IRON ALLOYS

Abstract

The present disclosure relates generally to alloys, and in particular, to iron alloys.

Claims

1. An alloy comprising or consisting of: 35 to 70 at. % Fe; 10 to 50 at. % Cr; 1 to 25 at. % Mn; and 1 to 10 at. % Al.

2. The alloy of claim 1 comprising or consisting of: 37.5 to 67.5 at. % Fe; 12.5 to 47.5 at. % Cr; 2.5 to 25 at. % Mn; and 2.5 to 7.5 at. % Al.

3. The alloy of claim 1 comprising or consisting of: 40 to 65 at. % Fe; 15 to 45 at. % Cr; 5 to 25 at. % Mn; and 2.5 to 7.5 at. % Al.

4. The alloy of claim 1 comprising or consisting of: 40 to 65 at. % Fe; 15 to 45 at. % Cr; 5 to 25 at. % Mn; and 4 to 6 at. % Al.

5. The alloy of claim 1 comprising or consisting of: 40 to 65 at. % Fe; 15 to 45 at. % Cr; 5 to 20 at. % Mn; and 2.5 to 7.5 at. % Al.

6. The alloy of claim 1 comprising or consisting of: 40 to 65 at. % Fe; 15 to 45 at. % Cr; 5 to 20 at. % Mn; and 4 to 6 at. % Al.

7. The alloy of claim 1 comprising or consisting of: 40 to 65 at. % Fe; 15 to 45 at. % Cr; 5 to 25 at. % Mn; and 5 at. % Al.

8. The alloy of claim 1 comprising or consisting of: 40 to 65 at. % Fe; 15 to 45 at. % Cr; 5 to 20 at. % Mn; and 5 at. % Al.

9. The alloy of claim 1 comprising or consisting of: 45 to 65 at. % Fe; 25 to 45 at. % Cr; 2.5 to 7.5 at. % Mn; and 2.5 to 7.5 at. % Al.

10. The alloy of claim 9 comprising or consisting of: 45 to 60 at. % Fe; 25 to 45 at. % Cr, 2.5 to 7.5 at. % Mn; and 5 at. % Al.

11. The alloy of claim 9 or claim 10 comprising or consisting of: 45 to 60 at. % Fe; 25 to 45 at. % Cr; 5 at. % Mn; and 5 at. % Al.

12. The alloy of claim 1 comprising or consisting of: 45 to 65 at. % Fe; 20 to 40 at. % Cr; 7.5 to 12.5 at. % Mn; and 2.5 to 7.5 at. % Al.

13. The alloy of claim 12 comprising or consisting of: 45 to 65 at. % Fe; 20 to 40 at. % Cr; 7.5 to 12.5 at. % Mn; and 5 at. % Al.

14. The alloy of claim 12 or claim 13 comprising or consisting of: 45 to 65 at. % Fe; 20 to 40 at. % Cr; 10 at. % Mn; and 5 at. % Al.

15. The alloy of claim 1 comprising or consisting of: 40 to 65 at. % Fe; 15 to 40 at. % Cr; 12.5 to 17.5 at. % Mn; and 2.5 to 7.5 at. % Al.

16. The alloy of claim 15 comprising or consisting of: 40 to 65 at. % Fe; 15 to 40 at. % Cr; 12.5 to 17.5 at. % Mn; and 5 at. % Al.

17. The alloy of claim 15 or claim 16 comprising or consisting of: 40 to 65 at. % Fe; 15 to 40 at. % Cr; 15 at. % Mn; and 5 at. % Al.

18. The alloy of claim 1 comprising or consisting of: 40 to 60 at. % Fe; 15 to 35 at. % Cr; 17.5 to 22.5 at. % Mn; and 2.5 to 7.5 at. % Al.

19. The alloy of claim 18 comprising or consisting of: 40 to 60 at. % Fe; 15 to 35 at. % Cr; 17.5 to 22.5 at. % Mn; and 5 at. % Al.

20. The alloy of claim 18 or claim 19 comprising or consisting of: 40 to 60 at. % Fe; 15 to 35 at. % Cr; 20 at. % Mn; and 5 at. % Al.

21. The alloy of any one of the preceding claims wherein the alloy consists of 90 to 97.5 at. % [Fe+Cr+Mn] and a balance of Al.

22. The alloy of any one of the preceding claims wherein the alloy consists of 90 to 95 at. % [Fe+Cr+Mn] and a balance of Al.

23. The alloy of any one of the preceding claims wherein the alloy consists of 95 at. % [Fe+Cr+Mn] and 5 at. % Al.

24. The alloy of any one of the preceding claims wherein the alloy consists of: 75 to 90 at. % [Fe+Cr]; 5 to 20 at. % Mn; and a balance of Al.

25. The alloy of any one of the preceding claims wherein the alloy consists of: 75 to 90 at. % [Fe+Cr]; 5 to 20 at. % Mn; and 5 at. % Al.

26. The alloy of any one of the preceding claims wherein the alloy consists of: 10 to 30 at. % [Mn+Al]; 15 to 45 at. % Cr; and a balance of Fe.

27. The alloy of any one of the preceding claims wherein the alloy consists of: 10 to 25 at. % [Mn+Al]; 15 to 45 at. % Cr; and a balance of Fe.

28. An alloy comprising or consisting of: 35 to 70 at. % Fe; 10 to 50 at. % Cr, 1 to 25 at. % Mn; 1 to 10 at. % Al; and 0 to 3 at. % [Ti+Nb+V+W+Zr+Hf+B+Ta+Mo].

29. The alloy of claim 28 comprising or consisting of: 35 to 70 at. % Fe; 10 to 50 at. % Cr; 1 to 25 at. % Mn; 1 to 10 at. % Al; and up to 3 at. % [Ti+Nb+V+W+Zr+Hf+B+Ta+Mo].

30. The alloy of claim 28 comprising or consisting of: 37.5 to 67.5 at. % Fe; 12.5 to 47.5 at. % Cr; 2.5 to 25 at. % Mn; 2.5 to 7.5 at. % Al; and up to 2 at. % [Ti+Nb+V+W+Zr+Hf+B+Ta+Mo].

31. The alloy of claim 28 comprising or consisting of: 40 to 65 at. % Fe; 15 to 45 at. % Cr; 5 to 20 at. % Mn; 2.5 to 7.5 at. % Al; and up to 2 at. % [Ti+Nb+V+W+Zr+Hf+B+Ta+Mo].

