US3102974A - Subminiature relays - Google Patents

Subminiature relays Download PDF

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Publication number
US3102974A
US3102974A US15328A US1532860A US3102974A US 3102974 A US3102974 A US 3102974A US 15328 A US15328 A US 15328A US 1532860 A US1532860 A US 1532860A US 3102974 A US3102974 A US 3102974A
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Prior art keywords
armature
tube
wire
backstrap
aperture
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Expired - Lifetime
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US15328A
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Jr Richard H Williams
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Westinghouse Air Brake Co
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Westinghouse Air Brake Co
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Priority to US15328A priority Critical patent/US3102974A/en
Priority to FR855162A priority patent/FR1283140A/en
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01HELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
    • H01H50/00Details of electromagnetic relays
    • H01H50/16Magnetic circuit arrangements
    • H01H50/18Movable parts of magnetic circuits, e.g. armature
    • H01H50/30Mechanical arrangements for preventing or damping vibration or shock, e.g. by balancing of armature

Definitions

  • Subminiature relays are especially useful in airborne electronic applications and especially in missiles where relays are subjected to intense vibrations and severe shock conditions over a wide range of ambient temperature.
  • a relay including two coils mounted on two cores with one end of each of the cores aifixed to a backstrap. The other end of each of the cores passes through an aperture in a mounting bracket and forms a pole piece.
  • the armature is supported, i.e., suspended on a wire which is afiixed atone end to the backstrap and is free to rotate at its other end.
  • a tube or sleeve is circumposed on the wire. One end of the tube is ailixed to the armature and the other end is contracted around the wire.
  • the tube provides a relatively large bearing surface for the wire and strengthens the wire with respect to bending torque.
  • the armature is positioned between the pole pieces and is rotatable toward and away from pole pieces upon energization and deenergization respectively of the associated coils.
  • Insulative pins affixed to the armature actuate spring contacts mounted on a header plate.
  • FIG. 1 is a front elevational view of a preferred form of the relay with the relay casing in cross section;
  • FIG. 2 is a sectional view taken along lines 22 of FIG. 1 looking in the direction of the arrows to show armature operation;
  • FIG. 3 is a sectional view taken along lines 33 of FIG. 1 looking in the direction of the arrows to show the spring contact structure;
  • FIG. 4 is an isometric view of the relay supporting bracket of FIG. 1;
  • FIG. 5 is an elevational view of the armature suspension assembly of FIG. 1.
  • the relay assembly 11 is contained within an invertedcup-shaped casing l3 of any suitable material, such as brass or nickel silver. As seen from FIGS. 2 and 3,
  • Terminal pins 17 extend through the header 15 and are bonded and hermetically sealed thereto. Terminal pins 17 provide electrical connections from relay 11 to the associated external circuitry, not shown.
  • the height of relay 11 is approximately 1 inch, the width is of an inch and the depth is A of an inch.
  • the relay weighs approximately /2 ounce.
  • a pair of coils i9 and 21 are mounted on respective cores 23 and 25 which cores each have one end aflixed to a backstrap 27.
  • Backstrap 27 fits against the top of casing 13.
  • the other end of each of cores 23 and 25 pass through respective apertures f and g, see FIG. 4,
  • Cores 23 and 25 are circular in cross section; however, pole pieces 23a and 25a have been contoured to have a fiat surface to provide a better mating surface with armature 31.
  • Bracket 29 is the overall support for the relay assembly. As best seen from FIG. 4, bracket 29 is formed to have a center portion, not numbered, and four legs a, b, c and d; legs a and c are bent upward and are affixed as by welding to backstrap 2'7, and legs b and d are bent downward and are afiixed as by welding to header 15. Each of legs b and d, in addition, includes lateral extensions b and d on which are mounted respective permanent magnets 36 and 32 which magnets bias the armature 31 to an initial position.
  • wire 33 is of beryllium copper approximately & inch in diameter.
  • Wire 33 has one end, the upper end as oriented in FIG. 1, afiixed or anchored as by welding to backstrap 27 and passes between coils 19 and 21 and through an aperture e formed in the center portion of bracket 29; armature 31 is affixed to the other end of wire 33 as by welding.
  • An elongated tube or sleeve 35' is circumposed about wire 33.
  • One end of tube 35 is afiixed to armature 31 as by welding.
