US2732418A - Tube shield - Google Patents
Tube shield Download PDFInfo
- Publication number
- US2732418A US2732418A US2732418DA US2732418A US 2732418 A US2732418 A US 2732418A US 2732418D A US2732418D A US 2732418DA US 2732418 A US2732418 A US 2732418A
- Authority
- US
- United States
- Prior art keywords
- tube
- shield
- socket
- heat
- air
- 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
- 229910052782 aluminium Inorganic materials 0.000 claims description 12
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminum Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 12
- PNEYBMLMFCGWSK-UHFFFAOYSA-N al2o3 Chemical compound [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims description 8
- 239000011248 coating agent Substances 0.000 claims description 6
- 238000000576 coating method Methods 0.000 claims description 6
- 238000001816 cooling Methods 0.000 description 12
- 238000010276 construction Methods 0.000 description 10
- 210000002832 Shoulder Anatomy 0.000 description 8
- 239000000203 mixture Substances 0.000 description 8
- PAYRUJLWNCNPSJ-UHFFFAOYSA-N aniline Chemical compound NC1=CC=CC=C1 PAYRUJLWNCNPSJ-UHFFFAOYSA-N 0.000 description 6
- 230000001771 impaired Effects 0.000 description 6
- 239000011521 glass Substances 0.000 description 4
- 230000035939 shock Effects 0.000 description 4
- 230000001702 transmitter Effects 0.000 description 4
- 230000037250 Clearance Effects 0.000 description 2
- 210000002370 ICC Anatomy 0.000 description 2
- 241000428533 Rhis Species 0.000 description 2
- 239000006096 absorbing agent Substances 0.000 description 2
- 230000035512 clearance Effects 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 230000002708 enhancing Effects 0.000 description 2
- 238000011010 flushing procedure Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 230000000452 restraining Effects 0.000 description 2
- 229920002379 silicone rubber Polymers 0.000 description 2
- 239000004945 silicone rubber Substances 0.000 description 2
Images
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J5/00—Details relating to vessels or to leading-in conductors common to two or more basic types of discharge tubes or lamps
- H01J5/02—Vessels; Containers; Shields associated therewith; Vacuum locks
- H01J5/12—Double-wall vessels or containers
Definitions
- the present invention provides a tube shield for air cooled vacuum tubes of the type employed in radio transmitters.
- An object of the invention is to provide a novel and improved means for dissipating the radiant heat which is generated by the electrode structures of such tubes and preventing the radiant heat from being reflected back into the tube or transferred to surrounding parts and equipment.
- Another object of the invention is to provide safety means responsive to temperature to interrupt the current supply to the tube in the event of failure of the cooling means, thus protecting the tube from danger due to excessive heat.
- a further object of the invention is to provide means for supporting and holding the vacuum tube in the socket by lateral and vertical support means which tolerate a safe degree of tube displacement.
- Another object is to provide improved cooling means for the electrode seals and tube surface.
- the means by which the desired temperature control is accomplished by my invention consist in the introduction into the immediate vicinity of the tube of a cylindrical shield which substantially envelopes the tube and which presents an inner surface capable of absorbing radiant heat from the tube and having suicient area so that the absorbed heat can be transferred in turn to the cooling air by conduction with a low temperature gradient.
- Air is passed between the shield and the tube in sutlicient volume to accomplish the adequate removal of heat from the tube shield.
- the air ow is also suieient in Volume to provide glass and electrode seal cooling of the tube.
- the flow of air can be maintained in sufiicient volume with a low air pressure gradient by the arrangement herein contemplated, since large air passages are easily provided between the tube and the shield. This insures an economy of blower power. With provision for heat transfer first by radiation and then by conduction a high efficiency of cooling is achieved.
- thermostatically controlled means are pro- ICC vided to shut down the tube.
- a thermostat may be placed in contact with the shield and such construction offers a simple and safe means of shutting off the tube. It is apparent, therefore, that under no condition can the tube be damaged by its own generated heat because adequate radiation cooling of the tube prevails until the thermostat operates to open the tube circuit in the event the air flow should be insumcient or entirely fail.
