US1628723A - Relay - Google Patents

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Publication number
US1628723A
US1628723A US564981A US56498122A US1628723A US 1628723 A US1628723 A US 1628723A US 564981 A US564981 A US 564981A US 56498122 A US56498122 A US 56498122A US 1628723 A US1628723 A US 1628723A
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US
United States
Prior art keywords
diaphragm
jet
chamber
fluid
contacts
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US564981A
Inventor
Ray E Hall
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HALL RES CORP
HALL RESEARCH Corp
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HALL RES CORP
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
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Publication date
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Priority to US564981A priority Critical patent/US1628723A/en
Application granted granted Critical
Publication of US1628723A publication Critical patent/US1628723A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01HELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
    • H01H45/00Details of relays
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15CFLUID-CIRCUIT ELEMENTS PREDOMINANTLY USED FOR COMPUTING OR CONTROL PURPOSES
    • F15C1/00Circuit elements having no moving parts
    • F15C1/18Turbulence devices, i.e. devices in which a controlling stream will cause a laminar flow to become turbulent ; Diffusion amplifiers
    • 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
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S116/00Signals and indicators
    • Y10S116/18Wave generators
    • 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
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S200/00Electricity: circuit makers and breakers
    • Y10S200/05Fluid pressure: fluid amplifier
    • 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
    • Y10T137/00Fluid handling
    • Y10T137/206Flow affected by fluid contact, energy field or coanda effect [e.g., pure fluid device or system]
    • Y10T137/2273Device including linearly-aligned power stream emitter and power stream collector

Definitions

  • Application mea may ai, 1922. serial ia. 564,981.
  • the object of this invention is to provide a relay that will require a signal .of long duration to close contact, but which will open quickly upon a break in the signal.
  • a further ob'ect of the invention is to produce a call or wireless telephones that will notl be affected by telegra h signals or otherI electrical disturbances o short duration.
  • Fig. 1 is a sectional viewof a jet rel'ay showing one application of the invention
  • Fig. 2 is a section on line 2-2 of Fig. 1;
  • Fig. 3 is a, plan view of the diaphragm chamber. with the diaphragm removed.
  • the relay is shown supported by a plate which may be secured to any suitable casing, or the like.
  • a frame 11 mounted on the'plate is a frame 11 in which are arranged the nozzle 12, funnel 13 and the telephone 14.
  • the nozzle 12 communicates through the pipe 15 with a suitable source of fluid under proper pressure.
  • the funnel 13 communicates with the diaphragm chamber 16 of the telephone 14. .
  • the nozzle and funnel are adjustably mounted so as to permit them to be accurately arranged in the particular relation required.
  • the jet 17 issuing from ⁇ the nozzle 12j passes through. a passage 18 into a diaphragm chamber 19 formed in the facejof a disk 20 and supported on the plate -10.
  • the diaphra 21 fo a wall of the chamber is laid over the 20 and secured against the plate 10 by a ring 22 which may be made fast by. screws or the like.
  • the passage 18 is formed in a tube with the disk 20 and at its lend communi- ⁇ chamber an valve 25 preventingthe ready relief of pres-V tends to keep the valve seated. In order to 1 provide free communication the. sides .of
  • valve chamber aresharply inclined as indicated at 28.
  • the diaphragm carries a disk 29 fixed to a contact 30 carried by the end of a resilient arm 31 fastened to the ring 22 as indicated at 32.
  • Co-operating with the contact 30 is a contact 33 Acarried by an arm 34 which may be adjusted by a thumb screw 35.
  • the arm 34 is secured to the ring ⁇ .22 by a screw 36 similar to that illustrated at 32 and these screws may serve as binding Aposts to connect the contacts 30 and 33 in lthe circuit of a magnet 37 which includes a battery or the like 38.
  • the magnet 37 when energized will move an armature 39 to close a circuit Awith the contact 40 to ring a bell or perform chamber through a by-pass 41.
  • a by-pass that Will require approximately 10 seconds to permit the contacts to close will prevent telegraph signals, static discharges and practically all other electrical disturbances likely to be found under present conditions from operating the relay.
  • the period necessary for the escape of the trapped fluid Within the diaphragm chamber can be regulated to suit particular conditions and the relay can be made to operate for any desired period.. Consequently, the relay can be adjusted so that it will not be affected by static discharges or telegraph signals of any intensity, wave length or pitch and will be operated onl by va signal of long duration ⁇ Which is pre etermned.
  • the jet 17 will be modified for only a corresponding period durin which the fluid within the diaphragm cham r will hold the contacts open. .
  • the jet will assume its normal phase, open the valve 25 and continue to apply fluid to the diaphragm chamber with usual pressure. Any number of short si nals can be received. without affecting the re ay.
  • the diaphragm 21 will penetratect sulciently to close the contact and operate the leaf 39 or other detector;
  • I claimz' A l The combination of means to produce a jet of fluid, means-to impress vibrations on said jet to make it assume varying phases, a resilient maximn adapted-to move in one direction when acted upon by the 'et and to react in the opposite direction w en the action of the jet as abated, and .fluidvent x means to adjust the reaction of said resilient medium.

