US3185756A - Heat-dissipating tube shield - Google Patents

Heat-dissipating tube shield Download PDF

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US3185756A
US3185756A US26170A US2617060A US3185756A US 3185756 A US3185756 A US 3185756A US 26170 A US26170 A US 26170A US 2617060 A US2617060 A US 2617060A US 3185756 A US3185756 A US 3185756A
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shield
heat
tube
cylinder
finned
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US26170A
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Donald K Allison
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Cool Fin Electronics Corp
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Cool Fin Electronics Corp
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Priority to GB14114/61A priority patent/GB942837A/en
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    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K7/00Constructional details common to different types of electric apparatus
    • H05K7/20Modifications to facilitate cooling, ventilating, or heating
    • H05K7/2039Modifications to facilitate cooling, ventilating, or heating characterised by the heat transfer by conduction from the heat generating element to a dissipating body
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J19/00Details of vacuum tubes of the types covered by group H01J21/00
    • H01J19/74Cooling arrangements
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J5/00Details relating to vessels or to leading-in conductors common to two or more basic types of discharge tubes or lamps
    • H01J5/02Vessels; Containers; Shields associated therewith; Vacuum locks
    • H01J5/12Double-wall vessels or containers
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K9/00Screening of apparatus or components against electric or magnetic fields
    • H05K9/0007Casings
    • H05K9/002Casings with localised screening
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/4935Heat exchanger or boiler making
    • Y10T29/49377Tube with heat transfer means
    • Y10T29/49378Finned tube