32. The alloy of claim 28 comprising or consisting of: 40 to 65 at. % Fe; 15 to 45 at. % Cr; 5 to 20 at. % Mn; 5 at. % Al; and up to 2 at. % [Ti+Nb+V+W+Zr+Hf+B+Ta+Mo].

33. The alloy of claim 28 comprising or consisting of: 40 to 65 at. % Fe; 15 to 45 at. % Cr; 5 to 20 at. % Mn; 2.5 to 7.5 at. % Al; and up to 1 at. % [Ti+Nb+V+W+Zr+Hf+B+Ta+Mo].

34. The alloy of claim 28 comprising or consisting of: 40 to 65 at. % Fe; 15 to 45 at. % Cr; 5 to 20 at. % Mn; 5 at. % Al; and up to 1 at. % [Ti+Nb+V+W+Zr+Hf+B+Mo].

35. The alloy of any one of the preceding claims wherein the alloy comprises at least 15 at. % Cr.

36. The alloy of any one of the preceding claims wherein the alloy comprises at least 40% at. % Fe.

37. The alloy of any one of the preceding claims wherein the at. % ratio of Mn:Al is at least 1.

38. The alloy of any one of the preceding claims wherein the at. % ratio of Fe:Cr is at least 1.

39. The alloy of any one of the preceding claims wherein the at. % ratio of Fe:Mn is at least 2.

40. The alloy of any one of the preceding claims wherein the alloy has an ultimate tensile strength of between about 500 and 900 MPa.

41. The alloy of any one of the preceding claims wherein the alloy has a 0.2%-offset yield strength of between about 400 and 900 MPa.

42. The alloy of any one of the preceding claims wherein the alloy has an as-cast hardness (HV) of between about 175 and 280.

43. The alloy of any one of the preceding claims wherein the alloy has an as-cast hardness (HV) of between about 183 and 272.

44. The alloy of any one of the preceding claims wherein the alloy has a density of between about 6.9 and 7.38 g/cm.sup.3.

45. The alloy of any one of the preceding claims wherein the alloy has a density of between about 7.19 and 7.38 g/cm.sup.3.

46. The alloy of any one of the preceding claims wherein the alloy has a single phase body-centred cubic (bcc) crystal structure.

47. The alloy of any one of claims 1 to 45 wherein the alloy has two phases with a bcc crystal structure.

48. The alloy of any one of claims 1 to 45 wherein the alloy comprises at least about 90 vol. % bcc crystal structure.

49. The alloy of any one of the preceding claims wherein the alloy comprises 0 to 1 at. % incidental impurities.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0056] FIG. 1: Tensile properties of alloys of the present disclosure. *indicates an addition of 0.2 at. % Ti to the overall alloy composition e.g. [Fe.sub.65Cr.sub.25Mn.sub.5Al.sub.5].sub.99.8Ti.sub.0.2. **indicates an addition of 0.2 at. % Ti and 0.2 at. % Nb to the overall alloy composition e.g. [Fe.sub.65Cr.sub.25Mn.sub.5Al.sub.5].sub.99.6Ti.sub.0.2Nb.sub.0.2.

[0057] FIG. 2: X-ray diffraction trace showing the bcc structure of an alloy after solution treatment at 850? C., and a week of heat treatment at 400? C. then quenching.

DETAILED DESCRIPTION

[0058] The term about is understood to refer to a range of +/?10%, preferably +/?5% or +/?1% or, more preferably, +/?0.1%.

[0059] Throughout this specification, unless the context requires otherwise, the word comprise, or variations such as comprises or comprising will be understood to imply the inclusion of a stated element, integer or step, or group of elements, integers or steps, but not the exclusion of any other element, integer or step, or group of elements, integers or steps. Thus, in the context of this specification, the term comprising means including principally, but not necessarily solely.

[0060] Any numerical range recited herein is intended to include all sub-ranges of the same numerical precision subsumed within the recited range. For example, a range of 1.0 to 5.0 is intended to include all sub-ranges between (and including) the recited minimum value of 1.0 and the recited maximum value of 5.0, that is, having a minimum value equal to or greater than 1.0 and a maximum value equal to or less than 5.0, such as 2.1 to 4.5. Any maximum numerical limitation recited herein is intended to include all lower numerical limitations subsumed therein and any minimum numerical limitation recited herein is intended to include all higher numerical limitations subsumed therein.

[0061] The present disclosure provides alloys comprising or consisting of: 35 to 70 at. % Fe; 10 to 50 at. % Cr; 1 to 25 at. % Mn; and 1 to 10 at. % Al. It will be understood that the alloys described herein may comprise incidental impurities. Those skilled in the art will understand, for example, that carbon impurities may arise from iron smelting and raw materials, and that nitrogen impurities may arise from atmospheric nitrogen during melt processing. Nickel may also arise as an unavoidable impurity due to the recycling loop of stainless steels. Incidental silicon impurities may arise from scrap metal refinement loops. Cobalt is another potentially unavoidable impurity. Preferably, the incidental impurities do not exceed 1 at. %, or 0.5 at. %, or preferably, 0.1 at. %, or more preferably, 0.05 at. %.

