CA2523588A1 - Multi-scale cermets for high temperature erosion-corrosion service - Google Patents

Multi-scale cermets for high temperature erosion-corrosion service Download PDF

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Publication number
CA2523588A1
CA2523588A1 CA 2523588 CA2523588A CA2523588A1 CA 2523588 A1 CA2523588 A1 CA 2523588A1 CA 2523588 CA2523588 CA 2523588 CA 2523588 A CA2523588 A CA 2523588A CA 2523588 A1 CA2523588 A1 CA 2523588A1
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CA
Canada
Prior art keywords
cermet
cermet composition
group
phase
vol
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
CA 2523588
Other languages
French (fr)
Inventor
Narasimha-Rao Venkata Bangaru
Jayoung Koo
Changmin Chun
Hyun-Woo Jin
John Roger Peterson
Robert Lee Antram
Christopher John Fowler
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
ExxonMobil Technology and Engineering Co
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of CA2523588A1 publication Critical patent/CA2523588A1/en
Abandoned legal-status Critical Current

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Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C29/00Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides
    • C22C29/14Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides based on borides
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C29/00Alloys based on carbides, oxides, nitrides, borides, or silicides, e.g. cermets, or other metal compounds, e.g. oxynitrides, sulfides
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C30/00Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/31504Composite [nonstructural laminate]
    • Y10T428/31678Of metal

Abstract

A cermet composition represented by the formula (PQ)(RS)Xcomprising: a ceramic phase (PQ), a binder phase (RS) and X wherein X is at least one member selected from the group consisting of an oxide dispersoid E, an intermetallic compound F and a derivative compound G wherein said ceramic phase (PQ) is dispersed in the binder phase (RS) as particles of diameter in the range of about 0.5 to 3000 microns, and said X is dispersed in the binder phase (RS) as particles in the size range of about 1 nm to 400 nm.

Claims (15)

1. A cermet composition represented by the formula (PQ)(RS)X
comprising: a ceramic phase (PQ), a binder phase (RS) and X wherein X is at least one member selected from the group consisting of an oxide dispersoid E, an intermetallic compound F and a derivative compound G wherein said ceramic phase (PQ) is dispersed in the binder phase (RS) as particles of diameter in the range of about 0.5 to 3000 microns, and said X is dispersed in the binder phase (RS) as particles in the size range of about 1 nm to 400 nm.
2. The cermet composition of claim 1 wherein the ceramic phase (PQ) comprises a metal P selected from the group consisting of Al, Si, Mg, Group IV, Group V, Group VI elements and mixtures thereof and Q, which is selected from the group consisting of carbide, nitride, boride, carbonitride, oxide and mixtures thereof, wherein ceramic phase (PQ) ranges from of about 30 to 95 vol% based on the volume of cermet composition.
3. The cermet composition of claim 2 wherein the ceramic phase (PQ) the molar ratio of P to Q can vary in the range of 0.5:1 to 30:1.
4. The cermet composition of claim 2 wherein the ceramic phase (PQ) ranges from of about 55 to 95 vol% based on the volume of the cermet.
5. The cermet composition of claim 1 wherein the binder phase (RS) comprises a base metal R selected from the group consisting of Fe, Ni, Co, Mn and mixtures thereof and an alloying metal S selected from Si, Cr, Ti, Al, Nb, Mo and mixtures thereof and wherein the binder phase (RS) is in the range of 4.5 to 70 vol% based on the volume of the cermet and the base metal R to alloying metal S mass ratio ranges from 50/50 to 90/10.
6. The cermet composition of claim 1 wherein the oxide dispersoids E is selected from the group consisting of oxides Al, Ti, Nb, Zr, Hf, V, Ta, Cr, Mo, W, Fe, Mn, Ni, Si, Y and mixtures thereof and ranges from of about 0.1 to 10 vol% based on the volume of the cermet.
7. The cermet composition of claim 1 wherein the intermetallic compound F is selected from the group consisting of gamma prime (.gamma.') and beta (.beta.) such as Ni3Al, Ni3Ti, Ni3Nb, NiAl, Ni2AlTi, NiTi, Ni2AlSi, FeAl, Fe3Al, CoAl, Co3Al, Ti3Al, Al3Ti, TiAl, Ti2AlNb, TiAl2Mn, TaAl3, NbAl3 and mixtures thereof and ranges from of about 0.1 to 10 vol% based on the volume of the cermet.
8. The cermet composition of claim 1 wherein the derivative compound G is derived from ceramic phase (PQ) or ceramic phase (PQ) and binder phase (RS) and ranges from about 0.01 to 10 vol% based on the volume of the cermet.
9. The cermet composition of claim 1 having a fracture toughness greater than about 3 MPa.cndot.m1/2.
10. The cermet composition of claim 1 having an erosion rate less than about 1×10 -6cc/gram of SiC erodant.
11. The cermet composition of claim 1 having corrosion rate less than about 1×10 -10 g2/cm4.cndot.s or an average oxide scale of less than 150 µm thickness when subject to 100 cc/min air at 800°C for at least 65 hours.
12. The cermet composition of claim 1 having an erosion rate less than about 1×10 -6cc/gram of SiC erodant and a corrosion rate less than about 1×10 -10 g2/cm4.cndot.s or an average oxide scale of less than 150 µm thickness when subject to 100 cc/min air at 800°C for at least 65 hours.
13. A method for protecting a metal surface subject to erosion at temperatures up to 850°C, the method comprising providing the metal surface with a cermet composition according to claims 1-12.
14. A method for protecting a metal surface subject to erosion at temperatures in the range of 300°C to 850°C, the method comprising providing the metal surface with a cermet composition according to claims 1-12.
15. The method of claim 13 wherein said surface comprises the inner surface of a fluid-solids separation cyclone.
CA 2523588 2003-05-20 2004-05-18 Multi-scale cermets for high temperature erosion-corrosion service Abandoned CA2523588A1 (en)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US47199503P 2003-05-20 2003-05-20
US60/471,995 2003-05-20
US10/829,819 US7316724B2 (en) 2003-05-20 2004-04-22 Multi-scale cermets for high temperature erosion-corrosion service
US10/829,819 2004-04-22
PCT/US2004/015553 WO2004104246A1 (en) 2003-05-20 2004-05-18 Multi-scale cermets for high temperature erosion-corrosion service

