrument, and calculating the normal phase spectrum apparent radiation intensity of the material at the temperature displayed by the temperature control patrol instrument by using the signals obtained by the Fourier infrared spectrometer.
2. A high-efficiency measurement method for thermal radiation characteristics of materials with different thicknesses of a high-temperature infrared hood is characterized by comprising the following steps:
firstly, building a high-efficiency measuring system for the heat radiation characteristics of materials with different thicknesses of the high-temperature infrared hood according to claim 1;
step two, in the initial stage, the heating furnace is not started, the sample is not placed in the heating furnace, the black body furnace is started, and the temperature of the black body furnace is set to be TbObtaining the infrared radiation L of the black body by using a Fourier infrared spectrometerobj
Thirdly, placing the infrared hood sample in a high-temperature heating furnace for heating until the temperature of the infrared hood sample material reaches the specified temperature TwinAfter the infrared radiation L is uniformly distributed, the infrared radiation L penetrating through the infrared hood sample material is obtained by an infrared detectortot
Step four, controlling the temperature of the sample material to keep the temperature of the sample material at TwinChanging the black body temperature T without changebIn the state, repeating the second step and the third step to obtain a plurality of groups of blackbody temperatures Tb,iInfrared radiation L in the stateobj,iAnd Ltot,i(ii) a Wherein subscript i represents the ith measurement;
step five, when the temperature of the material is not changed, the radiation characteristic parameter is a fixed value, and through statistics of the test result, a least square method is utilized to fit a plurality of groups of blackbody temperatures Tb,iInfrared radiation L in the stateobj,iAnd Ltot,iAnd then the temperature T is obtainedwinTransmittance tau of uniformly distributed infrared hood sample materialT,winAnd self-radiation LT,win
Step six, equally dividing the infrared hood sample into n layers along the thickness direction, and obtaining the apparent spectral transmittance of the infrared hood sample material with unit thickness delta according to the energy conservation relation
Figure FDA0003572945690000011
Self-radiation
Figure FDA0003572945690000012
And based on
Figure FDA0003572945690000013
Obtaining apparent normal spectral emissivity
Figure FDA0003572945690000014
Step seven, solving an algorithm according to the radiation transmission inverse problem, and assuming that the refractive index of the infrared hood sample material is
Figure FDA0003572945690000015
Absorption coefficient of
Figure FDA0003572945690000021
Calculating to obtain the apparent spectral radiation intensity of any angle on the emergent interface of the infrared hood sample material by solving a radiation transmission equation
Figure FDA0003572945690000022
Apparent normal spectral emissivity estimation
Figure FDA0003572945690000023
And an apparent spectral transmittance estimate
Figure FDA0003572945690000024
Step eight, obtaining the apparent normal spectral emissivity of the infrared hood sample material obtained in the step six
Figure FDA0003572945690000025
And apparent spectral transmittance
Figure FDA0003572945690000026
And seventhly, obtaining the estimated value of the apparent normal emissivity of the infrared hood sample material
Figure FDA0003572945690000027
And an apparent spectral transmittance estimate
Figure FDA0003572945690000028
Substituting into the following objective function calculation formula to obtain the objectiveValue of standard function Fobj
Figure FDA0003572945690000029
Step nine, judging the objective function value F in the step eightobjWhether or not it is smaller than a set threshold value xi,
if yes, the refractive index of the infrared hood sample material assumed in the step eight
Figure FDA00035729456900000210
Coefficient of absorption
Figure FDA00035729456900000211
The real refractive index and the absorption coefficient of the infrared hood sample material are obtained;
if not, returning to the seventh step, and updating the refractive index of the infrared hood sample material according to the inverse problem algorithm
Figure FDA00035729456900000212
Coefficient of absorption
Figure FDA00035729456900000213
Resetting the refractive index and absorption coefficient of the infrared hood sample material and recalculating until the objective function value F in the step eightobjIs less than a set threshold xi to obtain the real refractive index of the infrared hood sample material
Figure FDA00035729456900000214
Coefficient of absorption
Figure FDA00035729456900000215
In combination with step six, a temperature T is now obtainedwinSelf-irradiation of sample material
Figure FDA00035729456900000216
Refractive index
Figure FDA00035729456900000217
Coefficient of absorption
Figure FDA00035729456900000218
