GB1225840A - - Google Patents

Info

Publication number
GB1225840A
GB1225840A GB1225840DA GB1225840A GB 1225840 A GB1225840 A GB 1225840A GB 1225840D A GB1225840D A GB 1225840DA GB 1225840 A GB1225840 A GB 1225840A
Authority
GB
United Kingdom
Prior art keywords
control
streams
stream
jet
ports
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
Application number
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.)
Filing date
Publication date
Application filed filed Critical
Publication of GB1225840A publication Critical patent/GB1225840A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F15C1/08Boundary-layer devices, e.g. wall-attachment amplifiers coanda effect
    • F15C1/10Boundary-layer devices, e.g. wall-attachment amplifiers coanda effect for digital operation, e.g. to form a logical flip-flop, OR-gate, NOR-gate, AND-gate; Comparators; Pulse 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
    • 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]
    • Y10T137/2229Device including passages having V over T configuration
    • Y10T137/224With particular characteristics of control input
    • Y10T137/2245Multiple control-input passages
    • 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]
    • Y10T137/2229Device including passages having V over T configuration
    • Y10T137/2251And multiple or joined power-outlet passages

Abstract

1,225,840. Fluidic devices. TATEISI ELECTRONICS CO. 18 Oct., 1968 [20 Oct., 1967], No. 49439/68. Heading G4P. [Also in Division G3] A fluidic element comprises a passage for a control stream which controls the deflection of, but does not come into contact with, a main fluid jet. In a bi-stable element, Fig. 1, a jet stream F 1 flows to output ports 11 or 12. Control streams G 1 and G 2 enter input ports 17, 18 and traverse the ends of, but do not enter, passages 19, 20 and exit to ports 21, 22. Openings 25, 26 vent to atmosphere. Stream F 1 flows along passage 9 adherent to the left side thereof (Fig. 3). If control stream G 2 flows it lowers pressure in passage 20 to switch the jet to the output 10. Similarly it may be switched back to its former flow along passage 9 by the presence of control stream G 1 . In a further system (Figs. 5, not shown) the control streams pass from input to output through passages transverse to the passages 19, 20, and lying in the plane of body 1. In a further element (Fig. 9) input ports 57a, 57b, 57c pass control streams to port 59, the streams causing a pressure reduction in passage 54 to switch jet F4. The element acts as an OR/NOR gate. The input ports and control passages may be in a plane perpendicular to that of the body 1, Fig. 15 (not shown). In a further element (Fig. 11) control streams G8, G9 are developed from plural streams entering inlet ports 64a-64c, 65a-65c which are summed in series or parallel to enter passages 66, 67 traversing the ends of spaces 68, 69 to outlet ports 70, 71. The jet stream F5 entering a control region is deflected proportionally to the pressure difference between control streams G8, G9, i.e. to the difference between the number of input streams constituting each. In a further element, Fig. 12, a single control stream G10 developed from two interacting input streams at 75a, b is applied to deflect jet F6 in response to the presence of the two inputs to provide AND/NAND action. In a further element (Fig. 13, not shown) the control streams developed by pairs of interacting input streams interact to develop a main control stream only when all inputs are present, providing AND/NAND operation. In a further element (Fig. 14, not shown) for AND/NAND OR/NOR action in plural stages, a control stream derived from plural inputs as in Fig. 9 and from a plurality of pairs of inputs as in Fig. 13 (not shown) are combined in pairs and plural such pairs are assembled into a set. In a further arrangement (Fig. 16) for OR or NOR action passage 96 is connected to a diaphragm 96 linked to operate a low pressure valve 99 controlling the main jet stream F10. In a further system, Fig. 17, for combined AND/OR action either of control streams G15, G16 impinging on one side of main jet stream F11 deviates it from outlet 108 to 109, while simultaneous flow of control streams G17, G18 operating to reduce pressure on the other side of jet stream F11 similarly deviates it from outlet 108 to 109.
GB1225840D 1967-10-20 1968-10-18 Expired GB1225840A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP6758767 1967-10-20