- Fig. 1 is an elevation of the tube shield and associated. parts
- Fig. 2 is a top plan of the tube shield on enlarged scale with parts broken away;
- Fig. 3 is a vertical sectional elevation taken on the; angular line 3-3 of Fig. 2;
- Fig. 4 is a fragmentary sectional detail on further en larged scale of the holding means of Figs. l, 2 and 3;
- Fig. 5 is an enlarged fragmentary detail in elevation4 of modified retainer means for the shield.
- Fig. 6 is an enlarged section of the parts shown in Fig.. 5 taken an line 6 6 of Fig. 5.
- the numeral 1 represents: the cylindrical casing of the tube shield.
- the socket plate is provided with socket holes for tube terminals through which in known manner the terminal prongs on a tube 3 extend into a socket 6a.
- the sides of the tins 4 extend radially and inwardly to provide ample clearance for the tube 3.
- the tube shield is proportioned to telescope over and fit upon the retainer ring 5.
- each spring clip has its upper free end portion 9a curved outwardly and flaring in width for a distance and then reduced in width so as to form lateral shoulders the continuation beyond the shoulders constituting a tongue portion having straight sides and conforming substantially in width to that of the portion attached to the casing 1.
- the lateral shoulders engage notches 1t? of two serrated posts 11 screwed into the flange 5 and the socket plate d.
- the tongue portion of the member 9a extends between the two serrated posts il, effectively restraining the tube shield from rotation. iingagement of the edges of tie shoulders of the pction 9a with the serrated posts maintains the tube shieid in its proper axial position with respect to the tube.
- rhis spring clip comprises a flat spi" g 9b the lower portion of which is attached to the tub-e shield by a spacing block 9c.
- a block 9d' is attached to, the outer and upper portion of the flat spring.
- the ends of the block 9d have wedge-shaped extensions 9e which are directed so as to engage the notches 151 of serrated posts 11 and accordingly lock the tube shield against axial or radial movement.
- pad supports 13 In the upper portion of the tube shield there are radially mounted on the inner surface pad supports 13. shown as three in number and spaced apart in Fig. 2. Pad receiving component 13a of the pad support 13 is angularly bent upwardly in order that pad 14 mounted Y on its lower surface will exert both lateral and downward pressure against the glass envelope of the tube 3.
- the pressure exerted by the pads against the'tubes is not a rigid or'unyielding one in as much as' the action of the ilexible spring clips 9 against the serrated posts 11, while indirectly supporting the tube in its socket, permits a certain amountrof tolerance or play in tube movement in the event of shock or jarring.
- the pads 14 also serve as shock absorbers for the tube.
- the pads are made of sponge material such as silicone rubber and must be able to withstand relatively high operating temperatures.
- ns which are in the vertical planes of the pad supports are necessarily shorter than the other tins.
- the shield is preferably metallic and aluminum has been found to be a satisfactory metal for most purposes.
- the inner surface of the aluminum tube shield and the aluminum ius is treated electrolyti-:aiiy to produce a surface of aluminum oxide and this surface is dyed with a dull biack aniline dye to render it heat absorptive and non-reflecting.
- the air which is circulated between the tube and the cylinder and hns is blown by a blower 15 through large holes 15a in the socket plate 6 and spaced about the tube socket.
- the tube shield is open ended at its top and the air to which the heat energy is transmitted rises and is permitted to escape the vicinity of the tube and its surrounding parts through the vent 16.
- thermostat On the outer surface of the cylindrical tube shield 1 is a bracket 17 which holds a thermostat 18.
- the thermostat being in metallic Contact with the tube shield partakes of its temperature and houses, for example, a bimetallic switch 19 which makes or breaks circuit of a relay 20 which in turn controls the making or breaking of the main power circuit for the tube, as indicated in Fig. 1.
