Movatterモバイル変換


[0]ホーム

URL:


US3857049A - Pulsed droplet ejecting system - Google Patents

Pulsed droplet ejecting system
Download PDF

Info

Publication number
US3857049A
US3857049AUS00405759AUS40575973AUS3857049AUS 3857049 AUS3857049 AUS 3857049AUS 00405759 AUS00405759 AUS 00405759AUS 40575973 AUS40575973 AUS 40575973AUS 3857049 AUS3857049 AUS 3857049A
Authority
US
United States
Prior art keywords
transducer
liquid
orifice
pulse
conduit
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
US00405759A
Inventor
S Zoltan
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Gould Inc
Original Assignee
Gould Inc
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
Priority claimed from US00260013Aexternal-prioritypatent/US3840758A/en
Application filed by Gould IncfiledCriticalGould Inc
Priority to US00405759ApriorityCriticalpatent/US3857049A/en
Application grantedgrantedCritical
Publication of US3857049ApublicationCriticalpatent/US3857049A/en
Anticipated expirationlegal-statusCritical
Expired - Lifetimelegal-statusCriticalCurrent

Links

Images

Classifications

Definitions

Landscapes

Abstract

An electro-acoustic transducer is coupled to liquid in a conduit which terminates in a small orifice adjacent to the transducer. Preferably, the acoustic impedance of the supply portion of the conduit is large compared with the acoustic impedance of the orifice. The liquid is under small or zero static pressure. Surface tension at the orifice prevents liquid flow when the transducer is not actuated. An electrical pulse with short rise time causes sudden volume change at the transducer, thereby creating an acoustic pressure pulse having sufficient amplitude to overcome the surface tension at the orifice and eject a small quantity of liquid therefrom. Thereafter, the pulse decays slowly, holding the rate of change of volume low enough so that the resulting pressure decrease is not sufficient to overcome the surface tension. Consequently, liquid flows from the supply portion of the orifice into the transducer to replace the liquid previously ejected, without drawing in air through the orifice.