Publications (1)

Publication Number Publication Date
GB1225840A true GB1225840A (en) 1971-03-24

Family

ID=13349184

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1225840D Expired GB1225840A (en) 1967-10-20 1968-10-18

Country Status (4)

Country Link
US (1) US3589381A (en)
DE (1) DE1804298A1 (en)
FR (1) FR1588445A (en)
GB (1) GB1225840A (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL7016798A (en) * 1970-11-17 1972-05-19
US3766945A (en) * 1972-04-21 1973-10-23 Us Navy Fluidic system for mixing two fluids
US3958602A (en) * 1975-03-12 1976-05-25 The United States Of America As Represented By The Secretary Of The Army Flueric laminar digital amplifier
US11739517B2 (en) 2019-05-17 2023-08-29 Kohler Co. Fluidics devices for plumbing fixtures

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3229705A (en) * 1963-03-29 1966-01-18 Ibm Fluid memory
US3258023A (en) * 1963-04-12 1966-06-28 Romald E Bowles Pneumatic eye
US3283766A (en) * 1963-04-22 1966-11-08 Sperry Rand Corp Separable fluid control system
US3208464A (en) * 1963-04-22 1965-09-28 Sperry Rand Corp Fluid stream deflecting means
US3232305A (en) * 1963-11-14 1966-02-01 Sperry Rand Corp Fluid logic apparatus
US3286086A (en) * 1964-12-03 1966-11-15 Bowles Eng Corp Pure fluid binary adder
US3425432A (en) * 1965-04-29 1969-02-04 Corning Glass Works Bistable fluid amplifier
US3417770A (en) * 1965-06-07 1968-12-24 Electro Optical Systems Inc Fluid amplifier system
US3388898A (en) * 1965-09-16 1968-06-18 Gen Motors Corp Fuel system
US3467122A (en) * 1965-09-27 1969-09-16 Bowles Eng Corp Liquid level sensor
US3457935A (en) * 1966-11-28 1969-07-29 Gen Electric Fluid amplifiers
US3495609A (en) * 1967-07-03 1970-02-17 Us Army Fluid induction amplifier
US3457937A (en) * 1967-08-15 1969-07-29 Honeywell Inc Fluid circuit
US3468326A (en) * 1967-10-19 1969-09-23 Bailey Meter Co Triggerable flip-flop fluid device

Also Published As

Publication number Publication date
FR1588445A (en) 1970-04-10
DE1804298A1 (en) 1969-06-19
US3589381A (en) 1971-06-29

Similar Documents

Publication Publication Date Title
US3570515A (en) Aminar stream cross-flow fluid diffusion logic gate
US3016063A (en) Fluid valve
US3148691A (en) Fluid controlled device
US3030979A (en) Induction fluid amplifier
US3537466A (en) Fluidic multiplier
US3170476A (en) Pure fluid amplifier
US3318329A (en) Fluid-operated logic devices
US3122062A (en) Arc discharge controlled fluid amplifier
US3232305A (en) Fluid logic apparatus
US3373759A (en) Flow control apparatus
GB1225840A (en)
GB999770A (en) Improvements in or relating to fluid logic elements
US3226023A (en) Fluid scalars
US3452772A (en) Pressure operated vortex controlled fluid analog amplifier
US3433408A (en) Binary counter
US3413994A (en) Variable gain proportional amplifier
GB992306A (en) Pure fluid logic device for performing the inhibit function
US3416551A (en) Fluid diffusion logic system
GB1086923A (en) Controlling fluid flow through apertures
US3208464A (en) Fluid stream deflecting means
US3486520A (en) Deflector fluidic amplifier
GB1067180A (en) Improvements in pure fluid devices
US3457935A (en) Fluid amplifiers
GB1364190A (en) Fluid operated device
US3461898A (en) Fluid pulse device

Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee