Compressed air fluid separator with vortex baffle

1. A fluid separator for a compressed air system comprising: a head cap defining an inlet port and an outlet port; a first body defining an inner air shaft extending from an upper end to an opposing lower end, the upper end in fluid communication with the inlet port, the inner air shaft to form a downward linear air flow to the lower end from an incoming air flow received via the inlet port; a vortex baffle disposed about the lower end of the inner air shaft; and a second body forming an outer air shaft about the inner air shaft and the vortex baffle, the outer air shaft extending from a lower end proximate to the vortex baffle to an upper end in fluid communication with the outlet port, the vortex baffle including: a base flange forming a bottom of the inner air shaft and defining a floor of the outer air shaft; and a plurality of airfoil fins disposed about a circumference of the inner air shaft, the airfoil fins and the base flange, including a portion forming the floor of the outer air shaft, to receive and convert the downwardly flowing linear airflow from the lower end of the inner air shaft to an upwardly flowing vortical air flow in the outer air shaft to the outlet port.

2. The fluid separator of claim 1 , the first and second bodies comprising tubular bodies, the first tubular body concentrically disposed within the second tubular body.

3. The fluid separator of claim 1 , the plurality of airfoil fins disposed about and spaced from an external circumference of the inner air shaft.

4. The fluid separator of claim 3 , a longitudinal dimension of the airfoil fins extending in an axial direction of the inner air shaft.

5. The fluid separator of claim 3 , the first tubular body including a plurality of exit air slots at the lower end of the inner air shaft, the vortex baffle receiving the downwardly flowing linear air flow from the inner air shaft via the exit air slots.

6. The fluid separator of claim 5 , the vortex baffle including a plurality of alignment tabs configured to engage the lower end of the inner air shaft and align the plurality of air foils with the exit air slots.

7. A fluid separator for a compressed air system comprising: a head cap defining an inlet port and an outlet port; a first body defining an inner air shaft extending from an upper end to an opposing lower end, the upper end in fluid communication with the inlet port; a vortex baffle including a base flange disposed about the lower end of the inner air shaft; and a second body forming an outer air shaft about the inner air shaft and the vortex baffle, the outer air shaft extending from a lower end proximate to the vortex baffle to an upper end in fluid communication with the outlet port; the vortex baffle coupled to the head cap by a threaded rod, the base flange including an integral threaded nut to receive the threaded rod.

8. The fluid separator of claim 7 , the base flange including finger tabs extending therefrom to facilitate tightening of the vortex baffle to the threaded rod.

9. The fluid separator of claim 7 , the first body disposed between the head cap and the vortex baffle, the vortex baffle to hold the first body in place when coupled to the threaded rod.

10. A compressed air water separator comprising:

outer air shaft having an upper end in fluid communication with an outlet port and a lower which is closed to form a sump basin;

an inner shaft disposed within the outer shaft and having an upper end in fluid communication with an inlet port and a lower end spaced from the sump basin, and having a plurality of exit air slots through sidewalls about a perimeter of the inner air shaft at the lower end; and

a vortex baffle disposed about a portion of the lower end of the inner shaft, the vortex baffle spaced from the inlet port and outlet port by at least a length of the inner shaft, the vortex baffle including:

base flange disposed below the lower end of the inner air shaft and forming a floor to the outer air shaft above the sump basin; and

a plurality of airfoil fins extending from the base flange and disposed about the perimeter of the inner air shaft proximate to the exit air slots.

11. The compressed air water separator of claim 10 , a longitudinal dimension of the exit air slots and a longitudinal dimension of the airfoil fins extending in the direction of longitudinal axes of the inner and outer air shafts.

12. The compressed air water separator of claim 11 , the vortex baffle including alignment features to engage alignment feature on the lower end of the inner air shaft to ensure a desired alignment of the airfoil fins with the exit air slots.

13. The compressed air water separator of claim 10 , including a mesh filter disposed within the outer air shaft about the inner air shaft between the vortex baffle and the outlet port.

14. A method of separating fluid from a compressed air flow comprising:

concentrically positioning an first air shaft within a second air shaft;

directing an incoming compressed air flow downwardly through the first air shaft from an upper end to a lower end to form a downwardly flowing linear air flow;

closing off a bottom of the first air shaft and forming a plurality of slots in sidewalls of the first air shaft at the lower end;

closing off a portion of the second air shaft below the lower end of the first shaft with a flange;

positioning a plurality of airfoil fins within the second air shaft about an exterior perimeter of the lower end of the first air shaft above the flange adjacent to the plurality of slots; and

transforming the downwardly flowing linear air flow exiting the lower end of the first air shaft via the slots into an upwardly flowing vortical air flow within the second air shaft from an lower end to an upper end via the airfoil fins and the flange.

15. The method of claim 14 , the airfoil fins extending longitudinally in a direction of a longitudinal axes of the first and second air shafts.

16. The method of claim 14 , positioning a mesh filter in the second air shaft between the lower end of the first air shaft and the upper end of the second air shaft.

17. The method of claim 14 , including:

forming a sump basin in a lower portion of the second air shaft below the lower end of the first air shaft in which fluids removed by centrifugal force from the vortical air flow collect by gravity.