Description

Zoltan PULSED DROPLET EJECTING SYSTEM [75] Inventor: Steven I. Zoltan, Shaker Heights,
Ohio
[73] Assignee: Gould Inc., Chicago, Ill. [22] Filed: Oct. 12, 1973 [21] Appl. No.: 405,759
Related US. Application Data [62] Division of Scr. Nov 260,013, June 5, 1972, which is a division of Ser. No. 70,838, Sept. 9, 1970, Pat. No.
[52] U.S. Cl. 3l0/8.l [51] Int. Cl H04r 17/00 [58] Field of Search ..'3lO/88.3,
310/8.58.7, 9.1, 9.4, 9.6; 259/DIG. 41, 1 R, DIG. 44; 417/322; 346/75, 146
451 Dec. 24, 1974 m Primary Examiner-Mark O. Budd Attorney, Agent, or Firm-Eber J. Hyde [57] ABSTRACT An electro-acoustic transducer is coupled to liquid in a conduit which terminates in a small orifice adjacent to the transducer. Preferably, the acoustic impedance of the supply portion of the conduit is large compared with the acoustic impedance of the orifice. The liquid is under small or zero static pressure. Surface tension at the orifice prevents liquid flow when the transducer is not actuated. An electrical pulse with short rise time causes sudden volume change at the transducer, thereby creating an acoustic pressure pulse having sufficient amplitude to overcome the surface tension at the orifice and eject a small quantity of liquid therefrom. Thereafter, the pulse decays slowly, holding the rate of change of volume low enough so that the re sulting pressure decrease is not sufficient to overcome the surface tension. Consequently, liquid flows from the supply portion of the orifice into the transducer to replace the liquid previously ejected, without drawing in air through the orifice.
2 Claims, 10 Drawing Figures Patented Dec. 24, 1974 3,357,049
3 Sheets-Sheet L Patented Dec. 24, 1974 3,357,049
3 Sheets-Sheet 2 Patented Dec. 24, 1974 3,857,049
3 Sheets-Sheet 3 PULSED DROPLET EJECTING SYSTEM This is a division of application Ser. No. 260,013, filed June 5, I972 which application was a division of Ser. No. 70,838, filed Sept. 9, 1970, now US. Pat. No. 3,683,212.
BACKGROUND OF THE INVENTION 1. Field of the Invention This invention pertains to a system for ejecting small quantities of liquid suitable for use in apparatus such as ink jet printers and recorders.
2. Description of the Prior Art Printers and recorders of various kinds have been developed which employ a stream of ink droplets. The ink under static pressure is expelled through a small orifice. The emerging stream of ink breaks up into droplets which tend to be of non-uniform size and spacing. It has been found that ultrasonic vibrations of suitable frequency applied to the nozzle or to the ink supply tend to regularize the spacing and size of the droplets. In some application, such as character printers and facsimile recorders, it is necessary to prevent, controllably, some of the droplets from reaching the record medium. In U.S. Pat. No. 3,298,030 to Lewis and Brown,
the unwanted droplets are deflected electrostatically away from the record medium into an ink dump. In US. Pat. No. 3,416,153 to Hertz et al., the ink jet is propelled through an opening in a shield to the record medium. When droplets are not wanted, the stream is dispersed by an electric field so that it is intercepted by the shield. These methods of droplet control are relativelycomplicated and expensive.
SUMMARY OF THE INVENTION The principal object of this invention is to provide a system which ejects a small quantity of liquid only upon electrical command.
Another object is to provide such a system which does not require a pressurized liquid supply.
Another object is to provide a system which ejects liquid upon electrical command, the quantity at each command being controllable.
According to the invention a conduit having a small orifice is supplied with liquid from a reservoir. An elec troacoustic transducer adapted to displace a small volume of liquid in response to an electrical signal is coupled to the liquid adjacent to the orifice. The orifice is sufficiently small so that surface tension prevents exit of liquid through the orifice under quiescent conditions. Means are provided for applying to the transducer. each time it is desired to have liquid expelled from the orifice, an electrical pulse having polarity tending to cause exit displacement of liquid from said transducer.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 shows a system according to the invention partly in section and partly schematic.
FIG. 1a shows a modification of the system of FIG. 1.
FIG. lb shows another modification of the system of FIG. 1.
FIG. 2 shows one of many alternate circuit arrangements suitable for use in this invention.
FIG. 2a shows a modification of the circuit of FIG. 2.
DESCRIPTION OF THE PREFERRED EMBODIMENTS Referring to FIG. 1, a reservoir shown schematically at'l contains ink or other liquid 2. A conduit indicated generally by reference characters 4 communicates with liquid 2 in the reservoir and-is filled with the liquid. Asmall orifice 5 in conduit 4 is provided for exit of liquid, shown as droplets 7.
Conduit 4 comprises a length ofsmall bore tubing 8,electroacoustic transducer 10, and orifice plate 11.Tube 8 may extend to the reservoir, or, as shown, conduit 4 may include a larger diameter portion 6, such as plastic tubing, connectingtube 8 with the reservoir.
Transducer 10 comprises a length of small diameter piezoelectricceramic tubing 13. The diameter may, for example, be about 0.05 inch.Tube 13 is provided withelectrode 14 on the inner surface andelectrode 16 on the outer surface. The electrodes, as shown, do not extend to the ends totube 13, but full length electrodes may be employed if desired.Tube 13 is polarized radially.
A thin wire 17 is wrapped aroundtube 13 in contact withouter electrode 16 and soldered thereto, as shown at 19. Wire 17 thus serves as one electrical terminal of the transducer.
Tube 8, madeof any suitable metal, such as copper or stainless steel, is cemented into the end ofceramic tube 13 by means of conductive epoxy 9 which contactsinner electrode 14. Thus,tube 8 serves as the second electrical terminal for the transducer.
For orifice plate 11, it is convenient to use a jewel watch bearing. Such jewels are readily available at low cost and have accurately controlled dimensions in the range suitable for the present use.Orifice 5 may, for example, have diameter and length on the order of 0.06 millimeter. Jewel ll may be attached to the end oftransducer 10 by means of an epoxy adhesive 12.
Transducer 10 operates by virtue of the well-known piezoelectric effect. When a d-c voltage is applied between the electrodes the length and the inside diameter of the tube both increase or decrease slightly, depending on the polarity in relation to the polarity of the polarizing d-c voltage used during manufacture. The response is nearly instantaneous, being retarded very slightly by inertia reaction.
When it is desired to have a small quantity of liquid expelled from orifice S, a short rise time voltage pulse is applied to the transducer atterminals 8 and 17, the polarity being selected to cause the contraction of the transducer. The resulting sudden decrease in the enclosed volume causes a small amount of liquid to be expelled fromorifice 5. Some liquid also is forced by the pressure pulse back intotube 8, but the amount is relatively small, due to the high acoustic impedance created by the length and small bore of the tube.
The voltage pulse is allowed to decay relatively slowly and the transducer, therefore, expands slowly to its initial volume. Due to the small rate of change of volume during decay, the accompanying pressure reduction is too small to overcome the surface tension atorifice 5. Consequently, liquid flows into the trans ducer fromtube 8 to replace the liquid previously expelled, without drawing in air throughorifice 5.
From the foregoing, it may be seen that the system of this invention ejects a small quantity of liquid on command. The command signal is the short rise time pulse. By means of simple circuitry, command pulses may be supplied to cause ejection of a succession of small quantities of liquid according to any desired time pattern, limited only by the maximum response speed of the system. In FIG. 1 a train of command pulses corresponding to exiting droplets 7 is illustrated at 22.
Static pressure on the liquid is not required. However, small positive or negative pressure does not interfere with operation. The chief requirement being that such static pressure alone must not be great enough to overcome the surface tension of the liquid atorifice 5.
