# US 5,344,160 A · Shaft sealing of steam turbines

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- Number: US 5,344,160 A
- Document ID: US5344160A
- Status: Granted
- Kind: A
- Application number: 07/986,573
- Filed: 1992-12-07
- Granted: 1994-09-06
- Earliest claimed: 1992-12-07
- Assignees: General Electric Company
- Inventors: Steven P. Scarlata; Adrian Missana
- Web page: https://patentgrep.com/patent/US5344160A

## CPC

- F16J 15/004: {forming of recuperation chamber for the leaking fluid}
- F01D 11/02: by non-contact sealings, e.g. of labyrinth type (for sealing space between rotor blade tips and stator F01D11/08)
- F16J: PISTONS {(specially adapted for dampers F16F9/32)}; CYLINDERS; SEALINGS
- F01D: NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES (machines or engines for liquids F03; non-positive displacement pumps F04D)

## Abstract

A shaft sealing system for a steam turbine includes at the high-pressure inlet end an outer air seal (40 ) and an outer steam seal (42 ) each comprised of segmented circumferential seals and a plurality of labyrinth seals (44, 46, 48). The low-pressure end of the turbine is provided with a segmented circumferential seal (60) substantially precluding ingress of air past the seal. The steam leaking past the inner two labyrinth seals (46 and 48) is returned to a stage of the turbine by a first leak-off pipe system (50). Air leaking past the air seal and steam leaking outwardly past the outer steam seal (42) is piped to the main condenser (58). High-pressure steam between the outer steam seal (42) and the outermost labyrinth seal (44) is piped via a second leak-off path (56) to a turbine stage downstream from the first-mentioned turbine stage.

## Claims

### Claim 1

In a multi-stage steam turbine having a first rotating member including a shaft, a second stationary member surrounding said first member and defining a steam flow path having a high-pressure inlet at one end of the turbine and a low-pressure outlet at its opposite end, a shaft sealing system adjacent the inlet and outlet ends of said turbine, comprising:
a pair of axially spaced labyrinth seals about said shaft adjacent said high-pressure inlet end and defining an annulus therebetween;
a pair of axially segmented circumferential seals about and contacting said shaft defining an annulus therebetween and spaced axially outwardly of said labyrinth seals;
an axially outermost segmented circumferential seal of said pair of segmented circumferential seals constituting an air seal sealing between ambient and the annulus between said segmented circumferential seals;
another of said pair of segmented circumferential seals constituting an outer steam seal sealing between said labyrinth seals and the annulus between said segmented circumferential seals,
means connecting the annulus between said labyrinth seals and a stage of said turbine for supplying steam leaked past an axially innermost one of said pair of labyrinth seals to a stage of said turbine;
segmented circumferential seal about said shaft adjacent the outlet end of said turbine for sealing between ambient and turbine exhaust flow; and
said outer steam seal and an outermost of said pair of labyrinth seals defining an annulus therebetween and means connecting the latter annulus with another stage of said turbine downstream of the first-mentioned turbine stage.

### Claim 2

In a multi-stage steam turbine having a first rotating member including a shaft, a second stationary member surrounding said first member and defining a steam flow path having a high-pressure inlet at one end of the turbine and a low-pressure outlet at its opposite end, a shaft system adjacent the inlet and outlet ends of said turbine, comprising:
a pair of axially spaced labyrinth seals about said shaft adjacent said high-pressure inlet end and defining an annulus therebetween;
a pair of axially spaced segmented circumferential seals about and contacting said shaft defining an annulus therebetween and spaced axially outwardly of said labyrinth seals;
an axially outermost segmented circumferential seal of said pair of segmented circumferential seals constituting an air seal sealing between ambient and the annulus between said segmented circumferential seals;
another of said pair of segmented circumferential seals constituting an outer steam seal sealing between said labyrinth seals and the annulus between said segmented circumferential seals;
means connecting the annulus between said labyrinth seals and a stage turbine for supplying steam leaked past an axially innermost one of said pair of labyrinth seals to a stage of said turbine;
segmented circumferential seal about said shaft adjacent the outlet end of said turbine for sealing between ambient and turbine exhaust flow; and
said outer steam seal and an outermost one of said pair of labyrinth seals defining an annulus therebetween and means connecting the latter annulus with another stage of said turbine downstream of the first-mentioned turbine stage; and including a main condenser for recovering the turbine exhaust flow and means connecting the annulus between said segmented circumferential seals and the main condenser for flowing combined leakage air and steam leaking past the air seal and the outer steam seal, respectively.

### Claim 3 (depends on 2)

A sealing system according to claim 2, wherein said outer steam seal and an outermost one of said pair of labyrinth seals define an annulus therebetween and means connecting the latter annulus with another stage of said turbine downstream of the first-mentioned turbine stage; and including a main condenser for recovering the turbine exhaust flow and means connecting the annulus between said segmented circumferential seals and the main condenser for flowing combined leakage air and steam leaking past the air seal and the outer steam seal, respectively.