Showing posts with label Blackbodies. Show all posts
Showing posts with label Blackbodies. Show all posts

Thursday, June 18, 2020

Human Body Temperature Black Body Source

Isotech Model 988

First introduced to assist in relation to the SARS outbreak during the early 2000s the Model 988 is now helping in relation to coronavirus. It can be used to increase the accuracy of non-contact fever detection systems helping in the fight against COVID-19.

Applications also include checking non-contact clinical thermometers.

This blackbody meets the demand for a simple, cost effective but high accuracy calibrator for the calibration of thermal imagers and infrared thermometers used at temperatures around human body temperature.

A 70 mm diameter ridged plate is heated or cooled with an internal solid state thermoelectric heat pump. The temperature of the plate can be set from 20 °C to 45 °C to a resolution of 0.1 °C.

The standard version has a 210 mm long tube mainly used with thermal imagers. A second version has a 40 mm tube more suited for checking medical thermometers.

More online at: https://www.isotechna.com/Low-Temperature-Calibrator-p/988.htm

Sunday, October 24, 2010

Fluke Calibrator Video

Emissivity makes a temperature difference for infrared thermometers.

In the YouTube video below, Frank Liebman, an engineer with Fluke Corporation's Hart Scientific Division demonstrates the impact that surface emissivity has on temperature measurement and temperature calibration using a modified Fluke blackbody calibrator and Fluke Thermal Imager.



We were surprised to see that no one commented on this video, despite an ending that leaves one hanging, at least us, with the obvious question: How do you do a radiometric calibration of a surface of unknown emissivity using a Fluke Blackbody Calibrator?

Do you have any ideas?

Wednesday, November 4, 2009

Electro Optical Industries BB Emissivity Coatings

Electro Optical Industries (EOI) uses one of two high emissivity coatings on the surface of its blackbodies.

The EOI mid-temperature coating is used on both cavity and flat plate blackbodies that have a maximum operating temperatures of up to 210 °C.



Read the rest by visiting their webpage at: www.electro-optical.com/eoi_page.asp?h=What%20Is%20Emissivity?

Friday, October 30, 2009

Blackbody Emissivity Primer

From the Electro-Optical Industries website:


Typical Material Spectral Emissivity
"Effective emissivity is the ratio of the total amount of energy exiting a blackbody to that which is predicted by Planck’s law. This is the value most frequently referred to as "emissivity".

Effective emissivity of a cavity type blackbody will normally be much higher than the surface emissivity due to the multiple energy bounces inside the body cavity."

You can read the rest on this useful and informative webpage: www.electro-optical.com/html/bb_rad/emissivity/emisivty.asp

Tuesday, May 12, 2009

Measurements of Pool-Fire Temperature Using IR Technique. (419 K)

By Qian, C.; Saito, K.

Ref: Combustion Institute/Central and Western States (USA) and Combustion Institute/Mexican National Section and American Flame Research Committee. Combustion Fundamentals and Applications. Joint Technical Meeting. Proceedings. April 23-26, 1995, San Antonio, TX, Gore, J. P., Editor(s), 81-86 pp, 1995.

Sponsor: National Institute of Standards and Technology, Gaithersburg, MD

Abstract:
We made an attempt to measure the flame temperature of four different diameter hexane-pool-fires using IR technique. Emissivities for these four flames were estimated based on measurements of transmitted energy from a blackbody radiant source. The average flame temperature half way to the flame tip was 700-800 deg C, which was in good agreement with thermocouple-temperature measurements by others for a 3 m diameter hexane pool fire.

Click here to download a pdf version of the report:Measurements of Pool-Fire Temperature Using IR Technique. (419 K)

Building and Fire Research Laboratory
National Institute of Standards and Technology
Gaithersburg, MD 20899 USA

Friday, December 12, 2008

EMISSIVITY EVALUATION OF FIXED POINT BLACKBODIES

A paper by Sergey Mekhontsev, Vladimir Khromchenko, Alexander Prokhorov, Leonard Hanssen
National Institute for Standards and Technology, Gaithersburg, MD, USA

Presented at the 9th International Symposium on Temperature and Thermal Measurements in Industry and Science (TEMPMEKO 2004), June 22-25, 2004, Dubrovnik, Croatia, Proceedings, Vol. 1, ed. by D. Zvizdic (2004), pp. 581-586.
ABSTRACT

