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GB1193800A - High Pressure Fluid Gland System for Rotary Shafts - Google Patents

High Pressure Fluid Gland System for Rotary Shafts

Info

Publication number
GB1193800A
GB1193800A GB5915068A GB5915068A GB1193800A GB 1193800 A GB1193800 A GB 1193800A GB 5915068 A GB5915068 A GB 5915068A GB 5915068 A GB5915068 A GB 5915068A GB 1193800 A GB1193800 A GB 1193800A
Authority
GB
United Kingdom
Prior art keywords
glands
pressure
conduit
branch
valve
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB5915068A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Westinghouse Electric Corp
Original Assignee
Westinghouse Electric Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Publication of GB1193800A publication Critical patent/GB1193800A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J15/00Sealings
    • F16J15/16Sealings between relatively-moving surfaces
    • F16J15/40Sealings between relatively-moving surfaces by means of fluid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/02Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
    • F01D11/04Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type using sealing fluid, e.g. steam
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/60Shafts
    • F05D2240/63Glands for admission or removal of fluids from shafts

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

1,193,800. Rotary shaft seals. WESTING- HOUSE ELECTRIC CORP. 12 Dec., 1968 [4 Jan., 1968], No. 59150/68. Heading F2B. [Also in Division F1] In a steam turbine shaft sealing arrangement comprising glands 11-16 packed with steam supplied from a high-pressure steam source via a common main conduit 18 and branch conduits 21-25 between the main conduit and the glands, a pressure reducing valve 31-35 is disposed in each of the branch conduits adjacent the glands. In the embodiment shown in which three turbines 1, 2 and 3 are mechanically connected in series, the glands 15 and 16 of turbine 3 are connected to a common branch conduit 25, the other glands being each directly connected to a branch conduit. The pressure reducing valves 31-35 are automatically controlled by gland pressure sensing lines 51-55 and a normally open manually operable valve 41-45 is connected in each branch conduit. The main conduit 18 includes a pressure relief valve 60 and is connected to the high-pressure steam source through an automatically controlled regulating valve 57 by a pressure sensing line 59. Outlet conduits 61-66 from the glands are connected either separately or collectively through a conduit 67 to a region of low pressure e.g. a condenser.
GB5915068A 1968-01-04 1968-12-12 High Pressure Fluid Gland System for Rotary Shafts Expired GB1193800A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US69579368A 1968-01-04 1968-01-04

Publications (1)

Publication Number Publication Date
GB1193800A true GB1193800A (en) 1970-06-03

Family

ID=24794485

Family Applications (1)

Application Number Title Priority Date Filing Date
GB5915068A Expired GB1193800A (en) 1968-01-04 1968-12-12 High Pressure Fluid Gland System for Rotary Shafts

Country Status (8)

Country Link
BE (1) BE726491A (en)
CH (1) CH501170A (en)
DE (1) DE1817012B2 (en)
ES (1) ES362089A1 (en)
FR (1) FR1600157A (en)
GB (1) GB1193800A (en)
NL (1) NL6818158A (en)
SE (1) SE345496B (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2253442A (en) * 1991-03-02 1992-09-09 Rolls Royce Plc Multi-stage seal for an axial flow turbine
GB2393766A (en) * 2002-10-03 2004-04-07 Alstom A sealing arrangement for a turbine
US10392956B2 (en) 2013-12-30 2019-08-27 Siemens Aktiengesellschaft Sealing system for a steam turbine, and steam turbine

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2158720C2 (en) * 1971-11-26 1982-12-16 Indramat Gesellschaft für Industrie-Rationalisierung und Automatisierung mbH, 8770 Lohr Servo controlled piston and cylinder - has labyrinth seal each end with multiple grooved section of leakage oil return chamber
CH550348A (en) * 1972-10-11 1974-06-14 Bbc Brown Boveri & Cie BARRIER MEDIUM LABYRINTH SEAL.
FR2569780B1 (en) * 1984-08-30 1989-03-31 Worthington Turbodyne SEALING AND PRESSURIZATION METHOD AND DEVICE FOR OIL-FREE AIR COMPRESSOR SHAFT OUTLETS
EP0268423B1 (en) * 1986-11-14 1992-10-21 Hitachi, Ltd. Gland sealing steam supply system for steam turbines
DE3709397C2 (en) * 1987-03-21 1997-10-09 Head Acoustics Gmbh Process for filtering sound signals
DE4041965A1 (en) * 1990-12-24 1992-07-02 Siegfried Stargard Packing fluid seal between high and low pressure zone in relatively moving components - has annular grooves and pressure reducing pipes
DE19742621A1 (en) * 1997-09-26 1999-04-08 Siemens Ag Shaft seal component for steam turbine machine
ATE228203T1 (en) 1997-09-26 2002-12-15 Siemens Ag HOUSING FOR A FLOW MACHINE

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2253442A (en) * 1991-03-02 1992-09-09 Rolls Royce Plc Multi-stage seal for an axial flow turbine
US5205706A (en) * 1991-03-02 1993-04-27 Rolls-Royce Plc Axial flow turbine assembly and a multi-stage seal
GB2253442B (en) * 1991-03-02 1994-08-24 Rolls Royce Plc An axial flow turbine assembly
GB2393766A (en) * 2002-10-03 2004-04-07 Alstom A sealing arrangement for a turbine
US7559554B2 (en) 2002-10-03 2009-07-14 Alstom Technology Ltd Sealing arrangement using brush seals
US10392956B2 (en) 2013-12-30 2019-08-27 Siemens Aktiengesellschaft Sealing system for a steam turbine, and steam turbine

Also Published As

Publication number Publication date
DE1817012B2 (en) 1971-06-24
FR1600157A (en) 1970-07-20
SE345496B (en) 1972-05-29
NL6818158A (en) 1969-07-08
CH501170A (en) 1970-12-31
DE1817012A1 (en) 1969-08-07
ES362089A1 (en) 1970-11-01
BE726491A (en) 1969-06-16

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee