US2673721A - Apparatus for cooling electron discharge devices - Google Patents
Apparatus for cooling electron discharge devices Download PDFInfo
- Publication number
- US2673721A US2673721A US220952A US22095251A US2673721A US 2673721 A US2673721 A US 2673721A US 220952 A US220952 A US 220952A US 22095251 A US22095251 A US 22095251A US 2673721 A US2673721 A US 2673721A
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- shield
- tube
- envelope
- springs
- heat
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- 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
- tion requires accessory equipment including a l blower.
- a l blower When tubes are placed in unattended substations it is undesirable to employ any machinery that would require maintenance, as would the rotating machinery and other parts of the blower equipment. Additionally, it is often desirable to connect the unit in which the tubes are incorporated, such asan amplifiendirectly and solely into the circuit.
- the amplifier may be contained in a sealed case connected directly into the coaxial cable Without any outside power supply. Then all the power to the amplifier must be transmitted over the cable itself. But the power requirements of a blower would be such that the power for the blower could not be transmitted over the cable and outside electrical connections would be necessary.
- a shield of a good heat conducting material around the vacuum tube.
- a plurality of helically wound springs are arranged within the shield and make contact with the glass envelope of the tube in the region of or opposite the internal elements of the tube. These springs thus have turns extending between the glass envelope of the tube and the inner surface of the shield.
- Each turn of the helical spring makes a conduction contact with the envelope of the tube, and each such contact is provided with two parallel heat conduction paths to the shield.
- the envelopes of tubes can generally be considered to be cylindrical but actually in the mass production of tubes eccentricities are often introduced so that the envelopes instead of being circular in cross section are more nearly oval or el liptical. Additionally, the temperature attained by the thermionic tube during operation may affect the glass envelope so that it does not retain its form but changes, accentuating the eccentric configuration. Also, in actual mass production the tubes are not all accurately centered on the pins in the base of the tube so that, on being placed in their sockets, the actual positions of the envelopes will vary. However, the springs which provide the conduction paths between the glass envelope and the shield, which of course is and remains always cylindrical, are flexible enough to allow for considerable variations without there beingany loss of contact points with bulb or envelope of the tube.
- ihe shield itself serves a dual function as it not only quickly removes the heat of the tube to itself by conduction along the helical springs, in accordance with this invention, but also it acts as an electrostatic and electromagnetic shield, as is Well known and as is generally necessary for many tube applications.
- conduction paths be provided between the glass envelope of a vacuum tube and an outer shield by a helical spring extending around the envelope and making contact therewith at a number of points.
- the envelope of the vacuum tube depress the inner turns of the helical spring so that considerable variations in the diameter and concentricity of the tube envelope can be accepted without loss of any points of thermal contact with the helical spring.
- the heat conducting shield surrounding the vacuum tube be mounted on a heat dissipating base and comprise a plurality of helical springs within the shield contacting the inner surface of the shield and contacting the envelope of the vacuum tube at a large number of distinct points.
- the springs define two parallel heat conduction paths from each of these points to the shield and thus to the heat dissipating base.
- FIG. 1 is a perspective view of one heat conducting shield illustrative of this invention mounted on a heat dissipating base and with a vacuum tube positioned therein;
- Fig. 2 is a side view of the assembly of Fig. 1, a portion of the shield being broken away to show the helical spring members contacting the envelope of the vacuum tube and the inner surface of the shield.
- the shield 19 may advantageously be a hollow cylinder of slightly larger inner diameter than the outer diameter of the glass envelope of the tube with which it will be employed. It may advantageously be of copper or other good heat conducting material and is supported in good thermal contact with a base II, also advantageously of good heat conducting material, as by an inner ring member I2 having fingers I3 extending upward and clamping ears l4 integral with the shield 10 and extending inward therefrom at its base.
- a vacuum tube or other electronic device 16 is mounted in a socket I! supported by the base ll.
- Metallic conduction of heat away from the envelope of the tube 6 to the shield l and thence to the base II is accomplished by helical springs 20 which are held in shallow grooves 2
- the axes of the helices are thus circles concentric with the cylindrical shield ID.
