Method for modelling a part, in particular a blading
US-2016063139-A1 · Mar 3, 2016 · US
US10301970B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10301970-B2 |
| Application number | US-201615182707-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 15, 2016 |
| Priority date | Jun 18, 2015 |
| Publication date | May 28, 2019 |
| Grant date | May 28, 2019 |
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An axial turbine includes an upstream turbine stage that includes: a cover disposed at a distal end of an upstream bucket and opposed to an inner wall of an upstream diaphragm outer ring across a gap; and a downstream diaphragm outer ring that is disposed downstream of the upstream turbine stage and that has an inner peripheral-side end wall shaped into a flare. The inner peripheral-side end wall of the downstream diaphragm outer ring has a flare angle formed to be greater than a slant angle of an inner peripheral-side wall of the cover. In the axial turbine, the inner peripheral-side end wall of the downstream diaphragm outer ring is formed to have a meridional shape that has at least one inflection point between the upstream turbine stage and a downstream turbine stage and such that a tangent at the inflection point with respect to a steam flow direction has a positive gradient.
Opening claim text (preview).
What is claimed is: 1. An axial turbine, comprising: an upstream turbine stage including: a plurality of upstream nozzles arrayed in a tangential direction between an upstream diaphragm outer ring and an upstream diaphragm inner ring; a plurality of upstream buckets disposed on an outer peripheral side of a turbine rotor and arrayed in the tangential direction; and a cover disposed at a distal end of at least one of the upstream buckets and opposed to an inner wall of the upstream diaphragm outer ring across a gap; and a downstream turbine stage including: a downstream diaphragm outer ring disposed downstream of the upstream turbine stage, the downstream diaphragm outer ring having an inner peripheral-side end wall shaped into a flare; a plurality of downstream nozzles arrayed in the tangential direction between the downstream diaphragm outer ring and a downstream diaphragm inner ring; and a plurality of downstream buckets disposed on the outer peripheral side of the turbine rotor and arrayed in the tangential direction, the inner peripheral-side end wall of the downstream diaphragm outer ring having a flare angle formed to be greater than a slant angle of an inner peripheral-side wall of the cover, wherein the inner peripheral-side end wall of the downstream diaphragm outer ring has a meridional shape curved into an S-shape that has an inflection point between the at least one of the upstream buckets and a front edge of the downstream nozzle such that a tangent at the inflection point with respect to a steam flow direction has a positive gradient. 2. The axial turbine according to claim 1 , wherein a radius position of the inner peripheral-side end wall of the upstream diaphragm outer ring, the radius position being opposed to an outer peripheral-side wall of the cover, is located outer side in a radius direction than a minimum radius position of the inner peripheral-side wall of the downstream diaphragm outer ring. 3. The axial turbine according to claim 1 , wherein the meridional shape of the inner peripheral-side end wall of the downstream diaphragm outer ring disposed between the upstream turbine stage and the downstream turbine stage is formed using a Bezier curve.
using blades (F01D5/148 takes precedence) · CPC title
in steam turbines · CPC title
Blades ({specially adapted for radial flow machines or engines F01D5/04}; blade roots F01D5/30; rotors with blades adjustable in operation F01D7/00; stator blades F01D9/02) · CPC title
Casings (modified for heating or cooling F01D25/14); Casing parts, e.g. diaphragms, casing fastenings (casings for rotary machines or engines in general F16M {; special arrangements in stators dealing with breaking-off of part of rotor F01D21/045}) · CPC title
by shrouding · CPC title
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