253MA Stainless Steel Tube S30815
253 MA has very high resistance to oxidation, especially at cyclically varying temperatures. See Figs. 3 and 4. The service temperature in air should not exceed about 1150°C (2100°F).
Isothermal oxidation at 1150°C (2100°F) for 100 h results in a corrosion rate of about 0.3 mm/year (13 mpy), and exposure at the same temperature for 1000 h causes about 0.2 mm/year (9 mpy).
Cyclic oxidation at 1150°C (2100oF) for 5 x 24 h, with cooling to room temperature every 24 hours gives a corrosion rate of less than 1.1 mm/year (43 mpy), which is only marginally greater than the corrosion rate at 1000°C (1830°F).

Cyclic oxidation testing for 1000 h (15 minutes at the testing temperature and 5 minutes at room temperature, making a total of 3000 cycles) places heavy demands on the elasticity and adhesive capacity of the oxide. The
test results in Fig. 4 show that the resistance of 253 MA in such difficult conditions is superior to that of both ASTM TP310 and EN 1.4828 (ASTM TP309). The very good properties of this grade in cyclic conditions
have been achieved by adding rare earth metals and silicon.
44f43252-9ebc-42d8-b507-40495a8f7d82.jpg_1180xaf.jpg

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SPECIFICATION
PRODUCT DISPLAY
MATERIAL / DOCUMENT DOWNLOAD


Outside diameter4mm-200mm
Wall thickness0.6mm-6.0mm
length1-6 meters, length can be customized
standardASTM/AISI/JUST/GB/DIN/EN


Applications

253 MA has come to be used extensively in the metallurgical, petrochemical and power industries. Typical applications are:

Tubes in waste heat recovery systems in the metallurgical industry, e.g. recuperators

Tubes in heat treatment furnaces, e.g. radiation tubes, thermocouple protection tubes, burner components, furnace rollers

Tubes for injection of pulverized coal in blast furnaces Tubing for fluidized-bed combustion plants

Furnace tubes for mud incineration plants

Tubes for carbon black process gas coolers/air heaters Tubes for the glass and cement industries

Styrene reactor tubes EDC cracking tubes

Convection tubes in ethylene cracking

Air preheater tubes in sulphuric acid gas converters Muffle tubes in continuous wire annealing furnaces


Corrosion resistance

Air

253 MA has very high resistance to oxidation, especially at cyclically varying temperatures. See Figs. 3 and 4. The service temperature in air should not exceed about 1150°C (2100°F).

Isothermal oxidation at 1150°C (2100°F) for 100 h results in a corrosion rate of about 0.3 mm/year (13 mpy), and exposure at the same temperature for 1000 h causes about 0.2 mm/year (9 mpy).

Cyclic oxidation at 1150°C (2100oF) for 5 x 24 h, with cooling to room temperature every 24 hours gives a   corrosion rate of less than 1.1 mm/year (43 mpy), which is only marginally greater than the corrosion rate at 1000°C (1830°F).

Cyclic oxidation testing for 1000 h (15 minutes at the testing temperature and 5 minutes at room temperature,   making a total of 3000 cycles) places heavy demands on the elasticity and adhesive capacity of the oxide. The

test results in Fig. 4 show that the resistance of 253 MA in such difficult conditions is superior to that of both ASTM TP310 and EN 1.4828 (ASTM TP309). The very good properties of this grade in cyclic conditions

have been achieved by adding rare earth metals and silicon.


1737356985739862581307097088.png

Figure 3. Oxidation in air during cyclic testing 5x24 h with cooling to room temperature every 24 h. Comparison of Alleima 253 MA with four other high temperature materials.

1 = EN 1.4828 (ASTM TP309)

2 = ASTM TP446 

3 = ASTM TP310

4 = Sandvik 253 MA 

5 = Alloy 800 H

1737357051739862857426513920.png

Figure 4. Oxidation in air during 1000 h cyclic exposure. The cycles comprise 15 min. at the testing temperature and 5 min at room temperature. The curves represent averages.


Carburizing atmosphere

Carburization can occur when a material comes into contact with hot gases with high carbon activity, e.g.

hydrocarbons. The degree of carburization depends on the composition of the material and on the carbon and oxygen contents of the gas.

Thanks to the relatively high chromium content and the addition of silicon and rare earth metals, a protective oxide is easily formed on the surface of 253 MA material. Carburization resistance is, therefore, good.Fig. 5    shows carburization after 500 h at different temperatures, in a mixture of about 10% methane and about 90%

argon containing 0.5% oxygen. As can be seen, Alleima 253 MA is less prone to carburization at high temperatures in these conditions than ASTM TP310 and Alloy 800H.

1737357062739862904868286464.png

Figure 5. Carburization of a cylindrical test piece at 0.5 mm (0.02 in.) distance from the surface after testing for 500 h at different temperatures in about 10% CH4+ about 90% Ar + 0.5% O2.

Other gaseous atmospheres

In addition to its very good oxidation resistance in air, 253 MA is also highly resistant to other

atmospheres. The highly protective oxide layer makes it possible to use this steel at high temperatures in atmospheres containing sulphur and other aggressive compounds.

Bending

Annealing after cold bending is not normally necessary, but this should be reviewed depending on the degree of bending and the operating conditions.

If cold bending has exceeded 10–20%, we recommend solution annealing for tubes that are to be used at  temperatures above about 800°C (1450°F), and when the highest possible creep strength is required in the bent tube.

Hot bending should be carried out at 1100–850°C (2050–1560°F) and should be followed by solution annealing.

254MA.jpg

Approvals

Approved for use in ASME Boiler and Pressure Vessel Code, Section I, III and VIII, Div. 1 (SA-182,SA-213,SA-240, SA-249 SA-312 and SA-479).


