EP1680278B1 - Pluralite de couches limites - Google Patents
Pluralite de couches limites Download PDFInfo
- Publication number
- EP1680278B1 EP1680278B1 EP03759379A EP03759379A EP1680278B1 EP 1680278 B1 EP1680278 B1 EP 1680278B1 EP 03759379 A EP03759379 A EP 03759379A EP 03759379 A EP03759379 A EP 03759379A EP 1680278 B1 EP1680278 B1 EP 1680278B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- layer
- layers
- cover layer
- ejection device
- nozzle
- 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
Links
- 230000004888 barrier function Effects 0.000 title claims description 18
- 239000012530 fluid Substances 0.000 claims abstract description 41
- 238000010304 firing Methods 0.000 claims abstract description 20
- 239000000758 substrate Substances 0.000 claims abstract description 18
- 239000000463 material Substances 0.000 claims description 62
- 238000000034 method Methods 0.000 claims description 17
- 239000010409 thin film Substances 0.000 claims description 15
- 239000011248 coating agent Substances 0.000 claims description 6
- 238000000576 coating method Methods 0.000 claims description 6
- 238000009736 wetting Methods 0.000 claims description 5
- ILBBNQMSDGAAPF-UHFFFAOYSA-N 1-(6-hydroxy-6-methylcyclohexa-2,4-dien-1-yl)propan-1-one Chemical compound CCC(=O)C1C=CC=CC1(C)O ILBBNQMSDGAAPF-UHFFFAOYSA-N 0.000 claims description 2
- 239000010408 film Substances 0.000 claims description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 6
- 239000004020 conductor Substances 0.000 description 4
- 239000004593 Epoxy Substances 0.000 description 3
- 229910052581 Si3N4 Inorganic materials 0.000 description 3
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- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- 230000032798 delamination Effects 0.000 description 3
- 239000011521 glass Substances 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- 238000002161 passivation Methods 0.000 description 3
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- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- NRTOMJZYCJJWKI-UHFFFAOYSA-N Titanium nitride Chemical compound [Ti]#N NRTOMJZYCJJWKI-UHFFFAOYSA-N 0.000 description 2
- RVSGESPTHDDNTH-UHFFFAOYSA-N alumane;tantalum Chemical compound [AlH3].[Ta] RVSGESPTHDDNTH-UHFFFAOYSA-N 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- 238000000708 deep reactive-ion etching Methods 0.000 description 2
- KPUWHANPEXNPJT-UHFFFAOYSA-N disiloxane Chemical class [SiH3]O[SiH3] KPUWHANPEXNPJT-UHFFFAOYSA-N 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 2
- 229910010271 silicon carbide Inorganic materials 0.000 description 2
- 235000012239 silicon dioxide Nutrition 0.000 description 2
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 description 2
- 239000002904 solvent Substances 0.000 description 2
- 230000008646 thermal stress Effects 0.000 description 2
- 230000007704 transition Effects 0.000 description 2
- 239000004925 Acrylic resin Substances 0.000 description 1
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- JBRZTFJDHDCESZ-UHFFFAOYSA-N AsGa Chemical compound [As]#[Ga] JBRZTFJDHDCESZ-UHFFFAOYSA-N 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910001218 Gallium arsenide Inorganic materials 0.000 description 1
- 229910018487 Ni—Cr Inorganic materials 0.000 description 1
- 239000004952 Polyamide Substances 0.000 description 1
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- 229910001069 Ti alloy Inorganic materials 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 230000002745 absorbent Effects 0.000 description 1
- 239000002250 absorbent Substances 0.000 description 1
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- 230000001070 adhesive effect Effects 0.000 description 1
- CSDREXVUYHZDNP-UHFFFAOYSA-N alumanylidynesilicon Chemical compound [Al].[Si] CSDREXVUYHZDNP-UHFFFAOYSA-N 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- BGTFCAQCKWKTRL-YDEUACAXSA-N chembl1095986 Chemical compound C1[C@@H](N)[C@@H](O)[C@H](C)O[C@H]1O[C@@H]([C@H]1C(N[C@H](C2=CC(O)=CC(O[C@@H]3[C@H]([C@@H](O)[C@H](O)[C@@H](CO)O3)O)=C2C=2C(O)=CC=C(C=2)[C@@H](NC(=O)[C@@H]2NC(=O)[C@@H]3C=4C=C(C(=C(O)C=4)C)OC=4C(O)=CC=C(C=4)[C@@H](N)C(=O)N[C@@H](C(=O)N3)[C@H](O)C=3C=CC(O4)=CC=3)C(=O)N1)C(O)=O)=O)C(C=C1)=CC=C1OC1=C(O[C@@H]3[C@H]([C@H](O)[C@@H](O)[C@H](CO[C@@H]5[C@H]([C@@H](O)[C@H](O)[C@@H](C)O5)O)O3)O[C@@H]3[C@H]([C@@H](O)[C@H](O)[C@@H](CO)O3)O[C@@H]3[C@H]([C@H](O)[C@@H](CO)O3)O)C4=CC2=C1 BGTFCAQCKWKTRL-YDEUACAXSA-N 0.000 description 1
- VNNRSPGTAMTISX-UHFFFAOYSA-N chromium nickel Chemical compound [Cr].[Ni] VNNRSPGTAMTISX-UHFFFAOYSA-N 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 238000004132 cross linking Methods 0.000 description 1
- 229910021419 crystalline silicon Inorganic materials 0.000 description 1
- 238000000151 deposition Methods 0.000 description 1
