Coated seal slot systems for turbomachinery and methods for forming the same

Patent metadata

Field	Value
Publication number	US-10100656-B2
Application number	US-201514834866-A
Country	US
Kind code	B2
Filing date	Aug 25, 2015
Priority date	Aug 25, 2015
Publication date	Oct 16, 2018
Grant date	Oct 16, 2018

Abstract

A coated seal slot system for turbomachinery includes a first turbine component comprising a first groove having at least one first coating attached to at least a portion of the first groove of the first turbine component, a second turbine component comprising a second groove having at least one second coating attached to at least a portion of the second groove of the second turbine component. The first and the second turbine components are disposable adjacent to each other with the first groove having the first coating and the second groove having the second coating together forming a coated seal slot extending across a gap between the first turbine component and the second turbine component. A seal is disposable in the coated seal slot and extendable across the gap between the first and the second turbine components and engageable with the first coating and the second coating to inhibit leakage of gas through the gap.

First claim

The invention claimed is:

1. A method for forming a coated seal slot for turbomachinery, the method comprising:
providing a first turbine component having a first groove;
providing a second turbine component having a second groove;
providing at least one first coating on at least a portion of the first groove of the first turbine component;
providing at least one second coating on at least a portion of the second groove of the second turbine component; and

wherein the first groove having the first coating and the second groove having the second coating which together form a coated seal slot extending across a gap formed between the first turbine component and the second turbine component, and a seal being disposable in the coated seal slot and engageable with the first coating and the second coating to inhibit leakage of gas through the gap, wherein the providing the first coating comprises applying a slurry onto the at least the portion of the first groove of the first turbine component and heat treating the slurry on the at least the portion of the first groove of the first turbine component, and the providing the second coating comprises applying a slurry onto the at least the portion of the second groove of the second turbine component and heat treating the slurry on the at least the portion of the second groove of the second turbine component.

2. A method for forming a coated seal slot for turbomachinery, the method comprising:
providing a first turbine component having a first groove;
providing a second turbine component having a second groove;
providing at least one first coating on at least a portion of the first groove of the first turbine component;
providing at least one second coating on at least a portion of the second groove of the second turbine component; and

wherein the first groove having the first coating and the second groove having the second coating which together form a coated seal slot extending across a gap formed between the first turbine component and the second turbine component, and a seal being disposable in the coated seal slot and engageable with the first coating and the second coating to inhibit leakage of gas through the gap, wherein the providing the first coating comprises applying a slurry in the first groove of the first turbine component, scraping some of the slurry from the first groove, and heat treating the remaining slurry in the first groove of the first turbine component, and the providing the second coating comprises applying a slurry in the second groove of the second turbine component, scraping some of the slurry from the second groove, and heat treating the remaining slurry on the second groove of the second turbine component.

3. A method for forming a coated seal slot for turbomachinery, the method comprising:
providing a first turbine component having a first groove;
providing a second turbine component having a second groove;
providing at least one first coating on at least a portion of the first groove of the first turbine component;
providing at least one second coating on at least a portion of the second groove of the second turbine component; and

wherein the first groove having the first coating and the second groove having the second coating which together form a coated seal slot extending across a gap formed between the first turbine component and the second turbine component, and a seal being disposable in the coated seal slot and engageable with the first coating and the second coating to inhibit leakage of gas through the gap, wherein the providing the first coating comprises bulk filling the first groove of the first turbine component with a slurry, drying or heat treating the slurry in the first groove of the first turbine component, and removing a portion of the dried or heat treated slurry to form the first coating, and the providing the second coating comprises bulk filling the second groove of the first turbine component with a slurry, drying or heat treating the slurry in the second groove of the first turbine component, and removing a portion of the dried or heat treated slurry to form the second coating.

4. The method of claim 3 wherein the removing the portion of the dried or heat treated slurry to form the first coating comprises machining the dried or heat treated slurry, and the removing the portion of the dried or heat treated slurry to form the second coating comprises machining the dried or heat treated slurry.

5. The method of claim 3 wherein the removing the portion of the dried or heat treated slurry to form the first coating comprises electrical discharge machining, laser machining, milling, wire saw grooving, or semiconductor dicing sawing the dried or heat treated slurry, and the removing the portion of the dried or heat treated slurry to form the second coating comprises electrical discharge machining, laser machining, milling, wire saw grooving, or semiconductor dicing sawing the dried or heat treated slurry.

Assignees

• Gen Electric

Inventors

• Bancheri Stephen Francis
• Venkataramani Venkat Subramaniam
• Kirby Glen Harold
• Sarawate Neelesh Nandkumar
• Antolino Nicholas Edward
• Sevincer Edip
• Marin Anthony Christopher

Classifications

• F01D25/005

  Selecting particular materials · CPC title

• F05D2230/90

  Coating; Surface treatment · CPC title

• F05D2240/11

  Shroud seal segments · CPC title

• F01D11/005

  Sealing means between non relatively rotating elements · CPC title

• B05D1/005

  Spin coating · CPC title