Apparatus for printing with ink jet chambers utilizing a plurality of orifices

Abstract
A dense array of ink jets is achieved by a fanning-in of chambers to a linear array of orifices. The ends of the chambers remote from the orifices have actuation locations which are coupled to elongated transducers having axes of elongation which are parallel to the axes of ejection of droplets from the orifices.
Description




BACKGROUND OF THE INVENTION




This invention relates to impulse or drop-on demand ink jet printers employing an array of ink jets which are capable of printing a substantial field of droplets on demand.




U.S. Pat. No. 4,714,934 discloses an ink jet apparatus of the type shown in

FIGS. 1 through 3

. The apparatus includes a print head


10


having a reservoir


12


and an imaging head of


14


. The print head


10


is juxtaposed to a target


16


which is advanced by means of a transport system, including rollers


18


and


20


, in an incremental fashion. As shown in

FIG. 1

, print head


10


includes an orifice plate


22


, including orifices


24


. In

FIG. 1

, the orifices are shown further apart from each other than they are in practice for purposes of illustration.




The orifices


24


actually comprise a plurality of sets of orifices which are more fully described with reference to

FIGS. 2 and 3

. The sets of orifices


24


are vertically displaced as a result of the inclination of the print head


10


with respect to the scanning direction depicted by arrow


26


. The orifices


24


are arranged in groups of three (3) and inclined on the orifice plate


22


so as to be substantially vertical when the print head


10


is inclined with respect to the scanning direction


26


as shown in FIG.


1


. The hash marks


28


and the orifice plate actually show this angle of inclination. The angle of the orifices


24


in each group with respect to the vertical as shown in

FIG. 2

is chosen such that when the orifice plate


22


is inclined as shown in

FIG. 1

, sets of orifices


24


will be vertical. As scanning in the direction depicted by the arrow


26


proceeds, there is no overlap of any droplets projected from the orifices so as to permit the apparatus as shown in

FIGS. 1 through 3

to create a vertical bar when the droplets are ejected sequentially in the proper timed relationship. Of course, the droplets can also produce an alphanumeric character by ejecting appropriate droplets on demand.




By changing the angle of inclination of the hash marks


28


, it is possible to change the angle of inclination of the print head


14


. However, if the angle of inclination is increased beyond a certain limit, it becomes impossible to print a continuous bar since the orifices cannot be spaced sufficiently close together to provide full coverage of the field. In addition, the chambers associated with those orifices become starved for ink when operated at a sufficiently high frequency. Moreover, it has not been possible to increase the number of chambers since cross-talk and limited real estate do not allow transducers to be coupled to the chambers.




As also shown in U.S. Pat. No. 4,714,934, the individual ink jets include feet which are coupled to the ink jet chambers. These feet


46


are secured to a foot plate by a resilient rubber-like material, such as silicone. As a consequence, ink within the ink jet chambers is exposed to a variety of materials including the foot, the silicone and the materials from which the remainder of the ink jet including the chamber and the orifices are made. This in turn produces compatibility problems which effectively limit the type of ink which may be employed in an ink jet apparatus.




SUMMARY OF THE INVENTION




In accordance with one important aspect of the invention, an ink jet apparatus is provided whereby the spacing between a plurality of impulse ink jets in an array is substantially reduced thereby increasing the ability to print high quality images with an in-line array of orifices while minimizing cross-talk.




In accordance with this object of the invention, an ink jet apparatus comprises an array of chambers, each of the chambers being terminated in at least one orifice such that the linear array of orifices is formed. Each of the chambers includes an actuation location laterally displaced from the linear orifice array. A plurality of elongated transducers is juxtaposed to the actuation locations respectively such that the transducers have an axis of elongation extending substantially parallel with the ejection axis of each orifice and laterally displaced with respect to the linear orifice array.




In accordance with one important aspect of the invention, the actuation locations of adjacent chambers in the array of ink jet devices are mutually laterally displaced.




In accordance with another important aspect of the invention, the axis of chambers are inclined at an acute angle with respect to the ejection axis of the chambers.




In accordance with another important aspect of the invention, the axes of the chambers are elbowed to include a first segment substantially parallel to the ejection axis and a second segment substantially perpendicular to the ejection axis.




In accordance with still another important aspect of the invention, the axes of elongation of adjacent transducers are parallel but laterally displaced with respect to the axis of ejection from each of the orifices.




In accordance with yet another important aspect of the invention, each of the chambers may include one or more orifices.