Description

R. E; HALL RELAY l Filed my 51, 1922' vMay 17, 1927.
Patented May 17,1927.
UNITED STATES `PATENT OFFICE.
RAY E. HALIMOF ROCK ISLAND, ILLINOIS, ASSIGNOB T0 HALL RESEARCH CORPORA- TION, F CHICAGO, ILLINOIS, A CORPORATION 0F DELAWARE.
RELAY.
Application mea may ai, 1922. serial ia. 564,981.
The object of this invention is to provide a relay that will require a signal .of long duration to close contact, but which will open quickly upon a break in the signal.
A vfurther object of the invention 1s to provide a jet relay in which the movable medium will respond quickly to the action.
of the normal jet and will react slowly when the jet assumes an abnormal phase due to the action of sound waves set up by the incoming signal.
A further ob'ect of the invention is to produce a call or wireless telephones that will notl be affected by telegra h signals or otherI electrical disturbances o short duration.
Further objects of the invention will b e-4 come apparent as the description is read in connection with theaccompanying drawing illustrating a selected embodiment of the invention and in which Fig. 1 is a sectional viewof a jet rel'ay showing one application of the invention;
Fig. 2 is a section on line 2-2 of Fig. 1; and
Fig. 3 is a, plan view of the diaphragm chamber. with the diaphragm removed.
- The relay is shown supported by a plate which may be secured to any suitable casing, or the like. Mounted on the'plate is a frame 11 in which are arranged the nozzle 12, funnel 13 and the telephone 14. The nozzle 12 communicates through the pipe 15 with a suitable source of fluid under proper pressure. The funnel 13 communicates with the diaphragm chamber 16 of the telephone 14. .Preferably the nozzle and funnel are adjustably mounted so as to permit them to be accurately arranged in the particular relation required.
The jet 17 issuing from` the nozzle 12j passes through. a passage 18 into a diaphragm chamber 19 formed in the facejof a disk 20 and supported on the plate -10. The diaphra 21 fo a wall of the chamber is laid over the 20 and secured against the plate 10 by a ring 22 which may be made fast by. screws or the like. The passage 18 is formed in a tube with the disk 20 and at its lend communi- `chamber an valve 25 preventingthe ready relief of pres-V tends to keep the valve seated. In order to 1 provide free communication the. sides .of
the valve chamber aresharply inclined as indicated at 28.
The diaphragm carries a disk 29 fixed to a contact 30 carried by the end of a resilient arm 31 fastened to the ring 22 as indicated at 32. Co-operating with the contact 30 is a contact 33 Acarried by an arm 34 which may be adjusted by a thumb screw 35. The arm 34 is secured to the ring`.22 by a screw 36 similar to that illustrated at 32 and these screws may serve as binding Aposts to connect the contacts 30 and 33 in lthe circuit of a magnet 37 which includes a battery or the like 38. The magnet 37 when energized will move an armature 39 to close a circuit Awith the contact 40 to ring a bell or perform chamber through a by-pass 41. When a signal operates the diaphragm in the telephone 14 it will set up sound waves that will pass the funnel 13 and act upon the jet at the mouth of thevnozzle 12 and cause it to assume varyin phases in which a small portion only will enter passage 18. Conse' quently, the dpressure within the diaphragm thev spring 27 will close the sure in the diaphragm 'chamber and holding the diaphragm distended. By provid-- ing the by-pass 41 leading from the diaphragm chamber to the atmosphere and adjusting the area thereof as by a screw 42, the time necessary to permit the diaphragm to react and close the contact 30 with the conaol tact 33 can be adjusted to any suitable period. In applying the invention to a call for wireless telephones, a by-pass that Will require approximately 10 seconds to permit the contacts to close will prevent telegraph signals, static discharges and practically all other electrical disturbances likely to be found under present conditions from operating the relay. By varying the by-pass, however, the period necessary for the escape of the trapped fluid Within the diaphragm chamber can be regulated to suit particular conditions and the relay can be made to operate for any desired period.. Consequently, the relay can be adjusted so that it will not be affected by static discharges or telegraph signals of any intensity, wave length or pitch and will be operated onl by va signal of long duration `Which is pre etermned.
If a signal of short duration operates the telephone le, the jet 17 will be modified for only a corresponding period durin which the fluid within the diaphragm cham r will hold the contacts open. .Immediately upon the cessation of the signal, the jet will assume its normal phase, open the valve 25 and continue to apply fluid to the diaphragm chamber with usual pressure. Any number of short si nals can be received. without affecting the re ay. When along signal produces any deformation of the jet, the diaphragm 21 will vreact sulciently to close the contact and operate the leaf 39 or other detector;
I am aware that changes may be made in the form, construction and arrangement of the invention, as set forth in the selected embodiment herein, without de arting fromthe scope or sacrificing any o its material advantages, and I therefore reserve the ri ht to make all such changes as fairly all Within thev scope of the following claims.
I claimz' A l. The combination of means to produce a jet of fluid, means-to impress vibrations on said jet to make it assume varying phases, a resilient mediun adapted-to move in one direction when acted upon by the 'et and to react in the opposite direction w en the action of the jet as abated, and .fluidvent x means to adjust the reaction of said resilient medium. X
Y 2. Tfhe combination of means 'for producing a jet of fluid, means for impressing waves on said jet, a-resilient medium adapted to move in one direction under the action of the f jet and to react in the opposite direction when the action of the jetI is abated, meansv to retard the reaction of said resilient meium and means to permit the medium to react slowly.
3. The combination of means to produce a jet of iluid, means for impre vibrations on` said jet, a diaphragm adap to be acted *the 'contacts for a relatively long period.
upon by said'jet, a normally closed valve in the path of said jet, and a by-pass permitting escape of the fluid after it has acted on said diaphragm.
4. The combination of means for producing a jet of fluid, means for impressing vibrations on saidjet, a diaphragm chamber, a normally closed valve inthe path of said jet controlling egress of fluid from said chamber, a diaphragm forming a Wall .of said chamber and a by-pass connecting said chamber with the atmosphere.
5. The combination of means for producing a jet of fluid, means for impressing Waves on said jet, a diaphragm in the path of said jet, a chamber over which said diaphragm extends andinto Whichsaid jet is directed, a check valve controlling the escape of lluid from said chamber, and a by-pass communicating With said chamber.
6. The combination of a diaphragm, a chamber having one Wall thereof formed by said diaphragm, a contact movable with said diaphragm, a. relatively fixedl contact, means for directing a jet of fluid into said chamber to movesaid diaphragm in one direction, a valve controlling egress from said chamber, and a by-pass communicating with saidchamber.
7 'Ihe combination of a diaphragm, separable contacts operated'bysaid diaphragm, a fluid chamber having a Wall formed by said diaphragm,` a passage communicating with said chamber, a normally closed valve `controlling saidpassage, means for directing a jet of fluid through said passage into said chamber, means for impressing` waves on said jet, and means for .permitting-the escape of fluid from said chamber.
y 8. The combination including separable contacts, a resilient medium adapted to open and close said contacts, `means to bias said' Y medium in a direction to separate saidcontacts, means to abate the action of the last named means, and fluid vent means to retard the reaction of said medium. f
9. The combination 'including' separable contacts, a diaphragm for controlling said contacts, means for producin a fluid jet .to bias said diaphragm, means or abating the force of said jet, means for automatically checking the reaction of said diaphragm, and means to slowly relieve said dia hragm.
,10. The combination of relative y mov-\\V able contacts, a resilient medium for operating said contacts,'means to bias said me- 12 -dium inone direction to open said contacts,
means to abate the action ofthe last named means,and independent means to retard the reaction of said medium to prevent closing-V 11. T hefcombination of relatively movi able contacts, a resilient medium adapted to control said contacts, means to bias said medium to open said contacts, means to abate the action of the last named means, means to block the reaction of said resilient medium, and independent means to relieve the 5 medium slowly.
12. The combination of relativel)T movable contactsl a diaphragm for opening and closing said contacts, means for directing a jet into a chamber adjacent to said diaphragm, a check valve controlling the entrance to said chamber, means for abatlng the action of said jet, and means to slowly relieve the pressure in said chamber.
RAY E. HALL.
US564981A 1922-05-31 1922-05-31 Relay Expired - Lifetime US1628723A (en)

