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630 (17-4) Precipitation Hardening Stainless Steel Bar
630 is a 17-4 PH martensitic precipitation hardening stainless steel with a unique combination of high strength and good corrosive resistance. Supplied in either the H1075 (H580) aged condition with a tensile strength of 1000 Mpa minimum (HB 311 min.), or the H1150 (H620) double aged condition with a tensile strength of 930 Mpa minimum (HB 277 min.).

It is characterised by high tensile strength and high yield strength obtained by solution annealing, followed by a single or double low temperature (precipitation) age hardening treatment. Coupled with a corosion resistance comparable to 304 austenitic stainless steel in many corrosive environments.

630 in the H1075 (H580) aged condition can be re-aged if necessary at a higher temperature simply by heating at the required temperature for the required duration.

630 in the H1075 (H580) And H1150 (H620) aged condition, can also be re-aged at a lower temperature by re-solution annealing, followed by age hardening at the required temperature for the required duration.

It is used extensively by the Marine, Aerospace, Chemical, Petrochemical, Food Processing, Paper and general metalwork industries. Here it is employed for applications such as: Pump Shafts, Aircraft Fittings, Valve Stems, Hydraulic Fittings, Studs, Bushings, Screws, Fasteners, Couplings, Wear rings, Rollers and Food Handling Equipment etc..

Material Magnetic in all conditions.

Colour Code
Salmon
(Bar end) 
Stocked Sizes 15.88 mm to 304.8 mm diameter.
 Bar Finish Peeled, Cold Drawn, Turned and Centreless Ground.
Related Specifications
  Australia AS 2837-1986-630
Germany W.Nr 1.4542 X5CrNiCuNb17 4
W.Nr 1.4548 X5CrNiCuNb 17 4 4
Japan JIS G4303 SuS 630
USA AISI 630 AISI S17400
ASTM A564/A564M-99-630
SAE J467 17-4 PH
UNS S17400
Chemical Composition Min. Max.
  Carbon   0.07
Silicon   1.00
Manganese   1.00
Nickel 3.00  5.00
Chromium 15.00  17.50
Copper 3.00  5.00
Niobium 0.15  0.45
Phosphorous   0.04
Sulphur   0.03
Mechanical Test Requirements in Solution Annealed and Age Hardened Conditions - At Room Temperature
*Conditon Ruling
Section
UTS
MPa (Min)
Yield
MPa (Min)
Elongation
% in 50 mm (Min)
Hardness
Impact Charpy - V
Rc BHN ft/lbs (Min) Joules (Min)
A         38 Max 363 Max    
  Min. Min.  
H900 (H480) Up to 200 mm 1310 1170 10 40 388    
 
H925 (H495) Up to 200 mm 1170 1070 10 38 375 5 6.8
 
H1025 (H550)   1070 1000 12 35 331 15 20
 
H1075 (H580)   1000 860 13 32 311 20 27
 
H1100 (H595) Up to 200 mm 965 795 14 31 302 25 34
 
H1150 (H620)   930 725 16 28 277 30 41
 
H1150M (H620M)   795 502 18 24 255 55 75
 
H1150D (H620D)   860 725 16 24 255 30 41
  33 Max 311 Max  
*Refer Age Hardening temperature table

Typical Mechanical Properties - At Room Temperature
*Conditon UTS
MPa
Yield
MPa
Elongation
% in 50 mm
Hardness
Impact Charpy - V
Rc BHN ft/lbs Joules
A 1100 900 15 36 340 30 40
 
H900 (H480) 1375 1275 14 44 420 15 20
 
H925 (H495) 1310 1205 14 42 390 25 34
 
H1025 (H550) 1170 1140 15 38 350 35 47
 
H1075 (H580) 1140 1035 16 36 340 40 54
 
H1100 (H595) 1035 930 17 35 330 45 61
 
H1150 (H620) 1000 860 19 33 310 50 68
 
H1150M (H620M) 860 600 22 27 275 100 135
 
H1150 (H620D) 950 800 20 31 295 90 120
*Refer Age Hardening temperature table

Low Temperature Properties
Retains relatively good ductility at sub zero temperatures, with impact properties greatly improved at higher ageing temperatures:-

Typical sub zero charpy V-notch impact properties
Test
Temperature
      Impact Strength
H925 (H495) H1025 (H550) H1150 (H620)
oF oC ft - lb J ft - lb J ft - lb J
   
 10 -12 16 22 58 79 93 126
   
 -40  -40 9 12 40 54 76 103
   
 -112  -80 5 7 15 20 48 65
   
 -148  -100 5 7 12 16 37 50
   
  -320   -196 3 4 4 6 6 8
   
Cold Working
Cold bending etc. will be limited by the high yield strength in all conditions.

