Find below the search results for the material you've specified. Please note here this information is NOT to be used for design purposes, and in no event shall MSO be liable for any damages arising from the misuse of this information |
Titanium CP Grade 1 |
Related Metals: |
|
Titan 995-Ti-grade 1(tm)
Allvac 30(tm)
Commercially Pure Grade 1
RMI 25(tm)
Timetal(r) 75A
Timetal(r) 75A(tm)
|
Specifications: |
|
ASTM B265
ASTM B337
ASTM B338
ASTM B348
ASTM B381
ASTM F467 (1)
ASTM F468
ASTM F67
ASTM F67 (1)
DIN 3.7025
DMS 1536
MIL T-81556
MIL T-81915
UNS R50250
|
 |
Chemistry Data |
Carbon |
|
0.08 max |
Hydrogen |
|
0.015 max |
Iron |
|
0.2 max |
Nitrogen |
|
0.03 max |
Oxygen |
|
0.18 max |
Titanium |
|
Balance |
 |
General Information |
Principal Design Features |
This is an un-alloyed grade designed for excellent weldability, good strength, impact toughness, ductility and corrosion resistance. Beta Transus (F +/- 25) 1630. |
|
Applications |
Corrosion resistant applications in the chemical process industry, airframe and other areas where ease of formability is required. |
|
Machinability |
As a family, titanium and its alloys have developed a mystique as a nightmare to machine. This is simply not the case. Experienced operators have compared its characteristics to those found in 316 stainless steel. Recommended practice includes high coolan |
|
Forming |
May be hot or cold formed using hydropress, power brake, stretch or drop hammer methods. Similar in characteristics to 300 series stainless steels. |
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Corrosion Resistance |
Highly resistant to a wide variety of oxidizing and mildly reducing environments, including chlorides. |
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Welding |
Rated as "good" in terms of weldabilty. |
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Heat Treatment |
Not hardenable by heat treatment. |
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Forging |
Rough work at 871 C (1600 F), finish at 788-843 C (1450-1550 F) |
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Hot Working |
Hot forming will reduce both the springback and required forming forces, and will increase the overall ductility of the material. |
|
Cold Working |
The cold work characteristics of this material is similar to that of a moderately tempered austenitic stainless steel. In multiple cold forming operations, intermediate stress relief is recommended to prevent tearing or other material damage. Post-work an |
|
Annealing |
Heat to 704 C (1300 F),hold for 2 hours follow by air cooling. For intermediate stress relieving, heat to 482 F(900 C) and hold for 45 minutes. |
|
Other Physical Props |
Beta Transus (F +/- 25) 1630 |
|
 |
Physical Data |
Density (lb / cu. in.) |
|
0.163 |
Specific Heat (Btu/lb/Deg F - [32-212 Deg F]) |
|
0.124 |
Electrical Resistivity (microhm-cm (at 68 Deg F)) |
|
56 |
Melting Point (Deg F) |
|
3040 |
Thermal Conductivity |
|
9 |
Modulus of Elasticity Tension |
|
14.9 |
Reduction of Area |
|
30 |
Find below the search results for the material you've specified. Please note here this information is NOT to be used for design purposes, and in no event shall MSO be liable for any damages arising from the misuse of this information |
Stainless Steel 434 |
Related Metals: |
|
No Related Metal names.
|
Specifications: |
|
AISI 434
DIN 1.4113
UNS S43400
|
 |
Chemistry Data |
Carbon |
|
0.05 max |
Chromium |
|
|
Iron |
|
Balance |
Manganese |
|
0.5 max |
Molybdenum |
|
|
Phosphorus |
|
0.03 max |
Silicon |
|
0.5 max |
Sulphur |
|
0.01 max |
 |
General Information |
Principal Design Features |
Similar in chemistry and performance to 430 stainless steel, 434 has the addition of molybdenum to increase its resistance to corrosion. The alloy combines a ferritic structure with good fabricability and strength characteristics. |
|
Applications |
Primarily used in automotive trim applications and other exterior environments. |
|
Machinability |
Although not commonly available in machinable forms, 434 has been successfully machined using all standard methods. |
|
Forming |
Excellent ductility allows a wide variety of successful forming operations including shearing, blanking and deep drawing. |
|
Corrosion Resistance |
Resistant to mildly corrosive environments and atmospheric conditions. A dense polished finish will make this alloy resistant to all but the most direct salt water exposure. |
|
Welding |
434 can be successfully welded using most common methods. Standard type 308 filler material may be used, although if the part will undergo thermal cycling, it is recommended to use a filler material of similar composition. Material must be thoroughly clea |
|
Forging |
Begin forging after thorough soaking at 2000-2100 F and finish at 1350 F. |
|
Annealing |
Soak thoroughly at 1450-1600 F, air cool. |
|
Hardening |
This alloy does not respond to hardening by heat treatment. |
|
 |
Physical Data |
Density (lb / cu. in.) |
|
0.277 |
Specific Gravity |
|
7.65 |
Specific Heat (Btu/lb/Deg F - [32-212 Deg F]) |
|
0.11 |
Melting Point (Deg F) |
|
2750 |