Methods for manufacturing titanium aluminide components from articles formed by consolidation processes
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
C23C-016/06
C23C-016/48
B05D-003/12
B05D-007/14
B22F-003/12
B22F-003/15
C23C-010/48
C23C-010/60
C22C-001/04
C23C-014/16
B22F-003/105
출원번호
US-0564656
(2012-08-01)
등록번호
US-9120151
(2015-09-01)
발명자
/ 주소
Godfrey, Donald G.
Morris, Mark C.
Reimer, George
Hehmann, William F.
Legzdina, Daira
Fox, Richard
Hu, Yiping
Kington, Harry Lester
출원인 / 주소
HONEYWELL INTERNATIONAL INC.
대리인 / 주소
Ingrassia Fisher & Lorenz, P.C.
인용정보
피인용 횟수 :
1인용 특허 :
43
초록▼
Substantially defect-free titanium aluminide components and methods are provided for manufacturing the same from articles formed by consolidation processes. The method includes providing an intermediate article comprised of a titanium aluminide alloy and formed by a consolidation process. The interm
Substantially defect-free titanium aluminide components and methods are provided for manufacturing the same from articles formed by consolidation processes. The method includes providing an intermediate article comprised of a titanium aluminide alloy and formed by a consolidation process. The intermediate article is encapsulated with an aluminum-containing encapsulation layer. The intermediate article is compacted after the encapsulation step. A substantially defect-free titanium aluminide component comprises a compacted three-dimensional article comprised of titanium aluminide and formed by a consolidation process and an aluminum-containing encapsulation layer on at least one surface of the compacted three-dimensional article. The aluminum-containing encapsulation layer comprises an aluminide material, MCrAlY wherein M is cobalt, nickel, or a combination of cobalt and nickel, or TiAlCr.
대표청구항▼
1. A method for manufacturing a titanium aluminide component, the method comprising the steps of: providing an intermediate article comprised of a titanium aluminide alloy and formed by a consolidation process using additive manufacturing;encapsulating the intermediate article with an aluminum-conta
1. A method for manufacturing a titanium aluminide component, the method comprising the steps of: providing an intermediate article comprised of a titanium aluminide alloy and formed by a consolidation process using additive manufacturing;encapsulating the intermediate article with an aluminum-containing encapsulation layer; andcompacting the intermediate article after the encapsulation step. 2. The method of claim 1, wherein the step of encapsulating the intermediate article comprises forming the aluminum-containing encapsulation layer with TiAl, TiAl3, or a combination thereof to respectively form an aluminide encapsulation layer. 3. The method of claim 2, wherein the step of encapsulating the intermediate article comprises forming a TiAl aluminide encapsulation layer by a vapor aluminizing process. 4. The method of claim 3, wherein the step of encapsulating the intermediate article comprises forming the TiAl aluminide encapsulation layer having the following chemical composition: about 50 at. % aluminum and about 50 at. % titanium 5. The method of claim 1, wherein the step of encapsulating the intermediate article comprises forming a TiAl3 aluminide encapsulation layer comprising about 75 at. % aluminum and about 25 at. % titanium. 6. The method of claim 1, wherein the step of encapsulating the intermediate article comprises forming a MCrAlY encapsulation layer wherein the M is nickel, cobalt, or a combination of nickel and cobalt. 7. The method of claim 6, wherein the step of encapsulating the intermediate article comprises forming the MCrAlY encapsulation layer using an encapsulation process selected from the group consisting of EBPVD, cathodic arc, magnetron sputtering, and a thermal spray process selected from the group consisting of LPPS, HVOF, and Ar-shrouded plasma spray. 8. The method of claim 6, wherein the step of encapsulating the intermediate article comprises encapsulating the intermediate article with the MCrAlY encapsulation layer comprising Co27Cr9Al0.5Y, Ni30Cr11Al0.5Y, Co32Ni21Cr8Al0.5Y, or Ni23Co18Cr12.5Al0.5Y. 9. The method of claim 1, wherein the step of encapsulating the intermediate article comprises encapsulating the intermediate article with a TiAlCr encapsulation layer. 10. The method of claim 9, wherein the step of encapsulating the intermediate article comprises encapsulating the intermediate article with the TiAlCr encapsulation layer by EBPVD, cathodic arc, and magnetron sputtering vapor deposition processes. 11. The method of claim 9, wherein the step of encapsulating the intermediate article comprises encapsulating the intermediate article with the TiAlCr encapsulation layer comprising Ti-34/38Al-12/16Cr, wt %. 12. The method of claim 1, wherein the step of encapsulating the intermediate article comprises encapsulating an external surface, an internal passage surface, or both the internal passage surface and the external surface of the intermediate article. 13. The method of claim 1, wherein the step of compacting the intermediate article after the encapsulating step comprises hot isostatic pressing (HIP) the intermediate article with the aluminum-containing encapsulation layer. 14. A method for manufacturing a titanium aluminide component from an intermediate article formed by a consolidation process, the method comprising the steps of: encapsulating the intermediate article with an aluminum-containing encapsulation layer to form an encapsulated article, the intermediate article formed by the consolidation process using additive manufacturing and comprised of a titanium aluminide alloy material and the aluminum-containing encapsulation layer comprised of: (a) an aluminide encapsulation layer, (b) a MCrAlY encapsulation layer wherein the M comprises nickel, cobalt, or a combination of nickel and cobalt, or (c) a TiAlCr encapsulation layer; andcompacting the encapsulated article. 15. The method of claim 14, wherein the step of encapsulating the intermediate article comprises forming the aluminide encapsulation layer with TiAl, TiAl3, or a combination thereof. 16. The method of claim 14, wherein the step of encapsulating the intermediate article comprises encapsulating the intermediate article with the MCrAlY encapsulation layer comprising Co27Cr9Al0.5Y, Ni30Cr11Al0.5Y, Co32Ni21Cr8Al0.5Y, or Ni23Co18Cr12.5Al0.5Y.Co 17. The method of claim 14, wherein the step of encapsulating the intermediate article comprises encapsulating an external surface, an internal passage surface, or both the internal passage surface and the external surface of the intermediate article. 18. The method of claim 14, wherein the step of compacting the encapsulated article comprises hot isostatic pressing (HIP) the encapsulated article.
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