Excellent
Corrosion Resistance
Titanium is resistant to corrosive attack by salt water or
marine atmospheres. It also exhibits exceptional resistance
to a broad range of acids, alkalis, natural waters and chemicals.
Superior Erosion Resistance
Titanium offers superior resistance to erosion, cavitation
or impingement attack. Titanium is at least twenty times more
erosion resistant than the copper-nickel alloys.
High Heat Transfer Efficiency
Under "in service" conditions, the heat transfer
properties of titanium approximate those of admiralty brass
and copper-nickel. There are several reasons for this:
- Titanium's higher strength permits the use of thinner walled equipment.
- There appear to be unusual and beneficial characteristics in titanium's
inherent oxide film.
- The relative absence of corrosion in media where titanium is generally used
leaves the the surface bright for improved lamellar flow.
- Titanium's excellent erosion-corrosion resistance permits significantly
higher operating velocities.
Superior Strength-to-Weight Ratios
The densities of titanium-based alloys range between .160
lb/in3 (4.43 gm/cm3) and .175 lb/in3 (4.85 gm/cm3). Yield
strengths range from 25,000 psi (172 MPa) commercially pure
(CP) Grade 1 to above 200,000 psi (1380 MPa) for heat treated
beta alloys.
The combination of high strength and low density results
in exceptionally favorable strength-to-weight ratios for titanium-based
alloys are superior to almost all other metals and become
important in such diverse applications as deepwell tubestings
in the petroleum industry and surgical implants in the medical
field.



| Table 2 |
| PHYSICAL
PROPERTIES |
|
Property |
T (°F) |
T (°C) |
Value |
Value (Sl) |
|
Density |
72 |
22 |
0.160 lb in-3 |
4.42 g cm-3 |
|
Beta Transus |
1825 +/-25 |
996 +/-14 |
|
|
|
Melting (liquidus) Point
|
3000-3020+/-25 |
1650-1661+/-14 |
|
|
|
Thermal Conductivity
Mil Annealed |
68
600
1200 |
20
315
650 |
3.8 Btu hr-1ft-1 °F-1
6.1 Btu hr-1ft-1 °F-1
10.1 Btu hr-1ft-1 °F-1
|
6.6 W m-1K-1
10.6 W m-1K-1
17.5 W m-1K-1 |
|
Specific Heat |
68
800
1600 |
20
425
870 |
0.140 Btu lb-1 °F-1
0.140 Btu lb-1 °F-1
0.140 Btu lb-1 °F-1 |
0.586 J kg-1K-1
0.586 J kg-1K-1
0.586 J kg-1K-1 |
|
Electtical Resistivity |
32
600
1200 |
0
315
650 |
66 µ Ohm in
73 µ Ohm in
74 µ Ohm in |
1.68 µ Ohm m
1.86 µ Ohm m
1.98 µ Ohm m |
|
Magnetic Permeability |
|
|
1.00005 at 20 oersteds
|
|
Mean Coefficient of
Thermal Expansion |
32-212
70-800
70-1200 |
0-100
20-425
20-650 |
5.0 X 10-6in in-1 °F-1
5.2 X 10-6in in-1 °F-1
5.4 X 10-6in in-1 °F-1
|
9.0 X 10-6m m-1 °C-1
9.4 X 10-6m m-1 °C-1
9.7 X 10-6m m-1 °C-1
|
|
Young's Modulus
(Dependent on texture and heat treatment) |
68
450 |
20
230 |
15.5-17.7 Msi
13.8-16.2 Msi |
107-122 GPa
95-111 GPa |
|
Shear Modulus |
68 |
20 |
5.9-6.5 Msi |
41-45 GPa |
|
Poisson's Ratio |
68 |
20 |
.31 |
.31 |
| Table 3 |
| MINIMUM TENSILE
PROPERTIES OF TIMETAL 6-4 |
|
Product (in) |
Condition |
Specification |
Dir. |
Temperature
°F (°C) |
UTS
ksi (MPa) |
0.2% YS
ksi (MPa) |
Elongation
% |
Reduction
in Area % |
|
0.025-1.000
Sheet & Plate |
Annealeda |
ASTM B265 |
L & LT |
68(20) |
130(895) |
120(828) |
10b |
- |
|
</-3.00 RD or Thk. |
Annealed |
ASTM B348 |
L |
68(20) |
130(895) |
120(828) |
10 |
25 |
|
</-4.00 RD or Thk.