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- 238000001312 dry etching Methods 0.000 description 1
- 239000003822 epoxy resin Substances 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- -1 field oxide Substances 0.000 description 1
- 229920002313 fluoropolymer Polymers 0.000 description 1
- 239000004811 fluoropolymer Substances 0.000 description 1
- 238000009472 formulation Methods 0.000 description 1
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 1
- 229910052737 gold Inorganic materials 0.000 description 1
- 239000010931 gold Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 238000010348 incorporation Methods 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
- 238000007641 inkjet printing Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000004377 microelectronic Methods 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
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- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 238000000059 patterning Methods 0.000 description 1
- 229920002120 photoresistant polymer Polymers 0.000 description 1
- 229920002647 polyamide Polymers 0.000 description 1
- 229910021420 polycrystalline silicon Inorganic materials 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 229920001721 polyimide Polymers 0.000 description 1
- 229920001296 polysiloxane Polymers 0.000 description 1
- 238000005488 sandblasting Methods 0.000 description 1
- WNUPENMBHHEARK-UHFFFAOYSA-N silicon tungsten Chemical compound [Si].[W] WNUPENMBHHEARK-UHFFFAOYSA-N 0.000 description 1
- 238000004544 sputter deposition Methods 0.000 description 1
- 229910052715 tantalum Inorganic materials 0.000 description 1
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical group [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 description 1
- 238000005382 thermal cycling Methods 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- MAKDTFFYCIMFQP-UHFFFAOYSA-N titanium tungsten Chemical compound [Ti].[W] MAKDTFFYCIMFQP-UHFFFAOYSA-N 0.000 description 1
- 238000012876 topography Methods 0.000 description 1
- 238000001039 wet etching Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B41—PRINTING; LINING MACHINES; TYPEWRITERS; STAMPS
- B41J—TYPEWRITERS; SELECTIVE PRINTING MECHANISMS, i.e. MECHANISMS PRINTING OTHERWISE THAN FROM A FORME; CORRECTION OF TYPOGRAPHICAL ERRORS
- B41J2/00—Typewriters or selective printing mechanisms characterised by the printing or marking process for which they are designed
- B41J2/005—Typewriters or selective printing mechanisms characterised by the printing or marking process for which they are designed characterised by bringing liquid or particles selectively into contact with a printing material
- B41J2/01—Ink jet
- B41J2/135—Nozzles
- B41J2/16—Production of nozzles
- B41J2/1621—Manufacturing processes
- B41J2/1626—Manufacturing processes etching
- B41J2/1629—Manufacturing processes etching wet etching
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B41—PRINTING; LINING MACHINES; TYPEWRITERS; STAMPS
- B41J—TYPEWRITERS; SELECTIVE PRINTING MECHANISMS, i.e. MECHANISMS PRINTING OTHERWISE THAN FROM A FORME; CORRECTION OF TYPOGRAPHICAL ERRORS
- B41J2/00—Typewriters or selective printing mechanisms characterised by the printing or marking process for which they are designed
- B41J2/005—Typewriters or selective printing mechanisms characterised by the printing or marking process for which they are designed characterised by bringing liquid or particles selectively into contact with a printing material
- B41J2/01—Ink jet
- B41J2/135—Nozzles
- B41J2/14—Structure thereof only for on-demand ink jet heads
- B41J2/14016—Structure of bubble jet print heads
- B41J2/14088—Structure of heating means
- B41J2/14112—Resistive element
- B41J2/14129—Layer structure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B41—PRINTING; LINING MACHINES; TYPEWRITERS; STAMPS
- B41J—TYPEWRITERS; SELECTIVE PRINTING MECHANISMS, i.e. MECHANISMS PRINTING OTHERWISE THAN FROM A FORME; CORRECTION OF TYPOGRAPHICAL ERRORS
- B41J2/00—Typewriters or selective printing mechanisms characterised by the printing or marking process for which they are designed
- B41J2/005—Typewriters or selective printing mechanisms characterised by the printing or marking process for which they are designed characterised by bringing liquid or particles selectively into contact with a printing material
- B41J2/01—Ink jet
- B41J2/135—Nozzles
- B41J2/16—Production of nozzles
- B41J2/1601—Production of bubble jet print heads
- B41J2/1603—Production of bubble jet print heads of the front shooter type
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B41—PRINTING; LINING MACHINES; TYPEWRITERS; STAMPS
- B41J—TYPEWRITERS; SELECTIVE PRINTING MECHANISMS, i.e. MECHANISMS PRINTING OTHERWISE THAN FROM A FORME; CORRECTION OF TYPOGRAPHICAL ERRORS
- B41J2/00—Typewriters or selective printing mechanisms characterised by the printing or marking process for which they are designed