[0062] In some examples, the present disclosure provides an alloy comprising or consisting of: 35 to 70 at. % Fe; 10 to 50 at. % Cr; 1 to 25% Mn; and 1 to 10 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 40 to 70 at. % Fe; 15 to 50 at. % Cr; 1 to 25 at. % Mn; and 1 to 10 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 40 to 65 at. % Fe; 15 to 55 at. % Cr 1 to 25 at. % Mn; and 1 to 10 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 40 to 65 at. % Fe; 15 to 55 at. % Cr; 2 to 25 at. % Mn; and 2 to 10 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 40 to 65 at. % Fe; 15 to 55 at. % Cr; 5 to 25 at. % Mn; and 2 to 10 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 40 to 65 at. % Fe; 15 to 55 at. % Cr; 5 to 20 at. % Mn; and 2 to 10 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 40 to 65 at. % Fe; 15 to 55 at. % Cr; 5 to 20 at. % Mn; and 4 to 10 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 40 to 65 at. % Fe; 15 to 55 at. % Cr; 5 to 20 at. % Mn; and 4 to 8 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 40 to 65 at % Fe; 15 to 55 at. % Cr; 5 to 20 at. % Mn; and 5 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 35 to 65 at. % Fe; 20 to 55 at. % Cr; 1 to 25 at. % Mn; and 1 to 10 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 35 to 65 at. % Fe; 20 to 55 at. % Cr; 5 to 25 at. % Mn; and 1 to 10 at % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 35 to 65 at. % Fe; 20 to 55 at. % Cr; 5 to 25 at. % Mn; and 4 to 6 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 40 to 65 at. % Fe; 20 to 50 at. % Cr; 5 to 20 at. % Mn; and 4 to 6 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 40 to 70 at. % Fe; 15 to 50 at. % Cr 1 to 25 at. % Mn; and 5 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 40 to 65 at. % Fe; 15 to 55 at. % Cr; 5 to 20 at. % Mn; and 5 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 35 to 65 at % Fe; 20 to 55 at. % Cr, 5 to 25 at. % Mn; and 5 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 40 to 65 at. % Fe; 15 to 55 at. % Cr, 5 to 25 at. % Mn; and 4 to 6 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 40 to 65 at. % Fe; 15 to 55 at. % Cr; 5 to 22.5 at. % Mn; and 4 to 6 at. % Al. In some examples, the alloy of the present disclosure comprises 0 to 1 at. % incidental impurities. The incidental impurities may, for example, be Ni or Co.

[0063] In some examples, the present disclosure provides an alloy having 30 to 75 at. % Fe, such as 35 to 70 at. % Fe, 37 to 67 at. % Fe, 37 to 65 at. % Fe, 37 to 63 at. % Fe, 40 to 60 at. % Fe, 42 to 58 at. % Fe, 45 to 55 at. % Fe, or 47 to 52 at. % Fe. In some examples, the alloy comprises 45 to 50 at. % Fe, such as 50 to 55 at. % Fe, 55 to 60 at % Fe, or 60 to 65 at. % Fe. In some examples, the alloy comprises 40 to 65 at. % Fe, such as 45 to 65 at. % Fe, 50 to 65 at. % Fe, 55 to 65 at. % Fe, or 60 to 65 at. % Fe. In some example, the alloy comprises 40 to 60 at. % Fe, 40 to 55 at. % Fe, 40 to 50 at % Fe, or 40 to 45 at. % Fe.

[0064] In some examples, the Cr content of the presently disclosed alloys is greater than 10 at. %, such as greater than 11 at. %, or great than 12 at. %, greater than 13 at. %, greater than 14 at. %, such as at least 15 at. %, or at least 20 at. %, at least 25 at. %, at least 30 at. %, at least 35 at %, at least 40 at. %, or at least 45 at. %. In some examples, the present disclosure provides an alloy having 10 to 50 at % Cr, such as 12 to 47 at. % Cr, 15 to 45 at. % Cr, 17 to 43 at. % Cr, 20 to 40 at. % Cr, 22 to 38 at. % Cr, 25 to 35 at. % Cr, in 27 to 33 at. % Cr. In some examples, the alloy comprises 15 to 20 at % Cr, such as 20 to 25 at. % Cr, 25 to 30 at. % Cr, 35 to 40 at. % Cr, or 40 to 45 at. % Cr. In some examples, the alloy comprises 15 to 45 at. % Cr, such as 20 to 45 at. % Cr, 25 to 45 at. % Cr, 30 to 45 at % Cr, or 35 to 45 at. % Cr.

[0065] In some examples, the present disclosure provides an alloy having 1 to 25 at. % Mn, such as 2 to 23 at. % Mn, 5 to 20 at. % Mn, 7 to 18 at. % Mn or 10 to 15 at. % Mn. In some examples, the alloy comprises 5 to 20 at % Mn, such as 5 to 15 at. % Mn, or 5 to 10 at. % Mn. In some examples, the alloy comprises 10 to 20 at. % Mn or 15 to 20 at. % Mn.

[0066] In some examples, the present disclosure provides an alloy having 1 to 10 at. % Al, such as 2 to 9 at. % Al, 3 to 8 at. % Al, 4 to 7 at. % Al, 4 to 6 at. % Al, or 5 at. % Al. In some examples, the alloy comprises 1 to 9 at. % Al, 1 to 8 at. % Al, 1 to 7 at % Al, 1 to 6 at % Al, 1 to 5 at. % Al, 1 to 4 at. % Al, or 1 to 3 at. % Al. In some examples, the alloy comprises 2 to 10 at. % Al, 3 to 10 at. % Al, 4 to 10 at. % Al, 5 to 10 at. % Al, 6 to 10 at. % Al, 7 to 10 at. % Al, or 8 to 10 at. % Al.

[0067] In some examples, the present disclosure provides an alloy comprising or consisting of: 65 at. % Fe; 25 at. % Cr; 5 at. % Mn; and 5 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 60 at % Fe; 30 at. % Cr; 5 at. % Mn; and 5 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 55 at. % Fe; 35 at. % Cr; 5 at. % Mn; and 5 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 50 at % Fe; 40 at. % Cr; 5 at. % Mn; and 5 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 45 at. % Fe; 45 at. % Cr; 5 at. % Mn; and 5 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 65 at. % Fe; 20 at. % Cr; 10 at. % Mn; and 5 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 60 at. % Fe; 25 at. % Cr; 10 at. % Mn; and 5 at % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 55 at. % Fe; 30 at. % Cr; 10 at. % Mn; and 5 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 50 at. % Fe; 35 at. % Cr; 10 at. % Mn; and 5 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 45 at. % Fe; 40 at. % Cr; 10 at. % Mn; and 5 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 65 at. % Fe; 15 at. % Cr, 15 at. % Mn; and 5 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 60 at. % Fe; 20 at. % Cr; 15 at. % Mn; and 5 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 55 at. % Fe; 25 at. % Cr; 15 at. % Mn; and 5 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 50 at. % Fe; 30 at. % Cr; 15 at. % Mn; and 5 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 45 at. % Fe; 35 at. % Cr; 15 at. % Mn; and 5 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 40 at. % Fe; 40 at. % Cr; 15 at. % Mn; and 5 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 60 at. % Fe; 15 at. % Cr, 20 at. % Mn; and 5 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 55 at. % Fe; 20 at. % Cr; 20 at. % Mn; and 5 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 50 at. % Fe; 25 at. % Cr; 20 at. % Mn; and 5 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 45 at. % Fe; 30 at. % Cr; 20 at. % Mn; and 5 at. % Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 40 at. % Fe; 35 at. % Cr; 20 at. % Mn; and 5 at. % Al. In some examples, the present disclosure provides an alloy substantially as described in Table 1 or Table 2.