  • Tube 35 passes through aperture e in bracket 29 and its outer surface provides a bearing surface against the sides of the aperture when the armature 31 rotates.
  • the other or upper end of tube 35 is reduced in size to form a contracted portion 35a which closely surrounds wire 33 to serve as a relatively low-friction, side-thrust bearing; alternatively, the diameter of the opening, i.e., the inner surface of tube 35 may be made smaller along part or all of the length of the tube for the same purpose.
  • armature 31 is positioned to have one end extending between the pole piece 23a and the permanent magnet 39 which is iaifixed to leg b of bracket 29.
  • the other end of armature 31 extends between the pole piece 25:; and the permanent magnet 32 which is affixed to leg d of bracket 29.
  • Armature 31 has a conventional type of rotary action, that is, when the coils l9 and 21 are energized, the armature swings toward the pole pieces 23a and 25a and torsionally stresses or twists wire 33.
  • the armature is returned to its initial position due to the torsional torque of wire 33, the pressure.
  • Tube 35 also functions to strengthen Wire 33 with respect to bending torques.
  • fineflwire 33 and tube 35 provide the advantage of utilizing a thin wire to provide loW torsional torque While also providing the advantages which would be obtained if a relatively thicker Wire were used, namely higher resistance to bending stresses andla larger stronger bearing surface.
  • the Wire suspension forarmature 31 possesses various advantages;
  • the Wire suspension holds the armature in place Without end play such as would be present with conventional bearing'construction.
  • wire 33 acts as a torsion spring to provide some restoring torque to tend to return the armature to its normal position when the coils are deenergized.
  • the single end anchoring permits the use of a larger and stronger suspension Wire for a'given torsional force and also allows for expansion or contraction of various parts due to temperature changes without adversely afiecting the operation of the relay.
  • a pair of contact actuating members 34 and 36 each consisting of -metal rods terminating in a sphere of insulating material, such as glass, are attached to opposite ends of armature 31.
  • Members 34 and 36 transfer the motion of armature 31 to movable contact springs 39 and 41 mounted on the header plate 15, see FIG. 3.
  • Movable contacts 39 and 41 each have one end afiixed to a respective terminal pin 17 and the other end extends" between'twoother terminal pins 17.
  • Springs 43 have one end rigidly, afiixed to pins 17 and the other or free ends are arranged to be contacted by the free ends of movable contacts 39 and 41.
  • Movable contacts 39 and 41th us make'contact with a resilient surface for reducing contact bounce and'rnaking the relay contacts less jsnbject tobeingYundesirably opened or closed due to severe shock and'vibration stresses.
  • a relay including an armature, a baclistrap and pole pieces, means for mounting said armature adjacent said pole pieces for rotation through a predetermined are and comprising, a tube secured at one end to said tarmature and free at the other end, a torsionally'flexible member internally extending completely through said tube along its longitudinal axis, one end of said member being suspended from said b ackstrap and the other end being secured to said armature, and a bracket member positioned between said backstrap and said armature including an aperture with said tube extending through said aperture with clearance so that the surfaces of said'bracket member which define said aperture provide a bearing surface for said tube during rotation of said armature.
  • a relay includingan armature, a backstrap and pole pieces, means for mounting said arnratureadjacent said pole pieces for rotation through a predetermined arc and comprising, a torsionally flexible member suspended at one end from said vbackstrr'ap and being secured to said armature rat a point removed from its suspended end, a
  • bracket member disposed between the suspended end of said flexible member and said armature and having-anaperture in coaxial alignment With said member, and 'a tube fixed to said armature at one end extending through said aperture with clearance and being constricted and" unattached atlits other end adjacent the suspended end of said torsionally flexible member to serve as a relatively low-friction side-thrust bearing for said torsionally flexible member during rotation of said armature.
  • a relay comprising a magnetizable member including a backstrap and pole pieces, an armature adapted to magnetically coact With said pole pieces, a torsionally flexible Wire suspending saidarrnature from said backstrap, a tube free at one end and, secured at the other end to and rotatable With said armature With said Wire extending internally through said tribe along its longitudinal axis for strengthening the bending torque of said flexible Wire, and a bracket between said armature and said backstrap encircling said tube in, such manner that said bracket provides a bearing surfacefor said tube.

