# US 8,739,539 B2 · Alternative partial steam admission arc for reduced noise generation

> Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt

- Number: US 8,739,539 B2
- Document ID: US8739539B2
- Status: Granted
- Kind: B2
- Application number: 13/290,278
- Filed: 2011-11-07
- Published: 2012-05-10
- Granted: 2014-06-03
- Earliest claimed: 2010-11-08
- Assignees: Dresser-Rand Company
- Applicants: Joseph A. Tecza
- Inventors: Joseph A. Tecza
- Web page: https://patentgrep.com/patent/US8739539B2

## CPC

- F01D 9/047: {Nozzle boxes}
- F01D 9/041: {using blades (F01D5/148 takes precedence)}
- F05D 2220/31: in steam turbines
- F05D 2260/96: Preventing, counteracting or reducing vibration or noise
- F05D 2260/961: by mistuning rotor blades or stator vanes with irregular interblade spacing, airfoil shape
- F01D: NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES (machines or engines for liquids F03; non-positive displacement pumps F04D)
- F05D: INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS

## Abstract

A diaphragm for a steam turbine is disclosed that has at least one arc of admission. The arc of admission has a plurality of nozzles arranged about the circumference of the diaphragm and are configured to eject a working fluid at succeeding rotor blades axially-spaced from the diaphragm. The flow area of the first few nozzle vanes in the arc of admission is gradually increased along the arcuate length of the diaphragm, thereby mitigating the load impulse absorbed by each rotor blade as it enters the arc of admission. The flow area of the last few nozzle vanes in the arc of admission is gradually decreased so that each rotor blade does not suddenly go from full load impulse to zero and thereby contribute to the fatigue of the rotor blade and create unwanted noise.

## Claims

### Claim 1

An arc of admission for a steam turbine, comprising:
an outer arcuate wall radially-offset from an inner arcuate wall, the inner and outer arcuate walls each extending from a first end to a second end; and
a plurality of nozzle vanes circumferentially-spaced between the first end and the second end and arranged between the outer and inner arcuate walls, the plurality of nozzle vanes including a first set of nozzle passages disposed at the first end and a second set of nozzle passages disposed at the second end, wherein the first and second sets of nozzle passages define a flow area that is reduced.

### Claim 2 (depends on 1)

The arc of admission of claim 1, wherein the inner and outer arcuate walls extend circumferentially about 90 degrees.

### Claim 3 (depends on 1)

The arc of admission of claim 1, wherein the flow area of each adjacent nozzle passage in the first set gradually increases from the first end toward the second end.

### Claim 4 (depends on 3)

The arc of admission of claim 3, wherein the first set includes three nozzle passages.

### Claim 5 (depends on 1)

The arc of admission of claim 1, wherein the flow area of each adjacent nozzle passage in the second set gradually increases from the second end toward the first end.

### Claim 6 (depends on 5)

The arc of admission of claim 5, wherein the second set includes three nozzle passages.

### Claim 7 (depends on 1)

The arc of admission of claim 1, wherein the flow area of each nozzle passage is reduced by decreasing a height of the first and second sets of nozzle passages.

### Claim 8 (depends on 7)

The arc of admission of claim 7, wherein the height of the first and second sets of nozzle passages is reduced by moving the outer arcuate wall radially-inward.

### Claim 9 (depends on 7)

The arc of admission of claim 7, wherein the height of the first and second sets of nozzle passages is reduced by moving the inner arcuate wall radially-outward.

### Claim 10 (depends on 7)

The arc of admission of claim 7, wherein the height of the first and second sets of nozzle passages is reduced by moving the outer arcuate wall radially-inward and the inner arcuate wall radially-outward.

### Claim 11

A steam turbine, comprising:
a steam chest fluidly coupled to a plurality of supply pipes regulated by a corresponding plurality of valves, the steam chest being configured to supply a working fluid to the plurality of supply pipes when the corresponding plurality of valves are in an open position; and
a diaphragm fluidly coupled to each supply pipe and having an outer arcuate wall radially-offset from an inner arcuate wall, the diaphragm defining a first arc of admission having a plurality of nozzle vanes arranged between the inner and outer arcuate walls and circumferentially-spaced between a first end and a second end, wherein a first set of nozzle passages adjacent the first end and a second set of nozzle passages adjacent the second end have a height that is reduced.

### Claim 12 (depends on 11)

The steam turbine of claim 11, wherein the height of each adjacent nozzle passage in the first set of nozzle passages gradually increases from the first end toward the second end.

### Claim 13 (depends on 12)

The steam turbine of claim 12, wherein the height of each adjacent nozzle passage in the second set of nozzle passages gradually increases from the second end toward the first end.

### Claim 14 (depends on 13)

The steam turbine of claim 13, wherein the circular diaphragm further defines a second arc of admission having a first end, a second end, and a third set of nozzle passages arranged at the first end of the second arc of admission, wherein the third set of nozzle passages has a height that is reduced.

### Claim 15 (depends on 14)

The steam turbine of claim 14, wherein the third set of nozzle passages is arranged circumferentially-adjacent the second set of nozzle passages of the first arc of admission, the height of each adjacent nozzle passage in the third set of nozzle passages gradually increasing from the first end of the second arc of admission toward the second end of the second arc of admission.

### Claim 16 (depends on 11)

The steam turbine of claim 11, wherein the height of the first and second sets of nozzle passages is reduced by moving the outer arcuate wall radially-inward.

### Claim 17 (depends on 11)

The steam turbine of claim 11, wherein the height of the first and second sets of nozzle passages is reduced by moving the inner arcuate wall radially-outward.

### Claim 18 (depends on 11)

The steam turbine of claim 11, wherein the height of the first and second sets of nozzle passages is reduced by moving the outer arcuate wall radially-inward and the inner arcuate wall radially-outward.

### Claim 19

A method of reducing sudden load impulses on rotor blades, comprising:
injecting a working fluid into an arc of admission having a plurality of nozzle vanes circumferentially-spaced between a first end and a second end, the plurality of nozzle vanes including a first set of nozzle passages disposed at the first end and a second set of nozzle passages disposed at the second end, wherein the first and second sets of nozzle passages have a reduced flow area; and
ejecting the working fluid from the arc of admission and downstream toward rotor blades rotating about a central axis, wherein a load impulse imparted by the working fluid on each rotor blade progressively increases across the first set of nozzle passages and then progressively decreases across the second set of nozzle passages.

### Claim 20 (depends on 19)

The method of claim 19, wherein the working fluid is steam.