Stud Bolts
Carbon Steel
Round Head
Common Bolt
Round
DIN, ANSI, JIS, GOST
B6
Machinery
Polishing
C&N
Plywood Box, Plywood Case, Wooden Pallet
ASTM F468 UNS R56400
China
Product Description
ASTM F468 UNS R56400 represents grade specification for Titanium Grade 5 Bolts, Screw Fasteners. It covers both coarse and fine threaded Ti Alloy 5 Bolts, screws, stud bolts. Below is the chemical, mechanical and other requirements. ASTM F468 UNS R56400 Fasteners carry EN 10204 Type 3.1 Certification.
F468 F467 Uns R56400 Titanium Gr5 Stud Bolt and Nuts
F468 F467 Uns R56400 Titanium Gr5 Stud Bolt and Nuts Washers
The grade 5 Titanium alloy is considered to be the workhorse among the titanium alloy industries. It is a fully heat treatable alloy and can be quickly welded to form parts for aerospace machines, as well as marine and offshore applications. It is one of the critical components for engine parts of many vessels.
When compared to pure commercial Titanium, this is found to be stiffer and has the same thermal properties. It also has excellent fatigue resistance and low thermal expansion capability, making it suitable for subsea gas and oil industries.
grade 5 (Ti-6Al-4V) titanium which is the most widely used titanium alloy.
Common Names:
F468 F467 Uns R56400 Titanium Gr5 Stud Bolt
ASTM F468 Grade 5 Titanium stud bolt measurement
A Tensile stress areas are computed using the following formula: As = 0.7854 [D- (0.9743/n)]2
Where:
As = Tensile stress area, in.2,
D = Nominal size (basic major diameter), in., and,
n = number of threads per inch.
F468 F467 Uns R56400 Titanium Gr5 Stud Bolt and Nuts
F468 F467 Uns R56400 Titanium Gr5 Stud Bolt and Nuts Washers
The grade 5 Titanium alloy is considered to be the workhorse among the titanium alloy industries. It is a fully heat treatable alloy and can be quickly welded to form parts for aerospace machines, as well as marine and offshore applications. It is one of the critical components for engine parts of many vessels.
When compared to pure commercial Titanium, this is found to be stiffer and has the same thermal properties. It also has excellent fatigue resistance and low thermal expansion capability, making it suitable for subsea gas and oil industries.
grade 5 (Ti-6Al-4V) titanium which is the most widely used titanium alloy.
Common Names:
- Ti6Al4V
- Ti-6Al-4V
- Ti 6-4
- TC4
F468 F467 Uns R56400 Titanium Gr5 Stud Bolt
ASTM F468 Grade 5 Titanium stud bolt measurement
ASTM F468 Grade 5 UNS R56400 Chemical Requirements
| Composition, % Titanium and Titanium Base AlloysA | |||||||||||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| UNS Designation | Alloy | General Name | Aluminum | Carbon | Iron | Titanium | Hydrogen | Nitrogen | Oxygen | Palladium | Vanadium | Chromium | Molybdenum | Zirconium | Tin | Silicon | ResidualsB | ||
| Each | Total | ||||||||||||||||||
| R56400 | 5C | Titanium grade 5C | 5.50 - 6.75 | 0.10 | 0.40 | balance | 0.0125 | 0.05 | 0.20 | 3.50 - 4.50 | 0.10 | 0.40 |
ASTM F468 UNS R56400 Mechanical Properties
| Alloy | Mechanical Property Marking | Nominal Thread Diameter, inch | HardnessA | Full Size Tests B | Machined Specimen Tests | |||
|---|---|---|---|---|---|---|---|---|
| Tensile Strength, min, ksi | Yield Strength, min, ksiC | Tensile Strength, min, ksi | Yield Strength, min, ksiC | Elongation in 4D, min %D | ||||
| Titanium Alloys | ||||||||
| Ti 5 Class AH | F 468DT | all | 30 - 39 HRC | 130 - 165 | 125 | 130 | 120 | 10 |
| Ti 5 Class BH | F 468HT | all | 30 - 39 HRC | 130 - 165 | 125 | 130 | 120 | 10 |
Tensile Stress Areas and Threads per Inch
| Nominal Size, inch. | Coarse Threads – UNC | Fine Threads – UNF | 8 Thread Series – 8UN | |||
|---|---|---|---|---|---|---|
| Threads / inch | Stress AreaA, in2 | Threads / inch | Stress AreaA, in2 | Threads / inch | Stress AreaA, in2 | |
| 1/4 | 20 | 0.0318 | 28 | 0.0364 | - | - |
| 5/16 | 18 | 0.0524 | 24 | 0.0580 | - | - |
| 3/18 | 16 | 0.0775 | 24 | 0.0878 | - | - |
| 7/16 | 14 | 0.1063 | 20 | 0.1187 | ||
| 1/2 | 13 | 0.1419 | 20 | 0.1599 | ||
| 9/16 | 12 | 0.1820 | 18 | 0.2030 | ||
| 5/8 | 11 | 0.2260 | 18 | 0.2560 | ||
| 3/4 | 10 | 0.3340 | 16 | 0.3730 | ||
| 7/8 | 9 | 0.4620 | 14 | 0.5090 | ||
| 1 | 8 | 0.6060 | 12 | 0.6630 | ||
| 1 1/8 | 7 | 0.7630 | 12 | 0.8560 | 8 | 0.790 |
| 1 1/4 | 7 | 0.9690 | 12 | 1.0730 | 8 | 1.000 |
| 1 3/8 | 6 | 1.1550 | 12 | 1.3150 | 8 | 1.233 |
| 1 1/2 | 6 | 1.4050 | 12 | 1.5810 | 8 | 1.492 |
A Tensile stress areas are computed using the following formula: As = 0.7854 [D- (0.9743/n)]2
Where:
As = Tensile stress area, in.2,
D = Nominal size (basic major diameter), in., and,
n = number of threads per inch.
Test Methods
| Alloy | Test Method |
| Titanium | E120, E1409 |