- the connection between the thermostat and the power to the tube may be established, of course, in various ways and the precise means adopted constitute no part of this invention. It is an important aspect of the invention, however, that thermostatic safety means are provided in the event of failure or impairment of air circulation within the tube shield. 1t is the heat absorbing and non-renecting characteristics of the tube shield and fins which are exposed to the air flow which aiord the primary protection to the tube and enhance its life expectancy.
- the metallic nature of the tube shield which substantially encloses the tube, protects it from the interference of radio frequency waves generated by the transmitter and which can greatly reduce the efhciency of radio tubes and conversely shields the surrounding equipment from radio frequency waves produced by the tubes.
- the shield may, for example, consist of two half-cylinders
- The'tubes may thus be afforded the protection of the tube shields, though the structural requirements of the transmitters ⁇ may limit the space above the tubes to less than the height of the tube shield. Where this space is greater than the height of the tube shield the latter may be of integral construction as shown.
- shield retaining means surrounding the socket, a cylindrical open ended metallic shield secured to said retaining means having axially disposed radial extensions on its inner face to provide substantial heat dissipating area, said face being substantially non-reilective of radiant heat, and biower means connected to force air through the space between the tube and the open ended shield in heat conducting contact with the shield.
Description
Jan. 24 1956 F A. LINDLEY JR 2,732,418
um man www.. 11mm Smets-mi2 Jan. 24, 1956 F. A. LINDLEY, JR
TUBE SHIELD 3 Sheets-Sheet 5 Filed Dec. l 1951 Cmorncj United States Patent TUBE SHIELD Frederick A. Lindley, Jr., Flushing, N. Y., assignor t Smith-Meeker Engineering C0., New York, N. Y., a corporation of New York Appiication December 1, 1951, Serial No. 259,405
4 Claims. (Cl. 174-16) The present invention provides a tube shield for air cooled vacuum tubes of the type employed in radio transmitters.
An object of the invention is to provide a novel and improved means for dissipating the radiant heat which is generated by the electrode structures of such tubes and preventing the radiant heat from being reflected back into the tube or transferred to surrounding parts and equipment.
Another object of the invention is to provide safety means responsive to temperature to interrupt the current supply to the tube in the event of failure of the cooling means, thus protecting the tube from danger due to excessive heat.
A further obiect of the invention is to provide means for supporting and holding the vacuum tube in the socket by lateral and vertical support means which tolerate a safe degree of tube displacement.
Another object is to provide improved cooling means for the electrode seals and tube surface.
Usually heretofore provision has been made for a nominally small amount of air to be blown over the tube and particularly the seals where leads are brought out from the electrodes. Principal reliance however, has been placed upon radiation to dissipate the heat energy generated within the tubes. Because little consideration has been given to means for effective disposal of the radiant energy, damage has often resulted to surrounding equipment due to their excessive increase in temperature. Also the ability of the tube to dissipate its heat properly is impaired when reflection of the radiant energy back into the tube is permitted. Such reflection can cause excessive tube temperature, shortened tube life, and generally poor circuit performance.
The means by which the desired temperature control is accomplished by my invention consist in the introduction into the immediate vicinity of the tube of a cylindrical shield which substantially envelopes the tube and which presents an inner surface capable of absorbing radiant heat from the tube and having suicient area so that the absorbed heat can be transferred in turn to the cooling air by conduction with a low temperature gradient. Air is passed between the shield and the tube in sutlicient volume to accomplish the adequate removal of heat from the tube shield. The air ow is also suieient in Volume to provide glass and electrode seal cooling of the tube. The flow of air can be maintained in sufiicient volume with a low air pressure gradient by the arrangement herein contemplated, since large air passages are easily provided between the tube and the shield. This insures an economy of blower power. With provision for heat transfer first by radiation and then by conduction a high efficiency of cooling is achieved.
The ability of the tube shield to absorb radiant energy would be very little impaired though the shield temperature rises substantially. Should, however, the air ow become impaired or even fail and the tube shield become excessively hot, thermostatically controlled means are pro- ICC vided to shut down the tube. For example, a thermostat may be placed in contact with the shield and such construction offers a simple and safe means of shutting off the tube. It is apparent, therefore, that under no condition can the tube be damaged by its own generated heat because adequate radiation cooling of the tube prevails until the thermostat operates to open the tube circuit in the event the air flow should be insumcient or entirely fail.
