US1757212A - Shaft packing suitable for steam turbines - Google Patents

Shaft packing suitable for steam turbines Download PDF

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Publication number
US1757212A
US1757212A US185629A US18562927A US1757212A US 1757212 A US1757212 A US 1757212A US 185629 A US185629 A US 185629A US 18562927 A US18562927 A US 18562927A US 1757212 A US1757212 A US 1757212A
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Prior art keywords
gland
pressure
steam
pockets
steam turbines
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Expired - Lifetime
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US185629A
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Parsons Charles Algernon
Cook Stanley Smith
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
    • F01D11/04—Preventing 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16J—PISTONS; CYLINDERS; SEALINGS
    • F16J15/00—Sealings
    • F16J15/16—Sealings between relatively-moving surfaces
    • F16J15/40—Sealings between relatively-moving surfaces by means of fluid

Definitions

  • the invention relates to shaft packings are also connected together and toa'point'of suitable for steam turbines and particularly the low-pressure turbine, G, ata pressure to those of the kind in which a so-called slightly below atmosphere by means ofthe reservoir is connected to pockets provided piping, e. i v f v in theglands of stufiing boxes.
  • a rotary engine comprising i'ncom b-ination a plurality of pressure stages; engine shafting; glands for said shafting in connection with each of said plurality of stages,
  • a rotary engine comprising incombination a plurality of pressure stages including a sub-atmospheric stage; engine shafting; 'glandsfor said shafting in; connection with "each of said plurality of stages, each gland having at least two axially-disposed gland pockets, an outer pocket and an inner pocket a reservoir system at a pressure slightly above atmosphere to which all said outer gland pockets are connected; and a second reservoir system to which all said inner gland pockets are connected, said second reservoir system being connected to a point of said sub-atmospheric stage.

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

Description

May 6, 1930. i c. A..PARSONS-EI' AL a 1,757,212
SHAFT PACKING SUITABLE FOR STEAM TURBINES Filed April 21, 1927 Patented May. 6, 1930 l r p r ITED STATES PAT NT-foamy CHARLES ALGEBNON PARSONS Nns'rANLEY-SMITH oooK, or' 'NEWoAsTLE-oN-TYNE,
ENGLAND; sAInoooK ASSIGNOR To sAInPARsoivs SHAFT PACKING SUITABLE FOR STEAM TUBBINES Application filed April 21, 192?, Serial No. 185,629, and in GreatBritain May 12, 1926.
The invention relates to shaft packings are also connected together and toa'point'of suitable for steam turbines and particularly the low-pressure turbine, G, ata pressure to those of the kind in which a so-called slightly below atmosphere by means ofthe reservoir is connected to pockets provided piping, e. i v f v in theglands of stufiing boxes. Y The arrangement as above described is 5 In a certain constructional form of such preferred in orderto stage the pressure drop packings proposed for steam turbines, the across each gland but as'the flow in the lOW- reservoir constitutes a pipe connection bepressureturbine is necessarilyinwards from tween the gland pockets respectively of the the outer lg d iti ngtlnecessary th t it high-pressure and low-pressure turbine inner gland pockets, 0 should inall-cases c0 stages, so that leakage steam from the highbe connected to the sub-"atmospheric point. pressure turbine into the high-pressure gland Vfith like glands a hown, it will b e 7 pocket passes by Way of the reservoir to the that the resistance to fiovv in the glands of the low-pressure gland pocket. If the pressure different stages can be made identical, the
in the reservoir in such a case is adjusted corpressure in the reservoir being maintained at 65 rectly for the low-pressure gland pocket, the a i t. o ly very slightly above the atmosresulting pressure in the high-pressure gland vpflnereso th t, l ka f th te .l la d pocket, owing to the resistance of pipes of toth engine r i du d t a ligibl practicable dimensions, may be so hlgh as to ntityforeach stage andthe iloiv is incause considerable leakage Of steam lIltO the Wards for the uterglayul poeket each. unit. 70 engine room. As a oonsequenceyin addition to adding to The main object of the present invention 1S the comfort engin e eom taff, the heat to Provide improvements designed to Over in the steam is saved and also the heat necescome such difliculties. sarily expended in the-evaporator to replace With such an object the invention consists 1 t f d Waten 75 in the combination Of parts hereinafter de- The upply of steam to the reservoir 111337 scribed and particularly pointed out in the be drawn from the loyv-p essure team for the 7 claims. auxiliaries, auxiliary exhaust steam, steam The accompanying dra l g Shows (llatapped from the main turbines, or other congrammatically one form of the invention. i t Source, I so In carrying the invention into effect "The use of Wet steam for the glands is cording to this fornl ppl l a m preferred inasmuch as if the turbines are unit steam turbine havmg high-pressure, nki with superheated Steam, any 1 k termediate-pressure and low pressure unlts, a becomes veryhighly superheated by l'espectlvely Separate sage throughthe glands and is practically t gland. of labyrmth or Othel: V invisible so that it cannot be seen Whether i f the Shafts of the three; unzlts 1S the gland is Working correctly; the present Vlded Wlth gland Pockets a q foruint invention enablesall the outer pockets to be A, 52 for mm B and 011 a? for t Whlch supplied With saturated steam.
a0 ma 1 0 annu1ar for.m an i fi i If desired, the usual connections, 7, f, may
g? i at a f fijg i gf gi g; be provided fromother gland pockets, a 6
me anfou g k bino ML at pressures above atmosphere to lower presremote t er? p00 e S b i sure sta es for the purpose of sta in' the ly spaced with packlng on both sldes thereof b e c 4.3 as shown. All the outer pockets, gland toreduce leakage' are Connected by Suitable Piping; (Z150 a resale We Wish it to beunderstood that the terms i R the i i may it lf f th super-atmospherlo glands and sub-atmosreseivoir) Supplied *f Steam f any pheric glands as used in the above specifica- Suitable Source by way f th 1 t 11 d tlon and 1n the claims appendant thereto g pipe While n the inner k t Z mean that the relative glands pack against internal pressures which are respectively above and below atmospheric pressure.
The details of the invention may take other forms than those specifically described above. Having now described our invention, what we claim as new and desir'e'to secure byiLetters Patent is 1. A rotary engine comprising i'ncom b-ination a plurality of pressure stages; engine shafting; glands for said shafting in connection with each of said plurality of stages,
each gland having atyleast two axially=disposed gland pockets, an outer pocket and an inner pocket; a reservoir system at a pressure slightly above atmosphere to which all said outer gland pockets 'are connected; and a second reservoir system at a pressure below atmosphere to which all 'said inner gland pockets are connected. V 1
2. A rotary engine comprising incombination a plurality of pressure stages including a sub-atmospheric stage; engine shafting; 'glandsfor said shafting in; connection with "each of said plurality of stages, each gland having at least two axially-disposed gland pockets, an outer pocket and an inner pocket a reservoir system at a pressure slightly above atmosphere to which all said outer gland pockets are connected; and a second reservoir system to which all said inner gland pockets are connected, said second reservoir system being connected to a point of said sub-atmospheric stage. a e V In testimony whereof we have'fsigned our names to this specification.
CHARLES ALGERNON PARSONS. STANLEY SMITH 3 COOK.
US185629A 1926-05-12 1927-04-21 Shaft packing suitable for steam turbines Expired - Lifetime US1757212A (en)