[0068] Elements such as titanium (Ti), niobium (Nb), vanadium (V), tungsten (W), zirconium (Zr), hafnium (Hf), tantalum (Ta) and molybdenum (Mo) may, in some examples, be added to the alloy in order to remove carbon and nitrogen impurities. These elements react with carbon and nitrogen, forming carbides and nitrides respectively, which can then be removed from the alloy, for example, by skimming from its molten surface. Molybdenum may also strengthen the alloy and improve its corrosion resistance. Boron (B) may also be added to remove impurities and/or to increase the grain boundary strength of the alloy. In that regard, the present disclosure provides an alloy comprising or consisting of: 35 to 70 at. % Fe; 10 to 50 at. % Cr; 1 to 25 at. % Mn; 1 to 10 at. % Al; and 0 to 3 at. % [Ti+Nb+V+W+Zr+Hf+Ta+B+Mo]. It will be understood that in such examples, the alloy may comprise any one or more elements selected from the group consisting of Ti, Nb, V, W, Zr, Hf, Ta, B and Mo, as long as the total content of those one or more elements combined does not exceed 3 at. % in the alloy. Preferably the alloy of the present disclosure comprises up to 2.75 at. % [Ti+Nb+V+W+Zr+Hf+Ta+B+Mo], such as up to 2.5 at. % [Ti+Nb+V+W+Zr+Hf+Ta+B+Mo], or up to 2 at. %[Ti+Nb+V+W+Zr+Hf+Ta+B+Mo], up to 1.75 at. %[Ti+Nb+V+W+Zr+Hf+Ta+B+Mo], up to 1.5 at. %[Ti+Nb+V+W+Zr+Hf+Ta+B+Mo], up to 1.25 at. %[Ti+Nb+V+W+Zr+Hf+Ta+B+Mo], up to 1 at. %[Ti+Nb+V+W+Zr+Hf+Ta+B+Mo], up to 0.75 at. %[Ti+Nb+V+W+Zr+Hf+Ta+B+Mo], up to 0.5 at. % [Ti+Nb+V+W+Zr+Hf+Ta+B+Mo] or up to 0.25 at. % [Ti+Nb+V+W+Zr+Hf+Ta+B+Mo].

[0069] In some examples, the present disclosure provides an alloy comprising or consisting of: 35 to 70 at. % Fe; 10 to 50 at. % Cr; 1 to 25 at. % Mn; 1 to 10 at. % Al; and up to 3 at. % [Ti+Nb+V+W+Zr+Hf+Ta+Mo]. In some examples, the present disclosure provides an alloy comprising or consisting of: 35 to 70 at. % Fe; 10 to 50 at. % Cr; 1 to 25 at. % Mn; 1 to 10 at. % Al; and up to 3 at. % [Ti+Nb+V+W+Zr+Hf+Ta+B+Mo]. In some examples, the present disclosure provides an alloy comprising or consisting of: 35 to 70 at. % Fe; 10 to 50 at. % Cr; 1 to 25 at. % Mn; 1 to 10 at. % Al; and up to 2 at. % [Ti+Nb+V+W+Zr+Hf+Ta+B+Mo]. In some examples, the present disclosure provides an alloy comprising or consisting of: 35 to 65 at. % Fe; 15 to 50 at. % Cr; 5 to 25 at. % Mn; 2.5 to 7.5 at. % Al; and up to 2 at. % [Ti+Nb+V+W+Zr+Hf+Ta+B+Mo]. In some examples, the present disclosure provides an alloy comprising or consisting of: 35 to 65 at. % Fe; 15 to 50 at. % Cr; 5 to 25 at. % Mn; 2.5 to 7.5 at. % Al; and up to 1 at. % [Ti+Nb+V+W+Zr+Hf+Ta+B+Mo]. In some examples, the present disclosure provides an alloy comprising or consisting of: 35 to 65 at. % Fe; 15 to 50 at. % Cr; 5 to 25 at. % Mn; 5 at. % Al; and up to 2 at. % [Ti+Nb+V+W+Zr+Hf+Ta+B+Mo]. In some examples, the present disclosure provides an alloy comprising or consisting of: 35 to 65 at. % Fe; 15 to 50 at. % Cr; 5 to 25 at. % Mn; 2.5 to 7.5 at. % Al; and up to 2 at. % [Ti+Nb+V+W+Zr+Hf+B+Ta]. In some examples, the present disclosure provides an alloy comprising or consisting of: 35 to 65 at. % Fe; 15 to 50 at. % Cr; 5 to 25 at. % Mn; 2.5 to 7.5 at. % Al; and up to 3 at. % Mo. In some examples, the present disclosure provides an alloy comprising or consisting of: 35 to 70 at. % Fe; 10 to 50 at. % Cr; 1 to 25 at. % Mn; 1 to 10 at. % Al; and up to 0.2 at. % Ti. In some examples, the present disclosure provides an alloy comprising or consisting of: 35 to 70 at. % Fe; 10 to 50 at. % Cr; 1 to 25 at. % Mn; 1 to 10 at. % Al; and up to 0.4 at. % [Ti+Nb]. In some examples, the present disclosure provides an alloy comprising or consisting of: 40 to 65 at. % Fe; 15 to 45 at. % Cr; 5 to 25 at. % Mn; 2.5 to 7.5 at. % Al; and up to 0.2 at. % Ti. In some examples, the present disclosure provides an alloy comprising or consisting of: 40 to 65 at. % Fe; 15 to 45 at. % Cr; 5 to 20 at. % Mn; 2.5 to 7.5 at. % Al; and up to 0.4 at. % [Ti+Nb]. In some examples, the present disclosure provides an alloy comprising or consisting of: 40 to 65 at. % Fe; 15 to 45 at. % Cr; 5 to 20 at. % Mn; 2.5 to 7.5 at. % Al; up to 0.2 at. % Ti; and up to 0.2 at. % Nb. In some examples, the present disclosure provides an alloy comprising or consisting of: 35 to 65 at. % Fe; 15 to 50 at. % Cr; 5 to 25 at. % Mn; 2.5 to 7.5 at. % Al; and up to 1 at. % [Ti+Nb+V+W+Zr+Hf+B+Mo]. In some examples, the present disclosure provides an alloy comprising or consisting of: 35 to 65 at. % Fe; 15 to 50 at. % Cr; 5 to 25 at. % Mn; 5 at. % Al; and up to 2 at. % [Ti+Nb+V+W+Zr+Hf+B+Mo].