Corrosion Resistance
Superior to the martensitic stainless range in all conditions, and equal to 302 or 304 austenitic stainless grades in most environments.

For optimum corrosion resistance, surfaces must be free of scale and foreign particles. Finished parts should be passivated.

Forging
Heat uniformly to 2150/2200 oF (1177/1204 oC) - Hold for 1 hour at temperature prior to commencing forging.

Do not forge below 1850 oF (1010 oC).

Finished forgings should be cooled in air to below 90 oF (32 oC) prior to further processing in order to obtain optimum grain size and mechanical properties.

Finally forgings will require to be solution annealed prior to age hardening as required.

Heat Treatment
Solution Annealed - Condition A
Heat to 1900 +/- 25 oF (1040 +/- 15 oC) - *Hold for 30 Minutes

Sections up to 75 mm -  Oil Quench To Below 90 oF (32 oC)

Sections over 75mm -  Air Cool To Below 90 oF (32 oC)

*Actual holding time should be long enough to ensure that the part is heated thoroughly through out its section

Age Hardening
Material in the solution annealed condition may be age hardened as follows:-

Condition Heat to       Hold for
Hours
      Cool To Below
90 oF (32 oC)
±15 oF ±9 oC
 
H900 (H480) 900 oF 480 oC   1   Air
 
H925 (H495) 925 oF 495 oC   4   Air
 
H1025 (H550) 1025 oF 550 oC   4   Air
 
H1075 (H580) 1075 oF 580 oC   4   Air
 
H1100 (H595) 1100 oF 595 oC   4   Air
 
H1150 (H620) 1150 oF 620 oC   4   Air
 
H1150M (H620M)* 1400 oF 760 oC   2   Air
    Plus 1150 oF 620 oC   4   Air
 
H1150D (H620D)* 1150 oF 620 oC   4   Air
    Plus 1150 oF 620 oC   4   Air
 
    *Denotes Double Overaged  
 
Notes on Heat Treatment And It's Effect On Structure - Corrosion Resistance Etc.
The martensitic transformation temperature range for this grade is:-
       Ms - 270 oF (132 oC)
Mf - 90 oF (32 oC)

Therefore to ensure complete transformation to martensite, it is most important that parts are always cooled to below 90 oF (32 oC) within 24 hours following Solution Annealing and before Age Hardening Treatment which should also be followed by an air cool to below 90 oF (32 oC).

The age hardening tempers the martensite resulting in an improvement in toughness. The higher the ageing temperature the more refined the martensite leading to greater ductility but slightly lower strength.

N.B. Temperature control is critical during age hardening and any variations outside the given range could lead to less than satisfactory results.

In the solution annealed condition resistance to stress corrosion cracking is low - improving at age hardening temperatures from 1025 oF (550 oC) upwards to a maximum at 1150 oF (620 oC) double aged.

Dimensional Changes During Heat Treatment
Age hardening results in a slight dimensional contraction as follows:-

Condition A to condition H900 (H480) - contraction 0.0004/0.0006 M/M

Condition A to condition H1150 (H620) - contraction 0.0009/0.0012 M/M

Machining
Machinability in the solution annealed condition is similar to 302 and 304 austenitic stainless steel grades.

Machinablity in the H900 (H480) condition is limited, improving as the age hardening temperature is increased to optimum machinability similar to 304 austenitic stainless steel grade in the H1150 (H620) condition.

Removing Heat Tint
The heat tint formed during age hardening, whilst having little effect on corrosion resistance, may be removed when required for appearance purposes by pickling or electro polishing.

Elevated Temperature Use
Excellent oxidation resistance up to 1100 oF (540 oC).

Exposure to temperature range 600 - 900 oF (290 - 480 oC) long term may result in reduced toughness but this can sometimes be minimilized by using higher ageing temperatures. As a general guide for short term exposure at elevated temperatures the ageing temperature should be at least 50 oF (28 oC) above the working temperature.

Welding
May be welded satisfactorily by shielded fusion and resistance welded processes, however oxyacetylene welding is not recommended due to the posibility of carbon pick up Filler metal when required should be similar to the parent metal if strength is important otherwise standard austenitic stainless filler wire 308L may be satisfactory. Pre-heating is not generally required.

Welding in the solution annealed condition may be carried out satisfactorily, however welding in the H1150 (H620) condition reduces the effects of high welding stresses.

Following welding in the solution annealed condition, parts can be directly age hardened as required, however those in the H1150 (H620) condition should be re-solution annealed and then age hardened as required.

Interlloy believes the information provided is accurate and reliable. However no warranty of accuracy, completeness or reliability is given, nor will any responsibility be taken for errors or omissions.
Copyright Interlloy Pty Ltd