When the actuating electrical pulses have energy below the level required to overcome the surface tension at the orifice, droplets are not expelled, but under stroboscopic illumination the liquid can be observed bulging out of the orifice momentarily during each pulse. At somewhat higher drive energy levels, well developed single droplets are expelled, one for each pulse. At still higher energy level, additional liquid is expelled in the form of additional, separate droplets, or the total amount of liquid expelled at each drive pulse may take the form of long cylinders of liquid with rounded ends. Thus, the quantity of liquid expelled at each pulse can be controlled by controlling the energy in the driving pulse. This enables use of the invention in recorders required to print with controlled shading, i.e., with gray scale, without the necessity of producing multipler ink spots per picture element.
Considerable latitude is available in the design of systems according to this invention. The interacting design variables are numerous and, as yet, a mathematical design technique has not been developed. However, the following guide lines and example should enable those skilled in electroacoustics' to arrive at a satisfactory design.
To avoid wasting an excessive part of each transducer pulse in driving liquid from the transducer toward the reservoir, it is desirable to have relatively high acoustic impedance looking from the transducer into the supply portion of the conduit, as provided bysmall bore tube 8 in FIG. 1. However, this is not a requirement. Satisfactory performance may be obtained without providing any constriction in the conduit. A suitable arrangement is shown in FIG. la.
In FIG. la, liquid from a reservoir, not shown, is supplied totransducer 10 by plastic hose 6' which is forced over the end of the transducer. Electrical connection to theinner electrode 14 is provided by extending the electrode over the end ofceramic tube 13 to the outer surface, as shown at 14'. Thin wire conductor 17 is secured toelectrode extension 14 by solder l9 and acts as a terminal for the transducer. With this arrangement, somewhat higher amplitude electrical pulses are required to expel liquid.
FIG. I!) shows a modification of the construction of FIG. la in which the supply line acoustic impedance is made at least as high as the impedance of the exit orifice, not including the effect of surface tension at the orifice. The modification consists in cementing to the inlet end of thetransducer 10 ajewel 11' having opening 5' with the same dimensions asexit orifice 5.
Although the arrangements of FIGs. 1a and 1b are satisfactory, generally it is desirable to provide higher acoustic impedance at the transducer inlet. In the construction of FIG. I, this is accomplished by use ofsmall bore tube 8, Other alternatives include a thin slit, or a porous member, or other acoustic resistance, at the transducer inlet through which the liquid must pass. Furthermore, some advantage would accrue when using a tube such as 8 in FIG. 1, by adding an acoustic resistance at the inlet end dimensioned to act as a matched acoustic termination for the tube as a transmission line. This would reduce, or eliminate, acoustic resonance effects intube 8. However, excellent results have been obtained without such termination.
The change in volume withintransducer 10, when the latter is pulsed, must exceed the volume of liquid to be ejected atorifice 5. The ceramic composition and the dimensions oftube 13 and the energy of the actuating pulses are factors that may be traded in arriving at a suitable design. Good results have been attained with transducer volume change calculated to be about four times the volume of the liquid to be expelled. For a fully electroded thin wall tube, unrestrained by end clamping or acoustic load, the fractional volume change due to the piezoelectric effect is approximately:
(AV/V) 3d E/t where (AV/V) volume change per unit volume d piezoelectric strain constant E applied voltage t= thickness of tube wall Care must be taken to measure wall thickness in units consistent with the units used in expressing d usually MKS units. The negative sign indicates contraction when the applied voltage has the same polarity as the original polarizing voltage.
Another requirement is that the rate of change of volume must be sufficient in relation to the acoustic impedance loading the transducer to develop enough pressure to overcome the surface tension atorifice 5.
A variety of simple circuits may be used to apply suitable command pulses to the transducer. FIG. 2 shows one example in which the capacitance of the transducer is used as part of the pulse shaping circuit. In FIG. 2,transducer 10 is shown schematically in cross section. The polarity signs indicate that the ceramic tube employed in this example was polarized during manufacture with the inner electrode positive, and the outer electrode negative. Ad-c supply 20, shown for simplicity, as a battery has the negative terminal connected to theinner electrode 14. The positive terminal ofsupply 20 is connected throughseries resistors 23, 25 to theouter electrode 16.Resistor 23 has a relatively high resistance andresistor 25 has a relatively low resistance.
Transistor 26 is used as a switch.Collector 32 is connected to the juncture betweenresistors 23 and 25, and theemitter 34 is connected to the negative side ofsupply 20.Control pulses 31 may be applied betweenbase 28 andemitter 34 viaterminals 29.
Under quiescent conditions, the switch is open and the transducer capacitance is charged to the voltage ofsupply 20. Since the polarity of the applied voltage is the opposite of the original polarizing polarity, the transducer is in an expanded state.
When apulse 31 is applied toterminals 29,transistor 26 switches to a low value of collector-emitter resistance for the duration of the pulse. This permits the capacitance of the transducer to discharge rapidly through alow resistance 25 and the transistor ON resistance. The transducer responds by contracting suddenly, expelling a small quantity of liquid atorifice 5, as previously described.
Whenpulse 31 falls approximately to zero,transistor 26 turns off, allowing the transducer capacitance to recharge throughresistors 23, 25 to the voltage ofsupply 20. Due to the higher value ofresistor 23, the charging takes place relatively slowly. The transducer responds by expanding slowly, drawing liquid fromtube 8 to replace the liquid expelled, as previously described. Thus, in response to controlpulses 31, the circuit provides short rise time command pulses having relatively long decay times, as shown at 33. For best results, the decay time should be at least four times the rise time.
rized in the following table, referring to the construction of FIG. 1:Ceramic tube 13 Composition lead zirconate-lead titanate type having the following published nominal characteristics:
K 3400 k .388 d 274 I meter/volt s l6.5 l0 meter /Newton 75 I0 kilograms/meter Length 12.7 millimeters Inside diameter .76 millimeter Wall thickness .25 millimeter Orifice Diameter .06 millimeter Length .06millimeter Supply tube 8 Inside diameter .4] millimeter Length l2.7 millimeters Liguid Water base ink having viscosity and surface tension similar to water Drive circuit FIG. 2b
Supply 50volts Transistor 26 MJ 42l Resistor 200ohms Resistor 23I000 ohms Inductor 36 2 millihenries Central pulse 31 Amplitude 3milliamperes Duration 20 microseconds Droplets Diameter of ink spot .l3 millimeter Exit velocity 1 to 2 meter/second Repetition rate up to 50.000/sccond for definitions of the characteristics listed for the ceramic material, reference may be made to: IRE Standards on Piezoelectric Crystals Measurements of Piezoelectric Ceramics. Proceedings of the IRE Vol. 49. No.7, July I961 (IEEE 1794961).
With the circuit of FIG. 2 there is a limit to thesupply voltage 20 beyond which depolarization of the ceramic may result. The limit depends on the composition of the ceramic material and on the wall thickness oftube 13. FIG. 3 illustrates a circuit arrangement that does not have these limitations but requires additional components.