It is another object of this invention to provide an impulse ink jet apparatus which has a high degree of compatibility with various inks. In accordance with this object of the invention, the ink jet apparatus includes an ink jet chamber, a transducer coupled to the chamber and a diaphragm separating the transducer from the chamber. In the preferred embodiment of the invention, the chamber and the diaphragm comprise a relatively inert material such as, for example, stainless steel.




The transducer is bonded to the diaphragm by a suitable adhesive such as for example, a silicone adhesive. The transducer may also be encapsulated in a silicone material for acoustic damping.




Preferably, the chamber is formed by sandwiching a plurality of stainless steel plates together including the diaphragm. The plates may comprise an orifice plate, chamber plate, a restrictor plate providing a restricted opening for ink to enter the chamber, the diaphragm and a spacer plate separating the diaphragm from the restrictor plate such that movement of the diaphragm does not affect the size of the restricted opening to the ink jet chamber.











DETAILED DESCRIPTION OF THE DRAWINGS





FIG. 1

is a perspective view of the prior art ink jet printing apparatus previously discussed;





FIG. 2

is a plan view of an orifice plate of the prior art apparatus shown in

FIG. 1

;





FIG. 3

is a fragmentary view of the fragment


3


of the prior art apparatus shown in

FIG. 2

;





FIG. 4

is a plan view of the orifice plate of an ink jet apparatus embodying this invention;





FIG. 5

is an enlarged view of the fragment


5


shown in

FIG. 4

;





FIG. 6

is a sectional view of the ink jet apparatus of

FIG. 4

taken along line


6





6


of

FIG. 5

;





FIG. 6A

is a partial view similar to

FIG. 6

but depicting a second embodiment of the invention (in this embodiment, the elongated portions of chambers


126


are implemented with right angles);





FIG. 7

is an enlarged fragmentary view of a fragment of

FIG. 6

;





FIG. 7A

is a view similar to

FIG. 7

but of the second embodiment depicted in

FIG. 6A

;





FIG. 8

is a plan view of an orifice plate representing another embodiment of the invention;





FIG. 9

is a fragmentary sectional view of the apparatus of

FIG. 8

taken along line


9





9


;





FIG. 10

is a plan view of the orifice plate of another ink jet apparatus representing yet another embodiment of the invention;





FIG. 11

is an enlarged fragmentary sectional view of the ink jet apparatus of

FIG. 10

;





FIG. 11A

is a view similar to

FIG. 11

but of yet another embodiment similar to that of

FIGS. 6A and 7A

;





FIG. 12

is a plan view of another ink jet apparatus orifice plate representing another embodiment of the invention;





FIG. 13

is a sectional view of the ink jet apparatus of

FIG. 12

taken along line


13





13


.











DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS




Referring to

FIGS. 4-6

, one preferred embodiment of the invention comprises an orifice plate


122


having groups of three orifices


124


forming a linear array. In all, a total of


64


groups of orifices


124


are shown. Each linear array of orifices


124


is inclined such that the orifices


124


are vertically disposed with respect to the scanning direction when incorporated in a print head similar to that shown in FIG.


1


. The angle of inclination of the orifice plate and thus the linear array of orifices


124


is 47.105 degrees so as to provide an overall field height h of 1.36 inches. As should be appreciated, the spacing between the groups of orifices


124


is necessarily small.




As shown in

FIGS. 5-7

, the orifices


124


terminate ink jet chambers


126


in drop-on-demand or impulse devices of the general type disclosed in U.S. Pat. No. 4,646,106, incorporated herein by reference. Because the chambers


126


are necessarily closely spaced, it is not possible to confine the chambers to the area between adjacent groups of orifices


124


. Rather, it is necessary to laterally extend the chambers


126


in opposite directions so as to provide actuation locations


128


which are laterally displaced from the linear array. As best shown in

FIG. 5

, the actuation locations


128


of adjacent chambers


126


are mutually laterally displaced. By virtue of this lateral displacement, there is sufficient room for elongated transducers


130


, shown in

FIG. 6

, to eject droplets of ink on demand from the orifices


124


without cross-talk between chambers.




As best shown in

FIGS. 6

,


6


A,


7


and


7


A, the chambers


126


or


126


′ may include either elongated sections


134


which are disposed at an acute angle with respect to the axis of ejection of droplets from orifice


124


as well as the axis of elongation of the transducers


130


or a elongated sections


134


′ which project along the axis of elongation of the transducers, then bend 90° towards the centerline or axis of ejection of droplets from orifice


124


and then bend 90° again traversing along the axis of ejection of droplets from orifice


124


.