Definitions

  • My invention relates to the electronic art, and more particularly to retentive heat-dissipating electrostatic shields for vacuum tubes, transistors, rectifiers, diodes, and similar electronic components.
  • Retentive tube shields as'hitherto produced and used suffer the defects of inferior heat absorptive and radioactive capabilities, excessive cost, undesirable weight, limited applicability, and inferior electrostatic shielding.
  • Some contemporary shields employ partially effective heat conductive liners which fit between the tube envelope and the JAN-shield to carry the tube heat to the shield and thence to the atmosphere.
  • this construction is the reverse of the ideal design for maximum heat dissipation and shielding, in that the heat must be conducted from the tube envelope to the shield liner (which contacts only a portion of the tube surface), thence through the thin-section metal of the liner to the annular shield (which only incompletely contacts the surface of the liner), and thereafter through the IAN shield to its outer radiative surface, of which the heat-dissipative area is only slightly greater than that of the tube.
  • This design suffers the obvious defects of localized temperature differentials in the tube envelope, which lead to cracks and tube failure; imperfect heat transfer from the tube to the atmosphere; excessive weight; and difficulty of manufacture and use.
  • a still further object of this invention is to provide a heat-dissipating shield structure which is bonded integrally to the tube envelope, and which is provided with means for securely retaining the tube-shield combination in the tube socket under conditions of severe vibration and shock.
  • An additional object of my invention is to provide a heat-dissipating shield which is bonded integrally to the vacuum tube or other electronic component, and which effectively protects the tube or component from mechanical damage.
  • Another important object of my invention is to provide a retentive heat-dissipative shield for vacuum tubes or similar components, which is in the form of a flexible and extensible finned cylinder, and which can be fitted easily to tube envelopes exhibiting considerable variations in diameter, which effectively retains the tube or com- 3,185,756 Patented May 25, 1965 ponent in its socket, and which can be manufactured economically.
  • FIGURE 1 shows a retentive heat-dissipating tube shield constructed in accordance with one embodiment of my invention
  • FIGURE 2 depictsa perspective view of one of the finned elements which in combination form the shield structure shown in FIGURE 1;
  • FIGURE 3 is an end view of the element shown in FIGURE 2;
  • FIGURE 4 illustrates one of the elements which cooperate to form another embodiment of retentive heatdissipating tube shield constructed in accordance with a different form of this invention
  • FIGURE 5 pictures a retentive heat-dissipating tube shield formed by combination of a group of the elements shown in FIGURE 4;
  • FIGURE 6 is a perspective view of a flexible cylindrical retentive tube shield which provides intimate spring contact with the tube envelope, in combination with augmented heat-dissipative surface;
  • FIGURE 7 depicts a sectional view of the retentive tube shield structure depicted in FIGURE 6.
  • a vacuum tube 1 is mounted in a tube socket which includes a terminal plate 2 and a cylindrical skirt 3 whose upper end terminates in an inwardly-formed lip 4.
  • bonded finned shield elements 5, 5, 5", 5", etc. which are formed to such contour that in their combination they effectively surround, shield, and protect the envelope of the vacuum tube 1, including the tube evacuation tip 1a.
  • FIGURES 2 and 3 The configuration of one of the finned shield elements for the cooling and protection of a vacuum tube having the configuration shown in FIGURE 1 is depicted in FIGURES 2 and 3;
  • FIGURE 2 presents a perspective view of one shield element; and
  • FIGURE 3 is anend view of the same element.
  • each shield element is slitted to form a spring tab 6.
  • the spring tabs 6 are formed and positioned, as shown in the figures, in such manner that when the vacuum tube 1 is inserted fully into the tube socket, the plurality of spring tabs engage the inwardly-formed lip 4 of the tube socket skirt 3 and thereby effectively position and retain the vacuum tube in the tube socket under conditions of severe vibration or shock.
  • the shield elements 5, 5, 5", 5", etc. are firmly bonded to the tube envelope by means of a resin, such as one of the epoxy resins, or by an elastomer, such as one of the silicone compounds.
  • a resin such as one of the epoxy resins
  • an elastomer such as one of the silicone compounds.
  • FIGURE 4 we see depicted here a heat-dissipative finned shield element 11", which is formed to that configuration required to enable the shield element to conform to the contours of a vacuum tube 7, as may be seen in FIGURE 5.
