US3419709A - Blackbody radiating device with a protective hood - Google Patents
Blackbody radiating device with a protective hood Download PDFInfo
- Publication number
- US3419709A US3419709A US552851A US55285166A US3419709A US 3419709 A US3419709 A US 3419709A US 552851 A US552851 A US 552851A US 55285166 A US55285166 A US 55285166A US 3419709 A US3419709 A US 3419709A
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- US
- United States
- Prior art keywords
- blackbody
- hood
- air
- protective hood
- housing
- 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.)
- Expired - Lifetime
Links
- 230000001681 protective effect Effects 0.000 title description 21
- 239000003570 air Substances 0.000 description 19
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 14
- 239000011261 inert gas Substances 0.000 description 14
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 11
- 229910002804 graphite Inorganic materials 0.000 description 11
- 239000010439 graphite Substances 0.000 description 11
- 230000005457 Black-body radiation Effects 0.000 description 10
- 230000005855 radiation Effects 0.000 description 9
- 229910052786 argon Inorganic materials 0.000 description 7
- 230000003628 erosive effect Effects 0.000 description 7
- 239000002826 coolant Substances 0.000 description 6
- 230000003647 oxidation Effects 0.000 description 5
- 238000007254 oxidation reaction Methods 0.000 description 5
- 239000012080 ambient air Substances 0.000 description 4
- 230000002939 deleterious effect Effects 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 229910052756 noble gas Inorganic materials 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000011010 flushing procedure Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 230000008676 import Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
Images
Classifications
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B3/00—Ohmic-resistance heating
- H05B3/10—Heater elements characterised by the composition or nature of the materials or by the arrangement of the conductor
- H05B3/12—Heater elements characterised by the composition or nature of the materials or by the arrangement of the conductor characterised by the composition or nature of the conductive material
- H05B3/14—Heater elements characterised by the composition or nature of the materials or by the arrangement of the conductor characterised by the composition or nature of the conductive material the material being non-metallic
- H05B3/145—Carbon only, e.g. carbon black, graphite
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01J—MEASUREMENT OF INTENSITY, VELOCITY, SPECTRAL CONTENT, POLARISATION, PHASE OR PULSE CHARACTERISTICS OF INFRARED, VISIBLE OR ULTRAVIOLET LIGHT; COLORIMETRY; RADIATION PYROMETRY
- G01J5/00—Radiation pyrometry, e.g. infrared or optical thermometry
- G01J5/52—Radiation pyrometry, e.g. infrared or optical thermometry using comparison with reference sources, e.g. disappearing-filament pyrometer
- G01J5/53—Reference sources, e.g. standard lamps; Black bodies
Definitions
- ABSTRACT OF THE DISCLOSURE A blackbody radiating device containing a heatable oxidizable body in a housing having an open end exposing said oxidizable body to ambient air. An opening in the wall of the :housing to provide a flow of inert gas over the oxidizable body and a protective hood aflixed to the open end of the housing so designed as to cool said inert gas when exiting from said open end 20 as to prevent egress of deleterious air into said housing.
- This invention relates to a means for improving blackbody radiation devices. More particularly, the invention relates to a means for improving the life of the radiating element used in blackbody radiation devices.
- Patent 3,205,343 assigned to the same assignee, there is disclosed a blockbody source.
- the source contains a radiating element which is generally made of graphite.
- the element is connected to an electrical source which resistively heats it to temperatures at which the radiation occurs. Erosion and oxidation of the graphite or other radiation element can be reduced by flushing with a slight flow of inert gas, such as argon.
- inert gas such as argon
- an object of this invention is to further enhance the life of a graphite or other oxidiza-ble element used in blockbody radiation devices.
- Another object of the invention is to provide a means for reducing the quantity of inert gas needed to protect the radiation element.
- FIG. 1 is a partially sectioned view of a blackbody radiation device without the improvement of the invention.
- FIG. 2 is a section of a blackbody radiation device incorporating the protective hood of the invention.
- the device contains an outer cylindrical shell or housing 13. Disposed concentrically within the housing is a radiation element 15 which is of a material such as graphite. A radiation surface 17 is medially disposed within the cylindrical radiating element and serves to radiate toward the open end 19. An aperture 21 is provided at the open end 19 to view the radiating surface 17.
- aninert noble gas is admitted into the device and flows through a passage 23 surrounding the element.
- the inert noble gas then enters the element through apertures 25 and flows within the cavity 27 between the radiating surface 17 and the end 19 of the device.
- the inert gas which can be argon is shown by the solid line arrows in the drawing.