Chemical composition (nominal)

Chemical composition (nominal) %

CSiMnPSCrNiNCe*
0.081.6≤0.8≤0.040≤0.03021110.170.05
* To cerium should be added the quantity of other rare earth metals, since the the additive takes the form of misch metal containing about 50% Ce.


Heat treatment

Tubes are delivered in the heat treated condition. If another heat treatment is needed after further processing, the following is recommended:

Stress relieving

850-950°C (1560-1740°F), 10-15 minutes, cooling in air.

Solution annealing

1050-1150°C (1920-2100°F), 5-20 minutes, rapid cooling in air or water.

Mechanical properties

Metric units, at 20°C

Proof strength
Tensile strengthElong.Elong.Hardness
Rp0.2a)Rp1.0a)RmAb)A2"Vickers
MPaMPaMPa%%
≥310≥350650-850≥40≥40≈190

1 MPa = 1 N/mm2

Imperial units, at 68°F

Proof strength
Tensile strengthElong.Elong.Hardness
Rp0.2a)Rp1.0a)RmAb)A2"Vickers
ksiksiksi%%
≥45≥5194-123≥40≥40≈190

a) Rp0.2 and Rp1.0 correspond to 0.2% offset and 1.0% offset yield strength, respectively.

b) Based on L0 = 5.65 √S0 where L0 is the original gauge length and S0 the original cross-section area


At high temperatures

Metric units


TemperatureProof strength
Tensile strength
°CRp.02Rp1.0Rm

MPaMPaMPa
100≥225≥265≥550
200≥189≥215≥475
300≥170≥200≥440
400≥160≥190≥425
500≥150≥180≥400
600≥140≥165≥340
Imperial units TemperatureProof strength
Tensile strength
°FRp.02Rp1.0Rm

ksiksiksi
200≥33.5≥39.0≥80.5
400≥26.0≥31.0≥68.5
600≥24.5≥28.5≥63.6
800≥23.0≥27.5≥61.0
1000≥21.0≥25.5≥55.0
1200≥19.5≥23.0≥46.5


TemperatureCreep strength 1%Creep rupture strength
°C10 000 h10 000 h10 000 h10 000 h

MPaMPaMPaMPa
525---162
550---128
575--167102
6001177013882
625935511264
65075429452
67559327643
70046256233
72537205027
75031164122
77525133318
800201127 (28)15 (16)
825179.422 (23)12 (14)
85014818 (20)10 (12)
875126.715 (17)8.8 (10)
900105.713 (14)7.5 (8.4)
9258.54.811 (12)6.6 (7.2)
9507.349.6 (10.5)5.7 (6.3)
9756.33.58.2 (9.0)5.0 (5.8)
10005.437.0 (7.8)4.3 (4.9)
1025--6.2 (6.6)3.8
1050--5.5 (5.7)3.3
1075--4.93
1100--4.32.6


TemperatureCreep strength 1%Creep rupture strength
°F10 000 h100 000 h10 000 h100 000 h

ksiksiksiksi
1000---20.9
1050---16.1
1100--21.212.6
115013.98.317.19.7
120010.96.113.87.5
12508.44.510.75.9
13006.53.58.64.6
13505.12.86.83.8
14004.12.25.52.9
14503.21.74.3 (4.4)2.5
15003.61.423.4 (3.6)1.9 (2.1)
15502.21.192.7 (3.0)1.5 (1.8)
16001.70.992.2 (2.5)1.25 (1.5)
16501.450.811.9 (2.0)1.07 (1.26)
17001.230.681.6 (1.7)0.93 (1.04)
17501.040.581.33 (1.46)0.80 (0.88)
18000.870.491.13 (1.03)0.70 (0.75)
1850--0.96 (1.03)0.59 (0.68)
1900--0.84 (0.88)0.51
1950--0.75 (0.77)0.45
2000--0.670.39
1737358160739867510822191104.pngFig. 1. Proof strength Rp0.2 and creep rupture strength at 10 000 and 100 000 h.1737358165739867529444966400.pngFig. 2 Relationship between nominal stress and minimum creep rate at 600 –1100°C (1110–2010°F).


Physical properties

Density: 7.8 g/cm3, 0.28 lb/in3


Relative magnetic permeability

1.003 (typical value)


Thermal conductivity
Temperature, °CW/m °C Temperature, °FBtu/ft h °F
2013687.5
100142008.5
200164009.5
3001860010.5
4002080011.5
50021100012.5
60023120013.5
70024140014.5
80025160015
90026180016
100028200017
110029--



Specific heat capacity
Temperature, °CJ/kg °CTemperature, °FBtu/ft h °F
20490680.12
1005152000.12
2005404000.13
3005656000.14
4005808000.14
50060010000.15
60061512000.15
70063014000.15
80064516000.16
90065518000.16
100066520000.16
1100680--



Thermal expansion1)
Temperature, °C
Temperature, °FPer °F
30-10016.586-2009.5
30-2001786-4009.5
30-3001786-6009.5
30-40017.586-80010
30-5001886-100010
30-6001886-120010
30-70018.586-140010.5
30-8001986-160010.5
30-9001986-180011
30-100019.5--
1) mean values in temperature ranges (x10-6)



Resistivity
Temperature, °C                                              µΩm
Temperature, °FµΩin.
200.846833.2
1000.9120035.4
2000.9740038.1
3001.0260040.3
4001.0780042.3
5001.11100044.1
6001.15120045.7
7001.18140047.1
8001.21160048.2
9001.23180049.2
10001.26200050.5
11001.29--


Modulus of elasticity1)
Temperature, °CMPaTemperature, °Fksi
202006828.5
20018540027
40017080024
600155120021.5
800135140020
1000120180017.5
1. (x103)



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