  • the lower ends of the shield elements are flared outward as shown, to form an enlarged cylindrical skirt, proportioned to fit snugly over the tube socket skirt 8 of FIGURE 5.
  • the plurality of finned shield elements 11, 11, 11", 11" are shown cut away for the sake of clarity.
  • the plurality of finned shield elements is securely bonded to the tube envelope 7 by a film 9 of heat-transfer bonding agent which, as hereinbefore set forth, may be formed of either rigid or elastomer plastic material.
  • a finned shield 18 includes a substantially cylindrical, longitudinally slotted surface formed by the contiguous arcuate sections 12, 12', 12", etc., which constitute an integral structure with heat-dissipating fins 13, 13, 13", etc. extending outwardly at opposite sides of the slots.
  • the radial flexibility of the structure permits the finned tube 18 to he slipped readily over tubular envelopes, such as those employed for vacuum tubes and similar electronic components, and maintains a constant inward spring force which serves to hold the arcuate sections 12, 12, 12", etc. in intimate contact with the surface of the tubular envelope.
  • FIG- URE 7 depicts a cross-sectional view of a tube envelope 16, enclosed and shielded by the finned shield 18 shown in FIGURE 6.
  • the efiiciency of heat transfer from the tube envelope 16 to the finned shield 18 may be enhanced by coating the inner arcuate surfaces with an elastomer 17.
  • the shield structure depicted in FIGURES 6 and 7 may be formed by hydro-forming, electro-forming, or other techniques well known in the metal-forming art, these echniques forming no part of the present invention.
  • the heat-dissipative shield structure 18 carries a cylindrical skirt 15 having a diameter which enables it to fit closely inside of the cylindrical skirt of the tube socket as hereinbefore described for FIGURE 1.
  • the skirt 15 is slitted and the strips so formed are shaped to provide spring tabs, of which the tab 14 is exemplary.
  • the outwardly-extending portions of the tabs are shaped and positioned in such manner that they lock securely under the inwardly-formed lip of the JAN socket skirt, as hereinbefore described for FIGURE 1.
  • the finned shield element 18 is slipped over a vacuum tube or other electronic component and the combination pressed securely into position in the tube socket.
  • the finned shield provides effective electrostatic shielding, thermal cooling, mechanical protection, and secure retention in the tube socket.
  • a heat dissipating electrical shield for an electronic component comprising: a finned cylinder formed from a continuous sheet of metal and having the outer surfaces of the cylinder and fins free to radiate remotely into the ambient atmosphere, each of said fins being double walled and being formed by two closely adjacent metal surfaces which extend outwardly from a narrow longitudinal slot in the wall of said cylinder and which are integrally connected at their outer ends, said cylindrical shield being thereby provided with radial resiliency whereby said shield is urged to contract; and a heat conducting bonding material between the inner surface of said cylinder and the outer surface of the electronic component to facilitate heat transfer therebetween.
  • a heat dissipating electrical shield for an electronic component comprising: a finned cylinder formed from a continuous sheet of metal and having the outer surfaces of the cylinder and fins free to radiate remotely into the ambient atmosphere, each of said fins being double walled and being formed by two closely adjacent metal surfaces which extend outwardly from a narrow longitudinal slot in the wall of said cylinder and which are integrally connected at their outer ends, said cylindrical shield being thereby provided with radial resiliency whereby said shield is urged to contract; a heat conducting bonding material between the inner surface of said cylinder and the outer surface of the electronic component to facilitate heat transfer therebetween; and retaining means on said shield for securing said shield to the skirt of a socket adapted to receive said component.
  • An electronic component comprising: an envelope of substantially closed-end, cylindrical form enclosing the elements of the component; shield means shaped and dimensioned to enclose both the cylindrical body and free end portion of said envelope in substantially continuous, heat-conductive contact therewith; heat radiative means extending outwardly from said shield means to augment the area thereof and disposed to radiate freely into the ambient atmosphere; and a heat-conductive plastic bond between the inner surface of said shield means and the outer surface of said envelope to increase the heat transfer therebetween and to secure the envelope and shield means together, said shield means having a depending portion interengaging with the skirt of a socket receiving said component in good thermal and electrical conducting relation.