[0070] In known ferritic steels, Fe and Cr can, in some instances, stabilise the sigma phase (?Fe.sub.50Cr.sub.50) which is detrimental to both corrosion resistance and mechanical performance with respect to ductility and toughness. Moreover, at temperatures below about 500? C., the atomic bonding between Fe and Cr in FeCr bcc (ferritic) alloys becomes repulsive, leading to FeCr segregation and the formation of an Fe- and Cr-rich two phase alloy in a process commonly referred to as ?+? phase separation. This can lead to detrimental embrittlement, sometimes called 475? C. embrittlement or simply 475 embrittlement. The alloys of the present disclosure comprise specific combinations of Mn and Al, which largely destabilise or eradicate the detrimental sigma phase that exists in known ferritic stainless steels. The alloys may therefore be particularly useful in medium- to high-temperature applications (eg, >500? C.), and more amenable to economical thermomechanical processing routes and welding processes. Moreover, a higher Mn content may reduce the extent and tendency of phase separation and subsequent embrittlement to a point where this effect is largely eradicated or negligible at moderate temperatures (eg, 200 to 500? C.) for extended time in service. In that regard, the alloy of the present disclosure is preferably a single phase alloy. In some examples, the alloy of the present disclosure comprises a bcc crystal structure. In some examples, the alloy of the present disclosure has a substantially single phase bcc crystal structure, excepting for incidental impurities. In some examples, the alloy of the present disclosure comprises at least about 75 vol. % bcc crystal structure, such as at least about 80 vol. % bcc crystal structure, or at least about 85 vol. % bcc crystal structure, at least about 90 vol. % bcc crystal structure, at least about 95 vol. % bcc crystal structure, at least about 96 vol. % bcc crystal structure, at least about 97 vol. % bcc crystal structure, at least about 98 vol. % bcc crystal structure, or at least about 99 vol. % bcc crystal structure. In some examples, the alloy of the present disclosure has a single phase bcc crystal structure. In some examples, the alloy of the present disclosure has two phases with a bcc crystal structure.

[0071] The present disclosure provides alloys comprising or consisting of: 5 to 30 at. % [Mn+Al]; 10 to 50 at. % Cr; and a balance of Fe. In some examples, the present disclosure provides an alloy comprising or consisting of: 10 to 25 at. % [Mn+Al]; 15 to 45 at. % Cr; and a balance of Fe. In some examples, the present disclosure provides an alloy comprising or consisting of: 10 to 15 at. % [Mn+Al]; 20 to 45 at. % Cr; and a balance of Fe. In some examples, the present disclosure provides an alloy comprising or consisting of: 20 to 25 at. % [Mn+Al]; 15 to 40 at. % Cr; and a balance of Fe. In some examples, the present disclosure provides an alloy comprising or consisting of: 10 to 25 at. % [Mn+Al]; 15 to 45 at. % Cr; and a balance of Fe, wherein the at. % ratio of Mn:Al is at least about 1. In some examples, the present disclosure provides an alloy comprising or consisting of: 10 to 25 at. % [Mn+Al]; 15 to 45 at. % Cr; and a balance of Fe, wherein the at. % ratio of Mn:Al is at least about 1, and wherein the at. % ratio of Fe:Cr is at least about 1. In some examples, the present disclosure provides an alloy comprising or consisting of: 10 to 25 at. % [Mn+Al]; 15 to 45 at. % Cr, and a balance of Fe, wherein the at. % ratio of Mn:Al is at least about 1, and wherein the alloy comprises at least 40 at. % Fe. In some examples, the present disclosure provides an alloy comprising or consisting of: 10 to 25 at. % [Mn+Al]; 15 to 45 at. % Cr; and a balance of Fe, wherein the at. % ratio of Fe:Cr is at least about 1, and wherein the alloy comprises at least 40 at. % Fe.

[0072] The alloys of the present disclosure preferably do not exhibit sigma transformation. It will be appreciated by those skilled in the art that, in the absence of the sigma phase and the minimisation of phase separation, the Cr-content in the presently described alloys may be higher compared to known stainless steels, thereby providing extended corrosion resistance without substantially degrading mechanical performance.

[0073] In some examples, the present disclosure provides an alloy comprising or consisting of: 70 to 95 at. % [Fe+Cr]; 2 to 25 at. % Mn; and a balance of Al. In such examples, Fe and Cr may be present in the alloy at any amount as long as their combined content is at least 70 at. % and no greater than 95 at. %. In some examples, the present disclosure provides an alloy comprising or consisting of: 75 to 95 at. % [Fe+Cr]; 2 to 20 at. % Mn; and a balance of Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 70 to 90 at. % [Fe+Cr]; 5 to 25 at. % Mn; and a balance of Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 75 to 90 at. % [Fe+Cr]; 5 to 20 at. % Mn; and a balance of Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 80 to 90 at. % [Fe+Cr]; 5 to 15 at. % Mn; and a balance of Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 75 to 90 at. % [Fe+Cr]; 5 to 25 at. % Mn; and a balance of Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 75 to 90 at. % [Fe+Cr]; 5 to 22 at. % Mn; and a balance of Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 70 to 95 at. % [Fe+Cr]; 2 to 25 at. % Mn; and a balance of Al, wherein the alloy comprises at least 15 at. % Cr. In some examples, the present disclosure provides an alloy comprising or consisting of: 70 to 90 at. % [Fe+Cr]; 5 to 25 at. % Mn; and a balance of Al, wherein the alloy comprises at least 15 at. % Cr. In some examples, the present disclosure provides an alloy comprising or consisting of: 80 to 90 at. % [Fe+Cr]; 5 to 15 at. % Mn; and a balance of Al, wherein the alloy comprises at least 15 at. % Cr. In some examples, the present disclosure provides an alloy comprising or consisting of: 75 to 90 at. % [Fe+Cr]; 5 to 20 at. % Mn; and a balance of Al, wherein the at. % ratio of Fe:Cr is at least 1. In some examples, the present disclosure provides an alloy comprising or consisting of: 75 to 90 at. % [Fe+Cr]; 5 to 20 at. % Mn; and a balance of Al, wherein the at. % ratio of Fe:Cr is at least 1, and wherein the alloy comprises at least 40 at. % Fe. 1. In some examples, the present disclosure provides an alloy comprising or consisting of: 75 to 90 at. % [Fe+Cr]; 5 to 20 at. % Mn; and a balance of Al, wherein the at. % ratio of Mn:Al is at least 1, and wherein the alloy comprises at least 40 at. % Fe.