- B41J2/005—Typewriters or selective printing mechanisms characterised by the printing or marking process for which they are designed characterised by bringing liquid or particles selectively into contact with a printing material
- B41J2/01—Ink jet
- B41J2/135—Nozzles
- B41J2/16—Production of nozzles
- B41J2/1621—Manufacturing processes
- B41J2/1626—Manufacturing processes etching
- B41J2/1628—Manufacturing processes etching dry etching
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B41—PRINTING; LINING MACHINES; TYPEWRITERS; STAMPS
- B41J—TYPEWRITERS; SELECTIVE PRINTING MECHANISMS, i.e. MECHANISMS PRINTING OTHERWISE THAN FROM A FORME; CORRECTION OF TYPOGRAPHICAL ERRORS
- B41J2/00—Typewriters or selective printing mechanisms characterised by the printing or marking process for which they are designed
- B41J2/005—Typewriters or selective printing mechanisms characterised by the printing or marking process for which they are designed characterised by bringing liquid or particles selectively into contact with a printing material
- B41J2/01—Ink jet
- B41J2/135—Nozzles
- B41J2/16—Production of nozzles
- B41J2/1621—Manufacturing processes
- B41J2/1631—Manufacturing processes photolithography
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B41—PRINTING; LINING MACHINES; TYPEWRITERS; STAMPS
- B41J—TYPEWRITERS; SELECTIVE PRINTING MECHANISMS, i.e. MECHANISMS PRINTING OTHERWISE THAN FROM A FORME; CORRECTION OF TYPOGRAPHICAL ERRORS
- B41J2/00—Typewriters or selective printing mechanisms characterised by the printing or marking process for which they are designed
- B41J2/005—Typewriters or selective printing mechanisms characterised by the printing or marking process for which they are designed characterised by bringing liquid or particles selectively into contact with a printing material
- B41J2/01—Ink jet
- B41J2/135—Nozzles
- B41J2/16—Production of nozzles
- B41J2/1621—Manufacturing processes
- B41J2/1632—Manufacturing processes machining
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B41—PRINTING; LINING MACHINES; TYPEWRITERS; STAMPS
- B41J—TYPEWRITERS; SELECTIVE PRINTING MECHANISMS, i.e. MECHANISMS PRINTING OTHERWISE THAN FROM A FORME; CORRECTION OF TYPOGRAPHICAL ERRORS
- B41J2/00—Typewriters or selective printing mechanisms characterised by the printing or marking process for which they are designed
- B41J2/005—Typewriters or selective printing mechanisms characterised by the printing or marking process for which they are designed characterised by bringing liquid or particles selectively into contact with a printing material
- B41J2/01—Ink jet
- B41J2/135—Nozzles
- B41J2/16—Production of nozzles
- B41J2/1621—Manufacturing processes
- B41J2/1632—Manufacturing processes machining
- B41J2/1634—Manufacturing processes machining laser machining
Definitions
- the present invention relates to fluid ejection devices, and more particularly to a plurality of barrier layers in a fluid ejection device.
- thermal actuated printheads tend to use resistive elements or the like to achieve ink expulsion
- mechanically actuated printheads tend to use piezoelectric transducers or the like.
- a representative thermal inkjet printhead has a plurality of thin film resistors provided on a semiconductor substrate.
- a barrier layer is deposited over thin film layers on the substrate. The barrier layer defines firing chambers about each of the resistors, an orifice corresponding to each resistor, and an entrance or fluid channel to each firing chamber.
- ink is provided through a slot in the substrate and flows through the fluid channel defined by the nozzle layer to the firing chamber. Actuation of a heater resistor by a "fire signal" causes ink in the corresponding firing chamber to be heated and expelled through the corresponding orifice.
- nozzle layer delamination may occur due to mechanical or thermal stresses.
- the nozzle layer has a different coefficient of thermal expansion than that of the semiconductor substrate.
- the thermal stresses may lead to delamination of the nozzle layer, or other thin film layers, ultimately leading to ink leakage and/or electrical shorts.
- the nozzle layer can undergo stresses due to nozzle layer shrinkage after curing of the layer, structural adhesive shrinkage during assembly of the nozzle layer, handling of the device, and thermal cycling of the fluid ejection device.
- a fluid ejection device comprises a substrate having a first surface; a fluid ejector formed over the first surface; and a cover layer defining a firing chamber formed about the fluid ejector, and defining a nozzle over the firing chamber.
- the cover layer is formed by at least two SU8 layers.
- Fig. 1 is a perspective view of an embodiment of a cartridge 101 having a fluid ejection device 103, such as a printhead.