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  • Engineering & Computer Science (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Shielding Devices Or Components To Electric Or Magnetic Fields (AREA)
  • Cooling Or The Like Of Semiconductors Or Solid State Devices (AREA)

Description

y 25, 1955 D. K. ALLISON HEAT-DISSIPATING TUBE SHIELD Filed May 2. 1960 INVENTOR. 004/410 4 444 1504/ zzor/ze a United States Patent 3,185,756 HEAT-DISSIPATING TUBE SHIELD Donald K. Allison, Albuquerque, N. Mex., assignor to Cool Fin Electronics Corporation, Los Angeles, Calif., a corporation of Nevada Filed May 2, 1960, Ser. No. 26,170 4 Claims. (Cl. 174-35) This application is a continuation-in-part of my copending application, Serial No. 814,091, entitled Heat Dissipating Shield, now Patent No. 3,023,264.
My invention relates to the electronic art, and more particularly to retentive heat-dissipating electrostatic shields for vacuum tubes, transistors, rectifiers, diodes, and similar electronic components.
Retentive tube shields as'hitherto produced and used suffer the defects of inferior heat absorptive and radioactive capabilities, excessive cost, undesirable weight, limited applicability, and inferior electrostatic shielding. Some contemporary shields employ partially effective heat conductive liners which fit between the tube envelope and the JAN-shield to carry the tube heat to the shield and thence to the atmosphere. As has been pointed out in my referenced co-pending application, this construction is the reverse of the ideal design for maximum heat dissipation and shielding, in that the heat must be conducted from the tube envelope to the shield liner (which contacts only a portion of the tube surface), thence through the thin-section metal of the liner to the annular shield (which only incompletely contacts the surface of the liner), and thereafter through the IAN shield to its outer radiative surface, of which the heat-dissipative area is only slightly greater than that of the tube. This design suffers the obvious defects of localized temperature differentials in the tube envelope, which lead to cracks and tube failure; imperfect heat transfer from the tube to the atmosphere; excessive weight; and difficulty of manufacture and use.
A further defect encountered in the currently-produced tube shields resides in the fact that these shields require special bases, and therefore cannot be fitted to existing equipment. Although some heat-dissipating shields have been devised which can be used with the standard JAN shielded socket, it has been found that these shields only imperfectly retain the vacuum tube or other component in the socket.
Therefore, it is an object of this invention to provide a retentive heat-dissipative shield structure which offers complete thermal contact of the shield with the tube surface to be cooled, and which in addition offers greatly augmented heat dissipative area.
It is a further object of my invention to provide retentive heat-dissipative shields for electronic elements, which can be produced and sold very economically.
A still further object of this invention is to provide a heat-dissipating shield structure which is bonded integrally to the tube envelope, and which is provided with means for securely retaining the tube-shield combination in the tube socket under conditions of severe vibration and shock.
An additional object of my invention is to provide a heat-dissipating shield which is bonded integrally to the vacuum tube or other electronic component, and which effectively protects the tube or component from mechanical damage.
Another important object of my invention is to provide a retentive heat-dissipative shield for vacuum tubes or similar components, which is in the form of a flexible and extensible finned cylinder, and which can be fitted easily to tube envelopes exhibiting considerable variations in diameter, which effectively retains the tube or com- 3,185,756 Patented May 25, 1965 ponent in its socket, and which can be manufactured economically.
These and other objects and advantages of my invention will be apparent to persons skilled in this art, from the study of the specifications and drawings, in which:
FIGURE 1 shows a retentive heat-dissipating tube shield constructed in accordance with one embodiment of my invention;
FIGURE 2 depictsa perspective view of one of the finned elements which in combination form the shield structure shown in FIGURE 1;
FIGURE 3 is an end view of the element shown in FIGURE 2;
FIGURE 4 illustrates one of the elements which cooperate to form another embodiment of retentive heatdissipating tube shield constructed in accordance with a different form of this invention;
FIGURE 5 pictures a retentive heat-dissipating tube shield formed by combination of a group of the elements shown in FIGURE 4;
FIGURE 6 is a perspective view of a flexible cylindrical retentive tube shield which provides intimate spring contact with the tube envelope, in combination with augmented heat-dissipative surface; and
FIGURE 7 depicts a sectional view of the retentive tube shield structure depicted in FIGURE 6.
Referring now to FIGURE 1, a vacuum tube 1 is mounted in a tube socket which includes a terminal plate 2 and a cylindrical skirt 3 whose upper end terminates in an inwardly-formed lip 4. To the vacuum tube 1 are bonded finned shield elements 5, 5, 5", 5", etc., which are formed to such contour that in their combination they effectively surround, shield, and protect the envelope of the vacuum tube 1, including the tube evacuation tip 1a.
The configuration of one of the finned shield elements for the cooling and protection of a vacuum tube having the configuration shown in FIGURE 1 is depicted in FIGURES 2 and 3; FIGURE 2 presents a perspective view of one shield element; and FIGURE 3 is anend view of the same element.
As is shown in FIGURES l, 2 and 3, the lower portion of each shield element is slitted to form a spring tab 6.
The spring tabs 6 are formed and positioned, as shown in the figures, in such manner that when the vacuum tube 1 is inserted fully into the tube socket, the plurality of spring tabs engage the inwardly-formed lip 4 of the tube socket skirt 3 and thereby effectively position and retain the vacuum tube in the tube socket under conditions of severe vibration or shock.
As has been hereinbefore stated, the shield elements 5, 5, 5", 5", etc., are firmly bonded to the tube envelope by means of a resin, such as one of the epoxy resins, or by an elastomer, such as one of the silicone compounds. These substances are cited only as examples, and it is to be understood that many other bonding agents may be used for this purpose. I have found thatthe rate of heat absorption from the tube envelope, and the rate of heat conduction through the bonding agent to the finned shield, are greatly increased by the addition of a heat absorptive substance, such as carbon black or colloidal graphite, to the bonding resin or elastomer.
