CA3093022A1 - Corrosion resistant alloy - Google Patents

Abstract

The invention relates to metallurgy and more particularly to nickel-based alloys intended for use in aggressive oxidising environments. The present nickel-based corrosion-resistant alloy contains: = 0.006 wt.% carbon, = 0.1 wt.% silicon, = 1.0 wt.% manganese, 22.8-24.0 wt.% chromium, = 0.75 wt.% iron, 12.0-14.0 wt.% molybdenum, 0.01-0.03 wt.% niobium, 0.01-0.06 wt.% titanium, 0.1-0.2 wt.% aluminium, 0.005-0.01 wt.% magnesium, = 0.015 wt.% phosphorus and < 0.012 wt.% sulphur, with the remainder being nickel and unavoidable impurities.

Description

Corrosion resistant alloy The invention relates to metallurgic engineering, to nickel-based alloys intended for use in aggressive oxidizing environments.
A corrosion-resistant alloy Nicrofer 6616 hMo alloy C-4 (No. 2.4610), containing wt.%:
14.5-17.5 Cr, 14.0-17.0 Mo, <3.0 Fe, <0.009 C, <1.0 Mn, <.05 Si, <.0 Co, <.7 Ti, <.020 P, <.010 S, nickel and other unavoidable impurities is known from the prior art (Catalogue "Cor-rosion-resistant, heat-resistant and high-strength steels and alloys", M., Prometey-Splav, 2008, pp. 304 ¨ 306).
The alloy is used for the manufacture of equipment operated in a wide range of chemical environments, at room and elevated temperatures. In particular, for adsorbers in flue gas desul-phuring; etching baths and acid recovery plants; acetic acid and agrochemicals plants.
The nearest analogue of the given invention is an alloy XH65MBY(311760) containing, wt.%: <0.02 C, <.1 Si, <1.0 Mn, 14.5-16.5 Cr, 15.0-17.0 Mo, 3.0-4.5 W, <0.5 Fe , <.012 S, 0.015 P, nickel and other unavoidable impurities (GOST 5632-2014 - prototype).
The alloy is used for the manufacture of welded structures (columns, heat exchangers, reactors) operating under elevated temperatures in aggressive redox environments, in the chemi-cal, petrochemical industry (production of acetic acid, epoxy resins, vinyl acetate, melamine, complex organic compounds) and other industries in the temperature range -70 to 500 C.
The XH65MB alloy and its welded joints can be used in KCI ¨ A1C13 ¨ ZrC14 media on-ly up to 500 C, because at a temperature above this value, the alloy, in addition to intergranular corrosion and corrosion cracking, sharply decreases the percentage elongation from 48% to 7.3-13% at 550 C and up to 2.5% at 625 C and the embrittlement of the metal appears when defor-mation is applied.
The objective of the invention is to create an alloy having a high level of corrosion prop-erties at temperatures up to T = 650 C in the working media of chloride plants (KCI A1C13 ¨
ZrC14).
The technical result of the invention is to obtain an alloy with a high level of plastic properties for the operation in the temperature range 550 C to 625 C and increased corrosion cracking resistance in chlorides KCI, A1C13 + (ZrCI4 HfC14) molten metal, at temperatures up to 650 C.
The specified technical result is achieved in that the alloy containing carbon, silicon, manganese, chromium, molybdenum, phosphorus, sulphur, iron, nickel and unavoidable impuri-ties, according to the invention additionally contains titanium, aluminium, niobium, magnesium with the following components ratio, wt.% :
Carbon <.006 Silicon <.l Manganese <1.0 Chromium 22.8-24.0 Iron .75 Molybdenum 12.0-14.0 Niobium 0.01-0.03 Titanium 0.01-0.06 Aluminium 0.1-0.2 Magnesium 0.005-0.01 Phosphorus <0.015 Sulphur <.012 Nickel and unavoidable impurities balance To obtain a stable structure and plastic properties, it is preferable that the content of [Cr] + [i ] ?_ 46,4 chromium, molybdenum and iron is related by the ratio: [Fe]
(1) (the ratio of the total weight percentage of chromium and molybdenum to the percentage of iron is not less than 46.4) To obtain a stable structure and high corrosion properties, it is preferable that the content of niobium and carbon is related by the ratio:
[Nb]
[C]