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  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Dc Machiner (AREA)

Description

United States Patent O 3,102,974 SUBMKNIATURE RELAYS Richard H. Williams, .lru, Pittsburgh, Pa", assignor to Westinghouse Air Brake Company, Wilrnerding, Pan, a corporation of Pennsylvania Filed Mar. 16, 1960, Ser. No. 15,323
3 Claims. (Cl. 317-176) My invention relates to relays and more particularly to relays of small size and light weight commonly referred to in the art as subminiature or crystal case relays.
Subminiature relays are especially useful in airborne electronic applications and especially in missiles where relays are subjected to intense vibrations and severe shock conditions over a wide range of ambient temperature.
Accordingly, it is a principal object of my invention to provide an improved subminiature relay which will withstand intense vibrations and severe shock while maintaining fast and sensitive operation over wide ranges of temperature. It is another object of my invention to provide an improved wire suspension for an armature which provides the low torsional torque of a fine wire while providing the high resistance to bending stresses and the stronger bearing surface of a relatively thick wire.
It is another object of my invention to provide a subminiature relay in which improved control of quality and manufacture is provided to thus give extra assurance of reliability.
In the attainment of the foregoing objects I provide a relay including two coils mounted on two cores with one end of each of the cores aifixed to a backstrap. The other end of each of the cores passes through an aperture in a mounting bracket and forms a pole piece. The armature is supported, i.e., suspended on a wire which is afiixed atone end to the backstrap and is free to rotate at its other end. A tube or sleeve is circumposed on the wire. One end of the tube is ailixed to the armature and the other end is contracted around the wire. The tube provides a relatively large bearing surface for the wire and strengthens the wire with respect to bending torque. The armature is positioned between the pole pieces and is rotatable toward and away from pole pieces upon energization and deenergization respectively of the associated coils. Insulative pins affixed to the armature actuate spring contacts mounted on a header plate.
Other objects and advantages of my invention will become apparent from the following description taken in connection with the accompanying drawing in which like reference characters refer to like elements throughout and in which:
FIG. 1 is a front elevational view of a preferred form of the relay with the relay casing in cross section;
FIG. 2 is a sectional view taken along lines 22 of FIG. 1 looking in the direction of the arrows to show armature operation;
FIG. 3 is a sectional view taken along lines 33 of FIG. 1 looking in the direction of the arrows to show the spring contact structure;
FIG. 4 is an isometric view of the relay supporting bracket of FIG. 1; and
FIG. 5 is an elevational view of the armature suspension assembly of FIG. 1.
I shall first describe one embodiment of a relay according to my invention, and shall then point out the novel features thereof in the appended claims.
Referring to the figures and particularly to FIGURE 1, the relay assembly 11 is contained within an invertedcup-shaped casing l3 of any suitable material, such as brass or nickel silver. As seen from FIGS. 2 and 3,
pins 17 extend through the header 15 and are bonded and hermetically sealed thereto. Terminal pins 17 provide electrical connections from relay 11 to the associated external circuitry, not shown.
In one embodiment, the height of relay 11 is approximately 1 inch, the width is of an inch and the depth is A of an inch. The relay weighs approximately /2 ounce.
A pair of coils i9 and 21 are mounted on respective cores 23 and 25 which cores each have one end aflixed to a backstrap 27. Backstrap 27 fits against the top of casing 13. The other end of each of cores 23 and 25 pass through respective apertures f and g, see FIG. 4,
formed on a bracket member 29 to provide pole pieces 23a and 25a for actuating an armature 31 as will become apparent. Cores 23 and 25 are circular in cross section; however, pole pieces 23a and 25a have been contoured to have a fiat surface to provide a better mating surface with armature 31.
Bracket 29 is the overall support for the relay assembly. As best seen from FIG. 4, bracket 29 is formed to have a center portion, not numbered, and four legs a, b, c and d; legs a and c are bent upward and are affixed as by welding to backstrap 2'7, and legs b and d are bent downward and are afiixed as by welding to header 15. Each of legs b and d, in addition, includes lateral extensions b and d on which are mounted respective permanent magnets 36 and 32 which magnets bias the armature 31 to an initial position.
Referring now particularly to FIGS. 4 and 5, armature 31 is suspended beneath the center portion of bracket 29 by a fine, flexible wire 33. In one embodiment wire 33 is of beryllium copper approximately & inch in diameter. Wire 33 has one end, the upper end as oriented in FIG. 1, afiixed or anchored as by welding to backstrap 27 and passes between coils 19 and 21 and through an aperture e formed in the center portion of bracket 29; armature 31 is affixed to the other end of wire 33 as by welding.
An elongated tube or sleeve 35' is circumposed about wire 33. One end of tube 35 is afiixed to armature 31 as by welding. Tube 35 passes through aperture e in bracket 29 and its outer surface provides a bearing surface against the sides of the aperture when the armature 31 rotates. The other or upper end of tube 35 is reduced in size to form a contracted portion 35a which closely surrounds wire 33 to serve as a relatively low-friction, side-thrust bearing; alternatively, the diameter of the opening, i.e., the inner surface of tube 35 may be made smaller along part or all of the length of the tube for the same purpose.
