A fluid tip for use with a spray gun. The fluid tip comprises an air cap and a paint nozzle. The air cap comprises an inner surface 206 and the paint nozzle comprises an outer surface 208 . The inner and outer surfaces define sides of an air channel 203 . The inner and outer surfaces are defined by contours, each contour terminating to form an air channel outlet 207 for discharging an air jet proximal a paint nozzle outlet of the paint nozzle. The contours are configured to provide a velocity profile 400 across the air channel outlet 207 of an air flow 401 through the air channel 203 in which velocities of air radially closer to the paint nozzle outlet are substantially higher than velocities radially further from the paint nozzle outlet.
1. A system, comprising:
a fluid tip configured to couple to a paint spray gun, wherein the fluid tip comprises:
an air cap comprising an inner surface;
a paint nozzle comprising an outer surface;
the inner and outer surfaces define sides of an air channel;
the inner and outer surfaces are defined by curvilinear contours that curve in a downstream direction of an air flow through the air channel and turn away from a radial direction toward and axial direction relative to a central axis of the fluid tip, each curvilinear contour terminating to form an air channel outlet configured to discharge an air jet to atomize paint exiting from a paint nozzle outlet of the paint nozzle;
the curvilinear contours are configured to provide a velocity profile across the air channel outlet of the air jet in which velocities of air radially closer to the paint nozzle are higher than velocities radially further from the paint nozzle outlet, wherein the paint nozzle comprises a paint nozzle inner diameter and a paint nozzle thickness, wherein the paint nozzle thickness is configured to be 4.44×the paint nozzle inner diameter for a paint of minimal viscosity.
2. The system of claim 1 , wherein the inner surface is defined by a convex contour in the downstream direction, and the outer surface is defined by a concave contour in the downstream direction.
3. The system of claim 1 , wherein the curvilinear contours overlap one another over an axial distance along the central axis of the fluid tip and extend directly to the air channel outlet, and the inner and outer surfaces extend in the axial direction at the air channel outlet.
4. The system of claim 1 , wherein the curvilinear contours are configured to cause the velocity profile of air jet at the air channel outlet to follow a parabolic distribution having a maximum velocity radially closest to the paint nozzle.
5. The system of claim 1 , wherein a separation distance between the nozzle outlet and the air channel outlet is based on a predetermined viscosity of paint flowing through the paint nozzle outlet.
6. The system of claim 5 wherein the separation distance is based on one or more of surface tension, density, and dynamic viscosity of the paint flowing through the paint nozzle outlet.
7. The system of claim 1 , wherein the air channel and/or the air channel outlet surrounds the paint nozzle.
8. The system of claim 1 , wherein the air channel and/or the air channel outlet are annular around the nozzle.
9. The system of claim 1 , wherein the air channel outlet is configured to discharge air in the same axial direction as paint discharged from the nozzle outlet.
10. The system of claim 1 , further comprising one or more horns protruding from an external surface of the air cap, each of the one or more horns comprising auxiliary air passages configured to discharge auxiliary an auxiliary air flow towards an atomisation region downstream of the paint nozzle outlet.
11. The system of claim 1 , comprising the paint spray gun having the fluid tip.
12. A system, comprising:
a fluid tip configured to couple to a paint spray gun, wherein the fluid tip comprises:
a paint channel extending to a paint nozzle outlet; and
an air channel extending to an air channel outlet, wherein the air channel outlet is configured to discharge an air jet to atomize paint exiting from the paint nozzle outlet, wherein a first surface having a first curvilinear contour defines a radially outer boundary of the air channel and a second surface having a second curvilinear contour defines a radially inner boundary of the air channel, the first and second curvilinear contours curve in a downstream direction of an air flow through the air channel and turn away from a radial direction toward an axial direction relative to a central axis of the fluid tip, and the first and second curvilinear contours are configured to provide a velocity profile across the air channel outlet of the air jet in which velocities of air radially closer to the paint nozzle outlet are higher than velocities radially further from the paint nozzle outlet, wherein the paint nozzle outlet comprises a paint nozzle inner diameter and a paint nozzle thickness, wherein the paint nozzle thickness is configured to be 4.44×the paint nozzle inner diameter for a paint of minimal viscosity.
13. The system of claim 12 , wherein the paint nozzle outlet is disposed at the central axis of the fluid tip, and the air channel is radially offset from the central axis of the tip.
14. The system of claim 12 , wherein the first and second curvilinear contours overlap one another over an axial distance along the central axis of the fluid tip.
15. The system of claim 14 , wherein the first and second curvilinear contours extend to the air channel outlet, and the first and second surfaces extend in the axial direction at the air channel outlet.
16. The system of claim 12 , wherein the fluid tip comprises an air cap removably positioned about a paint nozzle, the paint nozzle comprises the paint channel extending to the paint nozzle outlet, and the air cap at least partially defines the air channel extending to the air channel outlet.
17. The system of claim 16 , wherein the air cap comprises the first surface having the first curvilinear contour that defines the radially outer boundary of the air channel, and the paint nozzle comprises the second surface having the second curvilinear contour that defines the radially inner boundary of the air channel.
18. A system, comprising:
a fluid tip configured to couple to a paint spray gun, wherein the fluid tip comprises an air cap and a paint nozzle, wherein the air cap is configured to be positioned about the paint nozzle, the air cap comprises an inner surface, and the paint nozzle comprises an outer surface;
the inner and outer surfaces define sides of an air channel;
the inner and outer surfaces are defined by curvilinear contours that curve in a downstream direction of an air flow through the air channel and turn away from a radial direction toward an axial direction relative to a central axis of the fluid tip, each curvilinear contour terminating to form an air channel outlet configured to discharge an air jet to atomize paint exiting from a paint nozzle outlet of the paint nozzle; and
the curvilinear contours are configured to provide a velocity profile across the air channel outlet of the air jet in which velocities of air radially closer to the paint nozzle outlet are higher than velocities radially further from the paint nozzle outlet, wherein the paint nozzle comprises a paint nozzle inner diameter and a paint nozzle thickness, wherein the paint nozzle thickness is configured to be 4.44×the paint nozzle inner diameter for a paint of minimal viscosity.
19. The system of claim 18 , wherein the curvilinear contours overlap one another over an axial distance along the central axis of the fluid tip and extend directly to the air channel outlet, and the inner and outer surfaces extend in the axial direction at the air channel outlet.