Step ten, changing the temperature T of the sample materialwinRepeating the second to the ninth steps to obtain different temperatures Twin,jRefractive index of infrared hood sample Material
Figure FDA00035729456900000219
Coefficient of absorption
Figure FDA00035729456900000220
And self-radiation
Figure FDA00035729456900000221
Wherein the subscript j represents the jth set of measurements;
calculating to obtain self-radiation of infrared hood sample material with unit thickness delta in different directions
Figure FDA00035729456900000222
By different temperatures Twin,jRefractive index of sample material
Figure FDA00035729456900000223
Coefficient of absorption
Figure FDA00035729456900000224
And self-radiation
Figure FDA00035729456900000225
Establishing a radiation physical property database of infrared hood materials with different temperature unit thicknesses delta;
eleven, utilizing the idea of physical dispersion to shield the infrared head to be detectedUniformly dividing the mixture into m thin layers with the thickness delta; measuring by using a thermal infrared imager, and recording the temperature of each infrared hood thin layer as T under the working condition to be measuredwin,kWherein the subscript k ═ 1,2, …, m, denotes the kth thin layer; establishing a temperature field of the infrared hood according to the measurement result, and inquiring a radiation physical property database of the infrared hood materials with different temperature unit thicknesses delta established in the step ten to obtain the refractive index, the absorption coefficient, the self radiation distribution field and the radiation distribution fields in different directions of each infrared hood thin layer; and further obtaining the refractive index and the absorption coefficient of different positions in the infrared hood, and obtaining the directional radiation intensity and the directional emissivity of the infrared hood to be detected through superposition along the thickness direction.
3. The method of claim 2, wherein six steps are used to obtain the apparent spectral transmittance of the sample material of infrared hood at unit thickness Δ
Figure FDA0003572945690000031
Self-radiation
Figure FDA0003572945690000032
Comprises the following steps:
describing the transmission process of target radiation energy through an infrared hood test piece by using a radiation transmission equation, equally dividing an infrared hood material into n layers along the energy conservation in the radiation transmission direction, and assuming that the temperature T of an infrared optical window is uniformly distributed and the apparent spectral transmittance of each layer is uniform
Figure FDA0003572945690000033
And self-radiation
Figure FDA0003572945690000034
Isotropy, the total radiation transmitted through the 1 st layer of the infrared hood material is obtained according to the radiation transmission principle and the energy conservation relation
Figure FDA0003572945690000035
The infrared radiation transmitted through the 1 st to 2 nd layers is
Figure FDA0003572945690000036
Similarly, the total radiation transmitted through the 1 st to n th layers, i.e., the total radiation transmitted through the entire infrared hood, is
Figure FDA0003572945690000037
Further, the apparent spectral transmittance of the infrared hood material having a thickness of Δ and a temperature of T was estimated by the energy method
Figure FDA0003572945690000038
Transmittance tau of infrared detection infrared hoodT,winAlgebraic relationship of (c), and apparent spectral transmittance
Figure FDA0003572945690000039
Transmittance tau of infrared detection infrared hoodT,winAlgebraic relations with self radiation;
measuring the transmittance and the infrared radiation characteristic of an infrared hood with the thickness of x to further obtain the apparent spectral transmittance and the self-radiation thermal radiation characteristic data of the infrared optical window material with the unit thickness delta; infrared optical window material is infrared hood material.
4. The method of claim 3, wherein the apparent spectral transmittance of said material of said infrared hood is measured by measuring the thermal radiation characteristics of said material of different thickness
Figure FDA00035729456900000310
Infrared hood for infrared detectionTransmittance of (d) isT,winHas an algebraic relationship of
Figure FDA00035729456900000311
5. The method of claim 4, wherein the apparent spectral transmittance is measured by measuring the thermal radiation characteristic of a material of different thickness in a high temperature infrared hood
Figure FDA00035729456900000312
Transmittance tau of infrared detection infrared hoodT,winThe algebraic relation between the radiation and the self-radiation is
Figure FDA0003572945690000041
6. A method for efficiently measuring the thermal radiation characteristics of materials with different thicknesses for high temperature infrared hoods according to claim 3, 4 or 5, characterized in that the apparent normal spectral emissivity obtained in step six