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Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2610270A (en) * 1949-09-03 1952-09-09 Curtiss R Schafer Chopper
US2853574A (en) * 1956-01-18 1958-09-23 Hughes Aircraft Co Magnetic tape position indicating device
US2957957A (en) * 1956-01-13 1960-10-25 Thomas M Johnson Sound switch
US3078658A (en) * 1957-01-10 1963-02-26 Bristol Siddeley Engines Ltd Control of supersonic fluid flow in ducts
US3144037A (en) * 1961-02-16 1964-08-11 Sperry Rand Corp Electro-sonic fluid amplifier
US3176920A (en) * 1961-05-26 1965-04-06 Honeywell Inc Fluid operated pump
US3186422A (en) * 1962-12-31 1965-06-01 Gen Electric Fluid amplifier
US3234955A (en) * 1962-10-01 1966-02-15 Raymond N Auger Fluid amplifiers
US3262466A (en) * 1963-07-29 1966-07-26 Moore Products Co Flow control apparatus
US3269419A (en) * 1963-06-03 1966-08-30 Gen Electric Fluid amplifiers
US3324262A (en) * 1965-04-09 1967-06-06 Square D Co Fluid limit switch
US3362421A (en) * 1963-05-28 1968-01-09 Ibm Bounded free jet fluid amplifier with turbulent attachment
US3379165A (en) * 1966-06-16 1968-04-23 Honeywell Inc Object detecting system
US3428068A (en) * 1967-02-06 1969-02-18 Howie Corp Turbulence amplifier
US3429323A (en) * 1965-12-23 1969-02-25 Honeywell Inc Fluid amplifier
US3468328A (en) * 1965-10-15 1969-09-23 Bowles Eng Corp Distributed amplifier
US3468329A (en) * 1966-03-28 1969-09-23 Bendix Corp Pressure amplifier
US3469593A (en) * 1966-06-01 1969-09-30 Pitney Bowes Inc Fluidic device
US3490477A (en) * 1967-08-18 1970-01-20 Foxboro Co Rotated pattern fluidic element
US3502092A (en) * 1965-02-25 1970-03-24 Bowles Eng Corp Turbulence amplifier and circuits
US3517686A (en) * 1966-07-13 1970-06-30 Pitney Bowes Inc Fluid oscillator system
US3557811A (en) * 1968-10-18 1971-01-26 Factory Mutual Res Corp Dynamic flow sensor
US3561463A (en) * 1968-09-12 1971-02-09 Pitney Bowes Inc Control device
US3578013A (en) * 1968-05-08 1971-05-11 Dba Sa Vortices, particularly to their outlet

Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2610270A (en) * 1949-09-03 1952-09-09 Curtiss R Schafer Chopper
US2957957A (en) * 1956-01-13 1960-10-25 Thomas M Johnson Sound switch
US2853574A (en) * 1956-01-18 1958-09-23 Hughes Aircraft Co Magnetic tape position indicating device
US3078658A (en) * 1957-01-10 1963-02-26 Bristol Siddeley Engines Ltd Control of supersonic fluid flow in ducts
US3144037A (en) * 1961-02-16 1964-08-11 Sperry Rand Corp Electro-sonic fluid amplifier
US3176920A (en) * 1961-05-26 1965-04-06 Honeywell Inc Fluid operated pump
US3234955A (en) * 1962-10-01 1966-02-15 Raymond N Auger Fluid amplifiers
US3186422A (en) * 1962-12-31 1965-06-01 Gen Electric Fluid amplifier
US3362421A (en) * 1963-05-28 1968-01-09 Ibm Bounded free jet fluid amplifier with turbulent attachment
US3269419A (en) * 1963-06-03 1966-08-30 Gen Electric Fluid amplifiers
US3262466A (en) * 1963-07-29 1966-07-26 Moore Products Co Flow control apparatus
US3502092A (en) * 1965-02-25 1970-03-24 Bowles Eng Corp Turbulence amplifier and circuits
US3324262A (en) * 1965-04-09 1967-06-06 Square D Co Fluid limit switch
US3468328A (en) * 1965-10-15 1969-09-23 Bowles Eng Corp Distributed amplifier
US3429323A (en) * 1965-12-23 1969-02-25 Honeywell Inc Fluid amplifier
US3468329A (en) * 1966-03-28 1969-09-23 Bendix Corp Pressure amplifier
US3469593A (en) * 1966-06-01 1969-09-30 Pitney Bowes Inc Fluidic device
US3379165A (en) * 1966-06-16 1968-04-23 Honeywell Inc Object detecting system
US3517686A (en) * 1966-07-13 1970-06-30 Pitney Bowes Inc Fluid oscillator system
US3428068A (en) * 1967-02-06 1969-02-18 Howie Corp Turbulence amplifier
US3490477A (en) * 1967-08-18 1970-01-20 Foxboro Co Rotated pattern fluidic element
US3578013A (en) * 1968-05-08 1971-05-11 Dba Sa Vortices, particularly to their outlet
US3561463A (en) * 1968-09-12 1971-02-09 Pitney Bowes Inc Control device
US3557811A (en) * 1968-10-18 1971-01-26 Factory Mutual Res Corp Dynamic flow sensor

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