Inkjet printing with managed airflow for condensation control

1. A method for operating an inkjet printing system, comprising:

moving a receiver in a direction of receiver movement past a printing module having a plurality of inkjet printheads with a barrier between the inkjet printheads, each printhead having a face;

using a plurality of caps with each cap positioned about one of the inkjet printheads and extending from the barrier toward the receiver to create higher resistance flow areas between the cap and the receiver with each cap extending away from the face of the corresponding printhead to form a shielded region having an opening through which ink drops can pass from the plurality of inkjet printheads through one of the higher resistance flow areas to the receiver with the caps being separated to create lower resistance airflow channels between the caps, the barrier, and the receiver;

directing ink droplets from the inkjet printheads to pass through the openings, into the higher resistance flow areas and onto the receiver;

providing a cross-module air flow between the barrier and the receiver; and

deflecting the cross-module airflow into and through the lower resistance airflow channels without creating flows into the higher resistance flow areas that cause an artifact in a print; and

guiding the cross module airflow after the cross-module airflow passes the inkjet printheads of the first print line so that airflow that has passed the printheads of the first print line does not create flows that disrupt ink droplet placement by the inkjet nozzle arrays of the second print line, wherein said guiding of the cross module airflow is performed in part by trailing surfaces of the caps about the first plurality of printheads at the first print line that have a convex shape to guide cross-module airflow after cross-module airflow passes inkjet printheads of the first print line and by deflection surfaces of the caps about the second portion of the plurality of printheads that have a concave shape that corresponds to the convex shape of the trailing surfaces so that any attic cross module airflow that has passed the portion of the printheads of the first print line does not create conditions that can disrupt ink droplet placement by the portion of the plurality of inkjet printheads at the second print line, and wherein one portion of the inkjet printheads is arranged along a first print line and another portion of the plurality of inkjet printheads is arranged along a second print line, and wherein the movement of the receiver along the direction of receiver movement brings the receiver past the first print line and then past the second print line in a direction that is parallel to the direction of the cross-module airflow.

2. The method of claim 1 , wherein the caps are separated by a separation distance of between about 2 mm to 15 mm.

3. The method of claim 1 , wherein each cap has one of the lower resistance airflow channels on each side of the cap and further comprising deflecting the cross-module airflow incident on the cap so that a portion of the cross-module airflow passes the cap in a lower resistance airflow channel that is on one side of the cap and a generally equal portion of the cross-module airflow passes the cap on the other side of the cap.

4. The method of claim 1 , wherein the cross-module airflow is guided into lower resistance airflow channels between the caps through which the cross-module air flow can flow past the second print line without creating flows into the higher resistance flow areas that create an artifact in the print.

5. The method of claim 1 , wherein portions of the cross module airflow that are divided to flow around a cap of the first print line are combined at a confluence adjacent to a cap of the second print line.

6. The method of claim 1 , wherein at least a portion of the plurality of caps is along a first print line that is not parallel to a direction of receiver movement and further comprising at one end of the at least one print line, a cap having one side without an adjacent cap and further comprising a the step of shaping the airflow on the one side of the cap without the adjacent cap in a manner that is consistent with the airflow on the other side of the cap that is without the adjacent cap.

7. The method of claim 6 , wherein the side flow control structure creates a higher resistance flow area between the side flow control structure and the receiver and further creates a lower resistance airflow channel between the side flow control structure and a cap that is adjacent to the side flow control structure to provide a flow of cross-module airflow around the adjacent cap that does not create pressures in the lower resistance airflow channels that are sufficient to cause flows into the higher resistance flow areas that induce artifacts in a print.

8. The method of claim 6 , wherein the side flow control structure is heated above a condensation temperature of vaporized carrier fluid from the ink droplets.

9. The method of claim 1 , further comprising the step of maintaining consistent airflow characteristics between the receiver and the barrier across the width direction during printing when the receiver does not extend across an entire width direction.

10. The method of claim 1 , wherein the caps have deflection surfaces that include deflection surfaces that begin at vertices and that are sloped relative to the direction of receiver movement at generally equal deflection angles to divide cross module airflow and to guide the divided cross-module airflow into different ones of the lower resistance airflow channels.

11. The method of claim 10 , wherein the caps have a mirror symmetry about a central axis that extends along the direction of receiver movement through a center of the caps and through the vertices.

12. The method of claim 10 , wherein the deflection surfaces are generally flat and extend from the vertices at a slope of between 0.25 and 1.0 relative to the direction of receiver movement.

13. The method of claim 1 , further comprising flow guides that are positioned between the caps about the first portion of the plurality of printheads and supply ducts that supply the cross-module airflow between the barrier and the receiver, with each of the flow guides providing deflection surfaces that extend from a vertex to create a channeled flow of cross-module airflow that flows into engagement with the caps about the first portion of the plurality of printheads.

14. The method of claim 1 , wherein at least one of the caps extends upstream of the opening in the cap by a threshold distance so that resistance to flow in the higher resistance flow areas reduces the energy any portion of the cross-module airflow entering the higher resistance flow area to a level that is below a level that is necessary to deflect ink droplets in a manner that can create image artifacts.

15. The method of claim 1 , wherein at least one of the caps extends upstream from the opening in the cap by a threshold distance that is greater than one quarter of a width of a nozzle array of a printhead about which the cap is located.

16. The method of claim 1 , wherein at least one of the caps extends upstream from the opening in the cap by a threshold distance that is at least ten times more than a clearance distance between the at least one of the caps and the receiver in the higher resistance flow area formed between the cap and the receiver.

17. The method of claim 1 , wherein the cross-module airflow is supplied in a generally equal flow onto each of the caps.

18. The method of claim 1 , further comprising a plurality of individual supply ducts arranged across a width direction of the caps of a first print line to provide a generally equal flow of cross-module airflow onto each of the caps.

19. The method of claim 1 , wherein the caps are shaped and are separated to cause lower resistance airflow to pass inkjet printheads in portions of lower resistance airflow paths where the cap separation distances are generally constant.

20. The method of claim 1 , further comprising the step of containing an extent to which cross-module airflow can be deflected along a width direction.

21. The method of claim 1 , further comprising providing a vacuum assembly having a plurality of vacuum ports that are aligned with the lower resistance airflow channels and sized to provide a vacuum suction that is focused at the lower resistance airflow channels.

22. The method of claim 1 , wherein the lower resistance airflow channels have a constant width between the caps of the first print line and the caps of the second print line.