Referring now to FIGURE 4, we see depicted here a heat-dissipative finned shield element 11", which is formed to that configuration required to enable the shield element to conform to the contours of a vacuum tube 7, as may be seen in FIGURE 5. The lower ends of the shield elements are flared outward as shown, to form an enlarged cylindrical skirt, proportioned to fit snugly over the tube socket skirt 8 of FIGURE 5. As is shown in FIGURE 5, the plurality of finned shield elements 11, 11, 11", 11" (here shown cut away for the sake of clarity), are
provided with outwardly-formed grooves 10, in the shape of an inverted L, which fit over, and retentivcly lock to a pin 8a (and its diametric counterpart).
As shown in FIGURE 5, the plurality of finned shield elements is securely bonded to the tube envelope 7 by a film 9 of heat-transfer bonding agent which, as hereinbefore set forth, may be formed of either rigid or elastomer plastic material.
Referring now to FIGURES 6 and 7, a finned shield 18 includes a substantially cylindrical, longitudinally slotted surface formed by the contiguous arcuate sections 12, 12', 12", etc., which constitute an integral structure with heat-dissipating fins 13, 13, 13", etc. extending outwardly at opposite sides of the slots. The radial flexibility of the structure permits the finned tube 18 to he slipped readily over tubular envelopes, such as those employed for vacuum tubes and similar electronic components, and maintains a constant inward spring force which serves to hold the arcuate sections 12, 12, 12", etc. in intimate contact with the surface of the tubular envelope. FIG- URE 7 depicts a cross-sectional view of a tube envelope 16, enclosed and shielded by the finned shield 18 shown in FIGURE 6. The efiiciency of heat transfer from the tube envelope 16 to the finned shield 18 may be enhanced by coating the inner arcuate surfaces with an elastomer 17.
The shield structure depicted in FIGURES 6 and 7 may be formed by hydro-forming, electro-forming, or other techniques well known in the metal-forming art, these echniques forming no part of the present invention.
The heat-dissipative shield structure 18 carries a cylindrical skirt 15 having a diameter which enables it to fit closely inside of the cylindrical skirt of the tube socket as hereinbefore described for FIGURE 1. As likewise hereinbefore described in connection with FIGURES l and 2, the skirt 15 is slitted and the strips so formed are shaped to provide spring tabs, of which the tab 14 is exemplary. The outwardly-extending portions of the tabs are shaped and positioned in such manner that they lock securely under the inwardly-formed lip of the JAN socket skirt, as hereinbefore described for FIGURE 1.
In use, the finned shield element 18 is slipped over a vacuum tube or other electronic component and the combination pressed securely into position in the tube socket. The finned shield provides effective electrostatic shielding, thermal cooling, mechanical protection, and secure retention in the tube socket.
The foregoing forms of my invention are cited as exemplary only. Other embodiments of my invention will be apparent to those skilled in the art, and it is my intent that all such modified forms of this invention be included in the scope of the appended claims.
I claim:
1. A heat dissipating electrical shield for an electronic component comprising: a finned cylinder formed from a continuous sheet of metal and having the outer surfaces of the cylinder and fins free to radiate remotely into the ambient atmosphere, each of said fins being double walled and being formed by two closely adjacent metal surfaces which extend outwardly from a narrow longitudinal slot in the wall of said cylinder and which are integrally connected at their outer ends, said cylindrical shield being thereby provided with radial resiliency whereby said shield is urged to contract; and a heat conducting bonding material between the inner surface of said cylinder and the outer surface of the electronic component to facilitate heat transfer therebetween.
2. A heat dissipating electrical shield for an electronic component comprising: a finned cylinder formed from a continuous sheet of metal and having the outer surfaces of the cylinder and fins free to radiate remotely into the ambient atmosphere, each of said fins being double walled and being formed by two closely adjacent metal surfaces which extend outwardly from a narrow longitudinal slot in the wall of said cylinder and which are integrally connected at their outer ends, said cylindrical shield being thereby provided with radial resiliency whereby said shield is urged to contract; a heat conducting bonding material between the inner surface of said cylinder and the outer surface of the electronic component to facilitate heat transfer therebetween; and retaining means on said shield for securing said shield to the skirt of a socket adapted to receive said component.
3. An electronic component comprising: an envelope of substantially closed-end, cylindrical form enclosing the elements of the component; shield means shaped and dimensioned to enclose both the cylindrical body and free end portion of said envelope in substantially continuous, heat-conductive contact therewith; heat radiative means extending outwardly from said shield means to augment the area thereof and disposed to radiate freely into the ambient atmosphere; and a heat-conductive plastic bond between the inner surface of said shield means and the outer surface of said envelope to increase the heat transfer therebetween and to secure the envelope and shield means together, said shield means having a depending portion interengaging with the skirt of a socket receiving said component in good thermal and electrical conducting relation.
4. The electronic component defined in claim 3 in which said heat-conductive plastic bond is formed by an epoxy resin containing carbon black to improve the heat conductivity thereof.
References Cited in the file of this patent UNITED STATES PATENTS 2,653,800 Anton Sept. 29, 1953 2,711,382 Smith-Johannsen June 21, 1955 2,745,895 Lideen May 15, 1956 2,799,793 De Cain July 16, 1957 2,829,870 Poppe Apr. 8, 1958 2,859,383 Woods Nov. 4, 1958 2,862,991 Reardon Dec. 2, 1958 2,872,502 Ross Feb. 3, 1959 2,893,704 Passman July 7, 1959 2,905,742 Woods Sept. 22, 1959 3,023,264 Allison Feb. 27, 1962