Other benefits and advantages flowing from the typeol shield construction disclosed in my invention will appear in the accompanying drawings and the followingl detailed description in which Fig. 1 is an elevation of the tube shield and associated. parts;
Fig. 2 is a top plan of the tube shield on enlarged scale with parts broken away;
Fig. 3 is a vertical sectional elevation taken on the; angular line 3-3 of Fig. 2;
Fig. 4 is a fragmentary sectional detail on further en larged scale of the holding means of Figs. l, 2 and 3;,
Fig. 5 is an enlarged fragmentary detail in elevation4 of modified retainer means for the shield; and
Fig. 6 is an enlarged section of the parts shown in Fig.. 5 taken an line 6 6 of Fig. 5.
Referring to the drawings, the numeral 1 represents: the cylindrical casing of the tube shield. There are pro-- vided on the inner surface of the cylindrical casing 1 channel shaped tins 4 angularly displaced from each other and axially mounted on the inner surface extending substantially the height of the tube shield less the height of retainer ring 5 which is hanged and secured to` socket plate 6, as by rivets. The socket plate is provided with socket holes for tube terminals through which in known manner the terminal prongs on a tube 3 extend into a socket 6a. The sides of the tins 4 extend radially and inwardly to provide ample clearance for the tube 3. The tube shield is proportioned to telescope over and fit upon the retainer ring 5.
Another construction for a spring clip is shown in Figs. 5 and 6. rhis spring clip comprises a flat spi" g 9b the lower portion of which is attached to the tub-e shield by a spacing block 9c. A block 9d' is attached to, the outer and upper portion of the flat spring. The ends of the block 9d have wedge-shaped extensions 9e which are directed so as to engage the notches 151 of serrated posts 11 and accordingly lock the tube shield against axial or radial movement.
In the upper portion of the tube shield there are radially mounted on the inner surface pad supports 13. shown as three in number and spaced apart in Fig. 2. Pad receiving component 13a of the pad support 13 is angularly bent upwardly in order that pad 14 mounted Y on its lower surface will exert both lateral and downward pressure against the glass envelope of the tube 3.
and. thus prevent excessive lateral movement of the tube and support the' tube in its socket. The pressure exerted by the pads against the'tubes is not a rigid or'unyielding one in as much as' the action of the ilexible spring clips 9 against the serrated posts 11, while indirectly supporting the tube in its socket, permits a certain amountrof tolerance or play in tube movement in the event of shock or jarring. Being compressible the pads 14 also serve as shock absorbers for the tube. The pads are made of sponge material such as silicone rubber and must be able to withstand relatively high operating temperatures.
As shown the ns which are in the vertical planes of the pad supports are necessarily shorter than the other tins.
The shield is preferably metallic and aluminum has been found to be a satisfactory metal for most purposes. The inner surface of the aluminum tube shield and the aluminum ius is treated electrolyti-:aiiy to produce a surface of aluminum oxide and this surface is dyed with a dull biack aniline dye to render it heat absorptive and non-reflecting. The air which is circulated between the tube and the cylinder and hns is blown by a blower 15 through large holes 15a in the socket plate 6 and spaced about the tube socket. The tube shield is open ended at its top and the air to which the heat energy is transmitted rises and is permitted to escape the vicinity of the tube and its surrounding parts through the vent 16.
On the outer surface of the cylindrical tube shield 1 is a bracket 17 which holds a thermostat 18. The thermostat being in metallic Contact with the tube shield partakes of its temperature and houses, for example, a bimetallic switch 19 which makes or breaks circuit of a relay 20 which in turn controls the making or breaking of the main power circuit for the tube, as indicated in Fig. 1. The connection between the thermostat and the power to the tube may be established, of course, in various ways and the precise means adopted constitute no part of this invention. It is an important aspect of the invention, however, that thermostatic safety means are provided in the event of failure or impairment of air circulation within the tube shield. 1t is the heat absorbing and non-renecting characteristics of the tube shield and fins which are exposed to the air flow which aiord the primary protection to the tube and enhance its life expectancy.
