US3624899A - Method of making vacuum fuse - Google Patents

Method of making vacuum fuse Download PDF

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US3624899A
US3624899A US871260A US3624899DA US3624899A US 3624899 A US3624899 A US 3624899A US 871260 A US871260 A US 871260A US 3624899D A US3624899D A US 3624899DA US 3624899 A US3624899 A US 3624899A
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fusible element
fuse
vacuum
envelope
temperature
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Sidney R Smith Jr
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General Electric Co
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General Electric Co
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01HELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
    • H01H85/00Protective devices in which the current flows through a part of fusible material and this current is interrupted by displacement of the fusible material when this current becomes excessive
    • H01H85/02Details
    • H01H85/04Fuses, i.e. expendable parts of the protective device, e.g. cartridges
    • H01H85/041Fuses, i.e. expendable parts of the protective device, e.g. cartridges characterised by the type
    • H01H85/047Vacuum fuses
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01HELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
    • H01H85/00Protective devices in which the current flows through a part of fusible material and this current is interrupted by displacement of the fusible material when this current becomes excessive
    • H01H85/02Details
    • H01H85/36Means for applying mechanical tension to fusible member
    • 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
    • Y10T29/49002Electrical device making
    • Y10T29/49107Fuse making

Definitions

  • the stressing force of the spring is correlated with the tensile strength and thermal characteristics of the fusible element so that this force pulls the fusible element apart when the elements tensile strength is reduced, by the heating effect of overcurrent through the fuse, to a predetermined temperature level.
  • the predetermined tempearture level at which such rupture and subsequent fusion of the fusible element occurs is substantially lower than the temperature of fusion of the element when it is not stressed.
  • This invention relates to vacuum fuses and, more particularly, to a method for making such fuses in a manner such that they can be subjected to relatively high temperatures during their manufacturing cycle without fusing, and still be adapted to provide a relatively slow timecurrent characteristic.
  • vacuum fuse operating characteristics recommend their use in many applications, the cost of manufacturing vacuum fuses by many prior art manufacturing processes is often so great that it prohibits their utilization.
  • manufacturing methods are known by which vacuum fuses can be reliably produced at a more reasonable cost, but with a sacrifice in fuse operating characteristics.
  • these relatively inexpensive methods of producing vacuum fuses rely on a combination of gettering materials and reducing gas atmospheres during controlled-temperature manufacturing cycles to form the desired vacuums.
  • one such manufacturing method is disclosed in U.S. Pat. 2,934,392, De Santis et al., issued Apr. 26, 1960 and assigned to the assignee of the present invention.
  • the temperature cycles utilized necessarliy subject the fusible element of the fuse to relatively high temperatures, which are determined by the characteristics of the gettering material utilized as well as by the temperature required to hermetically seal the evacuated envelope being formed by brazing it.
  • relatively high temperature levels during the manufacturing process makes it necessary to provide the fuse being formed with a fusible element which has a temperature of fusion somewhat above the maximum temperature reached during the manufacturing process. Therefore, although relatively inexpensive vacuum fuses can be manufactured with such a pumpless process, the necessarily high temperature of fusion of their fusible elements has heretofore restricted their use to applications that require fast circuit interruption in response to relatively high overcurrents.
  • a major advantage of my invention is that it overcomes the above mentioned problems inherent in prior art vac- Patented Dec. 7, 1971 uum fuses by providing an inexpensively manufactured vacuum fuse that has a relatively slow time-current characteristic.
  • vacuum fuses constructed pursuant to the teaching of my invention provide all of the advantages inherent in presently known vacuum fuses while at the same time incorporating operating characteristics which enable them to be utilized to protect circuits against damage due to low, sustained overcurrents.
  • a vacuum fuse having a thermal-responsive fusible element is provided with spring means coupled to the fusible element to place it under tension.
  • the spring means serves to pull the fusible element apart and initiate its fusion when it is subjected to a predetermined temperature that reduces the tensile strength of the fusible element.
  • the tensioning force of the spring is correlated with the thermal and mechanical properties of the fusible element so that the predetermined temperature at which mechanical rupture is effected is substantially less than the temperature required to fuse the element in its unstressed condition.
  • spring tension is applied to stress the fusible element only after the element has been scaled within an evacuated envelope by a heating cycle that may raise the temperature of the envelope to a level approaching the temperature of fusion of the fusible element in its unstressed state.
  • a vacuum fuse having a tubular insulating housing 1 which may be formed of alumina or other suitable impervious material.
  • Metallic terminals '2 and 2 are sealed to opposite ends of the housing 1 by a process that will be described further below.
  • terminal 2 includes a cylindrically shaped housing 4 that is fastened to the end cap 3 by welding it thereto.
