Turbine arrangement
The invention relates to a turbine for generating work by a stagewise expansion of a gas, such as steam wherein a downstream stage guide average height is less than an adjacent upstream stage runner average height.
1. A turbine for generating work by a stagewise expansion of a gas, the turbine having an axial direction corresponding to an expansion flow of the gas and a radial direction, the turbine further comprising:
a casing inner surface;
a hub,
a first axial stage including:
a first guide fixed to the casing inner surface:
a first runner fixed to the hub downstream of the first guide, having:
a first runner tip radially distal from the hub,
a first runner average radial height between the first runner tip and the hub along an axial midpoint of the first runner;
a second axial stage, downstream of the first axial stage, including:
a second guide, fixed to the casing inner surface, having;
a second guide tip distal from the casing inner surface;
a second guide average radial height between the second guide tip and the casing inner surface along an axial midpoint of the second guide; and
a second runner, fixed to the hub downstream of the second guide, wherein the second guide average height is less than the first runner average height.
2. The turbine of claim 1 , wherein the hub has a hub radius-which is constant in a region extending between and including the first guide and the second runner.
3. The turbine of claim 1 , wherein the hub has a hub radius which is variable in a region extending between and including the first guide and the second runner such that the hub radius both increases and decreases.
4. The turbine of claim 1 further comprising:
a second runner tip radially distal from the hub, wherein:
a first runner radial height between the hub and the first runner tip increases along the axial direction such that a hade angle formed by the first runner tip is constant along the axial direction; and
a second runner radial height increases along the axial direction such that a hade angle formed by the second runner tip is constant along the axial direction.
5. The turbine of claim 1 , wherein the first guide, along the casing inner surface in the axial direction, forms a bellmouth shape and the second guide, along the casing inner surface in the axial direction, forms a bellmouth shape.
6. The turbine of claim 1 , further comprising:
a first guide tip distal from the casing inner surface, wherein:
a first guide radial height, between the casing inner surface and the first guide tip, decreases along the axial direction; and
a second guide radial height between the casing inner surface and the second guide tip decreases along the axial direction.
7. The turbine of claim 1 wherein a K value of the first runner varies from 0.25 at the hub to 0.16 at the first runner tip.
8. The turbine of claim 1 , wherein a K value of the second guide varies from 0.15 at casing inner surface to 0.25 at the second guide tip.
9. The turbine of claim 1 , wherein a back surface deflection of the first runner, the second runner, or both the first runner and the second runner is between 25 degree and 35 degrees.
10. The turbine of claim 1 , wherein the turbine is a gas turbine and a back surface deflection of the first runner and/or the second runner is between 25 degrees and 30 degrees.