- the helical springs and snap springs 22 may advantageously be of steel.
- the envelope of the tube bears against the inner portions of the turns of the helical springs 20 biasing them and thus slightly depresses them.
- Each turn of each helical spring thus makes contact with the glass envelope of the tube at one contact point and from that contact point two heat conducting paths are provided back to the shield In.
- a good thermal connection is made between the shield I0 and the turns of the'springs 20 by the relatively long portions of the spring coils held tightly in the grooves 2
- Variations in the initial configuration of the tube envelope such as lack of concentricity or differences in external diameter, are taken up by the flexible springs 20 which adjust to each particular tube.
- the differences in tube dimensions will only result in different amounts of depressions of the inner portions of the turns of the helical springs.
- any change in the external configuration of the tube during operation because of the internal generation of heat will be compensated for as the springs follow the variat ons in the envelope without losing any points of contact therewith.
- the shield 10 was of .065 inch copper tubing, 1% inches high and 1 /2 inches in diameter
- the springs 20 were of .010 inch steel wire helically wound with 20 turns per inch
- were of .055 inch steel wire.
- the base II was of copper and attached to the amplifier case so that the amplifier case also dissipated the heat conducted to it from the tube envelopes through the good metallic conduction paths of the springs 2!), the shield I0 and the base i I.
- Means for conducting heat from the envelope of an electron discharge device to a base member of heat conducting material which dissipates the heat conducted to it from the envelope comprising a cylindrical shield of heat conducting material attached to and in. thermal contact with said base member and surrounding the device, the inner periphery of said shield having a plurality of circular grooves therein, a plurality of helical springs Within said grooves, the axes of the helices of said springs being circles concentric with said shield, and spring means positioning said helical springs in said grooves in thermal contact with said shield, the turns of said springs away from said shield being depressed by the envelope of the electron discharge device, making contact with said envelope at a plurality of points and defining two parallel heat conductive paths from each of said points to said shield.
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- Cooling Or The Like Of Electrical Apparatus (AREA)
Description
March 30, 1954 F. R. DICKINSON 2 APPARATUS FOR COOLING ELECTRON DISCHARGE DEVICES Filed April. 13, 1951 m/ l EN TOR E R. DICKINSON ATTORNEY Patented Mar. 30, 1954 APPARATUS FOR COOLING ELECTRON DISCHARGE DEVICES Frank R. Dickinson, Glen Ridge, N. J assignor to Bell Telephone Laboratories, Incorporated, New York, N. Y., a corporation of New York Application April 13, 1951, Serial No. 220,952
1 Claim. 1
tion requires accessory equipment including a l blower. When tubes are placed in unattended substations it is undesirable to employ any machinery that would require maintenance, as would the rotating machinery and other parts of the blower equipment. Additionally, it is often desirable to connect the unit in which the tubes are incorporated, such asan amplifiendirectly and solely into the circuit. Thus in coaxial cables the amplifier may be contained in a sealed case connected directly into the coaxial cable Without any outside power supply. Then all the power to the amplifier must be transmitted over the cable itself. But the power requirements of a blower would be such that the power for the blower could not be transmitted over the cable and outside electrical connections would be necessary.
Without a forced air cooling the ventilation of tubes, and particularly when in a closed case, may not be sufficient to cool the tube envelopes. Heat may also be dissipated by radiation from the tube envelope or by conduction. The heat loss through radiation is not significant nor generally is that through conduction as the tube envelope is not in contact with any other bodies. Thus without forced air cooling the heat dissipation from a thermionic tube by conduction, convection, and radiation is insufiicient for many purposes.
It is important to reduce the temperature of tubes in order to prevent decrease of their operating lifetimes. Particularly when such tubes are placed in closed units for unattended operation it is desirable to have a long tube life in order to reduce the maintenance necessary to an absolute minimum. Thus a maximum amount of heat dissipation from the tube is desirable.