A new facility for the characterization of infrared spectral emittance of materials has recently been developed at NIST. The facility operation is based on measurements of a sample’s spectral radiance and surface temperature with help of a set of variable temperature blackbodies and a spectral comparator. For highest accuracy, variable temperature blackbodies are calibrated in spectral radiance against a pair of fixed-point blackbodies with interchangeable crucibles of In, Sn, and Zn, and Al, Ag, and Cu, respectively. The spectral emissivity of the fixed-point blackbodies also needs to be accurately characterized. We employ a multi-prong approach: (1) Monte Carlo ray-trace modeling and calculations, (2) hemispherical reflectance measurements of the crucible cavity material flat sample, as well as the cavity itself, (3) direct spectral emittance measurements of the same samples using the facility, and (4) comparison of the fixed point blackbodies with each other as well as with variable temperature heat pipe blackbodies, using filter radiometers and the facility’s Fourier transform spectrometer. The Monte Carlo code is used to predict the cavity emissivity with input of the cavity shape and the emissivity and specularity of the cavity material. The reflectance measurements provide emissivity data of both the material and the cavity at room temperature. The results are used to compare with and validate the code results. The direct emittance measurements of the material provide the temperature dependence of the material emittance as code input. The code predicted results for the cavities at their operating temperature (freeze points) are then compared with the relative spectral radiance measurements. Use of this complete set of evaluation tools enables us to obtain the spectral emissivity of the blackbodies with reliably determined uncertainties.

It presently can be downloaded in PDF format from the NIST website by CLICKING HERE

Friday, December 5, 2008

IR spectral characterization of customer blackbody sources:

"First calibration results"

A paper by S. Mekhontsev, M. Noorma, A. Prokhorov, and L. Hanssen from NIST in the USA, Presented at Thermosense XXVIII, ed. by Jonathan J. Miles, G. Raymond Peacock, and Kathryn M. Knettel, Proc. of SPIE 6205, 620503 (2006).

ABSTRACT:
We summarize recent progress in our infrared (IR) spectral radiance metrology effort. In support of customer blackbody characterization, a realization of the spectral radiance scale has been undertaken in the temperature range of 232 °C to 962 °C and spectral range of 2.5 µm to 20 µm. We discuss the scale realization process that includes the use of Sn, Zn, Al and Ag fixed-point blackbodies (BB), as well as the transfer of the spectral radiance scale to transfer standard BBs based on water, Cs and Na heat pipes. Further we discuss the procedures for customer source calibration with several examples of the spectral radiance and emissivity measurements of secondary standard BB sources. For one of the BBs, a substantial deviation of emissivity values from the manufacturer specifications was found. Further plans include expansion of the adopted methodology for temperatures down to 15°C and building a dedicated facility for spectral characterization of IR radiation sources.

It presently can be downloaded from the NIST website in PDF format by CLICKING HERE

Saturday, February 23, 2008

The RET Theory

Ircon, Inc., a leading producer of industrial radiation thermometers, line scanners and quantitative thermal imagers, in its training programs for many years used to teach something they called the RAT Theory.

Reflectance, Absorbtance and Transmittance, or the coefficients of them, abbreviated as R, A &T must sum to 100%, or R + A + T=1.

An easy way for newcomers to Infrared radiation thermometry to remember a very important concept.

The associated concept is that Absorbtance=Emittance, or A=E. Or the RAT theory could be written as R+E+T=1 and renamed the RET Theory.

So, while not as easily recalled, the RET Theory name just didn't catch on as easily as the RAT Theory.

(BTW, whenever I tried to teach some basics of Radiation Thermometry, I used to call it the TAR Theory because I thought it might "stick" better- it didn't - RAT wins by a landslide every time.)

All this is a lead in to the wonderful resources by the folks at  LabSphere for those who want to know or learn how to measure emittance or absorbtance through the roundabout way of measuring reflectance and transmittance first and then doing a bit of math.

They have a readily downloadable 26 page PDF document entitled "A Guide to Integrating Sphere Radiometry and Photometry".

It explains far more than the RAT or RET or TAR theories about optical radiation metrology.

I think it and many of their online aids are well worth a read.

