Turbine design for flow meter
A turbine wheel used in a turbine flow meter includes a hub configured to be freely rotatably fixed in position inside a fluid pipe section. A first cylindrical rim is centered about the hub and the longitudinal axis and spaced a distance apart from the hub. A first vane set extends outwardly from the hub to the first cylindrical rim, wherein a root of each vane of the first vane set is attached to the hub and a tip of each vane of the first vane set is attached to the first cylindrical rim. The first vane set may consist of one or two individual vanes. An external vane set may extend outwardly from the first cylindrical rim, wherein a root of each vane is attached to the first cylindrical rim and a tip of each vane is not attached to any cylindrical rim.
1 . A turbine wheel configured for use in a turbine flow meter, the turbine wheel comprising:
a hub centered about and defining a longitudinal axis, wherein the hub is configured to be freely rotatably fixed in position inside a fluid pipe section;
a first cylindrical rim centered about the hub and the longitudinal axis and spaced a distance apart from the hub, wherein connection between the hub and the first cylindrical rim is limited to a first set of no more than two vanes each having a root attached to the hub and a tip attached to the first cylindrical rim; and
an external vane set extending outwardly from the first cylindrical rim, wherein a root of each vane of the external vane set is attached to the first cylindrical rim and a tip of each vane of the external vane set is not attached to any cylindrical rim.
2 . The turbine wheel of claim 1 , wherein the first vane set is limited to one individual vane.
3 . The turbine wheel of claim 1 , wherein a pocket is formed in the first cylindrical rim, and wherein a magnet or a magnetically-permeable ferrous part is disposed within the pocket.
4 . The turbine wheel of claim 1 , wherein the hub, the first cylindrical rim, and the first vane set of the turbine wheel are formed as a single-shot, plastic injection molded, homogeneous part.
5 . The turbine wheel of claim 4 , wherein the single-shot, plastic injection molded, homogeneous part has a specific gravity at or between 0.9 to 1.0.
6 . The turbine wheel of claim 4 , wherein the single-shot, plastic injection molded, homogeneous part is formed from a polypropylene homopolymer.
7 . The turbine wheel of claim 1 , wherein each vane of the first set of no more than two vanes extends helically from a front face of the turbine wheel to a rear face of the turbine wheel.
8 . The turbine wheel of claim 1 , wherein attachment of the root of each vane of the first set of no more than two vanes to the hub extends from a front face of the turbine wheel to a rear face of the turbine wheel, and attachment of the tip of each vane of the first set of no more than two vanes to the first cylindrical rim extends from the front face of the turbine wheel to the rear face of the turbine wheel.
9 . The turbine wheel of claim 1 , wherein the first cylindrical rim and the first set of no more than two vanes are fixed with the hub for rotation with the hub inside the fluid pipe section.
10 . The turbine wheel of claim 1 , in combination with:
a pipe section, the turbine wheel being rotatable within the pipe section; and
front and rear bearings secured within the pipe section, wherein the hub of the turbine wheel is freely rotatably fixed to the front and rear bearings.
11 . A turbine wheel configured for use in a turbine flow meter, the turbine wheel comprising:
a hub centered about and defining a longitudinal axis, wherein the hub is configured to be freely rotatably fixed in position inside a fluid pipe section;
a first cylindrical rim centered about the hub and the longitudinal axis and spaced a distance apart from the hub, wherein connection between the hub and the first cylindrical rim is limited to a first set of no more than two vanes each having a root attached to the hub and a tip attached to the first cylindrical rim;
wherein the first vane set comprises first and second vanes angled such that a front end of the first vane and a rear end of the second vane extend radially outward from the hub to the first cylindrical rim in a first radial direction and a rear end of the first vane and a front end of the second vane extend radially outward from the hub to the first cylindrical rim in a second radial direction opposite the first radial direction;
wherein the front end of the first vane and the rear end of the second vane define a first passthrough area and the rear end of the first vane and the front end of the second vane define a second passthrough area, wherein a space in the turbine wheel for fluid to pass directly through is limited to the first and second passthrough areas.
12 . The turbine wheel of claim 1 , wherein the external vane set comprises more than two vanes.