Figure FDA0003572945690000042
The following were used:
Figure FDA0003572945690000043
in the formula, LT,bMeans that the temperature is the same as the temperature of the sample material per unit thickness, i.e. the temperature is TwinThe black body radiation intensity of (a).
7. The method for efficiently measuring the thermal radiation characteristics of materials with different thicknesses for a high-temperature infrared hood as claimed in claim 6, wherein the apparent spectral radiation intensity of any angle on the exit interface of the sample material of the infrared hood is calculated by solving the radiation transfer equation in step seven
Figure FDA0003572945690000044
Apparent normal spectral emissivity estimation
Figure FDA0003572945690000045
Comprises the following steps:
assuming an isotropic medium temperature of
Figure FDA0003572945690000046
Refractive index of
Figure FDA0003572945690000047
Absorption coefficient of
Figure FDA0003572945690000048
A reflectivity of
Figure FDA0003572945690000049
The thickness of the medium is delta; under one-dimensional conditions, when the medium is in steady state conditions and medium scattering is not considered, the radiation transfer equation reduces to:
Figure FDA00035729456900000410
solving the simplified radiation transfer equation to obtain the forward radiation
Figure FDA00035729456900000411
And backward radiation
Figure FDA00035729456900000412
Theta is an included angle between the forward radiation and the surface normal line and between the backward radiation and the surface normal line;
at the inner boundary x-0, the intensity of the radiation propagating in the positive direction includes a portion that reflects the intensity of the radiation incident on the interface, and therefore:
Figure FDA00035729456900000413
similarly, at the inner boundary x ═ L, the intensity of the radiation propagating in the negative direction also includes the portion that reflects the intensity of the radiation incident on the interface, i.e.:
Figure FDA00035729456900000414
combining the radiation transfer equation along the positive direction and the negative direction in the medium and two boundary conditions, and simplifying to obtain:
Figure FDA00035729456900000415
wherein,
Figure FDA0003572945690000051
and then the apparent spectral radiation intensity of any angle on the emergent interface is as follows:
Figure FDA0003572945690000052
the apparent normal spectral emissivity is:
Figure FDA0003572945690000053
in the formula, LT,bIs the black body radiation intensity corresponding to a temperature T and a wavelength λ;
due to the temperature of the isotropic medium
Figure FDA0003572945690000054
Refractive index
Figure FDA0003572945690000055
Coefficient of absorption
Figure FDA0003572945690000056
A reflectivity of
Figure FDA0003572945690000057
Is an assumed value and thus corresponds to the resulting apparent normal spectral emissivity
Figure FDA0003572945690000058
Namely the estimated value of the apparent spectral emissivity
Figure FDA0003572945690000059
8. The method of claim 7, wherein the forward radiation obtained by solving the simplified radiation transfer equation is used as a measure of the thermal radiation characteristics of materials of different thicknesses in high temperature infrared hoods
Figure FDA00035729456900000510
And backward radiation
Figure FDA00035729456900000511
The following:
Figure FDA00035729456900000512
Figure FDA00035729456900000513
9. the method of claim 7, wherein the apparent spectral transmittance estimate of step seven is used to determine the thermal radiation characteristics of materials of different thickness for high temperature infrared hoods
Figure FDA00035729456900000514
Calculated by bell's law.
10. The method of claim 9, wherein the estimate of apparent spectral transmittance obtained in step seven is used to determine the thermal radiation characteristics of materials of different thickness for high temperature infrared hoods
Figure FDA00035729456900000515
The specific process comprises the following steps:
apparent spectral transmittance
Figure FDA00035729456900000516
From bell's law:
Figure FDA00035729456900000517
due to the temperature of the isotropic medium
Figure FDA00035729456900000518
Refractive index
Figure FDA00035729456900000519
Coefficient of absorption
Figure FDA00035729456900000520
A reflectivity of
Figure FDA00035729456900000521
Is assumed to be a value, thereby obtaining an apparent spectral transmittance
Figure FDA0003572945690000061
Namely the estimated value of apparent spectral transmittance
Figure FDA0003572945690000062
CN202210324793.7A 2022-03-30 2022-03-30 High-efficiency measurement system and method for thermal radiation characteristics of materials with different thicknesses of high-temperature infrared hood Pending CN114646663A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202210324793.7A CN114646663A (en) 2022-03-30 2022-03-30 High-efficiency measurement system and method for thermal radiation characteristics of materials with different thicknesses of high-temperature infrared hood