- the cartridge houses a fluid supply, such as ink. Visible at the outer surface of the printhead are a plurality of orifices or nozzles 105 through which fluid is selectively expelled. In one embodiment, the fluid is expelled upon commands of a printer (not shown) communicated to the printhead through electrical connections 107.
- Fig. 2 illustrates a cross-sectional view of the printhead 103 of Fig. 1 where a slot 110 is formed through a substrate 115.
- Some of the embodiments used in forming the slot through a slot region (or slot area) in the substrate include wet etching, dry etching, DRIE, and UV laser machining.
- the substrate 115 is silicon.
- the substrate is one of the following: single crystalline silicon, polycrystalline silicon, gallium arsenide, glass, silica, ceramics, or a semiconducting material.
- single crystalline silicon polycrystalline silicon
- gallium arsenide glass
- silica silica
- ceramics or a semiconducting material.
- the various materials listed as possible substrate materials are not necessarily interchangeable and are selected depending upon the application for which they are to be used.
- a thin film stack 116 (such as an active layer, an electrically conductive layer, and a layer with micro-electronics) is formed or deposited on a front or first side (or surface) of the substrate 115.
- the thin film stack 116 includes a capping layer 117 formed over a first surface of the substrate.
- Capping layer 117 may be formed of a variety of different materials such as field oxide, silicon dioxide, aluminum oxide, silicon carbide, silicon nitride, and glass (PSG).
- a layer 119 is deposited or grown over the capping layer 117.
- the layer 119 is one of titanium nitride, titanium tungsten, titanium, a titanium alloy, a metal nitride, tantalum aluminum, and aluminum silicon.
- a conductive layer 121 is formed by depositing conductive material over the layer 119.
- the conductive material is formed of at least one of a variety of different materials including aluminum, aluminum with about 1 ⁇ 2 % copper, copper, gold, and aluminum with 1 ⁇ 2% silicon, and may be deposited by any method, such as sputtering and evaporation.
- the conductive layer 121 is patterned and etched to form conductive traces.
- a resistive material 125 is deposited over the etched conductive material 121.
- the resistive material is etched to form an ejection element 201, such as a fluid ejector, a resistor, a heating element, and a bubble generator.
- resistive materials are known to those of skill in the art including tantalum aluminum, nickel chromium, tungsten silicon nitride, and titanium nitride, which may optionally be doped with suitable impurities such as oxygen, nitrogen, and carbon, to adjust the resistivity of the material.
- the thin film stack 116 further includes an insulating passivation layer 127 formed over the resistive material.
- Passivation layer 127 may be formed of any suitable material such as silicon dioxide, aluminum oxide, silicon carbide, silicon nitride, and glass.
- a cavitation layer 129 is added over the passivation layer 127.
- the cavitation layer is tantalum.
- a cover layer such as a barrier layer, 124 is deposited over the thin film stack 116, in particular, the cavitation layer 129.
- the cover layer 124 is a layer comprised of a fast cross-linking polymer such as photoimagable epoxy (such as SU8 developed by IBM), photoimagable polymer or photosensitive silicone dielectrics, such as SINR-3010 manufactured by ShinEtsu TM , or an epoxy siloxane, such as PCX30 manufactured by Polyset Co. Inc. in Mechanicsville, NY.
- the cover layer 124 is made of a blend of organic polymers which is substantially inert to the corrosive action of ink. Polymers suitable for this purpose include products sold under the trademarks VACREL and RISTON by E. I. DuPont de Nemours and Co. of Wilmington, Del.
- Embodiments of the present invention include having any number and type of layers formed or deposited over the substrate, depending upon the application.
- the cover layer 124 defines a firing chamber 202 where fluid is heated by the corresponding ejection element 201 and defines the nozzle orifice 105 through which the heated fluid is ejected. Fluid flows through the slot 110 and into the firing chamber 202 via channels 203 formed with the cover layer 124. Propagation of a current or a "fire signal" through the resistor causes fluid in the corresponding firing chamber to be heated and expelled through the corresponding nozzle 105.
- the cover layer 124 includes two layers 205, 207.
- the first layer 205 such as a primer layer and a bottom layer, is formed over layer 129
- the second layer 207 (such as a top coat layer, a chamber layer, and a nozzle layer) is formed over layer 205.
- the first layer 205 at least partially defines the firing chamber 202
- the second layer 207 defines a ceiling of the fluid channel 203, the remainder of the firing chamber and walls, as well as the nozzle 105.
- the first layer 205 defines the firing chamber walls
- the second layer 207 defines the nozzle.
- layers 205 and 207 are formed of different materials. In this embodiment, layers 205 and 207 are formed of the same material. In alternative embodiments, the layers 205 and 207 are about the same thickness, or layer 207 is thicker than layer 205, or layer 205 is thicker than layer 207. In this embodiment, layer 205 is thinner than layer 207. In one embodiment, layer 205 has a thickness of about 2 to 15 microns, preferably 2 to 6 microns, preferably 2 microns. In one embodiment, layer 207 has a thickness of about 20 to 60 microns, preferably 30 microns. In one embodiment, the thickness of the primer layer is less than about 50% of the entire thickness of the layer 124.
