[미국특허]
Ferromagnetic alloy for induction cooking
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
C22C-038/40
C22C-019/05
출원번호
UP-0857481
(2004-06-01)
등록번호
US-7575712
(2009-08-31)
발명자
/ 주소
Fraisse, Herve
Waeckerle, Thierry
Grosbety, Yves
Coutu, Lucien
출원인 / 주소
Imphy Alloys
대리인 / 주소
Sughrue Mion, PLLC
인용정보
피인용 횟수 :
0인용 특허 :
7
초록▼
The invention concerns a ferromagnetic alloy whereof the chemical composition comprises, in wt. %: 32.5%≦Ni≦72.5%; 5%≦Cr≦18%; 0.01%≦Mn≦4%; C≦1%; optionally one or more elements selected among Mo, V, Co, Cu, Si, W, Nb and Al, the total contents of said elemen
The invention concerns a ferromagnetic alloy whereof the chemical composition comprises, in wt. %: 32.5%≦Ni≦72.5%; 5%≦Cr≦18%; 0.01%≦Mn≦4%; C≦1%; optionally one or more elements selected among Mo, V, Co, Cu, Si, W, Nb and Al, the total contents of said elements being not more than 10%, the remainder being iron and impurities resulting from preparation, the chemical composition further satisfying the following relationships: Cr-1.1Ni+23.25≦0%; 45Cr+11Ni≦1360; Ni+3Cr≧60% if Ni≧37.5; Cr≧7.5 if Ni≦37.5. The invention also concerns the use of said alloy for making heating elements for induction heated cooking appliances.
대표청구항▼
The invention claimed is: 1. A process for producing a heating element for cooking vessels for induction cooking comprising: forming a ferromagnetic alloy having a chemical composition comprising, in percent by weight: 32.5%≦Ni≦72.5%; 7.4%≦Cr≦18% 0.01%≦Mn≦
The invention claimed is: 1. A process for producing a heating element for cooking vessels for induction cooking comprising: forming a ferromagnetic alloy having a chemical composition comprising, in percent by weight: 32.5%≦Ni≦72.5%; 7.4%≦Cr≦18% 0.01%≦Mn≦4%; C≦1%; 0≦Cu≦0.01; and the balance being iron and impurities resulting from the smelting, wherein the chemical composition further satisfies the following relationships: Cr-1.1Ni+23.25≦0%; 45Cr+11Ni≦1360; Ni+3Cr≧60% if Ni≧37.5; and Cr≧7.5 if Ni≦37.5 and forming the heating element comprising the ferromagnetic alloy, wherein the heating element has a side wall. 2. The process as claimed in claim 1, wherein the chromium content of said alloy is greater than 13%. 3. The process as claimed in claim 1 or 2, wherein the nickel content of said alloy is between 34 and 50% and that the alloy does not contain Mo, V, Co, Cu, Si, W, Nb and Al. 4. The process as claimed in claim 1 or 2, wherein the nickel content of said alloy is greater than 52%. 5. The process as claimed in claim 1, wherein the nickel content of said alloy is between 48 and 52% and the chromium content is between 7.4 and 10%. 6. The process as claimed in claims 1 or 2, wherein the manganese content of said alloy is greater than or equal to 0.1%. 7. The process as claimed in claim 1 or 2, wherein said alloy has a Curie temperature Tc of between 30 and 350° C., a thermal expansion coefficient αTC between room temperature and Tc of greater than or equal to 6.5×10-6 K-1 and a saturation induction Bs of greater than or equal to 0.2 T and the maximum oxidation current Imax of said alloy in a voltage-current corrosion test in acid medium is less than 1 mA. 8. The process as claimed in claim 7, wherein the thermal expansion coefficient αTC between room temperature and Tc of said alloy is greater than or equal to 9×10-6 K-1 and the saturation induction Bs is greater than or equal to 0.5 T. 9. A process for producing a bottom of monolayer cooking vessels intended for induction cooking comprising, forming a monolayer of a ferromagnetic alloy having a chemical composition comprising, in percent by weight: ti 32.5%≦Ni≦72.5%; 13%≦Cr≦18%; 0.01%≦Mn≦4%; C≦1%; the balance being iron and impurities resulting from smelting, wherein the chemical composition further satisfies the following relationships: Cr-1.1Ni+23.25≦0%; 45Cr+11Ni≦1360; Ni+3Cr≧60% if Ni≧37.5; and Cr≧7.5 if Ni≦37.5 and forming the bottom of the monolayer cooking vessel comprising the ferromagnetic alloy, wherein the cooking vessel has a side wall. 10. The process as claimed in claim 1, wherein the chemical composition further comprises one or more elements selected from the group consisting of Mo, V, Co, Cu, Si, W, Nb and Al, the sum of the contents of these elements being less than or equal to 10%. 11. The process as claimed in claim 1, wherein the chemical composition does not contain any Mo, V, Co, Cu, Si, W, Nb and Al. 12. The process as claimed in claim 3, wherein the manganese content of said alloy is greater than or equal to 0.1%. 