  • one end of a metal bellows 5 is sealed in vacuumtight relation to the end cap 3 and the other end of the bellows S is sealed in vacuum-tight relation to the stem portion 6 of an electrode 7.
  • the vacuumtight seal between the end cap 3 and metal bellows 5 can be formed by welding these members together around the circumference of an aperture 3a formed through the center of the end cap 3 to provide a passageway for the electrode stem 6, as will be more fully described below.
  • a plate member 8 is first welded to the stem 6 and then the lower end of the bellows 5 is welded to the outer peripheral edge of the plate member 8. It will be seen that with this arrangement the terminal 2, which includes the end cap 3, the bellows 5, the electrode 7 with its stem portion 6, and plate member 8, serves to form a vacuum-tight seal between the housing 1 around the aperture 3a in end cap 3.
  • a second electrode 9, having a stem portion 10, is electrically and mechanically fastened to the center of end cap .2' by being brazed thereto.
  • An electric circuit is completed between the electrodes 7 and 9 by a thin fusible element 11, which may be a wire formed of a su table silver-tin alloy, or other suitable alloy. It will be understood that the dimensions of the fusible element 111, as well as its specific composition, will normally be determined by the time-current rating that the fuse is designed to provide. However, as is more fully discussed below, other considerations such as manufacturing temperature parameters, will necessarily influence the selection of a suitable fusible element 11.
  • Electrodes 7 and 9 may be of any desired configuration; however, in order to maintain the length of the fusible element 11 relatively short, the electrodes 7 and 9 are formed so that they may be spaced quite close to one another. At the same time, the mass of the electrodes 7 and 9 is kept large with respect to the mass of the fusible element 11, so that the electrodes 7 and 9 act as heat sinks for the fusible element 11 and, thus, make it possible to further shorten the length of the fusible element 11 without increasing its mechanical dimensions or tensile strength.
  • the fusible element 11 may be fastened to electrodes 7 and 9 in any suitable fashion, but in the preferred form of my invention the electrodes 7 and 9, and their associated stem portions 6 and 10 are slitted so that the opposite ends of fusible element 11 may be inserted, respectively, into the slits, as shown in the drawing at 11a and 11b.
  • the slitted ends of electrodes 7 and 9 are then clamped to the ends of the fusible element 11 by any conventional crimping process to form a strong mechanical and electrical connection therewith.
  • the fusible element 11 is mechanically loaded, to place it in tensile stress, by a coiled spring 12 that is compressed between the cylindrical portion 4 of terminal 2 and a retainer cap 13.
  • the cap 13 is provided with a threaded bore 14, which is adapted to be threaded on the end 6a of the stem portion 6 on electrode 7.
  • the characteristics of spring 12 are correlated with the tensile strength and thermal properties of the fusible element 11, so that the biasing force exerted by the spring 12 on the fusible element 11 will cause it to be pulled apart at a temperature substantially below its temperature of fusion, when the fusible element 11 is subjected to a predetermined temperature level that causes it to be softened sufficiently to reduce its tensile strength. Accordingly, by thus spring loading the fusible element 11, the time-current characteristic of the fuse is substantially improved; therefore, the fuse can be used to protect circuits against much slower temperature rises than vacuum fuses have heretofore been capable of satisfactorily protecting.
  • a retaining dish 15 is also aflixed to the stem 6 in any suitable manner, such as by brai ing, and a disc of titanium hydride 16 is placed in the dish 15.
  • the terminal 2 and the electrodes 7 and 9 assembled therewith are then positioned in the tubular housing 1 and the terminal 2' is brazed to the end of stem 10 on electrode 9. Since I prefer to use the purnpless method of evacuating articles which is described in United States Patent No.
  • the next step in my method of manufacture after the envelope has cooled to a suitable temperature is to mount the coil spring 12 in the cylinder 4 and compress it between the cup-shaped end cap 13, which is then rotatably threaded on the threaded end 6a at the end of stem portion 6 of the electrode 7.
  • the fusible element 11 is mechanically loaded under a predetermined mechanical stress by the compression force of coil spring 12. It will be apparent to those skilled in the art that the degree of tension force applied to the fusible element 11 can be finely adjusted by varying the degree of compression of the spring 12 which is determined by rotating it on. its thread mounting 6a closer to, or further from, the end cap 3.
  • the metal bellows and the coil spring 12 need only supply enough reciprocal motion to the electrode 7 to draw it far enough away from the electrode 9 to rupture the fusible element 11 when it is softened by being raised to a predetermined temperature level somewhat below its normal temperature of fusion.
  • the bellows 5 and spring 12 in the preferred form of my invention are adapted to move the electrodes 7 and 9 away from each other far enough so that the dielectric strength of the vacuum in the envelope is sufficient to interrupt the circuit (following a zero voltage cycle) even if the ends of fusible element 11 are not completely burned back by the relatively lowcurrent are drawn between them after the mechanical rupture of element 11. 4
  • the method for making a fuse means comprising the sequential steps of: (1) providing a fuse envelope having a fusible element therein and having means for electrically connecting said element to a source of electric current, (2) evacuating and sealing said envelope, and (3) mechanically loading said fusible element thereby to apply a predetermined mechanical stress to it that is eifective to cause said element to break and fuse at a temperature below the fusion temperature of said element in its unstressed condition.

