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US4893388A Expired / Lapsed US ⏱️ 0.0 years remaining

Method of modifying turbine rotor discs

Assignee: Siemens Energy Inc
•
Filing: 1988-12-08
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Granted: 1990-01-16
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Expires: 2008-12-08
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Abstract

Abstract A method for modifying an original blade supporting disc (8) which is integral with a turbine rotor (2), and which has an original outline, in order to create a modified disc (8) which has an outline different from the original outline and which provides a blade-supporting region (10) of increased size, including the steps of: machining away portions (14,16) of the original disc (8) which protrude beyond the outline of the modified disc (8); building up the original disc (8) with weld metal past the outline of the modified disc (8) at all locations (14,20) where the outline of the original disc (8), after the machining step, is enclosed by the outline of the modified disc (8); and machining away parts of the weld metal to the outline of the modified disc (8).

Inventors

  • 👤 Dennis R. Amos
  • 👤 Robert E. Clark
  • 👤 Roger W. Heinig
  • 👤 Stephen R. Reid

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-31 06:02
CPC Classifications
F; F01; F01D; F01D5/00; B; B23; B23P; B23P6/00; B23P6/002; B23P6/007; B23K; B23K9/00; B23K9/04; B23K9/044; B23K9/046; B23P15/00; B23P15/006; F01D5/005; Y; Y10; Y10T; Y10T29/00; Y10T29/49; Y10T29/49316; Y10T29/49318; Y10T29/4932; Y10T29/49718; Y10T29/49732; Y10T29/49734; Y10T29/49737; Y10T29/4998; Y10T29/49982; Y10T29/49986

Claims Analysis

Total Claims: 11
Claim 1
Independent Claim 132 words
A method for modifying an original blade supporting disc which is integral with a turbine rotor, and which has an original outline, in order to create a modified disc which has an outline different from the original outline and which provides a blade-supporting region of increased size, the original disk having at least one portion which must be removed in order to create the modified disc, comprising: machining away each said portion of the original disc; building up the original disc with weld metal past the eventual outline of the modified disc at all locations where the outline of the original disc, after said machining step, is to be enclosed by the outline of said modified disc; and machining away parts of the weld metal to the outline of the modified disc.
Claim 2
Independent Claim 132 words
A method for modifying an original blade supporting disc which is integral with a turbine rotor, and which has an original outline, in order to create a modified disc which has an outline different from the original outline and which provides a blade-supporting region of increased size, the original disk having at least one portion which must be removed in order to create the modified disc, comprising: machining away each said portion of the original disc; building up the original disc with weld metal past the eventual outline of the modified disc at all locations where the outline of the original disc, after said machining step, is to be enclosed by the outline of said modified disc; and machining away parts of the weld metal to the outline of the modified disc.
Claim 3
Dependent Claim 33 words
A method as defined in claim 1 wherein the modified disc has a blade-supporting base and said step of building up is carried out to form the entire cross section of the base.
Claim 4
Dependent Claim 49 words
A method as defined in claim 2 wherein the rotor has an axis, the original disc and the modified disc each have a center plane which extends perpendicular to the rotor axis, and the center planes are offset from one another in the direction parallel to the rotor axis.
Claim 5
Dependent Claim 23 words
A method as defined in claim 3 wherein said step of building up is carried out by a gas tungsten arc welding process.
Claim 6
Dependent Claim 69 words
A method as defined in claim 3 wherein said step of building up includes firstly providing a large volume of weld metal on at least one location; by performing a submerged arc or gas metal arc welding process to supply at least a substantial portion of said large volume, and secondly, performing a gas tungsten arc welding process to supply metal for the outer surface of the modified disc.
Claim 7
Dependent Claim 23 words
A method as defined in claim 2 wherein said step of building up is carried out by a gas tungsten arc welding process.
Claim 8
Dependent Claim 69 words
A method as defined in claim 2 wherein said step of building up includes firstly providing a large volume of weld metal on at least one location; by performing a submerged arc or gas metal arc welding process to supply at least a substantial portion of said large volume and secondly performing a gas tungsten arc welding process to supply metal for the outer surface of the modified disc.
Claim 9
Dependent Claim 44 words
A method as defined in claim 1 wherein the original disc and the modified disc each have a center plane, which extends perpendicular to the rotor axis and the center planes are offset from one another in the direction parallel to the rotor axis.
Claim 10
Dependent Claim 23 words
A method as defined in claim 1 wherein said step of building up is carried out by a gas tungsten arc welding process.
Claim 11
Dependent Claim 69 words
A method as defined in claim 1 wherein said step of building up includes firstly providing a large volume of weld metal on at least one location; by performing a submerged arc or gas metal arc welding process to supply at least a substantial portion of said large volume, and secondly, performing a gas tungsten arc welding process to supply metal for the outer surface of the modified disc.

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1993-01-15 1993-07-17 1994-01-16 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1997-01-15 1997-07-17 1998-01-16 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2001-01-15 2001-07-17 2002-01-16 $7700.00 Window Closed / Lapsed

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