13. The process as claimed claim 4, wherein the manganese content of said alloy is greater than or equal to 0.1%. 14. The process as claimed in claim 5, wherein the manganese content of said alloy is greater than or equal to 0.1%. 15. The process as claimed in claim 3, wherein said alloy has a Curie temperature Tc of between 30 and 350° C., a thermal expansion coefficient αTC between room temperature and Tc of greater than or equal to 6.5×10-6 K-1 and a saturation induction Bs of greater than or equal to 0.2 T and the maximum oxidation current Imax of said alloy in a voltage-current corrosion test in acid medium is less than 1 mA. 16. The process as claimed in claim 15, wherein the thermal expansion coefficient αTC between room temperature and Tc of said alloy is greater than or equal to 9 ×10-6 K-1 and the saturation induction Bc is greater than or equal to 0.5 T. 17. The process as claimed in claim 4, wherein said alloy has a Curie temperature Tcof between 30 and 350° C., a thermal expansion coefficient αTC between room temperature and Tc of greater than or equal to 6.5×10-6 K-1 and a saturation induction Bs of greater than or equal to 0.2 T and the maximum oxidation current Imax of said alloy in a voltage-current corrosion test in acid medium is less than 1 mA. 18. The process as claimed in claim 17, wherein the thermal expansion coefficient αTC between room temperature and Tc of said alloy is greater than or equal to 9×10-6 K-1 and the saturation induction Bs is greater than or equal to 0.5 T. 19. The process as claimed in claim 5, wherein said alloy has a Curie temperature Tc of between 30 and 350° C., a thermal expansion coefficient αTC between room temperature and Tc of greater than or equal to 6.5×10-6 K-1 and a saturation induction Bs of greater than or equal to 0.2 T and the maximum oxidation current Imax of said alloy in a voltage-current corrosion test in acid medium is less than 1 mA. 20. The process as claimed in claim 19, wherein the thermal expansion coefficient αTC between room temperature and Tc of said alloy is greater than or equal to 9×10-6 K-1 and the saturation induction Bs is greater than or equal to 0.5 T. 21. The process as claimed in claim 6, wherein said alloy has a Curie temperature Tc of between 30 and 350° C., a thermal expansion coefficient αTC between room temperature and Tc of greater than or equal to 6.5×10-6 K-1 and a saturation induction Bs of greater than or equal to 0.2 T and the maximum oxidation current Imax of said alloy in a voltage-current corrosion test in acid medium is less than 1 mA. 22. The process as claimed in claim 21, wherein the thermal expansion coefficient αTC between room temperature and Tc of said alloy is greater than or equal to 9×10-6 K-1 and the saturation induction Bs is greater than or equal to 0.5 T. 23. The process as claimed in claim 9, wherein the chemical composition further comprises one or more elements selected from the group consisting of Mo, V, Co, Cu, Si, W, Nb and Al, the sum of the contents of these elements being less than or equal to 10%. 24. A heating element for cooking vessels for induction cooking comprising: a ferromagnetic alloy having a chemical composition comprising, in percent by weight: 32.5%≦Ni≦72.5%; 7.4%≦Cr≦18% 0.01%≦Mn≦4%; C≦1%; 0≦Cu≦0.01; and the balance being iron and impurities resulting from the smelting, wherein the chemical composition further satisfies the following relationships: Cr-1.1Ni+23.25≦0%; 45Cr+11Ni≦1360; Ni+3Cr≧60% if Ni≧37.5; and Cr≧7.5 if Ni≦37.5 wherein the heating element has a side wall. 25. The heating element as claimed in claim 24, wherein the chromium content of said alloy is greater than 13%. 26. The heating element as claimed in claim 24 or 25, wherein the nickel content of said alloy is between 34 and 50% and that the alloy does not contain Mo, V, Co, Cu, Si, W, Nb and Al. 27. The heating element as claimed in claim 24 or 25, wherein the nickel content of said alloy is greater than 52%. 28. The heating element as claimed in claim 24, wherein the nickel content of said alloy is between 48 and 52% a and the chromium content is between 7.4 and 10%. 29. The heating element as claimed in claims 24 or 25, wherein the manganese content of said alloy is greater than or equal to 0.1%. 