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  • Fuses (AREA)

Abstract

A VACUUM FUSE MANUFACTURED BY SEALING A FUSIBLE ELEMENT WITHIN AN EVACUATED ENVELOPE WHILE THE ENVELOPE IS SUBJECTED TO A RELATIVELY HIGH TEMPERATURE. SUBSEQUENT TO THE SEALING OPERATION, THE FUSIBLE ELEMENT IS MECHANICALLY STRESSED BY A COIL SPRING. THE STRESSING FORCE OF THE SPRING IS CORRELATED WITH THE TENSILE STRENGTH AND THERMAL CHARACTERISTICS OF THE FUSIBLE ELEMENT SO THAT THIS FORCE PULLS THE FUSIBLE ELEMENT APART WHEN THE ELEMENT''S TENSILE STRENGTH IS REDUCED, BY THE HEATING EFFECT OF OVERCURRENT THROUGH THE FUSE, TO A PREDETERMINED TEMPERATURE LEVEL, THE PREDETERMINED TEMPERATURE LEVEL AT WHICH SUCH RUPTURE AND SUBSEQUENT FUSION OF THE FUSIBLE ELEMENT OCCURS IS SUBSTANTIALLY LOWER THAN THE TEMPERATURE OF FUSION OF THE ELEMENT WHEN IT IS NOT STRESSED.