[0074] In some examples, the present disclosure provides an alloy comprising or consisting of: 80 to 98 at. % [Fe+Cr+Mn] and a balance of AI. In some examples, the present disclosure provides an alloy comprising or consisting of: 80 to 95 at. % [Fe+Cr+Mn] and a balance of Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 85 to 95 at. % [Fe+Cr+Mn] and a balance of Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 90 to 95 at. % [Fe+Cr+Mn] and a balance of Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 90 to 98 at. % [Fe+Cr+Mn] and a balance of Al. In some examples, the present disclosure provides an alloy comprising or consisting of: 80 to 98 at. % [Fe+Cr+Mn] and a balance of Al, wherein the alloy comprises at least 15 at. % Cr. In some examples, the present disclosure provides an alloy comprising or consisting of: 85 to 95 at. % [Fe+Cr+Mn] and a balance of Al, wherein the alloy comprises at least 15 at. % Cr. In some examples, the present disclosure provides an alloy comprising or consisting of: 90 to 98 at. % [Fe+Cr+Mn] and a balance of Al, wherein the alloy comprises at least 15 at. % Cr.

[0075] In some the examples, the present disclosure provides an alloy having an at. % ratio of Mn:Al of at least about 1. In some examples, the at. % ratio of Mn:Al is at least about 1.1, such as at least about 1.25, or at least about 1.5, or at least about 1.75, or at least about 2, or at least about 2.25, or at least about 2.5, or at least about 2.75, or at least about 3, or at least about 3.25, or at least about 3.5, or at least about 3.75, or at least about 4. In some examples, the at. % ratio of Mn:Al is between about 1 and 5, such as between about 1 and 4.5 or between about 1 and 4.

[0076] In some the examples, the present disclosure provides an alloy having an at. % ratio of Fe:Cr of at least about 1. In some examples, the at. % ratio of Fe:Cr is at least about 1.1, such as at least about 1.25, or at least about 1.5, or at least about 1.75, or at least about 2, or at least about 2.25, or at least about 2.5, or at least about 2.75, or at least about 3, or at least about 3.25, or at least about 3.5, or at least about 3.75, or at least about 4, such as at least about 4.25. In some examples, the at. % ratio of Fe:Cr is between about 1 and 5, such as between about 1.23 and 5, or between about 1.25 and 4.75, or between about 1.5 and 4.75, or between about 1.5 and 4.5, or between about 1.5 and 4.3.

[0077] In some the examples, the present disclosure provides an alloy having an at. % ratio of Fe:Mn of at least about 1.5, such as at least about 1.75, or at least about 2, at least about 2.5, at least about 3, at least about 3.3, at least about 3.6, at least about 4, at least about 4.5, at least about 5, at least about 5.5, at least about 6, at least about 6.5, at least about 7, at least about 8, at least about 8.5, at least about 9, at least about 9.5, at least about 10, at least about 10.5, at least about 11, at least about 11.5, at least about 12, at least about 12.5, or at least about 13. In some examples, the at. % ratio of Fe:Mn is between about 1.5 and 14, or between about 2 and 13, between about 2.25 and 13, between about 2.5 and 13, between about 2.5 and 12, between about 2.75 and 13, between about 2.75 and 12, between about 2.6 and 13, or between about 2.75 and 11.

[0078] In some examples, the present disclosure provides an alloy having an ultimate tensile strength of between about 300 and 1,000 MPa, such as between about 400 and 1,000 MPa, or between about 450 and 1,000 MPa, between about 500 and 1,000 MPa, between about 500 and 950 MPa, between about 500 and 900 MPa, between about 510 and 880 MPa, between about 510 and 865 MPa, between about 520 and 865 MPa, or between about 538 and 865 MPa. The strength of the alloy may be increased by increasing Cr and Mn content.

[0079] In some examples, the present disclosure provides an alloy having a 0.2%-offset yield strength of between about 300 and 1,000 MPa, such as between about 400 and 1,000 MPa, or between about 400 and 950 MPa, between about 425 and 900 MPa, or between about 425 and 850 MPa.

[0080] In some examples, the present disclosure provides an alloy having a hardness (HV) (solution treated at 850? C.) of between about 165 and 300, such as between about 165 and 295, or between about 175 and 295, between about 180 and 295, between about 180 and 290, between about 180 and 285, between about 180 and 280, between about 180 and 276, between about 182 and 276, between about 185 and 276, between about 188 and 276, between about 193 and 276, between about 196 and 276, between about 203 and 276 or between about 204 and 276. Preferably, the alloy has a hardness (solution treated at 850? C.) of between 180 and 276.

[0081] In some examples, the present disclosure provides an alloy having an as-cast hardness (HV) of between about 200 and about 272, or between about 210 and about 260, or between about 220 and about 240, or between about 220 and about 270, or between about 220 and about 260, or between about 220 and about 250, or between about 183 and about 272, or between about 183 and about 250, or between about 183 and about 240, or between about 190 and about 230. Preferably, the alloy has an as-cast hardness of between about 183 and about 272.

[0082] The alloys of the present disclosure may have a density which is lower than that of 200, 300 and 400 series stainless steels. As such, they may produce lighter weight materials, and from a production/cost standpoint, they may provide more material volume per kilogram, or inversely, may be lighter per unit length of product. In some examples, the present disclosure provides an alloy having a density of between about 6.9 and about 7.38 g/cm.sup.3, or between about 7.0 and about 7.38 g/cm.sup.3, or between about 7.05 and about 7.36 g/cm.sup.3, or between about 7.1 and about 7.36 g/cm.sup.3, or between about 7.15 and about 7.35 g/cm.sup.3, or between about 7.22 and about 7.35 g/cm.sup.3 Preferably, the alloy has a density of between about 7.19 and 7.38 g/cm.sup.3.