In FIG. 3 the positive terminal ofsupply 20 is connected to theinner electrode 14 oftransducer 10 and the negative terminal is connected throughtransistor switch 26 andresistor 25 toouter electrode 16. When the transistor is off, no voltage appears at the transducer. When the transistor is on, the voltage ofsupply 20 is applied to the transducer with the same polarity used during polarization of the ceramic tube, thus, depolarization due to the excessive voltage cannot take place. Blockingcapacitor 35 couples the control pulses applied atterminals 29 to thetransistor base 28.Diode 37 permits the normal quiescent charge to be reestablished atcapacitor 35 as the control pulse falls to zero.
Underquiescent conditions transistor 26 is turned off and, therefore,transducer 10 has not charge. When acontrol pulse 31 occurs,transistor 26 turns on and the capacitance oftransducer 10 charges rapidly throughlow resistance 25 and the ON resistance of the transistor. This requires a low impedance supply at 20. The transducer responds by contracting rapidly, expelling liquid through the orifice. Aspulse 31 falls to zero,transistor 26 is turned off and the capacitance of the transducer discharges relatively slowly throughlarge resistance 23. The transducer responds by expanding slowly and drawing replacement liquid fromtube 8. An inductance may be connected in series with the transistor or transducer as in FIGS. 2a or 2b.
If the liquid is corrosive to the electrode material of the ceramic tube, the construction of FIG. 4 may be employed. In this case, the small boreliquid supply tube 38 extends throughtransducer tube 13. It is shown necked down at the end to formorifice 5 However. a watch jewel, such as 11 in FIG. I, or other orifice arrangement may be used.Transducer tube 13 surrounding the conduit is in stress transmitting engagement with the wall of the conduit by virtue ofepoxy cement 40 and, therefore, the transducer is coupled to the liquid within the conduit. This arrangement results in reduced sensitivity because of the stiffness ofconduit tube 38 and, therefore, higher pulse energy is required to expel liquid and it is advantageous to use a circuit such as shown in FIG. 3.
It is not necessary that the liquid flow through the transducer. For example, in FIG. 5,conduit 42 comprises smallbore supply section 8 enlarged at the end thereof for attachment of orifice plate 11. A Textension 41 couples to one end oftransducer 10. The other end oftransducer 10 is closed bycap 43. When a command pulse is applied, the transducer contracts suddenly, expelling liquid from the transducer intoconduit 42. The resulting acoustic pressure pulse ovecomes surface tension atorifice 5, causing ejection of liquid such as droplet 7. The high acoustic impedance ofsupply portion 8 retards flow back toward the reservoir. Subsequently, as the transducer expands slowly. liquid flows into the transducer fromsupply tube 8 This invention is not limited to the use of tubular piezoelectric transducers. Different geometries and constructions may be used, as well as different transducer principles. One variation is to replace piezoelectricceramic tube 13 of FIGS. 1, 4, with a tube formed from an electrostrictive material having little or no remanent polarization. In this case, a pulse of either polarity will cause the same volume contraction. and a circuit such as shown in FIG. 3 would be used.
Magnetostrictive transducers also may be employed. One way to do this is to use magnetostrictive material in formingtube 38 of FIG. 4.Transducer tube 13 then is replaced by an energizing winding magnetically coupled to the tube. To eject liquid, a short rise time current pulse is applied to the winding. Thereafter the current should decay slowly so that the surface tension at orifice 5' is not overcome while replacement liquid flows into the transducer portion oftube 38.
As another example, FIG. 6 shows a sectional view of a transducer-conduit assembly employing a thin piezoelectricceramic disc 44. It is clamped around the periphery between O-ring gaskets 46, 47 within a housing made up ofmembers 49, 50. A small cross sectionannular passageway 51 is formed around the disc by the inner walls ofbody members 49, 50, O-rings 46, 47, and the exposed edge ofdisc 44. A small boreliquid supply tube 8 is secured in opening 52 inbody member 50. The opening communicates with annular passageway 5].Tube 8 may extend to a liquid reservoir or may be coupled thereto by larger tube 6. Asecond opening 54 also communicates withannular passageway 51 and terminates at orifice plate 11. Thus, a liquid conduit is formed bysupply tubes 6 and 8, opening 52, two parallel portions ofannular passageway 51, opening 54, and
orifice plate 11.Ceramic disc 44, exposed to the liquid only at the rim, acts as an electroacoustic transducer coupled to the liquid adjacent toorifice 5.Flexible lead wires 55, 56 are soldered to theelectrodes 58, 59 ofdisc 44 and act as terminals for the transducer.
When it is desired to expel liquid from orifice 5 a short rise time voltage pulse is applied toterminal wires 55, 56 with polarity opposite the polarization polarity. This results in sudden expansion of the diameter oftransducer 44, displacing liquid fromannular passageway 51. The resulting acoustic pressure pulse expels liquid fromorifice 5. As the pulse slowly goes to zero, liquid is pulled intoannular passageway 51 fromtube 8 to replace the liquid previously expelled.
Although many different circuit arrangements may be constructed to drivetransducer 44, it is convenient to use a circuit similar to the circuit of FIG. 2. In this case, however, the negative side of supply is connected to the electrode oftransducer 44 that was negative during polarization. With this polarity, the quiescent voltage applied totransducer 44 holds the disc in diameter contracted condition. Whentransistor 26 is turned on by a pulse atterminals 29 the capacitance of the transducer discharges rapidly through the transistor andlow resistance 25. The transducer responds by expanding suddenly to the diameter it has prior to connection ofpower supply 20 and expels liquid, as previously described. When the control pulse falls to zero, the transducer recharages to the voltage ofsupply 20, contracting in diameter as it does so. to pull in fresh liquid fromtube 8.
While there have been described what are at present considered to be the preferred embodiments of this invention, it will be obvious to those skilled in the art that various changes and modifications may be made therein without departing from the invention, and it is aimed, therefore, in the appended claims to cover all such changes and modifications as fall within the true spirit and scope of the invention.
What I claim is:
l. A system adapted upon pulsing to expel a small quantity or a succession of small quantities of liquid in controlled manner, comprising:
a reservoir containing said liquid;
a conduit connected to said reservoir and communicating with the liquid therein and filled with said liquid under small or zero static pressure, said conduit having an exit orifice which is sufficiently small that surface tension in the absence of pulsing prevents said liquid from flowing therefrom; platelike piezoelectric transducer having two opposed major faces, and housing means sealed around the periphery of said transducer, said housing means forming a portion of said conduit with said ceramic transducer therein coupled to said liquid substantially only at the periphery of said transducer, substantially the full areas of said major.
faces of said transducer being free of coupling to said liquid, said transducer being adapted to expand parallel to said major faces to displace a small quantity of said liquids overcoming said surface tension to expel a small quantity of said liquid through said orifice and to contract prior to a subsequent expansion;
electrical circuit means connected to said transducer for applying thereto an electrical pulse of a given polarity to cause said transducer to expand and upon decay of said pulse to allow said transducer to contract;
said conduit during operation of said system at all times being open from said reservoir to said orifice whereby the liquid within said housing is replaced by liquid from said reservoir to make up for said expelled liquid upon termination of said pulse.
2. A system as described in claim 1 in which said transducer is a piezoelectric ceramic transducer, said major faces are circular, and said transducer is adapted to expand radially.