It is one object of this invention to increase the life of thermionic tubes, and particularly such tubes in unattended units.
It is a further object of this invention to increase the heat dissipation from vacuum. tubes without forced air cooling.
It is a still further object of this invention to substantially lower the temperature of the envelope of a thermionic vacuum tube by increas ing the conduction of heat therefrom.
These and other objects of this invention are achieved by positioning a shield of a good heat conducting material around the vacuum tube. A plurality of helically wound springs are arranged within the shield and make contact with the glass envelope of the tube in the region of or opposite the internal elements of the tube. These springs thus have turns extending between the glass envelope of the tube and the inner surface of the shield. Each turn of the helical spring makes a conduction contact with the envelope of the tube, and each such contact is provided with two parallel heat conduction paths to the shield. By Winding the springs fairly tightly a considerable number of such conduction points and paths are provided to conduct heat from the envelope of the tube to the shield. The shield in turn is mounted on a good heat conduction base or mounting chassis to Which the heat is dissipated.
The envelopes of tubes can generally be considered to be cylindrical but actually in the mass production of tubes eccentricities are often introduced so that the envelopes instead of being circular in cross section are more nearly oval or el liptical. Additionally, the temperature attained by the thermionic tube during operation may affect the glass envelope so that it does not retain its form but changes, accentuating the eccentric configuration. Also, in actual mass production the tubes are not all accurately centered on the pins in the base of the tube so that, on being placed in their sockets, the actual positions of the envelopes will vary. However, the springs which provide the conduction paths between the glass envelope and the shield, which of course is and remains always cylindrical, are flexible enough to allow for considerable variations without there beingany loss of contact points with bulb or envelope of the tube.
ihe shield itself serves a dual function as it not only quickly removes the heat of the tube to itself by conduction along the helical springs, in accordance with this invention, but also it acts as an electrostatic and electromagnetic shield, as is Well known and as is generally necessary for many tube applications.
It is therefore afeature of this invention that conduction paths be provided between the glass envelope of a vacuum tube and an outer shield by a helical spring extending around the envelope and making contact therewith at a number of points.
It is a further feature of this invention that the envelope of the vacuum tube depress the inner turns of the helical spring so that considerable variations in the diameter and concentricity of the tube envelope can be accepted without loss of any points of thermal contact with the helical spring.
It is a further feature of this invention that the heat conducting shield surrounding the vacuum tube be mounted on a heat dissipating base and comprise a plurality of helical springs within the shield contacting the inner surface of the shield and contacting the envelope of the vacuum tube at a large number of distinct points. In accordance with this feature, the springs define two parallel heat conduction paths from each of these points to the shield and thus to the heat dissipating base.
A complete understanding of the invention and the various desirable features thereof may be gained from consideration of the following detailed description and accompanying drawing, in which: Fig. 1 is a perspective view of one heat conducting shield illustrative of this invention mounted on a heat dissipating base and with a vacuum tube positioned therein; and
Fig. 2 is a side view of the assembly of Fig. 1, a portion of the shield being broken away to show the helical spring members contacting the envelope of the vacuum tube and the inner surface of the shield.
Referring now to the drawing, the shield 19 may advantageously be a hollow cylinder of slightly larger inner diameter than the outer diameter of the glass envelope of the tube with which it will be employed. It may advantageously be of copper or other good heat conducting material and is supported in good thermal contact with a base II, also advantageously of good heat conducting material, as by an inner ring member I2 having fingers I3 extending upward and clamping ears l4 integral with the shield 10 and extending inward therefrom at its base.
A vacuum tube or other electronic device 16 is mounted in a socket I! supported by the base ll. Metallic conduction of heat away from the envelope of the tube 6 to the shield l and thence to the base II is accomplished by helical springs 20 which are held in shallow grooves 2| around the inner periphery of the shield by wire or snap springs 22. The axes of the helices are thus circles concentric with the cylindrical shield ID. The helical springs and snap springs 22 may advantageously be of steel.
