Incremental printing of symbolic information – Ink jet – Ejector mechanism
Reexamination Certificate
1999-09-30
2001-10-30
Vo, Anh T. N. (Department: 2861)
Incremental printing of symbolic information
Ink jet
Ejector mechanism
Reexamination Certificate
active
06309042
ABSTRACT:
BACKGROUND OF THE INVENTION
The present invention is directed to marking materials. More specifically, the present invention is directed to marking materials particularly suitable for use in ballistic aerosol marking apparatus and processes. One embodiment of the present invention is directed to an apparatus for depositing a particulate marking material onto a substrate, comprising (a) a printhead having defined therein at least one channel, each channel having an inner surface and an exit orifice with a width no larger than about 250 microns, the inner surface of each channel having thereon a hydrophobic coating material; (b) a propellant source connected to each channel such that propellant provided by the propellant source can flow through each channel to form propellant streams therein, said propellant streams having kinetic energy, each channel directing the propellant stream through the exit orifice toward the substrate; and (c) a marking material reservoir having an inner surface, said inner surface having thereon the hydrophobic coating material, said reservoir containing particles of a particulate marking material, said reservoir being communicatively connected to each channel such that the particulate marking material from the reservoir can be controllably introduced into the propellant stream in each channel so that the kinetic energy of the propellant stream can cause the particulate marking material to impact the substrate, wherein either (i) the marking material particles of particulate marking material have an outer coating of the hydrophobic coating material; or (ii) the marking material particles have additive particles on the surface thereof, said additive particles having an outer coating of the hydrophobic coating material; or (iii) both the marking material particles and the additive particles have an outer coating of the hydrophobic coating material.
Ink jet is currently a common printing technology. There are a variety of types of ink jet printing, including thermal ink jet printing, piezoelectric ink jet printing, and the like. In ink jet printing processes, liquid ink droplets are ejected from an orifice located at one terminus of a channel. In a thermal ink jet printer, for example, a droplet is ejected by the explosive formation of a vapor bubble within an ink bearing channel. The vapor bubble is formed by means of a heater, in the form of a resistor, located on one surface of the channel.
Several disadvantages can be associated with known ink jet systems. For a 300 spot-per-inch (spi) thermal ink jet system, the exit orifice from which an ink droplet is ejected is typically on the order of about 64 microns in width, with a channel-to-channel spacing (pitch) of typically about 84 microns; for a 600 dpi system, width is typically about 35 microns and pitch is typically about 42 microns. A limit on the size of the exit orifice is imposed by the viscosity of the fluid ink used by these systems. It is possible to lower the viscosity of the ink by diluting it with increasing amounts of liquid (such as water) with an aim to reducing the exit orifice width. The increased liquid content of the ink, however, results in increased wicking, paper wrinkle, and slower drying time of the ejected ink droplet, which negatively affects resolution, image quality (such as minimum spot size, intercolor mixing, spot shape), and the like. The effect of this orifice width limitation is to limit resolution of thermal ink jet printing, for example to well below 900 spi, because spot size is a function of the width of the exit orifice, and resolution is a function of spot size.
Another disadvantage of known ink jet technologies is the difficulty of producing greyscale printing. It is very difficult for an ink jet system to produce varying size spots on a printed substrate. If one lowers the propulsive force (heat in a thermal ink jet system) so as to eject less ink in an attempt to produce a smaller dot, or likewise increases the propulsive force to eject more ink and thereby to produce a larger dot, the trajectory of the ejected droplet is affected. The altered trajectory in turn renders precise dot placement difficult or impossible, and not only makes monochrome greyscale printing problematic, it makes multiple color greyscale ink jet printing impracticable. In addition, preferred greyscale printing is obtained not by varying the dot size, as is the case for thermal ink jet, but by varying the dot density while keeping a constant dot size.
Still another disadvantage of common ink jet systems is rate of marking obtained. Approximately 80 percent of the time required to print a spot is taken by waiting for the ink jet channel to refill with ink by capillary action. To a certain degree, a more dilute ink flows faster, but raises the problem of wicking, substrate wrinkle, drying time, and the like, discussed above.
One problem common to ejection printing systems is that the channels may become clogged. Systems such as thermal ink jet which employ aqueous ink colorants are often sensitive to this problem, and routinely employ non-printing cycles for channel cleaning during operation. This clearing is required, since ink typically sits in an ejector waiting to be ejected during operation, and while sitting may begin to dry and lead to clogging.
Ballistic aerosol marking processes overcome many of these disadvantages. Ballistic aerosol marking is a process for applying a marking material to a substrate, directly or indirectly. In particular, the ballistic aerosol marking system includes a propellant which travels through a channel, and a marking material that is controllably (i.e., modifiable in use) introduced, or metered, into the channel such that energy from the propellant propels the marking material to the substrate. The propellant is usually a dry gas that can continuously flow through the channel while the marking apparatus is in an operative configuration (i.e., in a power-on or similar state ready to mark). Examples of suitable propellants include carbon dioxide gas, nitrogen gas, clean dry ambient air, gaseous products of a chemical reaction, or the like; preferably, non-toxic propellants are employed, although in certain embodiments, such as devices enclosed in a special chamber or the like, a broader range of propellants can be tolerated. The system is referred to as “ballistic aerosol marking” in the sense that marking is achieved by in essence launching a non-colloidal, solid or semi-solid particulate, or alternatively a liquid, marking material at a substrate. The shape of the channel can result in a collimated (or focused) flight of the propellant and marking material onto the substrate.
The propellant can be introduced at a propellant port into the channel to form a propellant stream. A marking material can then be introduced into the propellant stream from one or more marking material inlet ports. The propellant can enter the channel at a high velocity. Alternatively, the propellant can be introduced into the channel at a high pressure, and the channel can include a constriction (for example, de Laval or similar converging/diverging type nozzle) for converting the high pressure of the propellant to high velocity. In such a situation, the propellant is introduced at a port located at a proximal end of the channel (the converging region), and the marking material ports are provided near the distal end of the channel (at or further down-stream of the diverging region), allowing for introduction of marking material into the propellant stream.
In the situation where multiple ports are provided, each port can provide for a different color (for example, cyan, magenta, yellow, and black), pre-marking treatment material (such as a marking material adherent), post-marking treatment material (such as a substrate surface finish material, for example, matte or gloss coating, or the like), marking material not otherwise visible to the unaided eye (for example, magnetic particle-bearing material, ultraviolet-fluorescent material, or the like) or other marking material to be ap
McAneney T. Brian
McDougall Maria N. V.
Tripp Carl P.
Veregin Richard P. N.
Byorick Judith L.
Vo Anh T. N.
Xerox Corporation
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