- the argon enters, as described, the blackbody cavity through the apertures 25. It is heated in the blackbody, which is at 2000 K., to above 450 K. At this temperature, the argon becomes less dense than air. The heavier air, as depicted by the dotted arrows, enters at the bottom of the aperture 21 and forces the argon out through the upper portion of the aperture. As the air scours the bottom of the hot graphite cavity, it causes erosion by oxidation principally along the surface 29, which is the bottom portion of the cylindrical graphite element when the device is used in its normal horizontal position as shown. This erosion eventually causes failure of the blackbody radiation element 15.
- FIG. 2 there is shown the improvement of the invention wherein a protective hood 31 is threadably affixed at 33 to the front portion 19 of the blackbody radiation device.
- the cylindrical hood has an outer wall 33 and an inner corrugated wall 35. Between these walls is formed a cavity 37.
- An inlet 39 is provided to the cavity with an outlet 41 also in the wall 33 of the device.
- a coolant such as water enters the inlet 39, circulates within the cavity 37 and exits at the outlet 41.
- the corrugated surface 35 serves to increase the effective heat transfer area between the coolant and the gases within the hood.
- the corrugated inner wall 35 is shown in a generally frusto-conical configuration, tapering outwardly from the exit of the blackbody radiation device.
- the coolant water circulating in the hood extension 31 can pass from the hood into the main body 13 of the device to cool the walls thereof.
- an aperture can be provided between the coolant passages 33 of the main body of the radiation device and the hood, wherein the water can exit from the hood into the coolant passages 33.
- the device has been shown utilizing a liquid cooled outer protective jacket or hood, it is contemplated that in certain instances the air cooled one can be utilized. In those instances where the problem is not so severe, such as in a smaller aperture at lower temperature, a mere air cooled protective hood will suffice.
- the protective hood should extend a length and be cooled to the degree necessary to prevent air from entering the blackbody cavity. As indicated, this occurs by keeping the temperature of the inert gas at a point where it is heavier than the air so as to form a protective curtain.
- the hood as shown has an application which is obviously far broader than the particular blackbody radiating element.
- blackbody radiating elements .a window has been used over the opening through which readings are taken.
- the window presents optical problems. With the removal of the window, as shown in the particular device of the previous patent, the attendant problem of erosion from ambient air occurs. This same problem is prevalent in various furnaces and other heated bodies which are exposed to the air and require a continuous flow of inert gas to protect the heated bodies from oxidation. In all instances, if sufficient quantities of inert gas were available, then there would not be a need for a protective device as shown. The quantities of inert gas that would be required are in fact often unattainable or impractical.
- the herein invention presents botha simple, easy, and in some cases, the only means for preventing the rapid and gross deterioration of a radiating or heated element due to contact with air.
- a device containing a heatable oxidizable body in a housing having an open end exposing said oxidizable body to ambient air, and means in the wall of said housing defining an opening to flow an inert gas over said oxidizable body egressing from said opening is provided, the improvement which comprises:
- a protective hood affixed to said open end of said housing and extending away from said oxidizable body, said hood of suflicient length and having suificient heat absorbing characteristics whereby said inert gas is sufliciently cooled when exiting from said open end so as to prevent egress of deleterious air into said housing.
- a blackbody radiating device comprising:
- a housing provided with opening at one end thereof for an emitting radiation
- a blackbody radiation element disposed within said housing, said element open at one end thereof, said open end aligned with said open end of said housing for emitting radiation from the interior of said element
- a protective hood atfixed to said open end of said housing and extending away from said blackbody element, said hood being of sufficient length and having sufficient heat absorbing characteristics whereby said inert gas is suificiently cooled when exiting from said open end so as to prevent ingress of deleterious air into said housing.
Description
F/Li] 1968 A. G. DE BELL 3,419,709
' BLACKBODY RADIATING DEVICE WITH A PROTECTIVE HOOD Filed May 25. 1966 INVENTOUR. 1 t 4272/02 6. D5ZL ATTO NE) United States Patent Office 3,419,709 Patented Dec. 31, 1968 3,419,709 BLACKBODY RADIATING DEVICE WITH A PROTECTIVE HOOD Arthur G. De Bell, Woodland Hills, -Calif., assignor to North American Rockwell Corporation, a corporation of Delaware Filed May 25, 1966, Ser. No. 552,851 5 Claims. (Cl. 219553) ABSTRACT OF THE DISCLOSURE A blackbody radiating device containing a heatable oxidizable body in a housing having an open end exposing said oxidizable body to ambient air. An opening in the wall of the :housing to provide a flow of inert gas over the oxidizable body and a protective hood aflixed to the open end of the housing so designed as to cool said inert gas when exiting from said open end 20 as to prevent egress of deleterious air into said housing.