Claims (2)

1. A system adapted upon pulsing to expel a small quantity or a succession of small quantities of liquid in controlled manner, comprising: a reservoir containing said liquid; a conduit connected to said reservoir and communicating with the liquid therein and filled with said liquid under small or zero static pressure, said conduit having an exit orifice which is sufficiently small that surface tension in the absence of pulsing prevents said liquid from flowing therefrom; a platelike piezoelectric transducer having two opposed major faces, and housing means sealed around the periphery of said transducer, said housing means forming a portion of said conduit with said ceramic transducer therein coupled to said liquid substantially only at the periphery of said transducer, substantially the full areas of said major faces of said transducer being free of coupling to said liquid, said transducer being adapted to expand parallel to said major faces to displace a small quantity of said liquids overcoming said surface tension to expel a small quantity of said liquid through said orifice and to contract prior to a subsequent expansion; electrical circuit means connected to said transducer for applying thereto an electrical pulse of a given polarity to cause said transducer to expand and upon decay of said pulse to allow said transducer to contract; said conduit during operation of said system at all times being open from said reservoir to said orifice whereby the liquid within said housing is replaced by liquid from said reservoir to make up for said expelled liquid upon termination of said pulse.
US00405759A1972-06-051973-10-12Pulsed droplet ejecting systemExpired - LifetimeUS3857049A (en)

Priority Applications (1)

Application NumberPriority DateFiling DateTitle
US00405759AUS3857049A (en)1972-06-051973-10-12Pulsed droplet ejecting system

Applications Claiming Priority (2)

Application NumberPriority DateFiling DateTitle
US00260013AUS3840758A (en)1970-09-091972-06-05Pulsed droplet ejecting system
US00405759AUS3857049A (en)1972-06-051973-10-12Pulsed droplet ejecting system

Publications (1)

Publication NumberPublication Date
US3857049Atrue US3857049A (en)1974-12-24

Family

ID=26947675

Family Applications (1)

Application NumberTitlePriority DateFiling Date
US00405759AExpired - LifetimeUS3857049A (en)1972-06-051973-10-12Pulsed droplet ejecting system

Country Status (1)

CountryLink
US (1)US3857049A (en)