The metallic nature of the tube shield, which substantially encloses the tube, protects it from the interference of radio frequency waves generated by the transmitter and which can greatly reduce the efhciency of radio tubes and conversely shields the surrounding equipment from radio frequency waves produced by the tubes.
Where vertical space limitations are encountered, the shield may, for example, consist of two half-cylinders,
one being permanently xed in place and the other being 4 removably secured'fv to it'. The'tubes may thus be afforded the protection of the tube shields, though the structural requirements of the transmitters` may limit the space above the tubes to less than the height of the tube shield. Where this space is greater than the height of the tube shield the latter may be of integral construction as shown.
It is obvious that the hns may be integral with the shield, as by corrugations, and that other detail changes may be made in the construction shown in the drawings and above particularly vdescribed within the prin ciple and scope'of the invention as defined in the following claims.
What is claimed is:
1. in combination with a radio tube socket, a shield retainer, a cylindrical open ended aluminum shield surrounding the socket and secured by the retainer and having heat dissipating fins on its inner face, the inner sur face of the shield including ythe fins being treated to form a coating' of aluminum oxide thereon and being dyed with a dull black aniline dye, and blower means communicating with the space within the shield.
2. In combination with a radio tube socket, shield retaining means surrounding the socket, a cylindrical open ended metallic shield secured to said retaining means having axially disposed radial extensions on its inner face to provide substantial heat dissipating area, said face being substantially non-reilective of radiant heat, and biower means connected to force air through the space between the tube and the open ended shield in heat conducting contact with the shield.
3. The combination of claim 2 in which the said inner face has axial ns disposed thereon the exposed surface of which is substantially non-reective of radiant heat.
4. The combination of claim 3 in which the shield and iins are aluminum and the inner surface of the shield including the fins is treated to form a coating of aluminum oxide thereon and is dyed with a dull black aniline dye.
References Cited in the le of this patent UNITED STATES PATENTS 1,708,935 Christopher Apr. 16, 1929 2,080,913 Hafecost May 18, 1937 2,167,472 Bedford July 25, 1939 2,189,618 Slepian Feb. 6, 1940 2,192,047 Miles Feb. 27, 1940 2,277,147 Rogers Mar. 27, 1942 2,310,575 Cattaneo Feb. 9, 1943 2,348,852 Scharfnagel May 16, 1944 2,368,812 Eitel et al. Feb. 6, 1945 2,398,626 Del Camp Apr. 16, 1946 2,407,857 Verhoeff Sept. 17, 1946 2,445,582 Melville July 20, 1948 2,583,417 Eitel et al. Ian. 22, 1952
Claims (1)
1. IN COMBINATION WITH A RADIO TUBE SOCKET, A SHIELD RETAINER, A CYLINDRICAL OPEN ENDED ALUMINUM SHIELD SURROUNDING THE SOCKET AND SECURED BY THE RETAINER AND HAVING HEAT DISSIPATING FINS ON ITS INNER FACE, THE INNER SURFACE OF THE SHIELD INCLUDING THE FINS BEING TREATED TO FORM A COATING OF ALUMINUM OXIDE THEREON AND BEING DYED WITH A DULL BLACK ANILINE DYE, AND BLOWER MEANS COMMUNICATING WITH THE SPACE WITHIN THE SHIELD.