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202210324793.7A CN114646663A (en) 2022-03-30 2022-03-30 High-efficiency measurement system and method for thermal radiation characteristics of materials with different thicknesses of high-temperature infrared hood

Publications (1)

Publication Number Publication Date
CN114646663A true CN114646663A (en) 2022-06-21

Family

ID=81994576

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202210324793.7A Pending CN114646663A (en) 2022-03-30 2022-03-30 High-efficiency measurement system and method for thermal radiation characteristics of materials with different thicknesses of high-temperature infrared hood

Country Status (1)

Country Link
CN (1) CN114646663A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115825145A (en) * 2022-11-18 2023-03-21 哈尔滨工业大学 High-temperature liquid molten salt thermal radiation and heat conduction parameter combined measuring device and inversion method

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115825145A (en) * 2022-11-18 2023-03-21 哈尔滨工业大学 High-temperature liquid molten salt thermal radiation and heat conduction parameter combined measuring device and inversion method
CN115825145B (en) * 2022-11-18 2023-07-11 哈尔滨工业大学 High-temperature liquid molten salt heat radiation and heat conduction parameter combined measurement device and inversion method

Similar Documents

Publication Publication Date Title
CN110095192B (en) Thermal infrared imager comprehensive performance parameter testing system and method thereof
EP2082202B1 (en) Maximum blade surface temperature estimation for advanced stationary gas turbines in near-infrared (with reflection)
CN109655161B (en) Target infrared integral radiation intensity testing method and device based on thermal infrared imager
Ochs et al. A novel calibration method for an infrared thermography system applied to heat transfer experiments
CN108072459A (en) A kind of method for measuring steel billet temperature field and calculating its radiation intensity
KR20020035106A (en) Synthetic reference thermal imaging method
JP2012047739A (en) Thermal imaging method and apparatus for evaluating coating
CN106680224A (en) Measurement device and method for material oxidation ablation in high-temperature wind tunnel
CN111829666B (en) Four-level verification method of target infrared imaging simulation model
CN107957297A (en) A kind of thermal imaging system radiation calibration precision analytical method
CN110567591B (en) Temperature/emissivity inversion method suitable for ground thermal infrared data
KR101862106B1 (en) Calibration method of temperature measurement device using radiation heat image measurement unit camera
CN101907492A (en) Object emission spectrum-based temperature measurement method
CN114646663A (en) High-efficiency measurement system and method for thermal radiation characteristics of materials with different thicknesses of high-temperature infrared hood
Li et al. Effect of nonuniform radiation properties on flame temperature reconstruction based on light field imaging
CN108163223B (en) Portable aircraft infrared stealth performance evaluation device and method
CN115524012A (en) Multispectral radiation temperature measuring device based on thermal infrared imager and measuring method thereof
JP3568271B2 (en) Method and apparatus for measuring thermal constant using laser flash method
CN117109864A (en) Model surface thermal parameter non-contact measurement method applied to Gao Han flow field
CN103256999A (en) Distributed type optical fiber temperature measuring method
CN113008389B (en) Method for measuring temperature of divertor target plate of tokamak device based on single-wave filtering
Scharf et al. Four-band fiber-optic radiometry for determining the “true” temperature of gray bodies
CN100439900C (en) Method for testing material blackness coefficient
CN113063819A (en) System and method for researching radiation characteristic of engine environment thermal resistance coating
Sharma et al. Effect of ambient temperature on calibration of cooled thermal camera

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