Search Images Maps Play YouTube News Gmail Drive More »
Sign in
Screen reader users: click this link for accessible mode. Accessible mode has the same essential features but works better with your reader.

Patents

  1. Advanced Patent Search
Publication numberUS3419709 A
Publication typeGrant
Publication dateDec 31, 1968
Filing dateMay 25, 1966
Priority dateMay 25, 1966
Publication numberUS 3419709 A, US 3419709A, US-A-3419709, US3419709 A, US3419709A
InventorsDe Bell Arthur G
Original AssigneeNorth American Rockwell
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Blackbody radiating device with a protective hood
US 3419709 A
Abstract  available in
Images(1)
Previous page
Next page
Claims  available in
Description  (OCR text may contain errors)

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.

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US2952762 *Dec 5, 1957Sep 13, 1960 Black body radiation source
US3138697 *Oct 16, 1962Jun 23, 1964Barnes Eng CoBlack body radiation sources
US3205343 *Oct 19, 1962Sep 7, 1965North American Aviation IncBlackbody source
US3263016 *Oct 30, 1963Jul 26, 1966Metzler Allen JBlack-body furnace
FR1078795A * Title not available
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US3631708 *Dec 11, 1969Jan 4, 1972Barnes Eng CoLiquid bath reference cavity
US3771731 *Aug 21, 1972Nov 13, 1973Sanders Associates IncMechanically modulated combustion heated infrared radiation source
US3912934 *Sep 25, 1974Oct 14, 1975Us Air ForceVariable free stream buffer
US4019054 *Jul 21, 1975Apr 19, 1977Ricoh Company, Ltd.Apparatus for fixing toner images
US4184066 *Jul 13, 1977Jan 15, 1980Vyzkumny Ustav Hutnictvi ZelezaHeat radiation reference source for photothermometry
US4317042 *Jun 26, 1980Feb 23, 1982Bartell Frederick OBlackbody simulator with uniform emissivity
US4412126 *Feb 4, 1982Oct 25, 1983Sanders Associates, Inc.Infrared source
US4514639 *Jun 7, 1983Apr 30, 1985Bartell Frederick OBlackbody simulator with uniform emissivity
US4598206 *Jul 6, 1983Jul 1, 1986The Gillette CompanyInfrared radiation reference
US4672211 *Apr 25, 1985Jun 9, 1987Bartell Frederick OBlackbody simulator with uniform emissivity
US5602389 *Jul 13, 1995Feb 11, 1997Kabushiki Kaisha ToshibaInfrared sensor calibration apparatus using a blackbody
US6390668Jun 26, 2000May 21, 2002Peter Albert MaternaBlackbody source using a heat pipe principle and transition region
Classifications
U.S. Classification219/553, 250/504.00R, 165/186, 250/493.1
International ClassificationH05B3/14, G01J5/52
Cooperative ClassificationG01J5/522, H05B3/145
European ClassificationH05B3/14G, G01J5/52B