Claims (1)

1. A HEAT DISSIPATING ELECTRICAL SHIELD FOR AN ELECTRONIC COMPONENT COMPRISING: A FINNED CYLINDER FORMED FROM A CONTINUOUS SHEET OF METAL AND HAVING THE OUTER SURFACES OF THE CYLINDER AND FINS FREE TO RADIATE REMOTELY INTO THE AMBIENT ATMOSPHERE, EACH OF SAID FINS BEING DOUBLE WALLED AND BEING FORMED BY TWO CLOSELY ADJACENT METAL SURFACES WHICH EXTEND OUTWARDLY FROM A NARROW LONGITUDINAL SLOT IN THE WALL OF SAID CYLINDER AND WHICH ARE INTEGRALLY CONNECTED AT THEIR OUTER ENDS, SAID CYINDRICAL SHIELD BEING THEREBY PROVIDED WITH RADIAL RESILIENCY WHEREBY SAID SHIELD IS URGED TO CONTRACT; AND A HEAT CONDUCTING BONDING MATERIAL BETWEEN THE INNER SURFACE OF SAID CYLINDER AND THE OUTER SURFACE OF THE ELECTRONIC COMPONENT TO FACILITATE HEAT TRANSFER THEREBETWEEN.
US26170A 1960-05-02 1960-05-02 Heat-dissipating tube shield Expired - Lifetime US3185756A (en)

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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3260787A (en) * 1962-12-20 1966-07-12 Birtcher Corp Transistor heat dissipators
US3472944A (en) * 1966-05-20 1969-10-14 Imp Metal Ind Kynoch Ltd Assemblies of superconductor elements
US3868754A (en) * 1973-09-21 1975-03-04 Hatsuo Kawano Method of manufacturing a finned-tube heat exchanger
US6330908B1 (en) * 2000-03-15 2001-12-18 Foxconn Precision Components Co., Ltd. Heat sink
US6557626B1 (en) 2000-01-11 2003-05-06 Molex Incorporated Heat sink retainer and Heat sink assembly using same
US6830097B2 (en) 2002-09-27 2004-12-14 Modine Manufacturing Company Combination tower and serpentine fin heat sink device
US6851467B1 (en) * 1999-08-30 2005-02-08 Molex Incorporated Heat sink assembly
US20060011324A1 (en) * 2004-07-13 2006-01-19 Rogers C J Wound, louvered fin heat sink device