Publications (1)

Publication Number Publication Date
CA2523588A1 true CA2523588A1 (en) 2004-12-02

Family

ID=33479310

Family Applications (1)

Application Number Title Priority Date Filing Date
CA 2523588 Abandoned CA2523588A1 (en) 2003-05-20 2004-05-18 Multi-scale cermets for high temperature erosion-corrosion service

Country Status (15)

Country Link
US (2) US7316724B2 (en)
EP (1) EP1633901B1 (en)
JP (1) JP2007517978A (en)
KR (1) KR20060012007A (en)
AT (1) ATE417133T1 (en)
AU (1) AU2004242137B8 (en)
BR (1) BRPI0410417A (en)
CA (1) CA2523588A1 (en)
DE (1) DE602004018311D1 (en)
DK (1) DK1633901T3 (en)
ES (1) ES2319532T3 (en)
MX (1) MXPA05011601A (en)
RU (1) RU2360024C2 (en)
SG (1) SG141421A1 (en)
WO (1) WO2004104246A1 (en)

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US7731776B2 (en) * 2005-12-02 2010-06-08 Exxonmobil Research And Engineering Company Bimodal and multimodal dense boride cermets with superior erosion performance
US7842139B2 (en) * 2006-06-30 2010-11-30 Exxonmobil Research And Engineering Company Erosion resistant cermet linings for oil and gas exploration, refining and petrochemical processing applications
GB2465737B (en) * 2007-10-09 2013-03-20 Cameron Int Corp Erosion resistant material
CA2705769A1 (en) * 2007-11-20 2009-05-28 Exxonmobil Research And Engineering Company Bimodal and multimodal dense boride cermets with low melting point binder
US20110312860A1 (en) * 2010-06-17 2011-12-22 General Electric Company Wear-resistant and low-friction coatings and articles coated therewith
JP6202787B2 (en) * 2012-05-31 2017-09-27 株式会社アライドマテリアル Molybdenum heat-resistant alloy, friction stir welding tool, and manufacturing method
ES2751392T3 (en) * 2014-07-14 2020-03-31 MTU Aero Engines AG Al-rich high-temperature Ti-Al alloy
CN106498207B (en) * 2016-10-28 2017-10-27 成都理工大学 In-situ preparation contains Ni3The preparation method of the cermet of Al Binder Phase
CN106498208B (en) * 2016-10-28 2017-11-07 成都理工大学 Ni in Binder Phase3The generated in-situ cermet material preparation methods of Al
CN106498257B (en) * 2016-10-28 2017-10-27 成都理工大学 In-situ preparation contains Ni3The preparation method of the hard alloy of Al Binder Phase
CN106521206B (en) * 2016-10-28 2017-11-14 成都理工大学 A kind of preparation method of the cermet material of high temperature resistance softening
CN106521207B (en) * 2016-10-28 2017-11-14 成都理工大学 A kind of preparation method of the hard alloy of high temperature resistance softening
CN106319271B (en) * 2016-10-28 2018-01-30 成都理工大学 Ni in Binder Phase3The generated in-situ hard alloy preparation methods of Al
CN106636832B (en) * 2016-10-28 2018-05-22 成都理工大学 A kind of preparation method of the cermet material of the Binder Phase containing intermetallic compound
CN106636835B (en) * 2016-10-28 2018-05-22 成都理工大学 A kind of preparation method of the hard alloy of the Binder Phase containing intermetallic compound
CN109336614B (en) * 2018-10-31 2020-07-03 燕山大学 Preparation method of Sialon/Ti-22Al-25Nb ceramic matrix composite material
CN111647771B (en) * 2020-04-17 2021-10-15 中国航发北京航空材料研究院 Multi-element composite anti-oxidation Ti2AlNb alloy and preparation method thereof
CN111394637B (en) * 2020-04-17 2021-06-01 中国航发北京航空材料研究院 Ti2AlNb alloy and preparation method of bar thereof
CN111621659A (en) * 2020-06-29 2020-09-04 西安工程大学 Method for preparing Ti2AlNb alloy by powder metallurgy method

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Also Published As

Publication number Publication date
MXPA05011601A (en) 2006-01-23
US20070131054A1 (en) 2007-06-14
BRPI0410417A (en) 2006-05-30
RU2360024C2 (en) 2009-06-27
AU2004242137A1 (en) 2004-12-02
EP1633901B1 (en) 2008-12-10
RU2005136133A (en) 2006-06-27
DK1633901T3 (en) 2009-04-06
DE602004018311D1 (en) 2009-01-22
KR20060012007A (en) 2006-02-06
US7316724B2 (en) 2008-01-08
SG141421A1 (en) 2008-04-28
WO2004104246A1 (en) 2004-12-02
ES2319532T3 (en) 2009-05-08
AU2004242137B2 (en) 2009-07-16
ATE417133T1 (en) 2008-12-15
JP2007517978A (en) 2007-07-05
US20120177933A1 (en) 2012-07-12
EP1633901A1 (en) 2006-03-15
AU2004242137B8 (en) 2009-08-06

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Legal Events

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EEER Examination request
FZDE Discontinued

Effective date: 20140206