When the vacuum tube I6 is positioned within the shield I0 by being mounted in its socket 11, the envelope of the tube bears against the inner portions of the turns of the helical springs 20 biasing them and thus slightly depresses them. Each turn of each helical spring thus makes contact with the glass envelope of the tube at one contact point and from that contact point two heat conducting paths are provided back to the shield In. A good thermal connection is made between the shield I0 and the turns of the'springs 20 by the relatively long portions of the spring coils held tightly in the grooves 2| by the snap or wire springs 22.
Variations in the initial configuration of the tube envelope, such as lack of concentricity or differences in external diameter, are taken up by the flexible springs 20 which adjust to each particular tube. The differences in tube dimensions will only result in different amounts of depressions of the inner portions of the turns of the helical springs. Similarly, any change in the external configuration of the tube during operation because of the internal generation of heat will be compensated for as the springs follow the variat ons in the envelope without losing any points of contact therewith.
In one specific embodiment of this invention intended for use in a coaxial cable amplifier incorporated in a sealed case and located in isolated and unattended huts, the shield 10 was of .065 inch copper tubing, 1% inches high and 1 /2 inches in diameter, the springs 20 were of .010 inch steel wire helically wound with 20 turns per inch and the snap springs 2| were of .055 inch steel wire. The base II was of copper and attached to the amplifier case so that the amplifier case also dissipated the heat conducted to it from the tube envelopes through the good metallic conduction paths of the springs 2!), the shield I0 and the base i I.
With this specific illustrative embodiment of this invention when employed with amplifier tubes, such as triodes or pentodes, reductions in the temperature of the tube envelope of over 70 C. are easily attained. I
It is to be understood that the above-described arrangements are illustrative of the principles of the invention. Cther arrangements may be devised by those skilled in the art without departing from the spirit and scope of the invention.
What is claimed is: g
Means for conducting heat from the envelope of an electron discharge device to a base member of heat conducting material which dissipates the heat conducted to it from the envelope, comprising a cylindrical shield of heat conducting material attached to and in. thermal contact with said base member and surrounding the device, the inner periphery of said shield having a plurality of circular grooves therein, a plurality of helical springs Within said grooves, the axes of the helices of said springs being circles concentric with said shield, and spring means positioning said helical springs in said grooves in thermal contact with said shield, the turns of said springs away from said shield being depressed by the envelope of the electron discharge device, making contact with said envelope at a plurality of points and defining two parallel heat conductive paths from each of said points to said shield.
FRANK R. DICKINSON.
References Cited in the file of this patent UNITED STATES PATENTS Number Name 7 Date 750,885 Nelson Feb. 2; 904 1,191,191 Kitchen July 18. 1916 1,716,743 Still June 11, 1929 2,443,179 Grandmont et a1. Dec. 24, 1946 2,513,828 Usselman et a1 July 4, 1950 FOREIGN PATENTS 7 Number Country Date 113,331 Great Britain Aug. 21, 1917
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US220952A US2673721A (en) | 1951-04-13 | 1951-04-13 | Apparatus for cooling electron discharge devices |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US220952A US2673721A (en) | 1951-04-13 | 1951-04-13 | Apparatus for cooling electron discharge devices |
Publications (1)
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US2673721A true US2673721A (en) | 1954-03-30 |