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GB1757212X 1926-05-12

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1041059B (en) * 1957-08-05 1958-10-16 Licentia Gmbh Circuit of the stuffing box steam collecting line of a multi-housing steam turbine
DE1105431B (en) * 1959-04-22 1961-04-27 Sulzer Ag Device for the delivery of sealing steam for sealing points in steam power plants, especially steam turbine plants
US3003321A (en) * 1955-01-31 1961-10-10 English Electric Co Ltd Steam turbines
FR2628815A1 (en) * 1988-03-21 1989-09-22 Sunds Defibrator Jylha Oy SEAL FOR PASSING A ROTATING SHAFT
US6053699A (en) * 1998-07-27 2000-04-25 General Electric Company Steam turbine having a brush seal assembly
US20120294707A1 (en) * 2011-05-16 2012-11-22 General Electric Company Steam seal system
EP2650485A3 (en) * 2012-04-13 2018-02-28 General Electric Company Shaft sealing system for steam turbines

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3003321A (en) * 1955-01-31 1961-10-10 English Electric Co Ltd Steam turbines
DE1041059B (en) * 1957-08-05 1958-10-16 Licentia Gmbh Circuit of the stuffing box steam collecting line of a multi-housing steam turbine
DE1105431B (en) * 1959-04-22 1961-04-27 Sulzer Ag Device for the delivery of sealing steam for sealing points in steam power plants, especially steam turbine plants
FR2628815A1 (en) * 1988-03-21 1989-09-22 Sunds Defibrator Jylha Oy SEAL FOR PASSING A ROTATING SHAFT
US6053699A (en) * 1998-07-27 2000-04-25 General Electric Company Steam turbine having a brush seal assembly
US6260269B1 (en) * 1998-07-27 2001-07-17 General Electric Company Method for overhauling a steam turbine to increase its power
US20120294707A1 (en) * 2011-05-16 2012-11-22 General Electric Company Steam seal system
US8888444B2 (en) * 2011-05-16 2014-11-18 General Electric Company Steam seal system
EP2650485A3 (en) * 2012-04-13 2018-02-28 General Electric Company Shaft sealing system for steam turbines

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