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US4265594A Expired / Lapsed US ⏱️ 0.0 years remaining

Turbine blade having heat localization segments

Assignee: BBC BROWN BOVERI and Co Ltd
•
Filing: 1979-02-28
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Granted: 1981-05-05
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Expires: 1999-02-28
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Abstract

Abstract Turbine blades having heat localization segments, especially for use in gas turbines, are disclosed. The segments are provided with covering elements in the form of thin cover plates that are supported against the blade root. The segments are formed as one piece together with both the actual blade and with reinforcing elements. The segments are used to impede access of a hot working medium to the turbine rotor.

Inventors

  • 👤 Jean Eggmann

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-06 16:26
CPC Classifications
F; F01; F01D; F01D5/00; F01D5/12; F01D5/14; F01D5/141; F01D11/00; F01D11/001; F01D5/02; F01D5/08

Claims Analysis

Total Claims: 7
Claim 1
Independent Claim 120 words
A blade for a turbine section, of a gas turbine, comprising: a blade root; a blade member extending directly from the blade root; first and second heat localization segments including first and second covering elements respectively, the first and second covering elements being formed as one piece with the blade member and the blade root, said covering elements impeding access of a working medium to a rotor of the turbine; each covering element including a cover plate and supporting means for stiffening the cover plate, a portion of the cover plate adjacent the blade member and blade root being angled toward the blade member, said supporting means connecting the cover plate to an axial end face of the blade root.
Claim 2
Dependent Claim 120 words
A blade for a turbine section, of a gas turbine, comprising: a blade root; a blade member extending directly from the blade root; first and second heat localization segments including first and second covering elements respectively, the first and second covering elements being formed as one piece with the blade member and the blade root, said covering elements impeding access of a working medium to a rotor of the turbine; each covering element including a cover plate and supporting means for stiffening the cover plate, a portion of the cover plate adjacent the blade member and blade root being angled toward the blade member, said supporting means connecting the cover plate to an axial end face of the blade root.
Claim 3
Dependent Claim 14 words
The blade of claim 1 wherein the supporting means includes first and second braces.
Claim 4
Dependent Claim 16 words
The blade of claim 1 wherein the supporting means includes first and second triangular shaped ribs.
Claim 5
Dependent Claim 27 words
The blade of claim 1 wherein the supporting means includes a bracket plate and an intermediate brace connecting the bracket plate with one of the cover plates.
Claim 6
Dependent Claim 29 words
The blade of claim 1 wherein the first and second covering elements each include slot means for receiving a sealing strip to seal an expansion joint between adjacent blades.
Claim 7
Dependent Claim 21 words
The blade of claim 1 wherein the first and second covering elements are each provided with at least one sealing ridge.

References Cited (Backward Citations)

GB809268A Cited
US2858103A Cited
US3066910A Cited
GB1236920A Cited
US3597109A Cited
US3719431A Cited
US3761200A Cited
US3801220A Cited
US3905722A Cited
US4022544A Cited
DE2816791A1 Cited
DE2813834A1 Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1984-05-04 1984-11-03 1985-05-05 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1988-05-04 1988-11-03 1989-05-05 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1992-05-04 1992-11-03 1993-05-05 $7700.00 Window Closed / Lapsed

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