Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

Alluminide coatings containing silicon and yttrium for superalloys and method of forming such coatings

a technology of superalloys and alluminide coatings, which is applied in the direction of superimposed coating process, liquid/solution decomposition chemical coating, soldering apparatus, etc., can solve the problems of high production cost of platinum aluminide, inability to adhere well to the superalloy commonly used to form jet engine components, and increase the cost of jet engine components and the cost of refurbishing used jet engine components. , to achieve the effect of less production cost and competitive performan

Inactive Publication Date: 2006-03-16
AEROMET TECH
View PDF34 Cites 15 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

[0010] By virtue of the foregoing, there is provided an improved environmental coating, bond coat, and method of forming such coatings that include an aluminide layer containing minor concentrations of silicon and yttrium. The aluminide coating of the invention is competitive in performance with platinum aluminide and less expensive to produce than platinum aluminide.

Problems solved by technology

However, such protective ceramic thermal barrier coatings may not adhere well directly to the superalloys commonly used to form jet engine components and, while in service, tend to spall.
However, platinum aluminides are expensive to produce, which contributes to increasing the cost of jet engine components and the cost of refurbishing used jet engine components.

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Alluminide coatings containing silicon and yttrium for superalloys and method of forming such coatings
  • Alluminide coatings containing silicon and yttrium for superalloys and method of forming such coatings
  • Alluminide coatings containing silicon and yttrium for superalloys and method of forming such coatings

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0020] With reference to FIG. 1, a detailed view of a portion of a much larger jet engine component, generally indicated by reference numeral 10, is shown. The jet engine component 10 includes a metallic substrate 12 and an aluminide layer 14 coating an original surface 16 of the substrate 12. The metallic substrate 12 is made of any nickel-, cobalt-, or iron-based high temperature superalloy from which such jet engine components 10 are commonly made. For example, the substrate 12 may be the nickel-based superalloy Inconel 795 Mod5 A. The present invention is not intended to be limited to any particular jet engine component 10, which may be a turbine blade, a vane, a nozzle guide, or any other part requiring protection from high temperature oxidation and corrosion while operating in a jet engine. The substrate 12 may be masked to define areas across which the aluminide layer 14 is absent.

[0021] In this specific embodiment of the present invention, aluminide layer 14 operates as an ...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

PropertyMeasurementUnit
Temperatureaaaaaaaaaa
Timeaaaaaaaaaa
Concentrationaaaaaaaaaa
Login to View More

Abstract

Aluminide coatings or layers (14) for jet engine components (10) and a process for forming aluminide layers (14) that include additions of silicon and yttrium. A superalloy substrate (12) of the component (10) is initially coated with a layer of a silicon-containing material. The substrate (12) is then aluminided, for example by a chemical vapor deposition process, and is exposed to a yttrium-containing material during the aluminiding process to form the aluminide layer (14) containing silicon and yttrium. A ceramic thermal barrier layer (24) of yttria-stabilized zirconia may be optionally applied over the aluminide layer (14). Another optional zirconia layer (26) maybe provided between the aluminide layer (14) and the ceramic thermal barrier layer (24). The present invention provides a silicon- and yttrium-containing aluminide layer (14) having improved durability, either as a standalone environmental coating or as a bond coat for a subsequently-applied ceramic thermal barrier layer (24).

Description

FIELD OF THE INVENTION [0001] The present invention relates to formation of an intermetallic layer on a metal component and, more particularly, to formation of an intermetallic layer on an airflow surface of a jet engine metal component. BACKGROUND OF THE INVENTION [0002] Intermetallic layers are often applied to a surface of a metal component for protecting the underlying metal substrate of the component and thereby extending its useful life during operation. For example, the aerospace industry coats many components having airflow surfaces in a jet engine, like turbine blades, vanes, and nozzle guides, with an aluminide layer to protect the underlying base metal from high temperature oxidation and corrosion. [0003] A ceramic thermal barrier coating may be applied over the aluminide layer to insulate the jet engine component from combustion and exhaust gases, permitting the combustion and exhaust gases from the engine to be hotter than would otherwise be possible with an aluminide l...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
IPC IPC(8): B32B15/20
CPCC23C10/02Y10T428/12611C23C18/1204C23C18/1216C23C18/1225C23C18/1279C23C18/1295Y02T50/67C23C28/321C23C28/325C23C28/3455C23C6/00Y10T428/1259Y10T428/12549Y10T428/1275C23C18/06Y02T50/60
Inventor FAIRBOURN, DAVID C.
Owner AEROMET TECH
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products