Stock material or miscellaneous articles – All metal or with adjacent metals – Having metal particles
Reexamination Certificate
2000-12-14
2002-07-30
Jones, Deborah (Department: 1775)
Stock material or miscellaneous articles
All metal or with adjacent metals
Having metal particles
C428S559000, C428S573000, C428S601000, C427S142000, C029S889100, C029S897100, C228S119000
Reexamination Certificate
active
06426152
ABSTRACT:
BACKGROUND OF THE INVENTION
The present invention relates to a turbine casting having cast-in cooling bumps along a surface to provide improved heat transfer between a cooling medium and the opposite side of the casting. Particularly, the present invention relates to methods for salvaging castings with defective cast cooling bumps by applying a coating to areas of the defectively cast bumps to improve their heat transfer characteristics. The present invention also relates to the salvaged castings.
Various techniques have been devised to maintain the temperature of gas turbine components below critical levels. For example, a cooling medium such as coolant air from the turbine compressor or steam is often directed to the component along one or more component surfaces. Such flow is understood in the art as backside flow, where the cooling medium is directed at a surface of the component not directly exposed to high temperature gases of combustion. Enhanced heat transfer is also accomplished by providing cast cooling bumps along the backside flow surface. For example, cast cooling bumps may be provided in a gas turbine on the inside surfaces of the stage 1 and stage 2 nozzles. It will be appreciated that the outer surfaces of the nozzles are exposed to the hot gases and are subject to very high temperatures on the hot gas path exposed side thereof. A cooling medium such as steam or air flows through various cavities within the nozzles along the interior nozzle surfaces to provide backside cooling flow. The cast-in bumps on the interior surfaces of the nozzle have a generally hill-like shape and are spaced from one another to provide a coolant side surface area larger than that of the baseline smooth surface area.
In certain gas turbine components, for example, nozzles, the cast-in cooling bumps are sometimes defective. By defective cast bumps is meant that one or more bumps are missing from the surface of the cast part or the bump is only partially formed. These defects occur as a result of manufacturing process limitations. When the parts are cast and inspected, defective areas can be identified and the parts are sometimes scrapped. This results in a significant financial loss. Accordingly, there is a need to provide a method for salvaging cast parts of a turbine that have defective cast cooling bumps.
BRIEF SUMMARY OF THE INVENTION
In accordance with a preferred embodiment of the present invention, there is provided methods of salvaging a casting having cast cooling bumps projecting from a surface thereof wherein one or more areas of that surface have defectively cast bumps manifested by one or more missing or partially cast bumps. To accomplish the foregoing, the surface area or areas manifested by one or more missing or cast bumps are first identified by visual inspection or thermography. Once identified, the area or areas are cleaned and the defective bumps removed, e.g., by grinding or grit blasting. Thus, partially formed bumps may be ground down to the surface area between the bumps, or the smooth area or areas with partially formed bumps may simply be roughened. After cleaning, cooling enhancement material is applied to the surface area(s) manifesting defectively cast bumps and the spaces between the defectively cast bumps. Preferably, a coating containing particles, e.g., metal particles, is applied to the defective area. For example, a green braze tape coated with a metallic powder is set in intimate contact with the defective area and brazed thereto. The size of the metallic powder particles is selected to provide heat transfer enhancement on the local defective surface area. The alloy of the metallic powder particles is chosen to withstand the part operating conditions while providing a high thermal conductivity. The braze alloy must also withstand the part operating temperature while not diminishing other part properties, i.e., LCF. By applying the coating in the local area of the defectively cast bumps, the part can be salvaged and utilized, notwithstanding the lack of bumps or partial bump formation in one or more areas of the backside surface. It will be appreciated that this salvage or repair technique can be used on most or all of the gas turbine parts having cast bumps for enhancing heat transfer, such as shrouds, certain stator nozzles, buckets and the like.
In a preferred embodiment according to the present invention, there is provided a method of salvaging a casting having cast cooling bumps projecting from a surface thereof wherein at least one area of the surface has defectively cast bumps manifested by one or more missing or partially cast bumps, comprising the steps of identifying the defectively cast area and applying a coating on the defectively cast area to form an overlying coated surface forming a coated surface area in excess of the uncoated defective surface area to afford enhanced heat transfer across the casting relative to the heat transfer across the casting without applying the coating.
In a further preferred embodiment according to the present invention, there is provided a method of salvaging a casting having cast cooling bumps projecting from a surface thereof wherein at least one area of the surface has defectively cast bumps manifested by one or more missing or partially cast bumps, comprising the steps of identifying the defectively cast area, providing a brazing sheet having cooling enhancement material and fusing the brazing sheet to the defectively cast area such that the cooling enhancement material is bonded thereto.
In a still further preferred embodiment according to the present invention, there is provided a cast body having a cooling surface and an opposite surface for exposure to a high-temperature fluid medium, the cooling surface having a plurality of cast cooling bumps projecting therefrom and at least one area thereof having defectively cast bumps manifested by one or more missing or partially cast bumps, a coating overlying the defectively cast area forming a coated surface having an area in excess of the defectively cast area to afford enhanced heat transfer across the casting relative to the heat transfer across the coating without the coating.
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“39thGE Turbine State-of-the-Art Technology Seminar”, Tab 1, ““F” Technology—the First Half-Million Operating Hours”, H.E. Miller, Aug. 1996.
“39th GE Turbine State-of-the-Art Technology Seminar”, Tab 2, “GE Heavy-Duty Gas Turbine Performance Characteristics”, F. J. Brooks, Aug. 1996.
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“39th GE Turbine State-of-the-Art Technology Seminar”, Tab 4, “MWS6001FA—An Advanced-Technology 70-MW Class 50/60 Hz Gas Turbine”, Ramachandran et al., Aug. 1996.
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“39th GE Turbine State-of-the-Art Technology Seminar”, Tab 11, “Integra
Abuaf Nesim
Hasz Wayne Charles
Johnson Robert Alan
Lee Ching-Pang
Schaeffer Jon Conrad
General Electric Company
Jones Deborah
Nixon & Vanderhye
Savage Jason
LandOfFree
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