Referring now also to FIG. 2, armature 31 is positioned to have one end extending between the pole piece 23a and the permanent magnet 39 which is iaifixed to leg b of bracket 29. The other end of armature 31 extends between the pole piece 25:; and the permanent magnet 32 which is affixed to leg d of bracket 29. Armature 31 has a conventional type of rotary action, that is, when the coils l9 and 21 are energized, the armature swings toward the pole pieces 23a and 25a and torsionally stresses or twists wire 33. When the coils are deenergized the armature is returned to its initial position due to the torsional torque of wire 33, the pressure. of the movable contact springs 39 and 41, and due to the magnetic attraction of permanent magnets 30 and 32. When armature 31 rotates, tube 35 rotates in aperture e of bracket 29 and wire 33 is torsionally stressed or twists within tube 35. By circumposing tube 35 on wire 33a relatively larger 'and stronger bearing surfiace is essentially provided between-the faces of aperture e in bracket 29 and Wire'33, Otherwise, due to the small diameter of'wire 33, 'a jewel bearing would have to be employed to prevent excessive wean) Tube 35 also functions to strengthen Wire 33 with respect to bending torques. In effect, then, fineflwire 33 and tube 35 provide the advantage of utilizing a thin wire to provide loW torsional torque While also providing the advantages which Would be obtained if a relatively thicker Wire were used, namely higher resistance to bending stresses andla larger stronger bearing surface. I
I The Wire suspension forarmature 31 possesses various advantages; The Wire suspension holds the armature in place Without end play such as Would be present with conventional bearing'construction. As noted above, wire 33 acts as a torsion spring to provide some restoring torque to tend to return the armature to its normal position when the coils are deenergized. The single end anchoring permits the use of a larger and stronger suspension Wire for a'given torsional force and also allows for expansion or contraction of various parts due to temperature changes without adversely afiecting the operation of the relay.
A pair of contact actuating members 34 and 36 each consisting of -metal rods terminating in a sphere of insulating material, such as glass, are attached to opposite ends of armature 31. Members 34 and 36 transfer the motion of armature 31 to movable contact springs 39 and 41 mounted on the header plate 15, see FIG. 3.
Movable contacts 39 and 41 each have one end afiixed to a respective terminal pin 17 and the other end extends" between'twoother terminal pins 17. Springs 43 have one end rigidly, afiixed to pins 17 and the other or free ends are arranged to be contacted by the free ends of movable contacts 39 and 41. Movable contacts 39 and 41th us make'contact with a resilient surface for reducing contact bounce and'rnaking the relay contacts less jsnbject tobeingYundesirably opened or closed due to severe shock and'vibration stresses.
Although I have herein shown and described onlyone form of apparatus embodying my invention, it will be j understood that various changes land modifications may be made therein Within the scope of the appended claims Without departing from the spirit and scope of my invention. e Having thus described my invention, What I claim is: 1. In a relay including an armature, a baclistrap and pole pieces, means for mounting said armature adjacent said pole pieces for rotation through a predetermined are and comprising, a tube secured at one end to said tarmature and free at the other end, a torsionally'flexible member internally extending completely through said tube along its longitudinal axis, one end of said member being suspended from said b ackstrap and the other end being secured to said armature, and a bracket member positioned between said backstrap and said armature including an aperture with said tube extending through said aperture with clearance so that the surfaces of said'bracket member which define said aperture provide a bearing surface for said tube during rotation of said armature.
2. In a relay includingan armature, a backstrap and pole pieces, means for mounting said arnratureadjacent said pole pieces for rotation through a predetermined arc and comprising, a torsionally flexible member suspended at one end from said vbackstrr'ap and being secured to said armature rat a point removed from its suspended end, a
bracket member disposed between the suspended end of said flexible member and said armature and having-anaperture in coaxial alignment With said member, and 'a tube fixed to said armature at one end extending through said aperture with clearance and being constricted and" unattached atlits other end adjacent the suspended end of said torsionally flexible member to serve as a relatively low-friction side-thrust bearing for said torsionally flexible member during rotation of said armature.
I 3. A relay comprising a magnetizable member including a backstrap and pole pieces, an armature adapted to magnetically coact With said pole pieces, a torsionally flexible Wire suspending saidarrnature from said backstrap, a tube free at one end and, secured at the other end to and rotatable With said armature With said Wire extending internally through said tribe along its longitudinal axis for strengthening the bending torque of said flexible Wire, and a bracket between said armature and said backstrap encircling said tube in, such manner that said bracket provides a bearing surfacefor said tube.v
References Cited inthe file of this patent UNITED STATES PATENTS