The inclined or elbowed, elongated portions


134


(or


134


′) of the chambers


126


(or


126


′) create a fanning-in effect so as to permit alignment of the groups of orifices


124


in a linear array while providing separation of the elongated transducers


130


. Note that only a single orifice is shown in

FIGS. 7 and 7A

since the sections represented by

FIGS. 6

,


6


A,


7


and


7


A is through a single orifice. However, it will be appreciated that there are up to three orifices associated with each of the chambers


126


or


126


′ shown in

FIGS. 6

,


6


A,


7


and


7


A. By utilizing this fanning-in effect, it is possible to achieve greater chamber density. For example, it is possible to achieve a chamber-to-chamber spacing of less than 0.0500 inches, preferably less than 0.0400 inches, and optimally less than 0.0300 inches without cross-talk. The fan-in effect also allows chamber-to-chamber spacing of less than ten times the diameter or cross-sectional dimension of the chamber and preferably less than seven times this diameter.




As also shown in

FIGS. 6 and 6A

, the ink jet apparatus includes a restrictor plate


138


having openings


140


which connect the actuation locations


128


with manifolds


142


. The manifolds


142


service an aligned row of actuation locations


128


with ink while an other manifold


142


services another aligned row of actuation locations


128


with ink. Additional manifolds


142


external to the elbowed elongated portions


134


′ of the chambers in

FIG. 6A

create additional fluidic compliance and permit secondary servicing of center manifold


142


′ and downstream activation locations


128


.




In accordance with another important aspect of the invention, the ink which is ejected from the orifices


124


is separated from the transducer and its mounting materials by a relatively inert diaphragm


144


(see FIG.


6


). Preferably, the diaphragm comprises stainless steel. Diaphragm


144


moves with the transducers


130


so as to eliminate ink compatibility problems. In order to assure that deflection of the diaphragm


144


by the transducers


130


does not affect the size of the restrictor opening


140


, a spacer plate


146


is inserted between the diaphragm


144


and the restrictor plate


138


.




In accordance with an important aspect of the invention, the diaphragm


144


(

FIG. 6

) is secured to the transducers


130


by an elastomeric adhesive (e.g., silicone) which extends upwardly into openings


148


in a body


150


and forms a layer


152


along the top of the diaphragm


144


. As a consequence, retraction of the transducer


130


pulls the diaphragm


144


upwardly at the actuation locations


128


so as to permit additional ink from the manifolds


142


to enter the chambers


126


. When the transducers


130


are deenergized (i.e., electrically grounded), the diaphragm


144


will return to the quiescent, planar condition and droplets of ink


136


will be ejected from the orifices


124


as shown in

FIGS. 7 and 7A

. In addition to the silicone adhesive, the transducer is secured to the body


150


and a central mounting


156


by an LRTV silicone


154


. A conductive epoxy


158


(e.g., a silver epoxy) joins the transducers


130


to the mounting


156


at the extremity remote from the diaphragm


144


.




Referring now to

FIGS. 8 and 9

, another embodiment of the invention is shown wherein the angle of inclination α of an orifice plate


222


is reduced to 29.236 degrees so as to provide an overall field height of 0.92 inches. The orifices


224


are arranged in groups of two. Thus the density of chambers from end to end of the orifice plate,


64


chambers in all, remains the same although the number of orifices is reduced since there are only two orifices


224


per chamber. As in the case of the embodiment of

FIGS. 4

,


5


,


6


and


7


, the elongated portions of the chambers


226


are inclined so as to provide lateral displacement of the actuation locations of the chambers, which are not shown in

FIGS. 8 and 9

. However, it will be appreciated that the chambers look substantially as shown in

FIGS. 6 and 7

such that the elongated portions of chambers


226


are inclined with respect to the axis of ejection for the droplets


236


as well as the axis of elongation for the elongated transducers.