Description

United States Patent 3,624,899 METHOD OF MAKING VACUUM FUSE Sidney R. Smith, Jr., Myrtle Beach, S.C., assignor to General Electric Company Original application Apr. 24, 1968, Ser. No. 723,695, new Patent No. 3,510,819, dated May 5, 1970. Divided and this application Nov. 6, 1969, Ser. No. 871,260 Int. Cl. H01h 69/02 U.S. Cl. 29--623 2 Claims ABSTRACT OF THE DISCLOSURE A vacuum fuse manufactured by sealing a fusible element within an evacuated envelope while the envelope is subjected to a relatively high temperature. Subsequent to the sealing operation, the fusible element is mechanically stressed by a coil spring. The stressing force of the spring is correlated with the tensile strength and thermal characteristics of the fusible element so that this force pulls the fusible element apart when the elements tensile strength is reduced, by the heating effect of overcurrent through the fuse, to a predetermined temperature level. The predetermined tempearture level at which such rupture and subsequent fusion of the fusible element occurs is substantially lower than the temperature of fusion of the element when it is not stressed.
This is a division of application, Ser. No. 723,695, filed Apr. 24, 1968, now Pat. No. 3,510,819, which is assigned to the same assignee as this present application.
This invention relates to vacuum fuses and, more particularly, to a method for making such fuses in a manner such that they can be subjected to relatively high temperatures during their manufacturing cycle without fusing, and still be adapted to provide a relatively slow timecurrent characteristic.
Although vacuum fuse operating characteristics recommend their use in many applications, the cost of manufacturing vacuum fuses by many prior art manufacturing processes is often so great that it prohibits their utilization. On the other hand, manufacturing methods are known by which vacuum fuses can be reliably produced at a more reasonable cost, but with a sacrifice in fuse operating characteristics. In general, these relatively inexpensive methods of producing vacuum fuses rely on a combination of gettering materials and reducing gas atmospheres during controlled-temperature manufacturing cycles to form the desired vacuums. For example, one such manufacturing method is disclosed in U.S. Pat. 2,934,392, De Santis et al., issued Apr. 26, 1960 and assigned to the assignee of the present invention. In a pumpless process such as that taught in this patent, the temperature cycles utilized necessarliy subject the fusible element of the fuse to relatively high temperatures, which are determined by the characteristics of the gettering material utilized as well as by the temperature required to hermetically seal the evacuated envelope being formed by brazing it. The presence of such high temperature levels during the manufacturing process makes it necessary to provide the fuse being formed with a fusible element which has a temperature of fusion somewhat above the maximum temperature reached during the manufacturing process. Therefore, although relatively inexpensive vacuum fuses can be manufactured with such a pumpless process, the necessarily high temperature of fusion of their fusible elements has heretofore restricted their use to applications that require fast circuit interruption in response to relatively high overcurrents.
A major advantage of my invention is that it overcomes the above mentioned problems inherent in prior art vac- Patented Dec. 7, 1971 uum fuses by providing an inexpensively manufactured vacuum fuse that has a relatively slow time-current characteristic. Thus, vacuum fuses constructed pursuant to the teaching of my invention provide all of the advantages inherent in presently known vacuum fuses while at the same time incorporating operating characteristics which enable them to be utilized to protect circuits against damage due to low, sustained overcurrents.
Briefly stated, in one form of my invention a vacuum fuse having a thermal-responsive fusible element is provided with spring means coupled to the fusible element to place it under tension. The spring means serves to pull the fusible element apart and initiate its fusion when it is subjected to a predetermined temperature that reduces the tensile strength of the fusible element. The tensioning force of the spring is correlated with the thermal and mechanical properties of the fusible element so that the predetermined temperature at which mechanical rupture is effected is substantially less than the temperature required to fuse the element in its unstressed condition. In manufacturing fuses pursuant to the teaching of my invention, spring tension is applied to stress the fusible element only after the element has been scaled within an evacuated envelope by a heating cycle that may raise the temperature of the envelope to a level approaching the temperature of fusion of the fusible element in its unstressed state.
Further features and advantages of the invention will become apparent from the following description of the preferred embodiment thereof and from the accompanying drawing, the single figure of which is a side elevation, in cross section of a vacuum fuse embodying a preferred form of the invention.