- the primer layer 205 is a low viscosity SU8 material that is cured at 210°C.
- the material for the primer layer 205 is chosen for resistance to ink and for adhesion to the thin film stack 116 and the nozzle or chamber layer.
- the primer layer 205 is more flexible than the other layers of the cover layer 124.
- the primer layer 205 has more ink resistance than the other layers of the cover layer 124.
- the primer layer 205 is formed of NANO TM SU8 Flex CP which is a lower modulus SU8 formation.
- the primer layer 205 is a flexibilized epoxy.
- the primer layer 205 is a polyimide - polyamide layer.
- the primer layer 205 is SU8 with alternative Photo-Acid-Generator (PAG) loading that makes the material photosensitive.
- PAG Photo-Acid-Generator
- the primer layer 205 is cured to a higher temperature than that of other layers in the cover layer 124. With this higher temperature may come more resistance to ink, and more stress. However, the thickness of the layer 205 remains relatively thin to reduce undesirable cracking.
- the layer 207 has high resolution photolithographic characteristics. In one embodiment, the layer 207 is cured at 170°C.
- FIG. 4A-4D the process of forming the two layer (205, 207) barrier layer 124 is illustrated.
- the embodiment of Fig. 5 shows the flow chart corresponding to the process illustrated in Figs. 4A to 4D.
- the primer layer 205 is coated in step 500, and exposed in step 510.
- a nozzle layer material 207a coats the primer layer 205 in step 520 and as shown in Fig. 4A.
- the nozzle layer 207 is exposed in two masks as shown in Figs. 4B and 4C.
- step 540 and as shown in Fig. 4D, the remaining unexposed nozzle layer material 207a is developed and thereby removed.
- the nozzle layer forms the firing chamber 202 and nozzle 105.
- an additional top coat 209 is formed over the nozzle layer 207.
- the top coat 209 is photodefinable.
- the top coat 209 is formed of SU8.
- the top coat is non-wetting.
- the top coat 209 is a planarizing layer to planarize the often rough topography of the nozzle layer.
- the top coat 209 is a mask drawn to produce countersunk bores to reduce puddling.
- the top coat 209 has low surface energy.
- the top coat 209 is a siloxane based material.
- the top coat 209 is a fluoropolymer based material.
- the thickness of layer 209 is in the range of about 1 ⁇ 2 to 5 microns, preferably 1.1 microns.
- FIG. 7A-7H the process of forming the three layer (205, 206, 208) barrier layer 124 is illustrated.
- the embodiment of Fig. 8 shows the flow chart corresponding to the process illustrated in Figs. 7A to 7H.
- step 800 the thin films 116 forming the fluid ejectors are deposited over the substrate.
- step 810 the primer layer 205 is spun onto the thin film layers 116 and patterned.
- step 820 and as illustrated in Fig. 7A, a material 206a that forms the chamber layer is spun on.
- the material 206a is patterned or exposed to form the chamber layer 206.
- Fig. 7A-7H the process of forming the three layer (205, 206, 208) barrier layer 124 is illustrated.
- FIG. 8 shows the flow chart corresponding to the process illustrated in Figs. 7A to 7H.
- step 800 the thin films 116 forming the fluid ejectors are deposited over the substrate.
- step 810 the primer layer 205 is spun onto the
- step 830 and illustrated in Fig. 7D, fill material 300, such as resist, coats the chamber layer 206.
- the fill material 300 is planarized, by methods such as CMP, patterning and developing of material.
- step 850 and as illustrated in Fig. 7F, the chamber layer 206 and planarized material 300 is coated with a material 208a that forms the nozzle layer. As illustrated in Fig. 7G, the nozzle layer 208 is exposed.
- step 850 the material 208a is developed.
- step 860 and as illustrated in Fig. 7H, the fill material (such as resist) is removed.
- the method illustrated in Figs. 7A to 7H, and in flow chart Fig. 8 may be referred to as the lost wax method.
- the primer layer of Fig. 7H in this embodiment, has a thickness in the range of about 2 to 15 microns, more particularly 2 to 6 microns, even more particularly 2 microns.
- the chamber layer 206 and the nozzle layer 208 each have a thickness in the range of about 10 to 30 microns.
- at least one of the layers 206 and 208 have a thickness in the range of about 15 to 20 microns.
- at least one of the layers 206 and 208 have a thickness of 15 or 20 microns.
- the nozzle layer 208 is formed of a material similar to that of layer 207 described above.
- the chamber layer 206 is formed of a material similar to that of layer 207 described above.
- the chamber layer 206 is formed of an SU8 with a photobleachable dye for z-contrast.
