In the detailed description of the preferred embodiments of the invention presented below, reference is made to the accompanying drawings, in which:
The present description will be directed in particular to elements forming part of, or cooperating more directly with, apparatus in accordance with the present invention. It is to be understood that elements not specifically shown or described may take various forms well known to those skilled in the art.
Bernoulli's equation states:
P+½ρV2+ρgh=constant,
where p is pressure, ρ is density, V is velocity, h is elevation, and g is gravitational acceleration. When a steady flow impinges on a perpendicular plate, as shown in
Bernoulli's equation along the stagnation streamline gives
p
e+½ρVe2=p0+½ρV02,
where the point e is far upstream and point 0 is the stagnation point. Since the velocity at the stagnation point is zero,
p
e+½ρVe2=p0.
The stagnation pressure, p0, is the pressure measured at the point where the fluid comes to rest. It is the highest pressure found anywhere in the flowfield, and it occurs at the stagnation point. It is the sum of the static pressure and the dynamic pressure measured far upstream. The dynamic pressure is so named because it arises from the motion of the fluid. The dynamic pressure is not really a pressure at all. It is simply a convenient name for the quantity (half the density times the velocity squared) which represents the decrease in the pressure due to the velocity of the fluid. We can also express the pressure anywhere in the flow in the form of a non-dimensional pressure coefficient Cp, where
At the stagnation point Cp=1, which is its maximum value. In the freestream, far from the plate, Cp=0.
Referring to
An actuator 32, such as a piezoelectric, acoustic, thermal, or electrostatic actuator, inside pressure chamber 18 is operable to force ink from the pressure chamber through passage 22 and out of nozzle opening 24, causing a droplet 34 to be ejected from nozzle opening 24 toward a recording surface (not shown). During operation, one or both of the ink jet apparatus and the recording surface may be moved relative to the other. By selective ejection of droplets from an array of such nozzle openings along the nozzle plate, a desired image is produced on the recording surface.
Fluid enters pressure chamber 18 of print head 20 from passages 16 as shown by directional arrows 36 and 38. Fluid travels past actuator 32 and turns toward into passage 22 towards nozzle opening 24 as indicated by directional arrow 40. Just before passage 22, the flow splits (see directional arrows 42 and 44) and exits the firing chamber via ink return passages 30. A stagnation point exists directly inside nozzle opening 24, preventing air ingestion through the nozzle opening.
The stagnation point directly inside the nozzle opening allows printing at a higher frequency than the traditional drop on demand devices as a result of the forced refill after droplet ejection. By creating a stagnation point with flow symmetry above the nozzle opening by dual port input and output flow paths, this invention promotes proper jet directionality and improved refill time.
In ink jet print heads, suitable stagnation flow geometries can result from several formats, such as directing ink toward the nozzle opening perpendicular to the plane of the nozzle opening array as illustrated in
The mechanism by which the ejection of the droplet occurs differs upon choice of the energy source. Still referring to
In an alternative embodiment wherein thermal energy sources 46 and 48 are brought to the point of fluid vaporization, the thermal energy serves to decrease the effective area of fluid flow in direction 40, raising the pressure in the cavity just inside nozzle opening 24, and ejecting a droplet.
In yet alternative embodiment, side wall energy sources 46 and 48 may be piezoelectric (PZT) crystals. In which case, an acoustic energy pulse is sent through the fluid. The pulse is operable to raise the pressure in pressure chamber 18 and creates droplet 34.
The embodiment shown in
Stagnation flow geometry can be achieved between opposing in-flows that are parallel to the plane of the array wherein the fluid meets directly adjacent to the nozzle opening and exits the fire chamber in one or more directions, which are different from the input flow paths. Referring to
The invention has been described in detail with particular reference to certain preferred embodiments thereof, but it will be understood that variations and modifications can be effected within the spirit and scope of the invention.
10 ink jet apparatus
12 reservoir
14 ink supply
16 ink supply passage
18 pressure chamber
20 print head
22 passage
24 nozzle opening
26 nozzle plate
28 meniscus
30 ink return passage
32 actuator
34 ink droplet
36 directional arrow
38 directional arrow
40 directional arrow
42 directional arrow
44 directional arrow
46 energy source
48 energy source
50 actuator
52 actuator