Referring now to the drawing, there is shown a vacuum fuse having a tubular insulating housing 1 which may be formed of alumina or other suitable impervious material. Metallic terminals '2 and 2 are sealed to opposite ends of the housing 1 by a process that will be described further below. In addition to its sealed end cap portion 3, terminal 2 includes a cylindrically shaped housing 4 that is fastened to the end cap 3 by welding it thereto. On the opposite side, or bottom surface of the end cap portion 3, one end of a metal bellows 5 is sealed in vacuumtight relation to the end cap 3 and the other end of the bellows S is sealed in vacuum-tight relation to the stem portion 6 of an electrode 7. I have found that the vacuumtight seal between the end cap 3 and metal bellows 5 can be formed by welding these members together around the circumference of an aperture 3a formed through the center of the end cap 3 to provide a passageway for the electrode stem 6, as will be more fully described below. In order to form a vacuum-tight seal between the metallic bellows 5 and the stem 6 of electrode 7 in the preferred embodiment of my invention, a plate member 8 is first welded to the stem 6 and then the lower end of the bellows 5 is welded to the outer peripheral edge of the plate member 8. It will be seen that with this arrangement the terminal 2, which includes the end cap 3, the bellows 5, the electrode 7 with its stem portion 6, and plate member 8, serves to form a vacuum-tight seal between the housing 1 around the aperture 3a in end cap 3.
A second electrode 9, having a stem portion 10, is electrically and mechanically fastened to the center of end cap .2' by being brazed thereto. An electric circuit is completed between the electrodes 7 and 9 by a thin fusible element 11, which may be a wire formed of a su table silver-tin alloy, or other suitable alloy. It will be understood that the dimensions of the fusible element 111, as well as its specific composition, will normally be determined by the time-current rating that the fuse is designed to provide. However, as is more fully discussed below, other considerations such as manufacturing temperature parameters, will necessarily influence the selection of a suitable fusible element 11.
Electrodes 7 and 9 may be of any desired configuration; however, in order to maintain the length of the fusible element 11 relatively short, the electrodes 7 and 9 are formed so that they may be spaced quite close to one another. At the same time, the mass of the electrodes 7 and 9 is kept large with respect to the mass of the fusible element 11, so that the electrodes 7 and 9 act as heat sinks for the fusible element 11 and, thus, make it possible to further shorten the length of the fusible element 11 without increasing its mechanical dimensions or tensile strength. Accordingly, when the fusible element 11 is subject to an overcurrent are it vaporizes completely and almost instantaneously a very high dielectric is inserted into the circuit between the electrodes 7 and 9 by the substitution of the hard vacuum for the fusible element 11 in the fuse circuit. This simultaneous fusing and intro duction of a strong dielectric into the circuit causes the fuse to interrupt the overcurent which was flowing in the circuit, at the first current zero.
It will be understood that the fusible element 11 may be fastened to electrodes 7 and 9 in any suitable fashion, but in the preferred form of my invention the electrodes 7 and 9, and their associated stem portions 6 and 10 are slitted so that the opposite ends of fusible element 11 may be inserted, respectively, into the slits, as shown in the drawing at 11a and 11b. The slitted ends of electrodes 7 and 9 are then clamped to the ends of the fusible element 11 by any conventional crimping process to form a strong mechanical and electrical connection therewith. Pursuant to the teaching of my invention, the fusible element 11 is mechanically loaded, to place it in tensile stress, by a coiled spring 12 that is compressed between the cylindrical portion 4 of terminal 2 and a retainer cap 13. The cap 13 is provided with a threaded bore 14, which is adapted to be threaded on the end 6a of the stem portion 6 on electrode 7. When the fusible element 11 is in its unfused condition, as shown in the drawing, it retains the spring 12 in a compressed position so that the spring biases the electrodes 7 and 10 to move away from one another.
The characteristics of spring 12 are correlated with the tensile strength and thermal properties of the fusible element 11, so that the biasing force exerted by the spring 12 on the fusible element 11 will cause it to be pulled apart at a temperature substantially below its temperature of fusion, when the fusible element 11 is subjected to a predetermined temperature level that causes it to be softened sufficiently to reduce its tensile strength. Accordingly, by thus spring loading the fusible element 11, the time-current characteristic of the fuse is substantially improved; therefore, the fuse can be used to protect circuits against much slower temperature rises than vacuum fuses have heretofore been capable of satisfactorily protecting.
In manufacturing a fuse according to the teaching of my invention, I have found the following method of manufacture affords a reliable, high quality vacuum fuse at a minimum cost of manufacture. The fusible element 11 is first clamped between the electrodes 7 and 9, then the plate member 8 is welded to the stem 6 of electrode 7, and bellows and end cap 3 are, in turn, welded together as noted above. The cylindrical portion 4 of terminal 2 may be welded to end cap 3 in a separate operation or simultaneously with the welding operation that seals the bellows 5 to the end cap 3, as is done in the preferred practice of my method of manufacture. After plate member 8 is welded to stem 6, a retaining dish 15 is also aflixed to the stem 6 in any suitable manner, such as by brai ing, and a disc of titanium hydride 16 is placed in the dish 15. The terminal 2 and the electrodes 7 and 9 assembled therewith are then positioned in the tubular housing 1 and the terminal 