- z-contrast refers to the direction perpendicular to the substantially planar substrate.
- z-contrast refers to placing an absorbing material in the formulation to extinguish the light intensity from top to bottom.
- the 'contrast' refers to the sharpness of the transition between a photo acid concentration that causes the SU8 material to resist the developer and a concentration that is dissolved by the developer. In one embodiment, the sharper this transition; the more square the feature. In this embodiment, this photobleachable dye bleaches and becomes transparent at a sufficient dosage of electromagnetic energy.
- an additional top coat 209 is formed over the nozzle layer 208.
- the top coat 209 is similar to the top coat 209 described with respect to Fig. 6.
- FIG. 10A-10F the process of forming the four layer (205, 1206, 1000, 1208) barrier layer 124 is illustrated.
- the embodiment of Fig. 11 shows the flow chart corresponding to the process illustrated in Figs. 10A to 10F.
- step 1100 and in Fig., 10A the material 1206a for forming the chamber layer is coated over the primer layer 205.
- step 1110 and in Fig. 10B the chamber layer 1206 is exposed thereby forming walls about a chamber, and leaving the unexposed material 1206a within the chamber area.
- step 1120 and in Fig. 10C material 1000a for forming a photon barrier layer is coated over the chamber layer 1206 and the material 1206a.
- step 1140 and in Fig. 10E material 1208a for the nozzle layer is coated over the photon barrier layer material 1000a.
- step 1140 and in Fig. 10E the nozzle layer 1208 and the photon barrier layer 1000 is exposed.
- the material 1206a remains in the chamber 202 and the materials 1000a and 1208a remain in the nozzle 105.
- step 1150 and in Fig. 10F the materials 1206a, 1000a, and 1208a are developed and thereby removed from the chamber and nozzle.
- the photon barrier layer 1000 is cast from a solution comprising at least one of an epoxy or acrylic resin, a binder, a solvent, a PAG (photosensitive), and an i-line dye (photon barrier).
- the thickness of photon barrier layer 1000 is in the range of about 1/2 microns to 2 microns, preferably 1/2 micron.
- the photon barrier layer is minimized, while being sufficiently absorbent.
- the chamber layer 1206 and the nozzle layer 1208 are formed of a material similar to that of layer 207 described above. In one embodiment, the layer 1206 has a material similar to that of the layer 206.
- the photon barrier layer 1000 is formed of SU8 with photobleachable dye, similar to that described with respect to an embodiment of layer 206 above. In one embodiment, the SU8 with photobleachable dye allows greater dimensional control and straighter edges. For example, as shown in Fig. 10F, the corner edges between the chamber and nozzle are substantially square edges.
- an additional top coat 209 is formed over the nozzle layer 1208.
- the top coat 209 is similar to the top coat 209 described with respect to Fig. 6.
- At least one of the layers in the cover layer 124 in one of the previous embodiments is formed with the same initial basic coating material. However, that material is processed differently to give that layer different properties with respect to other layers in the cover layer 124. For example, in one embodiment, the one layer is exposed to a different dose of electromagnetic energy or cured at a different temperature than the remaining layers of the cover layer 124.
- the materials for the layers of the cover layer 124 are chosen for, at least one of the following characteristics: CTE matching, ink resistance, stress relief, non-wetting ability, wetting ability, ability to photocure, high resolution processing capability, smooth surface, compatibility, and intermixing capability.
- At least one of the layers in the cover layer 124 in one of the previous embodiments is formed with a material that is patterned, or etched using at least one of the following methods: abrasive sand blasting, dry etch, wet etch, UV assisted wet etch, exposure and developing, DRIE, and UV laser machining. In one embodiment, at least one of the layers in the cover layer 124 in one of the previous embodiments is formed with a dry film.
- the materials forming the primer, chamber and/or nozzle layers are photodefined through i-line exposure.
- the i-line exposure is a type of exposure, in particular, about 365 nm wavelength exposure.
- this photodefined pattern is covered with a resist material.
- the resist is a positive photoresist, in a particular embodiment it is SPR-220.
- the resist is typically baked in a convection oven at a temperature between 110°C and 190°C to stabilize the resist for the subsequent planarization and bore or nozzle layer processing.
- the solvent develop process that removes the unexposed chamber and nozzle layers is also used to remove the resist.
- At least one of the above-described embodiments maximizes trajectory control by reducing orifice-chamber alignment variability.
- ratios of SU8 ingredients, additives, and molecular weights of the SU8 oligomers are adjusted to give a range in the materials properties that are mentioned above.
- the present invention is not limited to thermally actuated fluid ejection devices, but may also include, for example, piezoelectric activated fluid ejection devices, and other mechanically actuated printheads, as well as other fluid ejection devices.
- the cover layer 124 of the present invention includes a plurality of layers, such as 4 layers, 5 layers, 6 layers, etc. Each of these layers may have either the same or a different material composition, depending upon the application.