Cited By (48)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
DE2715189A1 (en)*1976-04-281977-11-17Gould Inc INK SUPPLY SYSTEM FOR INK JET PEN
US4209794A (en)*1977-06-241980-06-24Siemens AktiengesellschaftNozzle plate for an ink recording device
DE3007189A1 (en)*1979-04-251980-11-06Xerox Corp DEVICE WORKING WITH PRESSURE IMPULSES FOR THE PRODUCTION OF LIQUID DROPS
US4243995A (en)*1979-06-011981-01-06Xerox CorporationEncapsulated piezoelectric pressure pulse drop ejector apparatus
US4393384A (en)*1981-06-051983-07-12System Industries Inc.Ink printhead droplet ejecting technique
US4516140A (en)*1983-12-271985-05-07At&T Teletype CorporationPrint head actuator for an ink jet printer
US4525645A (en)*1983-10-111985-06-25Southwest Research InstituteCylindrical bender-type vibration transducer
US4584590A (en)*1982-05-281986-04-22Xerox CorporationShear mode transducer for drop-on-demand liquid ejector
US4625373A (en)*1985-08-021986-12-02Advanced Color Technology, Inc.Method of making a printing head for an ink jet printer
JPS63139253A (en)*1986-11-171988-06-11アボット・ラボラトリーズDevice and method for mixing and printing reagent liquid
US4879568A (en)*1987-01-101989-11-07Am International, Inc.Droplet deposition apparatus
US5227813A (en)*1991-08-161993-07-13Compaq Computer CorporationSidewall actuator for a high density ink jet printhead
US5235352A (en)*1991-08-161993-08-10Compaq Computer CorporationHigh density ink jet printhead
US5327041A (en)*1991-07-051994-07-05Rockwell International CorporationBiaxial transducer
US5373314A (en)*1992-08-271994-12-13Compaq Computer CorporationInk jet print head
US5400064A (en)*1991-08-161995-03-21Compaq Computer CorporationHigh density ink jet printhead with double-U channel actuator
US5402162A (en)*1991-08-161995-03-28Compaq Computer CorporationIntegrated multi-color ink jet printhead
US5406319A (en)*1991-08-161995-04-11Compaq Computer CorporationEnhanced U type ink jet printheads
US5426455A (en)*1993-05-101995-06-20Compaq Computer CorporationThree element switched digital drive system for an ink jet printhead
US5433809A (en)*1991-08-161995-07-18Compaq Computer CorporationMethod of manufacturing a high density ink jet printhead
US5436648A (en)*1991-08-161995-07-25Compaq Computer CorporationSwitched digital drive system for an ink jet printhead
US5444467A (en)*1993-05-101995-08-22Compaq Computer CorporationDifferential drive system for an ink jet printhead
US5461403A (en)*1991-08-161995-10-24Compaq Computer CorporationDroplet volume modulation techniques for ink jet printheads
US5479684A (en)*1993-12-301996-01-02Compaq Computer CorporationMethod of manufacturing ink jet printheads by induction heating of low melting point metal alloys
US5505364A (en)*1993-12-301996-04-09Compaq Computer CorporationMethod of manufacturing ink jet printheads
US5521618A (en)*1991-08-161996-05-28Compaq Computer CorporationDual element switched digital drive system for an ink jet printhead
US5543009A (en)*1991-08-161996-08-06Compaq Computer CorporationMethod of manufacturing a sidewall actuator array for an ink jet printhead
US5557304A (en)*1993-05-101996-09-17Compaq Computer CorporationSpot size modulatable ink jet printhead
US5652609A (en)*1993-06-091997-07-29J. David SchollerRecording device using an electret transducer
US5747671A (en)*1995-10-201998-05-05Ngk Insulators, Ltd.Axial flow particle sensor
US5854645A (en)*1993-07-191998-12-29Oce-Nederland B.V.Inkjet array
US5969236A (en)*1996-08-201999-10-19Ngk Insulators, Ltd.Particle sensor
US6029896A (en)*1997-09-302000-02-29Microfab Technologies, Inc.Method of drop size modulation with extended transition time waveform
US6070973A (en)*1997-05-152000-06-06Massachusetts Institute Of TechnologyNon-resonant and decoupled droplet generator
US6114187A (en)*1997-01-112000-09-05Microfab Technologies, Inc.Method for preparing a chip scale package and product produced by the method
WO2000064678A1 (en)*1999-04-222000-11-02Silverbrook Research Pty. Ltd.Actuator control in a micro electro-mechanical liquid ejection device
US6188416B1 (en)1997-02-132001-02-13Microfab Technologies, Inc.Orifice array for high density ink jet printhead
US6325475B1 (en)1996-09-062001-12-04Microfab Technologies Inc.Devices for presenting airborne materials to the nose
US20030173873A1 (en)*2002-03-152003-09-18National Aeronautics And Space AdministrationElectro-active device using radial electric field piezo-diaphragm for control of fluid movement
AU770756B2 (en)*1999-04-222004-03-04Memjet Technology LimitedActuator control in a micro electro-mechanical liquid ejection device
US6727497B2 (en)1998-09-232004-04-27Wisconsin Alumni Research FoundationCharge reduction in electrospray mass spectrometry
US20040169137A1 (en)*2002-11-272004-09-02Westphall Michael S.Inductive detection for mass spectrometry
US6797945B2 (en)2001-03-292004-09-28Wisconsin Alumni Research FoundationPiezoelectric charged droplet source
US20040217186A1 (en)*2003-04-102004-11-04Sachs Emanuel MPositive pressure drop-on-demand printing
US20070102634A1 (en)*2005-11-102007-05-10Frey Brian LElectrospray ionization ion source with tunable charge reduction
US20080191584A1 (en)*2007-02-082008-08-14Malkin Matthew CSpring disc energy harvester apparatus and method
US20100237748A1 (en)*2007-02-082010-09-23The Boeing CompanySpring disc energy harvester apparatus and method
US9925547B2 (en)*2014-08-262018-03-27Tsi, IncorporatedElectrospray with soft X-ray neutralizer

