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US3597102A Expired / Lapsed US ⏱️ 0.0 years remaining

Turbines

Assignee: English Electric Co Ltd
•
Filing: 1969-06-10
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Granted: 1971-08-03
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Expires: 1989-06-10
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Abstract

Abstract To prevent leakage of fluid through a clearance passage defined between a turbine rotor and stator, a duct is formed in the stator from which an annular jet of fluid can be directed into the passage. The jet forms a moving curtain of fluid between rotor and stator. Axially adjacent the duct, a chamber may be formed in the stator, fluid from the curtain being deflected into the chamber and conveyed therefrom to a further duct in order to provide a further moving curtain between rotor and stator. The further moving curtain may be provided in the same clearance passage or in another located downstream therefrom.

Inventors

  • 👤 Robert George Unsworth
  • 👤 Robert Keith Burton

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-30 11:59
CPC Classifications
F; F01; F01D; F01D11/00; F01D11/08; F01D11/10

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 240 words
A turbine including a rotor having at least one rotor stage, and a stator having at least one stator stage, the rotor and the stator defining between them an annular clearance passage at each stage, there being provided a seal for at least one passage for maintaining a pressure difference between the upstream and downstream sides thereof, the seal including: means within the stator which define a first circumferentially extending duct which communicates with the passage; fluid-feeding means connected to the first duct for feeding a fluid thereto at a pressure greater than the pressure obtaining on either side of the passage, the first duct being arranged to direct an annular jet of fluid into the passage to provide therein a moving curtain of fluid which can be deflected owing to the said pressure difference, the said jet having sufficient initial velocity that changes of fluid momentum during deflection of the jet are sufficient to maintain the said pressure difference; further means within the stator which define a circumferentially extending chamber communicating with the passage at a point axially adjacent to the first duct; and fluid release means comprising a conduit connected to the chamber, such that at least part of the fluid in the said jet can be deflected into the chamber and released therefrom via the said conduit to a second duct for use in a further annular jet, whereby to form a further moving curtain of fluid.
Claim 2
Dependent Claim 240 words
A turbine including a rotor having at least one rotor stage, and a stator having at least one stator stage, the rotor and the stator defining between them an annular clearance passage at each stage, there being provided a seal for at least one passage for maintaining a pressure difference between the upstream and downstream sides thereof, the seal including: means within the stator which define a first circumferentially extending duct which communicates with the passage; fluid-feeding means connected to the first duct for feeding a fluid thereto at a pressure greater than the pressure obtaining on either side of the passage, the first duct being arranged to direct an annular jet of fluid into the passage to provide therein a moving curtain of fluid which can be deflected owing to the said pressure difference, the said jet having sufficient initial velocity that changes of fluid momentum during deflection of the jet are sufficient to maintain the said pressure difference; further means within the stator which define a circumferentially extending chamber communicating with the passage at a point axially adjacent to the first duct; and fluid release means comprising a conduit connected to the chamber, such that at least part of the fluid in the said jet can be deflected into the chamber and released therefrom via the said conduit to a second duct for use in a further annular jet, whereby to form a further moving curtain of fluid.
Claim 3
Dependent Claim 44 words
A turbine according to claim 1, wherein the first duct is arranged to impart to the said annular jet of fluid an axial component of velocity towards the upstream side of the passage, and the said chamber is disposed upstream of the first duct.
Claim 4
Dependent Claim 21 words
A turbine according to claim 1, wherein the said second duct is disposed in the same stage as the first duct.
Claim 5
Dependent Claim 28 words
A turbine according to claim 1, having a plurality of stages, whereIn the said second duct is disposed in a stage downstream from that containing the first duct.

References Cited (Backward Citations)

US2685429A Cited
US3011762A Cited
FR1163559A Cited
US2963268A Cited
GB867600A Cited
US3044744A Cited
US3239193A Cited
US3365172A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1974-08-02 1975-02-01 1975-08-03 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1978-08-02 1979-02-01 1979-08-03 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1982-08-02 1983-02-01 1983-08-03 $7700.00 Window Closed / Lapsed

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