(2) (the ratio of the weight percentage of niobium to the weight percentage of carbon is not less than 1.66).
It is preferably that the content of chromium, molybdenum, iron, niobium and carbon is related by the ratios:
[Cr] + [i 11>464 [Fe]
(1) [Nb]
At {C1 (2).
Comparative analysis with the prototype allows making a conclusion that the claimed al-loy differs from the known one with a lower carbon content (<0.006% instead of <0.02), molyb-denum (12.0-14.0% instead of 15.0-17.0%), increased chromium content (23.0-24.0% instead of 14.5-16.5%), iron (<0.75% instead of <0.5%) does not contain tungsten, as well as with the addi-tional introduction of elements such as niobium in an amount of 0.01-0.03%, titanium in an amount of 0.01-0.06%, aluminium in an amount of 0.1-0.2% and magnesium in an amount of 0.005-0.01%.
Moreover, in particular cases of the invention, the claimed ratios of elements are observed:
[Cr] + [i f] 46, 4 [Fe]
or [Arb] 1,66 [C]
[Cr] + [i f] 46,4 I¨Nb] 1,66 Or [Fe] at [C]
The limits of the content of alloying elements in the invention alloy are specified as a re-suit of a study of alloys properties with different composition options.
Exceeding the carbon content of more than 0.006% leads to a decrease in corrosion re-sistance in solutions of zirconium and hafnium salts due to an increase in the carbide formation process at high temperatures (the appearance of undesirable carbide phases).
The chromium content was found to be 22,8 - 24.0% to ensure the required heat re-sistance in hafnium and zirconium oxides. When chromium is introduced into the alloy in the amount of less than 22.8%, the required heat resistance is not ensured, and exceeding the content above 24.0% impairs the heat resistance of the alloy.
The introduction of molybdenum into nickel alloys increases the recrystallization temper-ature of solid solutions, inhibits their softening, increases heat resistance, and leads to an ductili-ty increase during short and long tests.
The range of molybdenum content of 12.0-14.0% is selected to provide the required me-chanical properties for both short-term and long-term loads and high temperatures. With the in-troduction of less than 12,0% of molybdenum, the mechanical properties are not met. When the content is above 14.0%, there is a decrease in ductility and, accordingly, a decrease in the pro-cessabil ity of the alloy during metallurgical processing.
Niobium in an amount of 0.01-0.03%, binds residual carbon and nitrogen to carbides, nitrides and carbonitrides, prevents the formation of chromium carbides and carbonitrides along the grain boundaries. The addition of niobium in an amount 6 to 10 times higher than the car-bon content in the alloy eliminates intergranular corrosion of the alloys and protects the welds

3 from destruction. When the niobium content is less than 0.01%, its interaction with residual carbon is ineffective, and the niobium content above 0.03% is not reasonable for carbide for-mation.
Exceeding the silicon content of more than 0.1% negatively affects the processability of the alloy, as well as leads to embrittlement of the alloy due to an increase of silicon silicates con-tent in it.
Increase of manganese content over 1.0% leads to the appearance of a fusible eutectic, which leads to the destruction of the ingot during pressure processing and reduces the heat resistance of the alloy, as well as leads to a decrease of local corrosion resistance.
Nickel is stable in HCI even at boiling point. However, in the presence of chlorides, ions of Fe(III) and other oxidizing agents corrosion of nickel and nickelchrome molybdenum alloys is enhanced, the limitation of the iron content of not more than 0.75% is due to this.
The introduction of titanium in an amount of 0.01-0.06% increases the corrosion re-sistance in melts of zirconium and hafnium salts, binds residual carbon to carbides and leads to the formation of a sufficient amount of Ni3Ti type intermetallic compound, which, at an operat-ing temperature of 500-700C, positively affects the heat resistance of the alloy. When the titani-um content is less than 0.01%, the requirements for corrosion resistance are not met, and the ex-cess of the titanium content above 0.06% leads to a decrease in the processability of the alloy and the formation of undesirable phases due to the reactivity of titanium.
Aluminium and magnesium in the amount of 0.1-0.2% and 0.005-0.01% are introduced into the alloy to remove residual oxygen, as well as, with regard to aluminium, to form an inter-metallic compound of the Ni3A1 type, which positively affects the heat resistance of the al-loy. When these elements are introduced in amounts less than specified, the necessary removal of residual oxygen is not achieved. If the content of these elements is exceeded, gross non-metallic inclusions are formed.
When the sulphur content exceeds 0.012% and phosphorus exceeds 0.015%, coarse non-metallic inclusions are formed that adversely affect the ductility of the alloy.
{Cr] +[l 11>464 Under the condition [Fell , when the ratio decreases below 46.4, the alloy structure becomes less stable (sigma phase is released), which has a neg-ative effect on plastic characteristics and corrosion resistance.