Claims (1)

1. IN A RELAY INCLUDING AN ARMATURE, A BACKSTRAP AND POLE PIECES, MEANS FOR MOUNTING SAID ARMATURE ADJACENT SAID POLE PIECES FOR ROTATION THROUGH A PREDETERMINED ARC AND COMPRISING, A TUBE SECURED AT ONE END TO SAID ARMATURE AND FREE AT THE OTHER END, A TORSIONALLY FLEXIBLE MEMBER INTERNALLY EXTENDING COMPLETELY THROUGH SAID TUBE ALONG ITS LONGITUDINAL AXIS, ONE END OF SAID MEMBER BEING SUSPENDED FROM SAID BACKSTRAP AND THE OTHER END BEING SECURED TO SAID ARMATURE, AND A BRACKET MEMBER POSITIONED BETWEEN SAID BACKSTRAP AND SAID ARMATURE INCLUDING AN APERTURE WITH SAID TUBE EXTENDING THROUGH SAID APERTURE WITH CLEARANCE SO THAT THE SURFACES OF SAID BRACKET MEMBER WHICH DEFINE SAID APERTURE PROVIDE A BEARING SURFACE FOR SAID TUBE DURING ROTATION OF SAID ARMATURE.
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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3377578A (en) * 1964-09-04 1968-04-09 Matsushita Electric Ind Co Ltd Device for imparting horizontally oscillatory rotating movement to articles
US3425011A (en) * 1964-09-04 1969-01-28 Matsushita Electric Ind Co Ltd Device for imparting horizontally oscillatory rotating movement to articles
DE1614038B1 (en) * 1967-02-17 1969-11-06 Le Proizv Objedinenije Electromagnetic relay
US3523263A (en) * 1968-01-12 1970-08-04 Robertshaw Controls Co Electromagnetic apparatus
US3800257A (en) * 1973-04-09 1974-03-26 Bicron Electronics Multicoil solenoid assembly
US4122420A (en) * 1977-01-13 1978-10-24 Esterline Electronics Corporation Permissive-make electromagnetic switch
US4121518A (en) * 1976-10-12 1978-10-24 Documation Incorporated High speed printer hammer assembly