Citations (3)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US2928409A (en)*1955-01-311960-03-15Textron IncNon-magnetic electro hydraulic transfer valve
US3150592A (en)*1962-08-171964-09-29Charles L StecPiezoelectric pump
US3264861A (en)*1964-06-081966-08-09Lockheed Aircraft CorpDynamic pressure generator

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US2928409A (en)*1955-01-311960-03-15Textron IncNon-magnetic electro hydraulic transfer valve
US3150592A (en)*1962-08-171964-09-29Charles L StecPiezoelectric pump
US3264861A (en)*1964-06-081966-08-09Lockheed Aircraft CorpDynamic pressure generator

Cited By (63)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
DE2715189A1 (en)*1976-04-281977-11-17Gould Inc INK SUPPLY SYSTEM FOR INK JET PEN
US4209794A (en)*1977-06-241980-06-24Siemens AktiengesellschaftNozzle plate for an ink recording device
DE3007189A1 (en)*1979-04-251980-11-06Xerox Corp DEVICE WORKING WITH PRESSURE IMPULSES FOR THE PRODUCTION OF LIQUID DROPS
US4243995A (en)*1979-06-011981-01-06Xerox CorporationEncapsulated piezoelectric pressure pulse drop ejector apparatus
US4393384A (en)*1981-06-051983-07-12System Industries Inc.Ink printhead droplet ejecting technique
US4584590A (en)*1982-05-281986-04-22Xerox CorporationShear mode transducer for drop-on-demand liquid ejector
US4525645A (en)*1983-10-111985-06-25Southwest Research InstituteCylindrical bender-type vibration transducer
US4516140A (en)*1983-12-271985-05-07At&T Teletype CorporationPrint head actuator for an ink jet printer
US4625373A (en)*1985-08-021986-12-02Advanced Color Technology, Inc.Method of making a printing head for an ink jet printer
JPS63139253A (en)*1986-11-171988-06-11アボット・ラボラトリーズDevice and method for mixing and printing reagent liquid
EP0268237A3 (en)*1986-11-171988-11-30Abbott LaboratoriesApparatus and process for reagent fluid dispensing and printing
AU603617B2 (en)*1986-11-171990-11-22Abbott LaboratoriesApparatus and process for reagent fluid dispensing and printing
US4879568A (en)*1987-01-101989-11-07Am International, Inc.Droplet deposition apparatus
US4887100A (en)*1987-01-101989-12-12Am International, Inc.Droplet deposition apparatus
USRE36667E (en)*1987-01-102000-04-25Xaar LimitedDroplet deposition apparatus
US5327041A (en)*1991-07-051994-07-05Rockwell International CorporationBiaxial transducer
US5554247A (en)*1991-08-161996-09-10Compaq Computer CorporationMethod of manufacturing a high density ink jet printhead array
US5436648A (en)*1991-08-161995-07-25Compaq Computer CorporationSwitched digital drive system for an ink jet printhead
US5400064A (en)*1991-08-161995-03-21Compaq Computer CorporationHigh density ink jet printhead with double-U channel actuator
US5402162A (en)*1991-08-161995-03-28Compaq Computer CorporationIntegrated multi-color ink jet printhead
US5406319A (en)*1991-08-161995-04-11Compaq Computer CorporationEnhanced U type ink jet printheads
US5235352A (en)*1991-08-161993-08-10Compaq Computer CorporationHigh density ink jet printhead
US5433809A (en)*1991-08-161995-07-18Compaq Computer CorporationMethod of manufacturing a high density ink jet printhead
US5543009A (en)*1991-08-161996-08-06Compaq Computer CorporationMethod of manufacturing a sidewall actuator array for an ink jet printhead
US5521618A (en)*1991-08-161996-05-28Compaq Computer CorporationDual element switched digital drive system for an ink jet printhead
US5461403A (en)*1991-08-161995-10-24Compaq Computer CorporationDroplet volume modulation techniques for ink jet printheads
US5227813A (en)*1991-08-161993-07-13Compaq Computer CorporationSidewall actuator for a high density ink jet printhead
US5373314A (en)*1992-08-271994-12-13Compaq Computer CorporationInk jet print head
US5444467A (en)*1993-05-101995-08-22Compaq Computer CorporationDifferential drive system for an ink jet printhead
US5557304A (en)*1993-05-101996-09-17Compaq Computer CorporationSpot size modulatable ink jet printhead
US5426455A (en)*1993-05-101995-06-20Compaq Computer CorporationThree element switched digital drive system for an ink jet printhead
US5652609A (en)*1993-06-091997-07-29J. David SchollerRecording device using an electret transducer
US5854645A (en)*1993-07-191998-12-29Oce-Nederland B.V.Inkjet array
US5505364A (en)*1993-12-301996-04-09Compaq Computer CorporationMethod of manufacturing ink jet printheads
US5479684A (en)*1993-12-301996-01-02Compaq Computer CorporationMethod of manufacturing ink jet printheads by induction heating of low melting point metal alloys
US5747671A (en)*1995-10-201998-05-05Ngk Insulators, Ltd.Axial flow particle sensor
US5969236A (en)*1996-08-201999-10-19Ngk Insulators, Ltd.Particle sensor
US6325475B1 (en)1996-09-062001-12-04Microfab Technologies Inc.Devices for presenting airborne materials to the nose
US6114187A (en)*1997-01-112000-09-05Microfab Technologies, Inc.Method for preparing a chip scale package and product produced by the method
US6188416B1 (en)1997-02-132001-02-13Microfab Technologies, Inc.Orifice array for high density ink jet printhead
US6070973A (en)*1997-05-152000-06-06Massachusetts Institute Of TechnologyNon-resonant and decoupled droplet generator
US6029896A (en)*1997-09-302000-02-29Microfab Technologies, Inc.Method of drop size modulation with extended transition time waveform
US6727497B2 (en)1998-09-232004-04-27Wisconsin Alumni Research FoundationCharge reduction in electrospray mass spectrometry
WO2000064678A1 (en)*1999-04-222000-11-02Silverbrook Research Pty. Ltd.Actuator control in a micro electro-mechanical liquid ejection device
US6457795B1 (en)1999-04-222002-10-01Silverbrook Research Pty LtdActuator control in a micro electro-mechanical device
CN1318215C (en)*1999-04-222007-05-30西尔弗布鲁克研究有限公司Liquid injector with micro-mechanoelectric device
AU770756B2 (en)*1999-04-222004-03-04Memjet Technology LimitedActuator control in a micro electro-mechanical liquid ejection device
US6797945B2 (en)2001-03-292004-09-28Wisconsin Alumni Research FoundationPiezoelectric charged droplet source
US6906322B2 (en)2001-03-292005-06-14Wisconsin Alumni Research FoundationCharged particle source with droplet control for mass spectrometry
US6856073B2 (en)2002-03-152005-02-15The United States Of America As Represented By The Administrator Of The National Aeronautics And Space AdministrationElectro-active device using radial electric field piezo-diaphragm for control of fluid movement
WO2003079409A3 (en)*2002-03-152004-05-13NasaElectro-active device using radial electric field piezo-diaphragm for control of fluid movement
US20030173873A1 (en)*2002-03-152003-09-18National Aeronautics And Space AdministrationElectro-active device using radial electric field piezo-diaphragm for control of fluid movement
US7078679B2 (en)2002-11-272006-07-18Wisconsin Alumni Research FoundationInductive detection for mass spectrometry
US20040169137A1 (en)*2002-11-272004-09-02Westphall Michael S.Inductive detection for mass spectrometry
US20040217186A1 (en)*2003-04-102004-11-04Sachs Emanuel MPositive pressure drop-on-demand printing
US7077334B2 (en)2003-04-102006-07-18Massachusetts Institute Of TechnologyPositive pressure drop-on-demand printing
US20070102634A1 (en)*2005-11-102007-05-10Frey Brian LElectrospray ionization ion source with tunable charge reduction
US7518108B2 (en)2005-11-102009-04-14Wisconsin Alumni Research FoundationElectrospray ionization ion source with tunable charge reduction
US20080191584A1 (en)*2007-02-082008-08-14Malkin Matthew CSpring disc energy harvester apparatus and method
US20100237748A1 (en)*2007-02-082010-09-23The Boeing CompanySpring disc energy harvester apparatus and method
US8415860B2 (en)*2007-02-082013-04-09The Boeing CompanySpring disc energy harvester apparatus and method
US9705430B2 (en)2007-02-082017-07-11The Boeing CompanyMethod of forming a disc spring-based energy harvesting device
US9925547B2 (en)*2014-08-262018-03-27Tsi, IncorporatedElectrospray with soft X-ray neutralizer

