Aerodynamic fairing structure for inkjet printing

1. A printing device, comprising:

an ink-dispensing structure which carries a printhead with a leading edge, and which moves in a printing sweep downstream across a printzone;

a fairing structure downstream from the leading edge of the printhead; and

a mounting structure which supports the fairing structure for movement with the printhead downstream from the leading edge of the printhead in a position configured to reduce aerodynamic turbulence associated with the leading edge of the printhead during movement of the printhead downstream across the printzone.

2. A printing device according to claim 1 , wherein the fairing structure is yieldably spring-biased toward a deployed position.

3. A printing device according to claim 1 , which further comprises a moveable capping structure movable into and out of a capping condition, and wherein the capping structure includes an engagement structure movable with the capping structure to selectively operatively engage the fairing structure to shift the fairing structure from a deployed position toward a nondeployed position.

4. A printing device according to claim 3 , further comprising a cleaning structure operatively associated with the engagement structure and operable to clean the fairing structure.

5. A printing device according to claim 1 , wherein the fairing structure is pivotally attached to the ink-dispensing structure.

6. A printing device according to claim 1 , wherein the fairing structure is slidably attached to the ink-dispensing structure.

7. A printing device, comprising:

an ink-dispensing structure which carries a printhead with a leading edge, and which moves in a printing sweep downstream across a printzone;

a fairing structure; and

a mounting structure which supports the fairing structure for movement with the printhead downstream from the leading edge of the printhead in a position configured to reduce aerodynamic turbulence associated with the leading edge of the printhead during movement of the printhead downstream across the printzone;

wherein the leading edge lies substantially in a plane which generally faces the printzone, and wherein the fairing structure defines a surface which, with the fairing structure in a deployed position, lies substantially in the plane, and which, with the fairing structure in a nondeployed position, lies spaced from the plane.

8. A printing device, comprising:

an ink-dispensing structure which carries a printhead with a leading edge, and which moves in a printing sweep downstream across a printzone;

a fairing structure;

a mounting structure which supports the fairing structure for movement with the printhead downstream from the leading edge of the printhead in a position configured to reduce aerodynamic turbulence associated with the leading edge of the printhead during movement of the printhead downstream across the printzone; and

an actuator structure disposed along a travel path of the printhead, the actuator structure being configured to operatively engage the fairing structure on selected movement of the fairing structure to shift the fairing structure from a deployed position toward a nondeployed position.

9. A printing device according to claim 8 , wherein the actuator structure includes a camming ramp structure mounted adjacent at least one end of travel.

10. A printing device according to claim 9 , further comprising a cleaning structure operatively associated with the actuator structure and operable to clean the fairing structure.

11. A method of reducing aerodynamic swath-height error in a printer having an ink-dispensing structure with a leading edge, comprising:

moving the ink-dispensing structure in a printing sweep downstream across a printzone during a printing operation;

establishing an aerodynamic fairing structure downstream of the leading edge of the ink-dispensing structure, the fairing structure being capable of reducing aerodynamic turbulence which would otherwise result in a vicinity of the leading edge of the printhead as the ink-dispensing structure moves across the printzone; and

selectively positioning the fairing structure in a position adjacent the leading edge of the ink-dispensing structure to reduce aerodynamic turbulence in the vicinity of the leading edge during said moving.

12. A method of reducing aerodynamic swath-height error in a printer having ink-dispensing printhead structure including a printhead which moves with an advancing leading edge in a printing sweep downstream across a printzone during a printing operation, the method comprising the steps of:

moving the printhead with the advancing leading edge downstream across the printzone; and

while moving the printhead, employing a likewise-advancing aerodynamic barrier at a location adjacent, traveling with, and downstream from the advancing leading edge of the printhead, thereby reducing aerodynamic turbulence adjacent the advancing leading edge of the printhead relative to aerodynamic turbulence which would otherwise be produced adjacent the advancing leading edge of the printhead upon moving the printhead downstream across the printzone.

13. Apparatus for reducing aerodynamic swath-height error in a printing device having an ink-dispensing structure which moves with an advancing leading edge in a printing sweep downstream across a printzone during a printing operation, the apparatus comprising:

fairing means for impacting air flow in said printzone; and

mounting means for mounting the aerodynamic fairing for movement with the printhead at a location downstream from the leading edge of the printhead, and in a position relative to the printhead which is effective, during movement of the printhead downstream, to displace aerodynamic turbulence which would otherwise result in a vicinity of the leading edge of the printhead during advancement of the printhead downstream.

14. The apparatus of claim 13 , wherein the leading edge of the printhead lies substantially in a plane which generally faces the printzone, and wherein the aerodynamic fairing defines a surface which also lies generally within the plane during movement of the printhead and aerodynamic fairing across the printzone.

15. A method of printing, comprising:

deploying a fairing adjacent the downstream portion of the printhead;

scanning a printhead and deployed fairing structure downstream across a printzone;

ejecting ink droplets from the printhead onto media, during said scanning;

controlling airflow turbulence between the printhead and the media; and

in response to said controlling, depositing the ejected droplets in a preselected pattern on the media to form a desired image.

16. The method of claim 15 , wherein said controlling airflow turbulence includes sheltering a leading edge of the printhead with the deployed fairing structure during said scanning.

17. A method of printing, comprising:

scanning a printhead downstream across a printzone;

ejecting ink droplets from the printhead onto media, during said scanning;

controlling airflow turbulence between the printhead and the media, including disrupting static air downstream from a leading edge of the printhead during said scanning; and

in response to said controlling, depositing the ejected droplets in a preselected pattern on the media to form a desired image.