This invention relates to a means for improving blackbody radiation devices. More particularly, the invention relates to a means for improving the life of the radiating element used in blackbody radiation devices.
In Patent 3,205,343 assigned to the same assignee, there is disclosed a blockbody source. The source contains a radiating element which is generally made of graphite. The element is connected to an electrical source which resistively heats it to temperatures at which the radiation occurs. Erosion and oxidation of the graphite or other radiation element can be reduced by flushing with a slight flow of inert gas, such as argon. However, in operation it was found that a portion of the ambient atmosphere, which was usually air, would still enter the element through the end-viewing aperture. This, in turn, caused oxidation and erosion of the graphite element more rapidly than desired.
Thus, an object of this invention is to further enhance the life of a graphite or other oxidiza-ble element used in blockbody radiation devices.
Another object of the invention is to provide a means for reducing the quantity of inert gas needed to protect the radiation element.
The object of this invention is accomplished by afiixing to the viewing end of the blackbody device a protective hood which is comprised of a water-cooled jacket extension. As will be shown in the description accompanying the figures, the extension prevents the air from entering the cavity of the blackbody device and causing any deleterious effect. The invention will be described in further detail with relation to the following drawings in which:
FIG. 1 is a partially sectioned view of a blackbody radiation device without the improvement of the invention.
FIG. 2 is a section of a blackbody radiation device incorporating the protective hood of the invention.
Referring now to FIG. 1, there is shown a blackbody radiation device 11 which essentially corresponds to the type of device shown in FIG. 3 of the referred to US. Patent 3,205,343. The details of the device other than the graphite radiating element are not of import to the herein invention and, thus, no details of the portion of the device extending from the front half of the graphite element toward the rear are shown. As described in the mentioned patent, the device contains an outer cylindrical shell or housing 13. Disposed concentrically within the housing is a radiation element 15 which is of a material such as graphite. A radiation surface 17 is medially disposed within the cylindrical radiating element and serves to radiate toward the open end 19. An aperture 21 is provided at the open end 19 to view the radiating surface 17. To prevent oxidation of the radiating element, aninert noble gas is admitted into the device and flows through a passage 23 surrounding the element. The inert noble gas then enters the element through apertures 25 and flows within the cavity 27 between the radiating surface 17 and the end 19 of the device. The inert gas which can be argon is shown by the solid line arrows in the drawing.
The argon enters, as described, the blackbody cavity through the apertures 25. It is heated in the blackbody, which is at 2000 K., to above 450 K. At this temperature, the argon becomes less dense than air. The heavier air, as depicted by the dotted arrows, enters at the bottom of the aperture 21 and forces the argon out through the upper portion of the aperture. As the air scours the bottom of the hot graphite cavity, it causes erosion by oxidation principally along the surface 29, which is the bottom portion of the cylindrical graphite element when the device is used in its normal horizontal position as shown. This erosion eventually causes failure of the blackbody radiation element 15.
Turning now to FIG. 2 there is shown the improvement of the invention wherein a protective hood 31 is threadably affixed at 33 to the front portion 19 of the blackbody radiation device. The cylindrical hood has an outer wall 33 and an inner corrugated wall 35. Between these walls is formed a cavity 37. An inlet 39 is provided to the cavity with an outlet 41 also in the wall 33 of the device. A coolant such as water enters the inlet 39, circulates within the cavity 37 and exits at the outlet 41. The corrugated surface 35 serves to increase the effective heat transfer area between the coolant and the gases within the hood. Additionally, as shown, the corrugated inner wall 35 is shown in a generally frusto-conical configuration, tapering outwardly from the exit of the blackbody radiation device. This serves to allow the full field of view of the heated cavity to be utilized. Due to the utilization of the protective hood, the hot argon leaving the aperture 21 of the blackbody device is cooled by contact with the water-cooled protective hood 31. The argon then drops below 450 K. and becomes heavier than the air. This forms a protective curtain which is effective in preventing the air from entering the aperture. As can be seen from the dotted arrows representing the air, the air progresses only slightly inwardly within the protective hood, but does not come close to reaching the confines of the blackbody cavity 27. This serves to prevent the erosion, previously described, of the graphite element and greatly prolongs the life thereof. Additionally, less inert gas is required to effect the desired result of protecting the graphite from air.
For example, as a possible alternative to the arrangement shown in FIG. 2, the coolant water circulating in the hood extension 31 can pass from the hood into the main body 13 of the device to cool the walls thereof. With this particular arrangement, an aperture can be provided between the coolant passages 33 of the main body of the radiation device and the hood, wherein the water can exit from the hood into the coolant passages 33.