Thursday, September 20, 2007

NASA Tech Reports Emittance Abstracts

A Search on the NASA website results in the following abstracts





 

DETERMINATION OF THE EMISSIVITY OF MATERIALS

Author(s): Askwyth, W. H.
Abstract: Space power systems - emissivity of candidate materials for snap-8 powerplant
NASA Center: NASA (non Center Specific)
Publication Year: 1962
Added to NTRS: 2006-11-06
Accession Number: 63N11697; Document ID: 19630001823; Report Number: PWA-2088





Determination of emissivity of materials quarterly progress report, 1 jul. - 30 sep. 1962

Author(s): Askwyth, W. H.; Hayes, R. J.
Abstract: No Abstract Available
NASA Center: NASA (non Center Specific)
Publication Year: 1962
Added to NTRS: 2006-11-06
Accession Number: 67N83465; Document ID: 19670084086; Report Number: NASA-CR-83756, PWA-2128





EMITTANCE OF MATERIALS SUITABLE FOR USE AS SPACECRAFT RADIATOR COATINGS

Author(s): Askwyth, W. H.; Hayes, R. J.; Mikk, G.
Abstract: Emittance measurements of materials suitable for spacecraft radiator coatings
NASA Center: NASA (non Center Specific)
Publication Year: 1963
Added to NTRS: 2006-11-06
Accession Number: 63A24987; Document ID: 19630028928





Measurement of spectral normal emittance of materials under simulated spacecraft powerplant operating conditions

Author(s): Askwyth, W. H.; House, R. D.; Lyons, G. J.
Abstract: Spectral normal emittance of materials under simulated space environment
NASA Center: NASA (non Center Specific)
Publication Year: 1963
Added to NTRS: 2006-11-06
Accession Number: 64N10959; Document ID: 19640001050





THE EMITTANCE OF MATERIALS SUITABLE FOR USE AS SPACECRAFT RADIATOR COATINGS

Author(s): Askwyth, W. H.; Hayes, R. J.; Mikk, G.
Abstract: Emittance of materials suitable for use as spacecraft radiator coatings
NASA Center: NASA (non Center Specific)
Publication Year: 1962
Added to NTRS: 2006-11-06
Accession Number: 63N10264; Document ID: 19630000390; Report Number: ARS PAPER-2538-62





THE EMITTANCE OF MATERIALS SUITABLE FOR USE AS SPACECRAFT RADIATOR COATINGS

Author(s): Askwyth, W. H.; Hayes, R. J.; Mikk, G.
Abstract: Measurements of total hemispherical emittance for materials suitable for high-temperature spacecraft radiation coatings
NASA Center: NASA (non Center Specific)
Publication Year: 1962
Added to NTRS: 2006-11-06
Accession Number: 63A11692; Document ID: 19630015633; Report Number: ARS PAPER 62-2538





A SIMPLE TECHNIQUE FOR DETERMINING TOTAL HEMISPHERICAL EMITTANCE BY COMPARING TEMPERATURE DROPS ALONG COATED FINS

Author(s): Askwyth, W. H.; Curry, R.; Lundberg, W. R.
Abstract: Determination of total hemispherical emittance by comparing temperature drops along coated fins
NASA Center: NASA (non Center Specific)
Publication Year: 1962
Added to NTRS: 2006-11-06
Accession Number: 62N17085; Document ID: 19620007085





Measurement of total hemispherical emittance of structural materials and coatings under simulated spacecraft conditions

Author(s): Askwyth, W. H.; Mikk, G.
Abstract: Hemispherical emittance of structural materials and amp coatings under simulated spacecraft conditions over wide temperature range
NASA Center: NASA (non Center Specific)
Publication Year: 1963
Added to NTRS: 2006-11-06
Accession Number: 64N10962; Document ID: 19640001053





Determination of the emissivity of materials

Author(s): Askwyth, W. H.; Hayes, R. J.; House, R. D.; Mikk, G.
Abstract: No Abstract Available
NASA Center: NASA (non Center Specific)
Publication Year: 1962
Added to NTRS: 2004-11-03
Accession Number: 76N78693; Document ID: 19760073652; Report Number: NASA-CR-148751, PWA-2206(VOL.1)





Determination of the emissivity of materials

Author(s): Askwyth, W. H.
Abstract: No Abstract Available
NASA Center: NASA (non Center Specific)
Publication Year: 1961
Added to NTRS: 2004-11-03
Accession Number: 82N70372; Document ID: 19820065104; Report Number: NASA-CR-164941, PWA-2043

Saturday, September 8, 2007

Beginner's Guide to (Spectral) Emissivity

Introductory Guide to Emissivity


Sketch of the concept of spectral emissivity measurement
This is an introductory page on the National Physical Laboratory (NPL) website in the UK.