4 [Nb] 44 , v In the condition tc.1 , with a ratio of less than 1.66, a decrease in the corrosion resistance of the alloy occurs.
The proposed ratio of the elements in the alloy were found experimentally and are opti-mal, since they allow obtaining the claimed comprehensive technical result.
When breaking the ratios of the elements, the properties of the alloy deteriorate, their instability is observed, and the complex effect is not achieved.
Examples of the invention implementation.
Alloy ingots were smelted in vacuum induction furnaces. The change in the plastic prop-erties of the studied alloys under the influence of temperatures of 550 C and 625 C after long ex-posure in the furnace for more than 1000 hours was controlled by bending samples to an angle of 90 degrees or more according to COST 14019-2003. Industrial corrosion cracking resistance tests of alloys were carried out in molten chlorides KC1, A1C13 (ZrCI4 HfC14) Table 1 shows the chemical composition of alloy ingots with various compositional options, as well as the prototype alloy. Table 2 shows the results of determining the plastic properties of the alloys indicated in table 1 by bending at an angle of 90 degrees according to GOST 14019-2003. Table 3 presents the results of industrial corrosion cracking resistance tests of the alloys indicated in Table I in molten chlorides KC1, AlC13 (ZrC14 HfC14), 100 hours, at T = 650 C.
As can be seen from tables 1, 2, the plastic properties of alloy at 550 and 625C with the claimed composition (alloys 1, 2) are higher than the properties of the prototype alloy, alloy 3, not satisfying the claimed composition, has lower plastic characteristics than alloys 1, 2 , which leads to the formation of cracks as a result of bending tests according to COST 14019-2003.
As it can be seen from table 3, the corrosion rate of alloys (alloys 1, 2) that satisfy the claimed composition is lower than the corrosion rate of the prototype alloy, visual inspection did not reveal the cracks, unlike the prototype alloy. The corrosion rate of alloy 3, which does not satisfy the claimed composition, exceeds the corrosion rate of alloys 1, 2 (however, lower than the corrosion rate of the prototype alloy), visual inspection revealed a crack in the sample.

5 Table 1 - Chemical composition of the investigated alloys Ni and una-Alloy C Mn Si Mo Cr Nb S P Fe Ti Al W
voidable Ratio (1) Ratio (2) impurities Alloy 1 0.00110.55 00.7 13.0 23.3 0.03 0.0028 0,01 0.54 <0.01 0.1 - balance 67.2 27.27 Alloy 2 0Ø31 0,10 13.1 22.9 0.02 0.005 0.005 0.75 0.05 0.1 - balance 48.0 3.45 Alloy 3 0.009 0.65 0.10 12.5 23.6 0.01 0.008 0.0090.84 0.04 0.1 - balance 42.98 1.11 Alloy acc to 0.017 0.63 0.0816.2 15.6 - 0.006 0.0090.45 - - 3.7 balance _ prototype

6 Table 2 - Results of determining plastic properties by bending at an angle of 90 degrees accord-ing to GOST 14019-2003 Exposure temperature, C
Alloy 550 C 625 C
Samples bending Exposure Exposure time, h Sample bending result result Titne, h Alloy acc.to pro- 720 Sample broken 720 Sample broken totype 1000 No cracks 1000 Crack 2065 Crack 2065 Crack 720 No cracks 720 No cracks Alloy 1 1000 No cracks 1000 No cracks 2065 No cracks 2065 No cracks 720 No cracks 720 No cracks Alloy 2 1000 No cracks 1000 No cracks 2065 No cracks 2065 No cracks 720 No cracks 720 No cracks Alloy 3 1000 No cracks 1000 Crack 2065 Crack 2065 Crack Table 3 - Results of industrial corrosion cracking resistance tests of alloys in chloride melts KCI, A1C13 (ZrCI4 HfC14), 100 h, at T = 650 C
Visual inspection Alloy Cracks after Corrosion rate, mm/year testing Crack in sample Pit corrosion in a sam-Alloy acc.to prototype 0.50 pie up to 0.1-0.2 mm deep No cracks Pit corrosion Alloy 1 in metal sample up to 0.16 0.1-0.2 mm deep No cracks Pit corrosion Alloy 2 in a sample up to 0.1- 0.21 0.2 mm deep Crack in sample Pit corrosion in a sam-Alloy 3 0.45 pie up to 0.1-0.2 mm deep

7

Claims (4)

Claim

1. A corrosion-resistant nickel-based alloy containing carbon, silicon, rnanganese, chromium, molybdenum, phosphorus, sulphur, iron, nickel and unavoidable impurities, wherein it additionally contains titanium, aluminium, niobium, magnesium with the following cornpo-nents ratio, wt.% :
Carbon 0.006 Silicon <0.1 Manganese <1.0 Chromium 22.8-24.0 Iron <.75 Molybdenum 12.0-14.0 Niobium 0.01-0.03 Titanium 0.01-0.06 Aluminium 0.1-0.2 Magnesium 0.005-0.01 Phosphorus <.015 Sulphur 0.012 Nickel and unavoidable impurities balance.

2. The alloy according to claim I, wherein the content of chromium, molybdenum and iron is related by the ratio:
[Cr] + [i 46, 4 [Fe]

3. The alloy according to claim 1, wherein the content of niobium and carbon is re-lated by the ratio:
[Nb]
1, vu [C]

4. The alloy according to claim 1, wherein the content of chromium, rnolybdenurn and iron is related by the ratio: =
[Cr]+[.i 46, 4 [Fe]
and the content of niobium and carbon is related by the ratio:
[Nb]
1, 66 [C]