Though the device has been shown utilizing a liquid cooled outer protective jacket or hood, it is contemplated that in certain instances the air cooled one can be utilized. In those instances where the problem is not so severe, such as in a smaller aperture at lower temperature, a mere air cooled protective hood will suffice. Thus, in accord with the concept of the invention, the protective hood should extend a length and be cooled to the degree necessary to prevent air from entering the blackbody cavity. As indicated, this occurs by keeping the temperature of the inert gas at a point where it is heavier than the air so as to form a protective curtain.
The invention as described in the attached figures has been with relation to the particular blackbody radiation device shown and claimed in the previously issued patent as referred to above. However, it is pointed out that the blackbody radiating element in such a device, as contemplated, does not of necessity have to have the peculiar configuration shown and claimed in that patent. Rather, the concept of the herein invention relating to the protective hood is applicable in any oxidizable radiating or heated element. Thus, in virtually any shape radiating or heated element which is open to the environment, the attendant problem of corrosion and erosion from ambient air would be overcome by the utilization of the protective hood of this invention.
The use of the hood as shown has an application which is obviously far broader than the particular blackbody radiating element. In blackbody radiating elements, .a window has been used over the opening through which readings are taken. The window, however, presents optical problems. With the removal of the window, as shown in the particular device of the previous patent, the attendant problem of erosion from ambient air occurs. This same problem is prevalent in various furnaces and other heated bodies which are exposed to the air and require a continuous flow of inert gas to protect the heated bodies from oxidation. In all instances, if sufficient quantities of inert gas were available, then there would not be a need for a protective device as shown. The quantities of inert gas that would be required are in fact often unattainable or impractical. Thus, the herein invention presents botha simple, easy, and in some cases, the only means for preventing the rapid and gross deterioration of a radiating or heated element due to contact with air.
Although the invention has been described and illustrated in detail, it is to be clearly understood that the same is by way of illustration and example only and is not to be taken by way of limitation, the spirit and scope of this invention being limited only by the terms of the appended claims.
I claim:
1. In a device containing a heatable oxidizable body in a housing having an open end exposing said oxidizable body to ambient air, and means in the wall of said housing defining an opening to flow an inert gas over said oxidizable =body egressing from said opening is provided, the improvement which comprises:
a protective hood affixed to said open end of said housing and extending away from said oxidizable body, said hood of suflicient length and having suificient heat absorbing characteristics whereby said inert gas is sufliciently cooled when exiting from said open end so as to prevent egress of deleterious air into said housing.
2. In a blackbody radiating device comprising:
a housing provided with opening at one end thereof for an emitting radiation,
a blackbody radiation element disposed within said housing, said element open at one end thereof, said open end aligned with said open end of said housing for emitting radiation from the interior of said element,
a radiating surface disposed within said blackbody element, whereby one side of said surface is exposed for viewing through said open end of said housing,
means for admitting an inert gas within said blackbody element between said partition and said open end,
the improvement which comprises:
a protective hood atfixed to said open end of said housing and extending away from said blackbody element, said hood being of sufficient length and having sufficient heat absorbing characteristics whereby said inert gas is suificiently cooled when exiting from said open end so as to prevent ingress of deleterious air into said housing.
3. The improvement of claim 2 wherein said protective hood is a double-walled body.
4. The improvement of claim 3 wherein said hood is provided with means for circulating a coolant therethrough.
5. The improvement of claim 2 wherein said hood is frusto-conical.
References Cited UNITED STATES PATENTS 2,952,762 9/1960 Williams et al 2l9-553 X 3,138,697 6/1964 Banca et al 219-353 3,205,343 9/1965 De Bell et al 219--553 3,263,016 7/1966 Branstetter et al 13-26 FOREIGN PATENTS 1,078,795 5/1954 France.
OTHER REFERENCES The Review of Scientific Instruments, R. H. McFee, Blackbody Source Unit With Electronic Temperature Control, January 1952, vol. 23, No. 1, pp. 52-53 (copy in 219553).
BERNARD A. GILHEANY, Primary Examiner.