2' is brazed to the end of stem 10 on electrode 9. Since I prefer to use the purnpless method of evacuating articles which is described in United States Patent No. 2,934,392 De S'antis et al., issued April 26, 1 960 and assigned to the assignee of the present invention, to form a vacuum in the envelope defined by the housing 1 and terminals 2 and 2', suitable solder washers 17 and 18 are mounted, respectively, between terminals '2 and 2' and the ends of housing 1. The envelope is then heated to a temperature range between approximately 780 degrees centigrade and 1000 degrees centigrade, dependent on the braze alloy used, and maintained in that range for approximately ten minutes while the envelope is flushed with a hydrogen atmosphere so that the pre-existing atmosphere in the envelope is reduced to substantially pure hydrogen and the titanium hydride disc 16 desorbs most of its hydrogen. As the temperature level increases from 780 degrees centigrade toward 1000 degrees centigrade, after about four or five minutes the solder washers 17 and 18 melt and form a vacuum-tight seal between the terminals 2 and 2' and the tubular housing 1. When these vacuum-tight seals are formed, the envelope is allowed to cool, and during this cooling process the titanium hydride disc 16 sorbs substantially all of the gases remaining in the envleope to develop a hard vacuum therein. This vacuum-forming step of my manufacturing process is more fully described in the above-referenced patent, including alternative methods for practicing this portion of the process. The important point to note with regard to my method of manufacture is that the thermal characteristics of fusible element 11 must be such that the element 11 does not fuse during the manufacturing process when it is subjected to the high temperatures required by the out-gasing and envelope sealing steps of the vacuum developing process.
Following the formation of the evacuated envelope, the next step in my method of manufacture after the envelope has cooled to a suitable temperature, is to mount the coil spring 12 in the cylinder 4 and compress it between the cup-shaped end cap 13, which is then rotatably threaded on the threaded end 6a at the end of stem portion 6 of the electrode 7. Thus, the fusible element 11 is mechanically loaded under a predetermined mechanical stress by the compression force of coil spring 12. It will be apparent to those skilled in the art that the degree of tension force applied to the fusible element 11 can be finely adjusted by varying the degree of compression of the spring 12 which is determined by rotating it on. its thread mounting 6a closer to, or further from, the end cap 3.
In the operation of my invention, it will be understood that the metal bellows and the coil spring 12 need only supply enough reciprocal motion to the electrode 7 to draw it far enough away from the electrode 9 to rupture the fusible element 11 when it is softened by being raised to a predetermined temperature level somewhat below its normal temperature of fusion. However, since the amount of current flowing through the fusible element 11 to cause it to reach this predetermined temperature level, may be relatively small, the bellows 5 and spring 12 in the preferred form of my invention are adapted to move the electrodes 7 and 9 away from each other far enough so that the dielectric strength of the vacuum in the envelope is sufficient to interrupt the circuit (following a zero voltage cycle) even if the ends of fusible element 11 are not completely burned back by the relatively lowcurrent are drawn between them after the mechanical rupture of element 11. 4
While I have shown and described a specific embodiment of my invention and a method of manufacturing it, I do not desire the invention to be limited to the particular form or method shown and described and I intend by the appended claims to cover all modifications falling within the true spirit and scope of my invention.
What I claim as new and desire to secure by Letters Patent of the United States is:
1. The method for making a fuse means comprising the sequential steps of: (1) providing a fuse envelope having a fusible element therein and having means for electrically connecting said element to a source of electric current, (2) evacuating and sealing said envelope, and (3) mechanically loading said fusible element thereby to apply a predetermined mechanical stress to it that is eifective to cause said element to break and fuse at a temperature below the fusion temperature of said element in its unstressed condition.
2. Themethod for making a fuse as defined in claim 1 wherein means for mechanically loading said fusible element are disposed outside of said envelope and include means for manually adjusting the degree of mechanical loading applied to said fusible element after it is encapsulated, and wherein flexible sealing means are provided through which a stressing force is transmitted from said loading means to said element without diminishing the vacuum in the envelope.
References Cited UNITED STATES PATENTS JOHN F. CAMPBELL, Primary Examiner V. A. DI PALMA, Assistant Examiner
US871260A 1968-05-13 1969-11-06 Method of making vacuum fuse Expired - Lifetime US3624899A (en)

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US87126069A 1969-11-06 1969-11-06

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3992771A (en) * 1974-05-22 1976-11-23 Emerson Electric Co. Method of making thermal limiter construction

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3992771A (en) * 1974-05-22 1976-11-23 Emerson Electric Co. Method of making thermal limiter construction

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