>4.00-6.00 |
Annealed
Annealed |
Mil-T-9047Gc
Mil-T-9047Gc |
All
All |
68(20)
68(20) |
130(896)
130(896) |
120(827)
120(827) |
10
10 |
25
20 |
|
><0.500
>0.500-1.000
>1.000-1.500
>1.500-2.000
>2.000-3.000 |
>STDd
STDd
STDd
rd,. sq,. hex
rd,. sq,. hex |
Mil-T-9047G
Mil-T-9047G
Mil-T-9047G
Mil-T-9047G
Mil-T-9047G |
|
68(20)
68(20)
68(20)
68(20)
68(20) |
165(1137)
160(1103)
155(1068)
150(1034)
140(965) |
155(1068)
150(1034)
145(999)
140(965)
130(896) |
10
10
10
10
10 |
20
20
20
20
20 |
| MINIMUM TENSILE PROPERTIES OF TIMETAL
6-4 ELI |
|
0.025-1.000
Sheet & Plate |
ST |
ASTM B265 |
L & LT |
68(20) |
120(828) |
110(759) |
10 |
- |
|
</-3.00 RD or Thk. |
Annealed |
ASTM B348 |
L |
68(20) |
120(828) |
110(759) |
10 |
25 |
|
></-1.75 RD or Thk.
1.75-2.50
2.50-4.00 |
Annealedd
Annealedd
Annealedd |
ASTM F136
ASTM F136
ASTM F136 |
L
L & LT
L, LT & ST |
68(120)
68(120)
68(120) |
125(860)
120(825)
120(825) |
115(795)
110(760)
110(760) |
10
8
8 |
25e
20
15 |
| a 1300°F/1hr/AC or slower.
b For materials less than .025 thick, the
elongation must be negotiated with the manufacturer.
c Partial list of tensile requirements from
the specification.
d Solution Treat
and Age (1650-1775°F)/2-120 min/WQ + 900-1275°F/2-8hr/AC
e Only for 0.187-<1.75? thick material. |
| Table 1 |
| CHEMICAL
COMPOSITION |
|
|
TIMETAL 6-4
ASTM Grade 5
Mil T-9047 |
TIMETAL 6-4 ELI
ASTM Grade 23
AMS 4981 |
TIMETAL 6-4-.1Ru
ASTM Grade 29 |
|
|
Min. |
Max. |
Min. |
Max. |
Min. |
Max. |
|
Aluminum |
5.5 |
6.75 |
5.5 |
6.5 |
5.5 |
6.5 |
|
Vanadium |
3.5 |
4.5 |
3.5 |
4.5 |
3.5 |
4.5 |
|
Nitrogen |
- |
0.05 |
- |
0.03 |
- |
0.03 |
|
Carbon |
- |
0.08 |
- |
0.08 |
- |
0.08 |
|
Oxygen |
- |
0.20 |
- |
0.13 |
- |
0.13 |
|
Iron |
- |
0.40 |
- |
0.25 |
- |
0.25 |
|
Hydrogen |
- |
0.015 |
- |
0.0125 |
- |
0.015 |
|
Ruthenium |
- |
- |
- |
- |
0.08 |
0.14 |
|
Residual Element, each |
- |
0.1 |
- |
0.1 |
- |
0.1 |
|
Residual Element, total |
- |
0.40 |
- |
0.40 |
- |
0.40 |
|