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* Cited by examiner, † Cited by third party
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JPS58187916A (en) * 1982-04-28 1983-11-02 West Electric Co Ltd Ultrasonic distance measuring device
GB2157077B (en) * 1984-04-05 1987-10-21 Burr Brown Corp Heat sinks for minimizing noise in precision electronic components
FR2818789A1 (en) * 2000-12-21 2002-06-28 Thomson Tubes Electroniques Cooling equipment for electronic components, comprises inner set of radial cooling fins, intermediate supporting cylinder and outer set of radial cooling fins with smaller angular spacing

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US2653800A (en) * 1950-10-23 1953-09-29 Anton Nicholas Electron tube heat-dissipating radiator and method of fabricating same
US2711382A (en) * 1951-02-08 1955-06-21 Gen Electric Method of forming and applying metal heat exchange fins
US2745895A (en) * 1951-06-09 1956-05-15 Ernest J Lideen Vacuum tube shield and heat radiator
US2799793A (en) * 1952-10-31 1957-07-16 Gen Precision Lab Inc Electronic tube shield
US2829870A (en) * 1954-07-14 1958-04-08 Int Standard Electric Corp Thermoconductive screening can for electronic tube
US2859383A (en) * 1954-02-17 1958-11-04 Int Electronic Res Corp Thermal conducting tube shield
US2862991A (en) * 1954-12-10 1958-12-02 Zenith Radio Corp Tube shield
US2872502A (en) * 1956-07-13 1959-02-03 Robert E Ross Tube shield
US2893704A (en) * 1957-05-20 1959-07-07 Collins Radio Co Cooling system
US2905742A (en) * 1956-02-06 1959-09-22 Int Electronic Res Corp Shield for electronic components
US3023264A (en) * 1959-05-18 1962-02-27 Cool Fin Electronics Corp Heat-dissipating shield

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2653800A (en) * 1950-10-23 1953-09-29 Anton Nicholas Electron tube heat-dissipating radiator and method of fabricating same
US2711382A (en) * 1951-02-08 1955-06-21 Gen Electric Method of forming and applying metal heat exchange fins
US2745895A (en) * 1951-06-09 1956-05-15 Ernest J Lideen Vacuum tube shield and heat radiator
US2799793A (en) * 1952-10-31 1957-07-16 Gen Precision Lab Inc Electronic tube shield
US2859383A (en) * 1954-02-17 1958-11-04 Int Electronic Res Corp Thermal conducting tube shield
US2829870A (en) * 1954-07-14 1958-04-08 Int Standard Electric Corp Thermoconductive screening can for electronic tube
US2862991A (en) * 1954-12-10 1958-12-02 Zenith Radio Corp Tube shield
US2905742A (en) * 1956-02-06 1959-09-22 Int Electronic Res Corp Shield for electronic components
US2872502A (en) * 1956-07-13 1959-02-03 Robert E Ross Tube shield
US2893704A (en) * 1957-05-20 1959-07-07 Collins Radio Co Cooling system
US3023264A (en) * 1959-05-18 1962-02-27 Cool Fin Electronics Corp Heat-dissipating shield

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3260787A (en) * 1962-12-20 1966-07-12 Birtcher Corp Transistor heat dissipators
US3472944A (en) * 1966-05-20 1969-10-14 Imp Metal Ind Kynoch Ltd Assemblies of superconductor elements
US3868754A (en) * 1973-09-21 1975-03-04 Hatsuo Kawano Method of manufacturing a finned-tube heat exchanger
US6851467B1 (en) * 1999-08-30 2005-02-08 Molex Incorporated Heat sink assembly
US6557626B1 (en) 2000-01-11 2003-05-06 Molex Incorporated Heat sink retainer and Heat sink assembly using same
US6330908B1 (en) * 2000-03-15 2001-12-18 Foxconn Precision Components Co., Ltd. Heat sink
US6830097B2 (en) 2002-09-27 2004-12-14 Modine Manufacturing Company Combination tower and serpentine fin heat sink device
US20060011324A1 (en) * 2004-07-13 2006-01-19 Rogers C J Wound, louvered fin heat sink device

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