Similar Documents

PublicationPublication DateTitle
US3857049A (en)Pulsed droplet ejecting system
US3683212A (en)Pulsed droplet ejecting system
US3902083A (en)Pulsed droplet ejecting system
US3840758A (en)Pulsed droplet ejecting system
SU1060098A3 (en)Method for controlling ink writing members and device for controlling ink writing member
US3832579A (en)Pulsed droplet ejecting system
US4005435A (en)Liquid jet droplet generator
US4112433A (en)Meniscus dampening drop generator
US4584590A (en)Shear mode transducer for drop-on-demand liquid ejector
US4233610A (en)Hydrodynamically damped pressure pulse droplet ejector
EP0046676B2 (en)Method of operating an on demand-type ink jet head and system therefor
US3452360A (en)High-speed stylographic apparatus and system
EP0816081A2 (en)Ink jet recording apparatus and method of driving the same
US4095238A (en)Piezoelectric drive element for the printer heads used in ink-operated mosaic printer units
GB2094233A (en)Ink jet apparatus
EP0548984A1 (en)Ink jet type recording head driving circuit
ES524161A0 (en) CONTROL SYSTEM OF A WRITING ELEMENT BY SELECTIVE INK JET
US3512172A (en)Ink drop writer nozzle
US4727379A (en)Accoustically soft ink jet nozzle assembly
EP0060881A1 (en)Ink jet printer
US3334350A (en)Magnetostrictive ink jet
US3965376A (en)Pulsed droplet ejecting system
US2713639A (en)Shock-excited oscillatory circuit
USRE35737E (en)Accoustically soft ink jet nozzle assembly
JP3322276B2 (en) Driving method and apparatus for inkjet recording head

[8]ページ先頭

©2009-2025 Movatter.jp