Referring now to

FIGS. 10

,


11


and


11


A, an orifice plate


322


is shown having a total of 64 channels terminating in orifices


324


. The orifices and channels or chambers are arrayed in linear fashion at an angle a of 14.135 degrees with respect to the scanning axis so as to provide an overall field dimension h equal to 0.46 inches. As shown in

FIG. 11

, the chambers


326


are once again inclined with respect to the axis of ejection of droplets


336


. As shown in

FIG. 6

, the elongated transducers are also inclined with respect to the chambers


326


. It will therefore be appreciated that, with reference to

FIGS. 10 and 11

, there are a total of 64 channels shown with 64 orifices, i.e., one orifice per chamber. This also applies to embodiments of

FIGS. 6A and 11A

in that there are a total of 64 channels shown with 64 orifices, i.e., one orifice per chamber.




Reference will now be made to

FIGS. 12 and 13

and the ink jet apparatus shown therein.

FIG. 12

depicts an orifice plate


422


having groups of orifices


424


, i.e., 3 orifices per channel or group. The chambers


426


extend laterally outwardly from the linear array of orifices


424


such that actuation locations


428


are laterally displaced from the linear array. As shown in

FIG. 13

, the chambers


428


are not inclined with respect to the axis of ejection of droplets


436


but are formed with a right angle configuration. A first portion


434


extends laterally outwardly from the orifice to the actuation location


428


. A single manifold


150


is shown which through the use of a restrictor plate, not shown serves all chambers extending laterally outwardly from the linear array.




With the various embodiments described, it will be appreciated that the center-to-center spacing between the chambers may be substantially reduced, thereby providing increased resolution. Heretofore, prior art of the types shown in

FIGS. 1-3

provide a center distance between chambers of approximately 0.0585 inches. Employing the principles of this invention, it is possible to reduce that center-to-center spacing of 64 chambers shown in

FIG. 4

to 0.02952 inches.




In accordance with an important aspect of the invention, in particular the use of a stainless steel diaphragm, it is possible to provide for an ink jet device wherein substantially all materials exposed to the ink are relatively inert. In this regard, it is possible to provide a restrictor plate


138


and diaphragm


144


and a spacer plate


146


which are all stainless steel. It is also possible and preferred to provide a chamber plate in which the chambers


126


and the manifolds


142


are formed which comprises stainless steel or another relatively inert material. Other relatively inert materials include Kapton, PET or Teflon.




It will be appreciated that various configurations of chambers, orifices and chamber shapes may be utilized. For example, the number of chambers may exceed


64


. For example, an array of 128 or 256 chambers or more may be utilized. It is also possible to terminate chambers in more than three orifices. For example, chambers terminating in four, five or six orifices or more are possible. Finally, it is possible to utilize various chamber shapes in addition to the inclined, elbowed or L-shaped chambers disclosed herein. It will further be appreciated that alignment of the array of orifices in linear fashion allows the use of various angles of inclination of the head thereby permitting a wide variety of applications of the ink jet apparatus.




Although preferred embodiments of the invention have been shown and described, it will be appreciated that various modifications may be made which will fall within the true spirit and scope of the invention as set forth in the appended claims.