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US220952A Expired - Lifetime US2673721A (en) | 1951-04-13 | 1951-04-13 | Apparatus for cooling electron discharge devices |
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Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2861782A (en) * | 1957-01-18 | 1958-11-25 | Swartz Elmer | Holder for electron tubes |
US2866845A (en) * | 1955-06-06 | 1958-12-30 | Ivan K Finney | High voltage insulation mounting |
US2879041A (en) * | 1956-10-15 | 1959-03-24 | Rca Corp | Heat radiator |
US2894177A (en) * | 1953-07-23 | 1959-07-07 | Bendix Aviat Corp | Vacuum tube mounting |
US4457360A (en) * | 1982-08-25 | 1984-07-03 | The Regents Of The University Of California | Multi-lead heat sink |
US5060716A (en) * | 1989-03-31 | 1991-10-29 | Heine William F | Heat dissipating device and combination including same |
US5305824A (en) * | 1993-09-27 | 1994-04-26 | Gasseling John B | Oil filter cooler |
US20060007652A1 (en) * | 2004-07-08 | 2006-01-12 | Yatskov Alexander I | Assemblies for holding heat sinks and other structures in contact with electronic devices and other apparatuses |
US20060146500A1 (en) * | 2004-12-09 | 2006-07-06 | Yatskov Alexander I | Assemblies for holding heat sinks and other structures in contact with electronic devices and other apparatuses |
US20070211428A1 (en) * | 2006-03-08 | 2007-09-13 | Cray Inc. | Multi-stage air movers for cooling computer systems and for other uses |
US20090201644A1 (en) * | 2008-02-11 | 2009-08-13 | Kelley Douglas P | Systems and associated methods for cooling computer components |
US20090244826A1 (en) * | 2008-04-01 | 2009-10-01 | Doll Wade J | Airflow management apparatus for computer cabinets and associated methods |
US20100097752A1 (en) * | 2008-10-17 | 2010-04-22 | Doll Wade J | Airflow intake systems and associated methods for use with computer cabinets |
US20100097751A1 (en) * | 2008-10-17 | 2010-04-22 | Doll Wade J | Air conditioning systems for computer systems and associated methods |
US20100317279A1 (en) * | 2007-12-17 | 2010-12-16 | Yatskov Alexander I | Cooling systems and heat exchangers for cooling computer components |
US8472181B2 (en) | 2010-04-20 | 2013-06-25 | Cray Inc. | Computer cabinets having progressive air velocity cooling systems and associated methods of manufacture and use |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US750885A (en) * | 1904-02-02 | Cooling means for explosive-engines | ||
US1191191A (en) * | 1914-03-18 | 1916-07-18 | Frederick Harcourt Kitchin | Cooling means for internal-combustion engines. |
GB113331A (en) * | 1917-02-23 | 1918-02-21 | Munster Simms And Company Ltd | Improved Air Heater for Internal Combustion Engines. |
US1716743A (en) * | 1926-11-17 | 1929-06-11 | Still William Joseph | Heat-transmitting tube |
US2413179A (en) * | 1943-09-20 | 1946-12-24 | Westinghouse Electric Corp | Radiator |
US2513828A (en) * | 1947-08-28 | 1950-07-04 | Rca Corp | Heat dissipating jacket |
-
1951
- 1951-04-13 US US220952A patent/US2673721A/en not_active Expired - Lifetime
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US750885A (en) * | 1904-02-02 | Cooling means for explosive-engines | ||
US1191191A (en) * | 1914-03-18 | 1916-07-18 | Frederick Harcourt Kitchin | Cooling means for internal-combustion engines. |
GB113331A (en) * | 1917-02-23 | 1918-02-21 | Munster Simms And Company Ltd | Improved Air Heater for Internal Combustion Engines. |
US1716743A (en) * | 1926-11-17 | 1929-06-11 | Still William Joseph | Heat-transmitting tube |
US2413179A (en) * | 1943-09-20 | 1946-12-24 | Westinghouse Electric Corp | Radiator |
US2513828A (en) * | 1947-08-28 | 1950-07-04 | Rca Corp | Heat dissipating jacket |
Cited By (31)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2894177A (en) * | 1953-07-23 | 1959-07-07 | Bendix Aviat Corp | Vacuum tube mounting |
US2866845A (en) * | 1955-06-06 | 1958-12-30 | Ivan K Finney | High voltage insulation mounting |