30. The heating element as claimed in claim 24 or 25, wherein said alloy has a Curie temperature Tc of between 30 and 350° C., a thermal expansion coefficient αTC between room temperature and Tc of greater than or equal to 6.5×10-6 K-1 and a saturation induction Bs of greater than or equal to 0.2 T and the maximum oxidation current Imax of said alloy in a voltage-current corrosion test in acid medium is less than 1 mA. 31. The heating element as claimed in claim 30, wherein the thermal expansion coefficient αTC between room temperature and Tc of said alloy is greater than or equal to 9×10-6 K-1 and the saturation induction Bs is greater than or equal to 0.5 T. 32. A heating element for producing bottoms of monolayer cooking vessels intended for induction cooking comprising, a monolayer of a ferromagnetic alloy having a chemical composition comprising, in percent by weight: 32.5%≦Ni≦72.5%; 13%≦Cr≦18% 0.01%≦Mn≦4%; C≦1%; the balance being iron and impurities resulting from smelting, wherein the chemical composition further satisfies the following relationships: Cr-1.1Ni+23.25≦0%; 45Cr+11Ni≦1360; Ni+3Cr≧60% if Ni≧37.5; and Cr≧7.5 if Ni≦37.5 wherein the heating element has a side wall. 33. The heating element as claimed in claim 24, wherein the chemical composition further comprises one or more elements selected from the group consisting of Mo, V. Co, Cu, Si, W, Nb and Al, the sum of the contents of these elements being less than or equal to 10%. 34. The heating element as claimed in claim 24, wherein the chemical composition does not contain any Mo, V, Co, Cu, Si, W, Nb and Al. 35. The heating element as claimed in claim 26, wherein the manganese content of said alloy is greater than or equal to 0.1%. 36. The heating element as claimed claim 27, wherein the manganese content of said alloy is greater than or equal to 0.1%. 37. The heating element as claimed in claim 28, wherein the manganese content of said alloy is greater than or equal to 0.1%. 38. The heating element as claimed in claim 26, wherein said alloy has a Curie temperature Tc of between 30 and 350° C., a thermal expansion coefficient αTC between room temperature and Tc of greater than or equal to 6.5×10-6 K-1 and a saturation induction Bs of greater than or equal to 0.2 T and the maximum oxidation current Imax of said alloy in a voltage-current corrosion test in acid medium is less than 1 mA. 39. The heating element as claimed in claim 38, wherein the thermal expansion coefficient αTC between room temperature and Tc of said alloy is greater than or equal to 9×10-6 K-1 and the saturation induction Bs is greater than or equal to 0.5 T. 40. The heating element as claimed in claim 27, wherein said alloy has a Curie temperature Tc of between 30 and 350° C., a thermal expansion coefficient αTC between room temperature and Tc of greater than or equal to 6.5×10-6 K-1 and a saturation induction Bs of greater than or equal to 0.2 T and the maximum oxidation current Imax of said alloy in a voltage-current corrosion test in acid medium is less than 1 mA. 41. The heating element as claimed in claim 40, wherein the thermal expansion coefficient αTC between room temperature and Tc of said alloy is greater than or equal to 9×10-6 K-1 and the saturation induction Bs is greater than or equal to 0.5 T. 42. The heating element as claimed in claim 28, wherein said alloy has a Curie temperature Tc of between 30 and 350° C., a thermal expansion coefficient αTC between room temperature and Tc of greater than or equal to 6.5×10-6 K-1 and a saturation induction Bs of greater than or equal to 0.2 T and the maximum oxidation current Imax of said alloy in a voltage-current corrosion test in acid medium is less than 1 mA. 43. The heating element as claimed in claim 42, wherein the thermal expansion coefficient αTC between room temperature and Tc of said alloy is greater than or equal to 9×10-6 K-1 and the saturation induction Bs is greater than or equal to 0.5 T. 44. The heating element as claimed in claim 29, wherein said alloy has a Curie temperature Tc of between 30 and 350° C., a thermal expansion coefficient αTC between room temperature and Tc of greater than or equal to 6.5×10-6 K-1 and a saturation induction Bs of greater than or equal to 0.2 T and the maximum oxidation current Imax of said alloy in a voltage-current corrosion test in acid medium is less than 1 mA. 45. The heating element as claimed in claim 44, wherein the thermal expansion coefficient αTC between room temperature and Tc of said alloy is greater than or equal to 9×10-6 K-1 and the saturation induction Bs is greater than or equal to 0.5 T. 46. The heating element as claimed in claim 32, wherein the chemical composition further comprises one or more elements selected from the group consisting of Mo, V, Co, Cu, Si, W, Nb and Al, the sum of the contents of these elements being less than or equal to 10%.
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