Claims
  • 1. An impulse jet apparatus comprising:a plurality of side-by-side orifices forming a linear array, wherein each of said orifices ejects droplets along an ejection axis and opens into at least one chamber, each of said chambers mutually laterally displaced from adjacent chambers, and each of said chambers having an actuation location laterally displaced from the linear array and offset along the linear array from the actuation locations of adjacent chambers.
  • 2. The impulse jet apparatus of claim 1, wherein the chambers have axis that are inclined at an angle with respect to said ejection axis.
  • 3. The impulse jet apparatus of claim 2, wherein said angle is acute.
  • 4. The impulse jet apparatus of claim 2, wherein said angle is obtuse.
  • 5. The impulse jet apparatus of claim 1, wherein the axis of the chambers are elbowed and include a first segment substantially parallel to the ejection axis and a second segment substantially perpendicular to the ejection axis.
  • 6. The impulse jet apparatus of claim 1, wherein the axis of the chambers are elbowed and include a first segment substantially perpendicular to the ejection axis and a second segment substantially parallel to the ejection axis.
  • 7. The impulse jet apparatus of claim 6, wherein said axis of the chambers further comprise a third segment perpendicular to the ink ejection axis.
  • 8. The impulse jet apparatus of claim 1, wherein said plurality of side-by-side orifices forming a linear array comprises groups of orifices arranged side-by-side.
  • 9. The impulse jet apparatus of claim 8, wherein for each of said groups of orifices, the orifices open into a single chamber.
  • 10. The impulse jet apparatus of claim 8, wherein each of said groups of orifices comprises three orifices.
  • 11. The impulse jet apparatus of claim 8, wherein each of said groups of orifices comprises two orifices.
  • 12. The impulse jet apparatus of claim 8, wherein each of said groups of orifices comprises between 1 and 10 orifices.
  • 13. The impulse jet apparatus of claim 8, having a chamber-to-chamber spacing between adjacent chambers less than 0.0500 inches.
  • 14. The impulse inkjet apparatus of claim 13, wherein said chamber-to-chamber spacing is less than 0.0400 inches.
  • 15. The impulse inkjet apparatus of claim 13, wherein said chamber-to-chamber spacing is less than 0.0300 inches.
  • 16. The impulse jet apparatus of claim 1, wherein said chambers have a portion extending from the actuation locations respectively arranged in a fanning-in effect.
  • 17. The impulse jet apparatus of claim 16, wherein said chamber-to-chamber spacing is less than 0.0300 inches and at least one of said chamber portions is inclined or elbowed.
  • 18. The impulse jet apparatus of claim 1, further comprisinga plurality of elongated transducers juxtaposed to said actuation locations respectively, and laterally displaced from said orifices respectively, said transducers having an axis of elongation extending substantially parallel with said ejection axis.
  • 19. The impulse jet apparatus of claim 18, wherein the axis of elongation of adjacent transducers are offset with respect to the axis of ejection.
  • 20. The impulse jet apparatus of claim 18, further comprising for each chamber, a diaphragm coupling the transducer to the chamber and separating the transducer from the volume of fluid within the chamber, said transducer being attached to said diaphragm such that the diaphragm is deformed so as to expand the chamber to an enlarged state when the transducer is energized and return the diaphragm to a planar state when the transducer is deenergized.
  • 21. The impulse jet apparatus of claim 20, wherein said transducer has an axis of elongation that intersects the diaphragm.
  • 22. The impulse jet apparatus of claim 20, further comprising adhesive means for attaching said transducer to said diaphragm.
  • 23. The impulse jet apparatus of claim 22, further comprising a chamber plate for forming said chamber, a restrictor plate providing a restricted opening for fluid to enter the chamber, and a spacer plate separating the diaphragm from the restrictor plate such that movement of said diaphragm does not restrict fluid from entering the chamber through the restricted opening.
  • 24. The impulse jet apparatus of claim 23, wherein said chamber plate, said restrictor plate, said diaphragm and said spacer plate comprise stainless steel.
  • 25. The impulse jet apparatus of claim 22, wherein said adhesive comprises a elastomeric adhesive for attaching said transducer to said diaphragm.
  • 26. The impulse jet apparatus of claim 20, further comprising for each chamber, a foot plate positioned between said diaphragm and said transducer.
CROSS-REFERENCES TO RELATED APPLICATION

This application is a continuation U.S. patent application Ser. No. 09/020,756, filed Feb. 9, 1998, now U.S. Pat. No. 5,966,148, which is continuation of U.S. patent application Ser. No. 08/530,946, filed Sep. 20, 1995, now U.S. Pat. No. 5,767,873, which is a continuation-in-part of U.S. application Ser. No. 08/310,967, filed Sep. 23, 1994, now abandoned.

US Referenced Citations (13)
Number Name Date Kind
4032929 Fischbeck et al. Jun 1977
4194210 Krause Mar 1980
4357614 Tamai Nov 1982
4379304 Heinzl et al. Apr 1983
4396924 Rosenstock Aug 1983
4439780 DeYoung et al. Mar 1984
4459601 Howkins Jul 1984
4646106 Howkins Feb 1987
4680595 Cruz-Uribe et al. Jul 1987
4714934 Rogers Dec 1987
4901093 Ruggiero et al. Feb 1990
5142296 Lopez et all. Aug 1992
5767873 Rogers et al. Jun 1998
Foreign Referenced Citations (5)
Number Date Country
0 443 628 Aug 1991 EP
56-93567 Jul 1981 JP
56-135078 Oct 1981 JP
57-188372 Nov 1982 JP
60-92865 May 1985 JP
Non-Patent Literature Citations (1)
Entry
“Ink Jet Head”, IBM Technical Disclosure Bulletin, New York, Mar. 1974, vol. 16(10).
Continuations (2)
Number Date Country
Parent 09/020756 Feb 1998 US
Child 09/287497 US
Parent 08/530946 Sep 1995 US
Child 09/020756 US
Continuation in Parts (1)
Number Date Country
Parent 08/310967 Sep 1994 US
Child 08/530946 US