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:

  1. Titanium's higher strength permits the use of thinner walled equipment.
  2. There appear to be unusual and beneficial characteristics in titanium's inherent oxide film.
  3. The relative absence of corrosion in media where titanium is generally used leaves the the surface bright for improved lamellar flow.
  4. 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

 


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