GB855040A - Sealing arrangement - Google Patents

Sealing arrangement

Info

Publication number
GB855040A
GB855040A GB3563557A GB3563557A GB855040A GB 855040 A GB855040 A GB 855040A GB 3563557 A GB3563557 A GB 3563557A GB 3563557 A GB3563557 A GB 3563557A GB 855040 A GB855040 A GB 855040A
Authority
GB
United Kingdom
Prior art keywords
rotor
nozzle
sealing fluid
stator
sealing
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
GB3563557A
Inventor
Alun Raymond Howell
Derek Guy Harcourt Higgins
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development Ltd
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 Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Priority to GB3563557A priority Critical patent/GB855040A/en
Publication of GB855040A publication Critical patent/GB855040A/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
    • F16J15/16Sealings between relatively-moving surfaces
    • F16J15/40Sealings between relatively-moving surfaces by means of fluid

Landscapes

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

Abstract

855,040. Stuffing-box substitutes. POWER JETS (RESEARCH & DEVELOPMENT) Ltd. Nov. 11, 1958 [Nov. 15, 1957], No. 35635/57. Class 122 (5). A sealing arrangement comprises a rotor 1 and stator 2 separated by a clearance gap 3 and an annular nozzle 9 for discharging a circumferentially-continuous sheet of sealing fluid across the gap so as to prevent the escape therealong of the fluid being sealed. The stator 2 is in the form of a casing 4 having inserts 5, 6 which together define a sealing fluid chamber 7 and the annular nozzle 9. In operation, pressurized sealing fluid, such as air, is fed into the chamber through a passage 8 and is discharged through the nozzle such that it impinges on the surface of the rotor; a gauze 10 is provided in the chamber to improve the fluid distribution before entering the nozzle. The nozzle may be arranged to direct the sealing fluid towards the direction of leakage flow as shown, or perpendicularly thereto. In a modification, an arcuate groove may be formed in the surface of the rotor opposite the nozzle so that the sealing fluid impinging on the rotor follows a scroll-shaped path, thereby increasing the sealing effect. In the modification shown in Fig. 2, the clearance gap between the rotor 1 and the insert 6 is greater than that between the insert 5 and an arcuate shoulder 11 is formed on the rotor so as to prevent turbulance of the sealing fluid impinging thereon. The arrangement may also., be applied to the case wherein the outer member 4 is the rotor and the inner member 1 the stator, and wherein the surfaces to be sealed lie normal or at an angle to the axis of rotation. The nozzle may be provided on the rotor instead of, or in addition to, the one on the stator and more than one nozzle on either member may be provided. Specification 774,503 is referred to.
GB3563557A 1957-11-15 1957-11-15 Sealing arrangement Expired GB855040A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3563557A GB855040A (en) 1957-11-15 1957-11-15 Sealing arrangement

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3563557A GB855040A (en) 1957-11-15 1957-11-15 Sealing arrangement

Publications (1)

Publication Number Publication Date
GB855040A true GB855040A (en) 1960-11-30

Family

ID=10379905

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3563557A Expired GB855040A (en) 1957-11-15 1957-11-15 Sealing arrangement

Country Status (1)

Country Link
GB (1) GB855040A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3685837A (en) * 1969-05-06 1972-08-22 William George Newell Sealing means
US4218066A (en) * 1976-03-23 1980-08-19 United Technologies Corporation Rotary seal
US4253684A (en) * 1979-05-14 1981-03-03 Monsanto Company Quick connect coupler with air shield
EP0972910A1 (en) * 1998-07-14 2000-01-19 Asea Brown Boveri AG Non-contact sealing of gaps in gas turbines
US6418637B1 (en) 1997-01-07 2002-07-16 Andritz-Ahlstrom Oy Method of sealing a rotary drum connection
GB2409247A (en) * 2003-12-20 2005-06-22 Rolls Royce Plc A seal arrangement
GB2443117A (en) * 2003-12-20 2008-04-23 Rolls Royce Plc A seal arrangement
EP2522812A1 (en) * 2006-06-30 2012-11-14 United Technologies Corporation Method of delivering fluid to a seal in a turbomachine
EP2754858A1 (en) 2013-01-14 2014-07-16 Alstom Technology Ltd Arrangement for sealing an open cavity against hot gas entrainment
US10301959B2 (en) 2013-05-31 2019-05-28 Cummins Ltd. Seal assembly

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3685837A (en) * 1969-05-06 1972-08-22 William George Newell Sealing means
US4218066A (en) * 1976-03-23 1980-08-19 United Technologies Corporation Rotary seal
US4253684A (en) * 1979-05-14 1981-03-03 Monsanto Company Quick connect coupler with air shield
US6418637B1 (en) 1997-01-07 2002-07-16 Andritz-Ahlstrom Oy Method of sealing a rotary drum connection
EP0972910A1 (en) * 1998-07-14 2000-01-19 Asea Brown Boveri AG Non-contact sealing of gaps in gas turbines
JP2000055210A (en) * 1998-07-14 2000-02-22 Asea Brown Boveri Ag Device for uncontactedly sealing gap between parts
US6276692B1 (en) 1998-07-14 2001-08-21 Asea Brown Boveri Ag Non-contact sealing of gaps in gas turbines
EP1347153A1 (en) * 1998-07-14 2003-09-24 ALSTOM (Switzerland) Ltd Non- contact sealing of gaps in gas turbines
GB2409247A (en) * 2003-12-20 2005-06-22 Rolls Royce Plc A seal arrangement
US7238001B2 (en) 2003-12-20 2007-07-03 Rolls-Royce Plc Seal arrangement
GB2443117A (en) * 2003-12-20 2008-04-23 Rolls Royce Plc A seal arrangement
GB2443117B (en) * 2003-12-20 2008-08-13 Rolls Royce Plc A seal arrangement
EP2522812A1 (en) * 2006-06-30 2012-11-14 United Technologies Corporation Method of delivering fluid to a seal in a turbomachine
EP2754858A1 (en) 2013-01-14 2014-07-16 Alstom Technology Ltd Arrangement for sealing an open cavity against hot gas entrainment
US9074488B2 (en) 2013-01-14 2015-07-07 Alstom Technology Ltd Arrangement for sealing an open cavity against hot gas entrainment
US10301959B2 (en) 2013-05-31 2019-05-28 Cummins Ltd. Seal assembly

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