V. Y. MAYEWSKY, Assistant Examiner.
US. Cl. X.R.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US552851A US3419709A (en) | 1966-05-25 | 1966-05-25 | Blackbody radiating device with a protective hood |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US552851A US3419709A (en) | 1966-05-25 | 1966-05-25 | Blackbody radiating device with a protective hood |
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US3419709A true US3419709A (en) | 1968-12-31 |
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US552851A Expired - Lifetime US3419709A (en) | 1966-05-25 | 1966-05-25 | Blackbody radiating device with a protective hood |
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Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3631708A (en) * | 1969-12-11 | 1972-01-04 | Barnes Eng Co | Liquid bath reference cavity |
US3771731A (en) * | 1972-08-21 | 1973-11-13 | Sanders Associates Inc | Mechanically modulated combustion heated infrared radiation source |
US3912934A (en) * | 1974-09-25 | 1975-10-14 | Us Air Force | Variable free stream buffer |
US4019054A (en) * | 1974-07-19 | 1977-04-19 | Ricoh Company, Ltd. | Apparatus for fixing toner images |
US4184066A (en) * | 1976-07-13 | 1980-01-15 | Vyzkumny Ustav Hutnictvi Zeleza | Heat radiation reference source for photothermometry |
US4317042A (en) * | 1980-06-26 | 1982-02-23 | Bartell Frederick O | Blackbody simulator with uniform emissivity |
US4412126A (en) * | 1982-02-04 | 1983-10-25 | Sanders Associates, Inc. | Infrared source |
US4514639A (en) * | 1980-06-26 | 1985-04-30 | Bartell Frederick O | Blackbody simulator with uniform emissivity |
US4598206A (en) * | 1983-07-06 | 1986-07-01 | The Gillette Company | Infrared radiation reference |
US4672211A (en) * | 1980-06-26 | 1987-06-09 | Bartell Frederick O | Blackbody simulator with uniform emissivity |
US5602389A (en) * | 1995-07-13 | 1997-02-11 | Kabushiki Kaisha Toshiba | Infrared sensor calibration apparatus using a blackbody |
US6390668B1 (en) | 1998-12-11 | 2002-05-21 | Peter Albert Materna | Blackbody source using a heat pipe principle and transition region |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1078795A (en) * | 1953-06-15 | 1954-11-23 | Anticonvectional device for infrared panels and ovens | |
US2952762A (en) * | 1960-09-13 | Black body radiation source | ||
US3138697A (en) * | 1962-10-16 | 1964-06-23 | Barnes Eng Co | Black body radiation sources |
US3205343A (en) * | 1962-10-19 | 1965-09-07 | North American Aviation Inc | Blackbody source |
US3263016A (en) * | 1963-10-30 | 1966-07-26 | Branstetter James Robert | Black-body furnace |
-
1966
- 1966-05-25 US US552851A patent/US3419709A/en not_active Expired - Lifetime
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2952762A (en) * | 1960-09-13 | Black body radiation source | ||
FR1078795A (en) * | 1953-06-15 | 1954-11-23 | Anticonvectional device for infrared panels and ovens | |
US3138697A (en) * | 1962-10-16 | 1964-06-23 | Barnes Eng Co | Black body radiation sources |
US3205343A (en) * | 1962-10-19 | 1965-09-07 | North American Aviation Inc | Blackbody source |
US3263016A (en) * | 1963-10-30 | 1966-07-26 | Branstetter James Robert | Black-body furnace |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3631708A (en) * | 1969-12-11 | 1972-01-04 | Barnes Eng Co | Liquid bath reference cavity |
US3771731A (en) * | 1972-08-21 | 1973-11-13 | Sanders Associates Inc | Mechanically modulated combustion heated infrared radiation source |
US4019054A (en) * | 1974-07-19 | 1977-04-19 | Ricoh Company, Ltd. | Apparatus for fixing toner images |
US3912934A (en) * | 1974-09-25 | 1975-10-14 | Us Air Force | Variable free stream buffer |
US4184066A (en) * | 1976-07-13 | 1980-01-15 | Vyzkumny Ustav Hutnictvi Zeleza | Heat radiation reference source for photothermometry |
US4317042A (en) * | 1980-06-26 | 1982-02-23 | Bartell Frederick O | Blackbody simulator with uniform emissivity |
US4514639A (en) * | 1980-06-26 | 1985-04-30 | Bartell Frederick O | Blackbody simulator with uniform emissivity |
US4672211A (en) * | 1980-06-26 | 1987-06-09 | Bartell Frederick O | Blackbody simulator with uniform emissivity |
US4412126A (en) * | 1982-02-04 | 1983-10-25 | Sanders Associates, Inc. | Infrared source |
US4598206A (en) * | 1983-07-06 | 1986-07-01 | The Gillette Company | Infrared radiation reference |
US5602389A (en) * | 1995-07-13 | 1997-02-11 | Kabushiki Kaisha Toshiba | Infrared sensor calibration apparatus using a blackbody |
US6390668B1 (en) | 1998-12-11 | 2002-05-21 | Peter Albert Materna | Blackbody source using a heat pipe principle and transition region |
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