Publications (1)
Publication Number | Publication Date |
---|---|
US2732418A true US2732418A (en) | 1956-01-24 |
Family
ID=3442109
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US2732418D Expired - Lifetime US2732418A (en) | Tube shield |
Country Status (1)
Country | Link |
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US (1) | US2732418A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2902262A (en) * | 1957-08-29 | 1959-09-01 | Malcolm S Morse | Temperature regulating tube shield |
US3376920A (en) * | 1966-08-31 | 1968-04-09 | Staver Co | Combination shield can and heat dissipator for electronic circuitry using a transistor |
US4709148A (en) * | 1985-02-07 | 1987-11-24 | Sherritt Gordon Mines Limited | Quadrupole mass spectrometers |
Citations (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1708935A (en) * | 1927-08-09 | 1929-04-16 | Bell Telephone Labor Inc | Coil and transformer |
US2080913A (en) * | 1935-05-21 | 1937-05-18 | Goat Radio Tube Parts Inc | Radio tube shield |
US2167472A (en) * | 1936-11-18 | 1939-07-25 | Gen Electric | Thermostatic control of electron discharge apparatus |
US2189618A (en) * | 1938-03-25 | 1940-02-06 | Westinghouse Electric & Mfg Co | Vapor electric tube |
US2192047A (en) * | 1939-02-02 | 1940-02-27 | Gen Electric | Discharge apparatus |
US2277147A (en) * | 1939-10-09 | 1942-03-24 | Elwood C Rogers | Enlarger |
US2310575A (en) * | 1940-05-17 | 1943-02-09 | Shell Dev | Ignition system for internal combustion engines |
US2348852A (en) * | 1940-01-27 | 1944-05-16 | Scharfnagel Rudolf | Electron tube |
US2368812A (en) * | 1942-06-30 | 1945-02-06 | Eitel Mccullough Inc | Electronic tube |
US2398626A (en) * | 1944-12-20 | 1946-04-16 | Cinch Mfg Corp | Shielded tube mounting |
US2407857A (en) * | 1941-02-27 | 1946-09-17 | Hartford Nat Bank & Trust Comp | X-ray tube |
US2445582A (en) * | 1945-11-07 | 1948-07-20 | Gen Electric | Thermionic valve and circuit mounting |
US2583417A (en) * | 1947-11-24 | 1952-01-22 | Eitel Mccullough Inc | Air-cooled socket for electron tubes |
-
0
- US US2732418D patent/US2732418A/en not_active Expired - Lifetime
Patent Citations (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1708935A (en) * | 1927-08-09 | 1929-04-16 | Bell Telephone Labor Inc | Coil and transformer |
US2080913A (en) * | 1935-05-21 | 1937-05-18 | Goat Radio Tube Parts Inc | Radio tube shield |
US2167472A (en) * | 1936-11-18 | 1939-07-25 | Gen Electric | Thermostatic control of electron discharge apparatus |
US2189618A (en) * | 1938-03-25 | 1940-02-06 | Westinghouse Electric & Mfg Co | Vapor electric tube |
US2192047A (en) * | 1939-02-02 | 1940-02-27 | Gen Electric | Discharge apparatus |
US2277147A (en) * | 1939-10-09 | 1942-03-24 | Elwood C Rogers | Enlarger |
US2348852A (en) * | 1940-01-27 | 1944-05-16 | Scharfnagel Rudolf | Electron tube |
US2310575A (en) * | 1940-05-17 | 1943-02-09 | Shell Dev | Ignition system for internal combustion engines |
US2407857A (en) * | 1941-02-27 | 1946-09-17 | Hartford Nat Bank & Trust Comp | X-ray tube |
US2368812A (en) * | 1942-06-30 | 1945-02-06 | Eitel Mccullough Inc | Electronic tube |
US2398626A (en) * | 1944-12-20 | 1946-04-16 | Cinch Mfg Corp | Shielded tube mounting |
US2445582A (en) * | 1945-11-07 | 1948-07-20 | Gen Electric | Thermionic valve and circuit mounting |
US2583417A (en) * | 1947-11-24 | 1952-01-22 | Eitel Mccullough Inc | Air-cooled socket for electron tubes |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2902262A (en) * | 1957-08-29 | 1959-09-01 | Malcolm S Morse | Temperature regulating tube shield |
US3376920A (en) * | 1966-08-31 | 1968-04-09 | Staver Co | Combination shield can and heat dissipator for electronic circuitry using a transistor |
US4709148A (en) * | 1985-02-07 | 1987-11-24 | Sherritt Gordon Mines Limited | Quadrupole mass spectrometers |
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