GB834923A - Improvements in or relating to sealing means - Google Patents

Improvements in or relating to sealing means

Info

Publication number
GB834923A
GB834923A GB287657A GB287657A GB834923A GB 834923 A GB834923 A GB 834923A GB 287657 A GB287657 A GB 287657A GB 287657 A GB287657 A GB 287657A GB 834923 A GB834923 A GB 834923A
Authority
GB
United Kingdom
Prior art keywords
chamber
gas
sleeve
pressure
oil
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
GB287657A
Inventor
Raymond Ernest Wigg
Norman Battle
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB287657A priority Critical patent/GB834923A/en
Priority to US710041A priority patent/US3051497A/en
Priority to CH5509458A priority patent/CH363533A/en
Publication of GB834923A publication Critical patent/GB834923A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • 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
    • F16J15/002Sealings comprising at least two sealings in succession
    • 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
    • F16J15/34Sealings between relatively-moving surfaces with slip-ring pressed against a more or less radial face on one member
    • F16J15/36Sealings between relatively-moving surfaces with slip-ring pressed against a more or less radial face on one member connected by a diaphragm or bellow to the other member
    • 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
    • F16J15/406Sealings between relatively-moving surfaces by means of fluid by at least one pump

Abstract

834,923. stuffing-box substitutes. ROLLSROYCE Ltd. Jan. 21, 1958 [Jan. 25, 1957], No. 2876/57. Class 122 (5). Sealing means between the shaft 12, Fig. 1, of a gas-turbine and its housing 10 comprises a sealed sleeve 28 mounted on the housing and encircling the shaft with a small clearance space which at one end communicates with the turbine chamber 18 and at the other with a liquid delivered at a higher pressure than that of the gas in the chamber 18, and helical grooving 26 formed in one of the surfaces bounding the clearance space. As shown in Fig. 1, the sleeve 28 surrounds a second sleeve 19 fixed to the shaft 12 and is connected to one end of a bellows 29, which, at its other end, is attached to a member 30 mounted in the housing 10, the surface of the sleeve 19 being formed with the grooves 26. The sleeve 28 is formed with a radial surface 32 which, when the shaft is stationary or running at slow speed, is urged into contact with a ring 20 mounted on the shaft 12 by the pressure of the gas, such as helium, contained within the chamber 18. In operation under normal running conditions, liquid, such as oil, is fed by a pump 35 through a pipe 36 into a chamber 34 at a higher pressure than that of the gas and thereby moves the surface 32 away from the ring 20 until a flange 33 abuts the member 30 so that liquid then tends to flow into the clearance space between the two sleeves 19, 28. The dimensions of the clearance space and the dimensions and handing of the grooves 26 are so selected that the oil drops in pressure as it moves towards the chamber 18 and the gas, which tends to leak from the chamber, rises in pressure until at a certain point between the ends of the sleeve 28 an oil/gas interface is formed. In order that the seal may be independent of variations in gas pressure in the chamber 18, a constant high-pressure gas supply may be admitted through a duct 24. The sleeve 19 is provided with a finger 21 which rotates in a groove 22 formed in the housing 10 so that any gas contaminated with oil vapour is discharged through an outlet 23. In the modification shown in Fig. 3, the oil-pump 35 is dispensed with and oil supplied to a bearing 16 is pressurized by means of helical grooves 41 formed in the surface of the main shaft 14, of opposite hand to the grooves 26. The grooves, in co-operation with a sleeve 40 surrounding the grooved surface, pump the oil into the chamber 34a to act upon the flange 33 in the manner previously described. To prevent any build-up of excessive pressure in the latter chamber, a relief valve 58 is located in a duct 57 leading to an oil drain and is urged into the closed position by a spring 59 and the pressure of the gas in the chamber 18 acting upon a diaphragm 62. A spring-urged rubbing-collar type seal 51a is mounted on a spherical seating 50 formed on the sleeve 40, although, in a further modification, this seal may be replaced by a bellows.
GB287657A 1957-01-25 1957-01-25 Improvements in or relating to sealing means Expired GB834923A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB287657A GB834923A (en) 1957-01-25 1957-01-25 Improvements in or relating to sealing means
US710041A US3051497A (en) 1957-01-25 1958-01-20 Sealing means between relatively rotating parts
CH5509458A CH363533A (en) 1957-01-25 1958-01-25 Combined shaft seal that works above a certain speed with barrier fluid and below this speed and when it is at a standstill with sliding surfaces

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB287657A GB834923A (en) 1957-01-25 1957-01-25 Improvements in or relating to sealing means

Publications (1)

Publication Number Publication Date
GB834923A true GB834923A (en) 1960-05-11

Family

ID=9747665

Family Applications (1)

Application Number Title Priority Date Filing Date
GB287657A Expired GB834923A (en) 1957-01-25 1957-01-25 Improvements in or relating to sealing means

Country Status (1)

Country Link
GB (1) GB834923A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0501122A1 (en) * 1991-02-28 1992-09-02 Gebr. Lödige Maschinenbau Gesellschaft mbH Bearing for stirrershaft or similar
DE29602685U1 (en) * 1996-02-15 1996-04-11 Burgmann Dichtungswerk Feodor Mechanical seal arrangement
EP2567754A1 (en) * 2011-09-08 2013-03-13 Alfa Laval Corporate AB A centrifugal separator
WO2014131413A1 (en) * 2013-03-01 2014-09-04 Schaeffler Technologies Gmbh & Co. Kg Sealing arrangement for a turbocharger shaft of an exhaust gas turbocharger

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0501122A1 (en) * 1991-02-28 1992-09-02 Gebr. Lödige Maschinenbau Gesellschaft mbH Bearing for stirrershaft or similar
DE29602685U1 (en) * 1996-02-15 1996-04-11 Burgmann Dichtungswerk Feodor Mechanical seal arrangement
US5909878A (en) * 1996-02-15 1999-06-08 Feodor Burgmann Dichtungswerke Gmbh & Co. Mechanical face seal assembly
EP2567754A1 (en) * 2011-09-08 2013-03-13 Alfa Laval Corporate AB A centrifugal separator
WO2013034495A3 (en) * 2011-09-08 2013-08-01 Alfa Laval Corporate Ab A centrifugal separator
CN103917299A (en) * 2011-09-08 2014-07-09 阿尔法拉瓦尔股份有限公司 A centrifugal separator
AU2012306540B2 (en) * 2011-09-08 2015-07-16 Alfa Laval Corporate Ab A centrifugal separator
CN103917299B (en) * 2011-09-08 2016-01-20 阿尔法拉瓦尔股份有限公司 Whizzer
US9931646B2 (en) 2011-09-08 2018-04-03 Alfa Laval Corporate Ab Centrifugal separator having a forcing device to create a radial leak flow
WO2014131413A1 (en) * 2013-03-01 2014-09-04 Schaeffler Technologies Gmbh & Co. Kg Sealing arrangement for a turbocharger shaft of an exhaust gas turbocharger

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