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1601205A (en) * 1924-04-19 1926-09-28 Union Switch & Signal Co Electrical relay
US1858876A (en) * 1929-10-09 1932-05-17 Union Switch & Signal Co Coding apparatus
US2824189A (en) * 1955-10-17 1958-02-18 Gen Electric Electro-magnetic switching device
US2919326A (en) * 1956-05-17 1959-12-29 Ibm Electrical relay and contact assembly
US2927177A (en) * 1958-01-21 1960-03-01 Otto R Nemeth Electric relay
US2931872A (en) * 1958-09-22 1960-04-05 Iron Fireman Mfg Co Polarized relay
US2946873A (en) * 1957-05-03 1960-07-26 Ericsson Telephones Ltd Electromagnetic relays
US2952755A (en) * 1957-11-22 1960-09-13 Westinghouse Air Brake Co Electrical relays
US2955174A (en) * 1957-12-02 1960-10-04 American Mach & Foundry Electrical relays
US3008070A (en) * 1958-05-19 1961-11-07 Otto R Nemeth Rotary solenoid

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1601205A (en) * 1924-04-19 1926-09-28 Union Switch & Signal Co Electrical relay
US1858876A (en) * 1929-10-09 1932-05-17 Union Switch & Signal Co Coding apparatus
US2824189A (en) * 1955-10-17 1958-02-18 Gen Electric Electro-magnetic switching device
US2919326A (en) * 1956-05-17 1959-12-29 Ibm Electrical relay and contact assembly
US2946873A (en) * 1957-05-03 1960-07-26 Ericsson Telephones Ltd Electromagnetic relays
US2952755A (en) * 1957-11-22 1960-09-13 Westinghouse Air Brake Co Electrical relays
US2955174A (en) * 1957-12-02 1960-10-04 American Mach & Foundry Electrical relays
US2927177A (en) * 1958-01-21 1960-03-01 Otto R Nemeth Electric relay
US3008070A (en) * 1958-05-19 1961-11-07 Otto R Nemeth Rotary solenoid
US2931872A (en) * 1958-09-22 1960-04-05 Iron Fireman Mfg Co Polarized relay

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3377578A (en) * 1964-09-04 1968-04-09 Matsushita Electric Ind Co Ltd Device for imparting horizontally oscillatory rotating movement to articles
US3380656A (en) * 1964-09-04 1968-04-30 Matsushita Electric Ind Co Ltd Device for imparting horizontally oscillatory rotating movement to articles
US3425011A (en) * 1964-09-04 1969-01-28 Matsushita Electric Ind Co Ltd Device for imparting horizontally oscillatory rotating movement to articles
DE1614038B1 (en) * 1967-02-17 1969-11-06 Le Proizv Objedinenije Electromagnetic relay
US3523263A (en) * 1968-01-12 1970-08-04 Robertshaw Controls Co Electromagnetic apparatus
US3800257A (en) * 1973-04-09 1974-03-26 Bicron Electronics Multicoil solenoid assembly
US4121518A (en) * 1976-10-12 1978-10-24 Documation Incorporated High speed printer hammer assembly
US4122420A (en) * 1977-01-13 1978-10-24 Esterline Electronics Corporation Permissive-make electromagnetic switch

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