It has several such sketches as on the left showing the concept of the "radiometric method" of emissivity measurement and discusses both the concepts and measurement methods used to quantify spectral and total emissivity values.

The page also features links to other resource materials on the subject and a list of reference books.

Wednesday, September 5, 2007

Red, White & Blue Blackbodies?

It is not an oxymoron, nor a quote from Yogi Berra.

Real Blackbodies do not exist, at least on Earth. Only approximations or simulations are real. We use them to calibrate IR Thermometers, Radiation Pyrometers and Thermal Imagers.

Technically they should have a spectral emissivity very close to 1.0. How close, you might ask? Read on.
Max Planck needed the concept of a perfect absorber of electromagnetic, thermal radiation to develop his theory of Thermal Emission of Radiation in 1899. Fortunately, Gustav Kirchhoff had already develped the foundation for them forty years earlier.

A perfect blackbody is perfectly absorbing to all the thermal radiation incident upon it. For that reason it had, necessarily, to be opaque and non-reflecting.

By logical reasoning, it was also clear that the same device had to be a perfect emitter of thermal radiation related to its absolute temperature, that is, temperature on the Absolute or Kelvin Temperature Scale.

There are several radiation equations or "Laws" that have been developed to describe the physics of thermal emission properties. They are well explained in a number of texts and shown in some detail in the online Hyper Physics website.

In an online Java applet, one can see visually also the three main radiation laws in graphic action; the temperature on the screen is shown on a column in a thermometer on the right side, and you can change it by clicking and/or dragging on it with your mouse.

If someone asks about the color of a blackbody, you can always refer them to this great set of webpages by Mitchell Charity at MIT.
They show both the temperature from 1000 K to 29,800 K (of course below about 700 K blackbodies actually look black to the human eye) . As can be seen on this page, red, white and blue blackbodies are possible!

There aren't many 29,800 K blackbodies on Earth, but astronomers & AstroPhysicists see them all the time. How do you think they measure the temperatures of stars?

So, now you know, there can be both Red and Blue Blackbodies!

The devices used by calibration laboratories to calibrate and check the calibration of IR Thermometers, Radiation Thermometers and Infrared Thermal Imagers are not perfect (and seldom Blue, but often appearing Black, Red, Orange, Yellow and even White), but they can be very close to perfect.

The closer to perfection, the higher the cost of them also.

A blackbody having a spectral emissivity of 0.99 would have, at best, an error of about ± 1% in emitted thermal radiation or radiance, at a stable operating temperature and could be used to calibrate Infrared Thermometers.

The thermometers would be limited in their calibration uncertainty, since the radiance they emit would be uncertain to at least ± 1%.

Depending upon the radiance to temperature relationship for the temperature in question, that could mean a bigger or smaller effective temperature calibration uncertainty that could be assigned to a thermometer being calibrated.

That's another issue for another time, but , if you can't wait, one of the best explanations (and a lot more) that we have seen on that subject is in a 547 KB, downloadable PDF file from Land Instruments.

Monday, August 20, 2007

Blackbody Radiation Visual Simulator

A VRML (3-D Virtual Reality Markup Language) demonstration of blackbody intensity distribution versus temperature and wavelength (This used to be on the University of Massachusetts website, but now is loacted on another site that its creator, Karen Strom has posted). It shows the shape of the Plank function for temperatures ranging from 1,000 K to 50,000 K for a range of wavelengths from the x-ray through the radio ranges.

Dark red lines color across the graphical display show the location of temperature isotherms. "Stickpins" on the red side of the distribution give the values of the temperature for 5 of these curves so that you can see the effect of varying the temperature.

This VRML + HTML package on Blackbody emission was constructed by Karen M. Strom who has retired from her scientific work life to pursue other interests. You can see what she is up to and contact her through her website:
www.karenstrom.com/

Increasing the accuracy of your temperature measurements.

Monitor Newsletter at Windmill Software ( https://www.windmill.co.uk/ ) regularly publishes useful articles related to measurement, control,...