[0083] The alloys described herein maintain a bcc crystal structure, and may exhibit similar processing advantages to stainless steels as well as high corrosion resistance, particularly with higher chromium contents. In some examples, the alloys of the present disclosure have a bcc microstructure. The alloys of the present disclosure may be useful in the production of mechanical fixing devices such as screws, nuts, bolts, plumbing fixtures (machined, forged or cast), domestic whitegoods, nuclear fuel tubes/cladding, pipes, such as steam pipes, construction and cladding components, motor vehicle exhaust systems, hot liquid transfer and cooling interchangers, domestic and industrial civil construction materials, such as press or roll-formed structural beams, sheets or rods, including weldable products or those intended for down-stream fabrication. The alloys described herein may also exhibit hard ferro magnetic properties and may be suitable for electromagnetic devices.

EXAMPLES

[0084] Nominal alloy composition ingots of volume 10.5 cm.sup.3 were produced in an electric arc furnace (Edmund Buehler AM) from high purity primary elements iron, chromium, manganese, aluminium and, in some cases, high purity additions of titanium and niobium. A titanium-gettered argon atmosphere was produced via purging of the melting chamber with high purity argon (three times over) and then evacuating to the melting chamber to within the order of 10.sup.4 mbar. The melting chamber was filled to 60% of atmospheric pressure with high purity argon. This was followed by melting a titanium getter. To ensure homogenous distribution of the small amounts of Ti and Nb, these elements were first formed into initial button-shaped ingots with approximately 10% of the required Fe by melting and inverting resultant ingots five times. This ingot was then melted with the required balance of Fe and the Cr and Mn to meet the nominal alloy composition, which was repeatedly melted and inverted at least three times. To reduce vaporisation, the Al balance was added after this initial alloy ingot was homogeneous. The complete composition was melted and inverted at least 5 more times to form the FeCrMnAl (+Ti,Nb) homogeneous ingot.

[0085] Alloyed ingots were mechanically cleaned/abraded to a lustrous finish, removing any surface oxide products. Castings were produced from the cleaned ingots in an electric arc furnace using copper moulds in a titanium-gettered argon atmosphere as described previously. Castings 6 mm in diameter?30 mm were produced independently for microstructural and hardness analysis, and these were sectioned into 3 mm long slices. Rectangular castings with a 16.5 mm by 11.7 mm cross section and length of 36-44 mm were produced for thermomechanical processing and tensile testing. The castings were mechanically abraded to remove surface defects then processed via hot rolling at 1000? C. in 0.25 mm increments to close any casting porosity or structural defects, to consolidate the material, and to refine and recrystallise the grain structure, essentially simulating industry processing. Samples were rolled from 11.7 mm thickness to 8 mm thickness. Samples were intermittently cooled and mechanically cleaned/abraded to remove any oxide scale and then returned to 1000? C. before the next rolling increment. The resulting ?16 mm?8 mm?48-56 mm ingots were mechanically cleaned/abraded and then sectioned into two 8 mm?8 mm?36-44 mm samples. Samples were further hot rolled at 1000? C. along both perpendicular long faces in 0.25 mm increments, with reheating in a 1000? C. furnace between steps, to 7 mm square cross section billets/bars with final lengths of 65-75 mm.

[0086] Following the hot rolling process, the strips were heat treated in a vacuum furnace at 850? C. for 6 hours to produce the final processed alloys in a hot rolled plus annealed condition. The strips were cut to lengths of 62 mm and machined into cylindrical tensile specimens with 4 mm gauge diameter and 20 mm gauge length in accordance with ASTM E8M. Tensile testing was conducted in accordance with ASTM A370 using an Instron tensile testing machine, laser extension meter and associated computer and data logger. The tensile strain rate for all samples was 1 mm/min. Measured response sample load and laser extension of the gauge section were recorded using software produced by Bluehill. Representative engineering stress-strain data are provided in FIG. 1, and characteristic mechanical properties are set out in Table 1.

[0087] Microstructural analysis was conducted on both as-cast and heat treated sections of the 6 mm diameter cylindrical castings. Samples were heat treated in a muffle furnace in evacuated quartz capsules for 850? C. for 6 hours for homogenization and then select samples were further heat treated at 350, 400, 450 and 500? C. for 7 days to confirm the absence of the sigma phase and the degree of any low-temperature phase separation (?+?). Hardness data is provided in Tables 1 and 2. Scanning electron microscopy including electron dispersive spectroscopy for composition analysis/confirmation was conducted on suitably prepared samples with a Hitachi S3400 electron microscope. X-ray diffraction was conducted on powdered samples with a PANalytical Empyrean 2 Co-sourceXRD to confirm a single phase bcc structure and absence of the sigma phase. FIG. 2 provides an x-ray diffraction trace showing the bcc structure of an alloy after homogenisation at 850? C. and a week at 400? C. Hardness testing was conducted using a Struers Durascan hardness testing machine with a 1 kg load and a 10 second dwell time. A minimum of 20 hardness indents were conducted for each sample. Density was measured using Archimedes' principle with a Mettler Toledo density test kit and Mettler Toledo 5-digit balance.

