GB855040A - Sealing arrangement - Google Patents
Sealing arrangementInfo
- 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
Links
Classifications
-
- 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
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.
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)
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 |
-
1957
- 1957-11-15 GB GB3563557A patent/GB855040A/en not_active Expired
Cited By (16)
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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