Airflow sensor for averaging total pressure

Claim 2

A flow sensor for compressible fluid having a fluid flow from an upstream direction toward a downstream direction, the flow sensor comprising: a smoothly contoured central hub having a total pressure chamber and a static pressure chamber disposed therein; a pair of wings extending radially outward from opposing sides of the total pressure chamber of the hub, the wings including a plurality of radially spaced holes oriented to generally face the upstream direction and an internal wing passageway connecting the spaced holes to the total pressure chamber; and a static tube having, a tube wall extending radially outward from the static pressure chamber of the hub from a first attached end to a second distal closed end, a generally upstream facing hole and a generally downstream facing hole disposed on opposing sides of the tube wall intermediate the first and second ends to define a fluid flow passage therethrough, and an internal tube passageway connecting the flow passage to the static pressure chamber.

Claim 3

The flow sensor of claim 1 wherein the flow passage of the static tube is shaped to provide a vortex effect, which reduces static pressure of the fluid within the static pressure chamber relative to static pressure of the fluid external to the static chamber.

Claim 4

The flow sensor of claim 1 wherein the radially spaced holes on the wings are substantially spaced per the Log-Tchebycheff rule.

Claim 5

The flow sensor of claim 1 wherein the radially spaced holes on the wings are substantially spaced per the Log-linear rule.

Claim 6

The flow sensor of claim 1 wherein the wings further comprise a first and second pair of wings extending radially outward from opposing sides of the total pressure chamber of the hub.

Claim 7

The flow sensor of claim 5 wherein the static tube further comprises a pair of tubes extending radially outward from opposing sides of the static pressure chamber of the hub.

Claim 8

The flow sensor of claim 1 wherein the fluid flow passage of the static tube is disposed proximate the second closed distal end.

Claim 9

The flow sensor of claim 1 wherein the wings further include an upstream facing edge having a substantially elliptical shape upon which the radially spaces holes are disposed.

Claim 10

The flow sensor of claim 1 wherein the hub further includes an upstream facing nose having a substantially elliptical shape.

Claim 11

The flow sensor of claim 1 wherein the compressible fluid further comprises air.

Claim 12

The flow sensor of claim 1 wherein the wings further include a distal end adapted to be mounted to a duct.

Claim 13

The flow sensor of claim 1 wherein the static tube further includes an end cap mounted to a free radial end portion of the static tube, the end cap having the second closed distal end disposed thereon and the fluid flow passage disposed therethrough.

Claim 14

An airflow sensor adapted to be mounted in a duct, the air having a fluid flow from an upstream direction toward a downstream direction, the flow sensor comprising: a smoothly contoured central hub having a generally bullet shaped nose facing the upstream direction, the hub including a total pressure chamber and a static pressure chamber disposed therein; a first and second pair of wings extending radially outward from opposing sides of the total pressure chamber of the hub, the wings including a plurality of radially spaced holes oriented to generally face the upstream direction and an internal wing passageway connecting the spaced holes to the total pressure chamber; and a pair of static tubes each having, a tube wall extending radially outward from opposing sides of the static pressure chamber of the hub from a first attached end to a second distal closed end, a generally upstream facing hole and a generally downstream facing hole disposed on opposing sides of the tube wall to define a fluid flow passage therethrough proximate the second distal end, and an internal tube passageway connecting the flow passage to the static pressure chamber; wherein the flow passages of the static tubes are shaped to provide a vortex effect, which reduces static pressure of the fluid within the static pressure chamber relative to static pressure of the fluid external to the static pressure chamber.

Claim 15

An airflow sensor adapted to be mounted in a duct, the air having a fluid flow from an upstream direction toward a downstream direction, the flow sensor comprising: a smoothly contoured central hub having a generally bullet shaped nose facing the upstream direction, the hub including a total pressure chamber and a static pressure chamber disposed therein; a first and second pair of wings extending radially outward from opposing sides of the total pressure chamber of the hub, the wings including a plurality of radially spaced holes oriented to generally face the upstream direction and an internal wing passageway connecting the spaced holes to the total pressure chamber; and a pair of static tubes each having, a tube wall extending radially outward from opposing sides of the static pressure chamber of the hub from a first attached end to a second distal closed end, a generally upstream facing hole and a generally downstream facing hole disposed on opposing sides of the tube wall to define a fluid flow passage therethrough proximate the second distal end, and an internal tube passageway connecting the flow passage to the static pressure chamber; wherein the flow passages of the static tubes are shaped to provide a vortex effect, which reduces static pressure of the fluid within the static pressure chamber relative to static pressure of the fluid external to the static pressure chamber.

Claim 16

The flow sensor of claim 13 wherein the radially spaced holes on the wings are substantially spaced per the Log-Tchebycheff rule.

Claim 17

The flow sensor of claim 13 wherein the radially spaced holes on the wings are substantially spaced per the Log-linear rule.

Claim 18

The flow sensor of claim 13 wherein the wings further include an upstream facing edge having a substantially elliptical shape upon which the radially spaces holes are disposed.

Claim 19

The flow sensor of claim 13 wherein nose of the hub further includes a substantially elliptical shape.

Claim 20

The flow sensor of claim 13 wherein the static tube further includes an end cap mounted to a free radial end portion of the static tube, the end cap having the second closed distal end disposed thereon and the fluid flow passage disposed therethrough.