US2879041A (en) * | 1956-10-15 | 1959-03-24 | Rca Corp | Heat radiator |
US2861782A (en) * | 1957-01-18 | 1958-11-25 | Swartz Elmer | Holder for electron tubes |
US4457360A (en) * | 1982-08-25 | 1984-07-03 | The Regents Of The University Of California | Multi-lead heat sink |
US5060716A (en) * | 1989-03-31 | 1991-10-29 | Heine William F | Heat dissipating device and combination including same |
US5305824A (en) * | 1993-09-27 | 1994-04-26 | Gasseling John B | Oil filter cooler |
US20060007652A1 (en) * | 2004-07-08 | 2006-01-12 | Yatskov Alexander I | Assemblies for holding heat sinks and other structures in contact with electronic devices and other apparatuses |
US7177156B2 (en) | 2004-07-08 | 2007-02-13 | Cray Inc. | Assemblies for holding heat sinks and other structures in contact with electronic devices and other apparatuses |
US20060146500A1 (en) * | 2004-12-09 | 2006-07-06 | Yatskov Alexander I | Assemblies for holding heat sinks and other structures in contact with electronic devices and other apparatuses |
US7193851B2 (en) * | 2004-12-09 | 2007-03-20 | Cray Inc. | Assemblies for holding heat sinks and other structures in contact with electronic devices and other apparatuses |
US7630198B2 (en) | 2006-03-08 | 2009-12-08 | Cray Inc. | Multi-stage air movers for cooling computer systems and for other uses |
US20070211428A1 (en) * | 2006-03-08 | 2007-09-13 | Cray Inc. | Multi-stage air movers for cooling computer systems and for other uses |
US8820395B2 (en) | 2007-12-17 | 2014-09-02 | Cray Inc. | Cooling systems and heat exchangers for cooling computer components |
US20100317279A1 (en) * | 2007-12-17 | 2010-12-16 | Yatskov Alexander I | Cooling systems and heat exchangers for cooling computer components |
US10082845B2 (en) | 2007-12-17 | 2018-09-25 | Cray, Inc. | Cooling systems and heat exchangers for cooling computer components |
US9596789B2 (en) | 2007-12-17 | 2017-03-14 | Cray Inc. | Cooling systems and heat exchangers for cooling computer components |
US9288935B2 (en) | 2007-12-17 | 2016-03-15 | Cray Inc. | Cooling systems and heat exchangers for cooling computer components |
US10588246B2 (en) | 2008-02-11 | 2020-03-10 | Cray, Inc. | Systems and associated methods for controllably cooling computer components |
US20090201644A1 (en) * | 2008-02-11 | 2009-08-13 | Kelley Douglas P | Systems and associated methods for cooling computer components |
US8170724B2 (en) | 2008-02-11 | 2012-05-01 | Cray Inc. | Systems and associated methods for controllably cooling computer components |
US9420729B2 (en) | 2008-02-11 | 2016-08-16 | Cray Inc. | Systems and associated methods for controllably cooling computer components |
US20090244826A1 (en) * | 2008-04-01 | 2009-10-01 | Doll Wade J | Airflow management apparatus for computer cabinets and associated methods |
US7898799B2 (en) | 2008-04-01 | 2011-03-01 | Cray Inc. | Airflow management apparatus for computer cabinets and associated methods |
US20100097751A1 (en) * | 2008-10-17 | 2010-04-22 | Doll Wade J | Air conditioning systems for computer systems and associated methods |
US8537539B2 (en) | 2008-10-17 | 2013-09-17 | Cray Inc. | Air conditioning systems for computer systems and associated methods |
US8081459B2 (en) | 2008-10-17 | 2011-12-20 | Cray Inc. | Air conditioning systems for computer systems and associated methods |
US7903403B2 (en) | 2008-10-17 | 2011-03-08 | Cray Inc. | Airflow intake systems and associated methods for use with computer cabinets |
US20100097752A1 (en) * | 2008-10-17 | 2010-04-22 | Doll Wade J | Airflow intake systems and associated methods for use with computer cabinets |
US9310856B2 (en) | 2010-04-20 | 2016-04-12 | Cray Inc. | Computer cabinets having progressive air velocity cooling systems and associated methods of manufacture and use |
US8472181B2 (en) | 2010-04-20 | 2013-06-25 | Cray Inc. | Computer cabinets having progressive air velocity cooling systems and associated methods of manufacture and use |
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