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- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Particle Formation And Scattering Control In Inkjet Printers (AREA)
- Laminated Bodies (AREA)
- Application Of Or Painting With Fluid Materials (AREA)
- Coating Apparatus (AREA)
Claims (12)
- Dispositif d'éjection de fluide (103) comprenant :■ un substrat (15) ayant une première surface ;■ un éjecteur de fluide (201) formé sur la première surface ; et■ une couche de couverture (124) définissant une chambre d'amorçage (202) formée autour de l'éjecteur de fluide (201), et définissant un éjecteur (105) au-dessus de la chambre d'amorçage (202),dans lequel la couche de couverture (124) est formée par au moins deux couches en SU.8.
- Dispositif d'éjection de fluide (103) selon la revendication 1, dans lequel chacune des couches en SU8 est formée à partir du même matériau.
- Dispositif d'éjection de fluide (103) selon la revendication 2, dans lequel chacune des couches en SU8 est traité différemment.
- Dispositif d'éjection de fluide (103) selon la revendication 1, dans lequel la couche de couverture (124) comporte une couche primaire (205) et une couche d'éjecteur (207), dans lequel la couche primaire (205) a une épaisseur qui est inférieure à 50% de l'épaisseur de la couche de couverture (124).
- Dispositif d'éjection de fluide (103) selon la revendication 1, dans lequel la couche primaire (205) est un SU8 à faible viscosité durci à 210°C.
- Dispositif d'éjection de fluide (103) selon la revendication 1, dans lequel la couche de couverture (124) a au moins trois couches comprenant une couche primaire (205) recouvrant de fines couches de pellicule, une couche de chambre définissant la chambre d'amorçage (202) et une couche d'éjecteur définissant l'éjecteur (105).
- Dispositif d'éjection de fluide (103) selon la revendication 1, comprenant en outre une couche de revêtement supérieure (207) formée par-dessus la couche de couverture.
- Dispositif d'éjection de fluide (103) selon la revendication 1, dans lequel au moins une des couches de la couche de couverture (124) est formée par un moulage à la cire perdue.
- Dispositif d'éjection de fluide (103) selon la revendication 1, dans lequel les matériaux pour les couches de la couche de couverture (124) sont choisis pour au moins une des caractéristiques suivantes : équivalence de coefficient de dilatation thermique, résistance à l'encre, détente, capacité de non mouillage, capacité de mouillage, capacité de photodurcissement, capacité de traitement à haute résolution, surface lisse, compatibilité et capacité de mélange.
- Dispositif d'éjection de fluide (103) selon la revendication 1, dans lequel au moins une des couches de la couche de couverture (124) est formée par un film sec.
- Dispositif d'éjection de fluide (103) selon la revendication 1, dans lequel la couche de couverture (124) comporte au moins quatre couches comprenant une couche primaire recouvrant de fines couches de pellicule, une couche de chambre définissant la chambre d'amorçage, une couche barrière de photons avec une couche d'éjecteur définissant l'éjecteur.
- Procédé de formage d'un dispositif d'éjection de fluide (103) comprenant les étapes consistant à :■ revêtir une fine pile de pellicules, comprenant un éjecteur de fluide (201) dans un premier matériau ;■ exposer le premier matériau pour former une première couche de couverture en SU8 ;■ revêtir le premier matériau d'un second matériau ;■ exposer le second matériau pour former une seconde couche de couverture en SU8 définissant une chambre ;■ développer pour enlever le second matériau non exposé de la chambre ;■ remplir la chambre de matière de protection ;■ aplanir la matière de protection ;■ revêtir la matière de protection d'un troisième matériau ;■ exposer le troisième matériau pour former une troisième couche de couverture en SU8 définissant un éjecteur ; et■ développer pour retirer la matière de protection et le troisième matériau.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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PCT/US2003/029809 WO2005035255A1 (fr) | 2003-09-17 | 2003-09-17 | Pluralite de couches limites |
Publications (2)