TABLE-US-00001 TABLE 1 Composition and mechanical properties of specific FeCrMnAl alloys compared to 304, 316, 430, 455M2 and 1018 steels. Average Hardness 0.2%-offset Ultimate (HV) Yield Tensile Tensile (solution Strength Strength Elongation treated Density Material/Alloy (MPa) (MPa) (% range) 850? C.) g/cm.sup.3 304 215 505 70 129 8.00 316 240 550 60 155 8.03 430 310 517 22-30 183 (162) 7.80 455M2 350 520 30 170 7.75 1018 mild steel 370 440 15 126 7.85 Fe.sub.65Cr.sub.25Mn.sub.5Al.sub.5 375 460 32-37 7.36 Fe.sub.65Cr.sub.25Mn.sub.5Al.sub.5* 425 525 26-30 7.36 Fe.sub.65Cr.sub.25Mn.sub.5Al.sub.5** 400 485 23 181 7.36 Fe.sub.60Cr.sub.30Mn.sub.5Al.sub.5** 474 561 27-29 195 7.35 Fe.sub.55Cr.sub.35Mn.sub.5Al.sub.5** 548 582 2.6 210 7.31 Fe.sub.50Cr.sub.40Mn.sub.5Al.sub.5** 719 779 8.7 236 7.27 Fe.sub.45Cr.sub.45Mn.sub.5Al.sub.5 272 7.19 Fe.sub.45Cr.sub.45Mn.sub.5Al.sub.5* 274 7.19 Fe.sub.45Cr.sub.45Mn.sub.5Al.sub.5** 850 865 3.8 266 7.19 Fe.sub.65Cr.sub.20Mn.sub.10Al.sub.5 183 7.36 Fe.sub.65Cr.sub.20Mn.sub.10Al.sub.5** 425 510 28-32 180 7.36 Fe.sub.60Cr.sub.25Mn.sub.10Al.sub.5** 460 549 34 185 7.34 Fe.sub.55Cr.sub.30Mn.sub.10Al.sub.5** 527 597 23-31 203 7.32 Fe.sub.50Cr.sub.35Mn.sub.10Al.sub.5** 622 674 4.7 221 7.23 Fe.sub.45Cr.sub.40Mn.sub.10Al.sub.5 240 7.26 Fe.sub.45Cr.sub.40Mn.sub.10Al.sub.5* 241 7.26 Fe.sub.45Cr.sub.40Mn.sub.10Al.sub.5** 757 794 3.9 248 7.26 Fe.sub.65Cr.sub.15Mn.sub.15Al.sub.5 187 7.35 Fe.sub.65Cr.sub.15Mn.sub.15Al.sub.5** 425 538 34 (30) 188 7.35 Fe.sub.60Cr.sub.20Mn.sub.15Al.sub.5** 454 541 30 182 7.33 Fe.sub.55Cr.sub.25Mn.sub.15Al.sub.5** 473 534 6.8 196 7.26 Fe.sub.50Cr.sub.30Mn.sub.15Al.sub.5 223 7.26 Fe.sub.50Cr.sub.30Mn.sub.15Al.sub.5** 565 618 5.9 217 7.26 Fe.sub.45Cr.sub.35Mn.sub.15Al.sub.5 223 7.27 Fe.sub.45Cr.sub.35Mn.sub.15Al.sub.5** 690 731 4.7 232 7.27 Fe.sub.40Cr.sub.40Mn.sub.15Al.sub.5** 276 7.24 Fe.sub.60Cr.sub.15Mn.sub.20Al.sub.5** 490 558 29 186 7.38 Fe.sub.55Cr.sub.20Mn.sub.20Al.sub.5** 454 532 32 193 7.34 Fe.sub.50Cr.sub.25Mn.sub.20Al.sub.5** 489 588 24 204 7.31 Fe.sub.45Cr.sub.30Mn.sub.20Al.sub.5** 525 582 21 225 7.28 Fe.sub.40Cr.sub.35Mn.sub.20Al.sub.5** 259 7.25 Fe.sub.50Cr.sub.20Mn.sub.25Al.sub.5** 424 517 33 7.29 Fe.sub.45Cr.sub.25Mn.sub.25Al.sub.5** 523 591 22 7.25 Fe.sub.40Cr.sub.30Mn.sub.25Al.sub.5** 7.22 *indicates an addition of 0.2 at. % Ti to the overall alloy composition e.g. [Fe.sub.65Cr.sub.25Mn.sub.5Al.sub.5].sub.99.8Ti.sub.0.2 **indicates an addition of 0.2 at. % Ti and 0.2 at. % Nb to the overall alloy composition e.g. [Fe.sub.65Cr.sub.25Mn.sub.5Al.sub.5].sub.99.6Ti.sub.0.2Nb.sub.0.2

TABLE-US-00002 TABLE 2 Composition and hardness of FeCrMnAl alloys with the addition of 0.2 at. % Ti and 0.2 at. % Nb in the following conditions: as- cast, solution treated (ST) at 850? C., slow cooled then heat treated (HT) at 350, 400, 450 and 500? C. for 7 days and quenched (Q), solution treated at 850? C. then slow cooled. ST + ST + ST + ST + HT HT HT HT Solution As 350? C. + 400? C. + 450? C. + 500? C. + treated Alloy Cast Q Q Q Q 850? C. Fe.sub.65Cr.sub.25Mn.sub.5Al.sub.5 189 202 282 307 224 181 Fe.sub.60Cr.sub.30Mn.sub.5Al.sub.5 201 230 313 334 300 195 Fe.sub.55Cr.sub.35Mn.sub.5Al.sub.5 217 231 345 380 359 210 Fe.sub.50Cr.sub.40Mn.sub.5Al.sub.5 253 249 377 402 381 236 Fe.sub.45Cr.sub.45Mn.sub.5Al.sub.5 272 314 392 429 448 266 Fe.sub.65Cr.sub.20Mn.sub.10Al.sub.5 183 202 237 211 202 180 Fe.sub.60Cr.sub.25Mn.sub.10Al.sub.5 191 225 280 282 198 185 Fe.sub.55Cr.sub.30Mn.sub.10Al.sub.5 200 220 311 316 217 203 Fe.sub.50Cr.sub.35Mn.sub.10Al.sub.5 256 358 368 251 221 Fe.sub.45Cr.sub.40Mn.sub.10Al.sub.5 251 261 385 393 318 248 Fe.sub.65Cr.sub.15Mn.sub.15Al.sub.5 189 208 196 207 191 188 Fe.sub.60Cr.sub.20Mn.sub.15Al.sub.5 188 220 203 195 190 182 Fe.sub.55Cr.sub.25Mn.sub.15Al.sub.5 190 241 222 217 202 196 Fe.sub.50Cr.sub.30Mn.sub.15Al.sub.5 211 251 301 241 224 217 Fe.sub.45Cr.sub.35Mn.sub.15Al.sub.5 239 275 342 319 269 232 Fe.sub.60Cr.sub.15Mn.sub.20Al.sub.5 186 197 185 179 178 186 Fe.sub.55Cr.sub.20Mn.sub.20Al.sub.5 193 222 199 192 186 193 Fe.sub.50Cr.sub.25Mn.sub.20Al.sub.5 204 235 219 209 205 204 Fe.sub.45Cr.sub.30Mn.sub.20Al.sub.5 225 261 279 255 230 225 Fe.sub.40Cr.sub.35Mn.sub.20Al.sub.5 259 305 334 326 266 259 Fe.sub.50Cr.sub.20Mn.sub.25Al.sub.5 187 Fe.sub.45Cr.sub.25Mn.sub.25Al.sub.5 210 Fe.sub.40Cr.sub.30Mn.sub.25Al.sub.5 224

[0088] It will be appreciated by those skilled in the art that the alloys of the present disclosure may be embodied in many other forms.