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EP1680278A1 EP1680278A1 (fr) | 2006-07-19 |
EP1680278B1 true EP1680278B1 (fr) | 2007-10-31 |
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EP03759379A Expired - Lifetime EP1680278B1 (fr) | 2003-09-17 | 2003-09-17 | Pluralite de couches limites |
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EP (1) | EP1680278B1 (fr) |
JP (1) | JP2007528803A (fr) |
KR (1) | KR101012210B1 (fr) |
CN (1) | CN100421945C (fr) |
AT (1) | ATE376935T1 (fr) |
AU (1) | AU2003275109A1 (fr) |
DE (1) | DE60317247T2 (fr) |
ES (1) | ES2295637T3 (fr) |
WO (1) | WO2005035255A1 (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2009078879A1 (fr) * | 2007-12-19 | 2009-06-25 | Hewlett-Packard Development Company, L.P. | Fusion de chambres sur un substrat |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP4881081B2 (ja) * | 2005-07-25 | 2012-02-22 | キヤノン株式会社 | 液体吐出ヘッドの製造方法 |
CN101903180B (zh) | 2007-12-20 | 2012-08-08 | 惠普开发有限公司 | 流体喷射器芯片和制造液滴生成器的方法 |
US8206998B2 (en) * | 2009-06-17 | 2012-06-26 | Canon Kabushiki Kaisha | Method for manufacturing liquid discharge head |
US9895885B2 (en) | 2012-12-20 | 2018-02-20 | Hewlett-Packard Development Company, L.P. | Fluid ejection device with particle tolerant layer extension |
CN104853923B (zh) * | 2012-12-20 | 2016-08-24 | 惠普发展公司,有限责任合伙企业 | 具有颗粒耐受层延伸部的流体喷射装置 |
CN103353708A (zh) * | 2013-06-14 | 2013-10-16 | 大连理工大学 | 一种多层负性光刻胶模具制作方法 |
CN104669787B (zh) * | 2013-11-28 | 2017-11-03 | 珠海赛纳打印科技股份有限公司 | 液体喷射装置及其制造方法 |
JP6333992B2 (ja) | 2013-12-26 | 2018-05-30 | 大連理工大学 | 液体ノズルと液体噴射装置の一体成形製造方法及びその装置 |
CN103770468B (zh) * | 2013-12-26 | 2016-02-03 | 大连理工大学 | 液体喷射装置及其一体成型制造方法 |
JP6360975B2 (ja) * | 2014-10-30 | 2018-07-18 | ヒューレット−パッカード デベロップメント カンパニー エル.ピー.Hewlett‐Packard Development Company, L.P. | インクジェットプリントヘッド |
WO2017074446A1 (fr) * | 2015-10-30 | 2017-05-04 | Hewlett-Packard Development Company, L.P. | Dispositif d'éjection de fluide |
JP6976081B2 (ja) * | 2016-06-23 | 2021-12-01 | キヤノン株式会社 | 液体吐出ヘッド用デバイス |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4719477A (en) | 1986-01-17 | 1988-01-12 | Hewlett-Packard Company | Integrated thermal ink jet printhead and method of manufacture |
US5317346A (en) | 1992-03-04 | 1994-05-31 | Hewlett-Packard Company | Compound ink feed slot |
JP3069247B2 (ja) * | 1994-07-29 | 2000-07-24 | アルプス電気株式会社 | サーマルヘッド |
US6162589A (en) | 1998-03-02 | 2000-12-19 | Hewlett-Packard Company | Direct imaging polymer fluid jet orifice |
CN1116985C (zh) * | 1998-06-30 | 2003-08-06 | 财团法人工业技术研究院 | 喷墨印头晶片的制造方法 |
TW369485B (en) * | 1998-07-28 | 1999-09-11 | Ind Tech Res Inst | Monolithic producing method for chip of ink-jet printing head |
-
2003
- 2003-09-17 DE DE60317247T patent/DE60317247T2/de not_active Expired - Lifetime
- 2003-09-17 AT AT03759379T patent/ATE376935T1/de not_active IP Right Cessation
- 2003-09-17 AU AU2003275109A patent/AU2003275109A1/en not_active Abandoned
- 2003-09-17 WO PCT/US2003/029809 patent/WO2005035255A1/fr active IP Right Grant
- 2003-09-17 KR KR1020067004418A patent/KR101012210B1/ko active IP Right Grant
- 2003-09-17 CN CNB038270722A patent/CN100421945C/zh not_active Expired - Lifetime
- 2003-09-17 JP JP2005509543A patent/JP2007528803A/ja active Pending
- 2003-09-17 ES ES03759379T patent/ES2295637T3/es not_active Expired - Lifetime
- 2003-09-17 EP EP03759379A patent/EP1680278B1/fr not_active Expired - Lifetime
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2009078879A1 (fr) * | 2007-12-19 | 2009-06-25 | Hewlett-Packard Development Company, L.P. | Fusion de chambres sur un substrat |
CN101903179B (zh) * | 2007-12-19 | 2013-09-25 | 惠普开发有限公司 | 基板上的熔丝腔 |
TWI500523B (zh) * | 2007-12-19 | 2015-09-21 | Hewlett Packard Development Co | 印刷頭及其製造方法 |
Also Published As
Publication number | Publication date |
---|---|
ES2295637T3 (es) | 2008-04-16 |
ATE376935T1 (de) | 2007-11-15 |
WO2005035255A1 (fr) | 2005-04-21 |
DE60317247T2 (de) | 2008-08-07 |
AU2003275109A1 (en) | 2005-04-27 |
DE60317247D1 (de) | 2007-12-13 |
CN1839046A (zh) | 2006-09-27 |
KR20060081706A (ko) | 2006-07-13 |
KR101012210B1 (ko) | 2011-02-08 |
CN100421945C (zh) | 2008-10-01 |
EP1680278A1 (fr) | 2006-07-19 |
JP2007528803A (ja) | 2007-10-18 |
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