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ASTM F468 Grade 5 Titanium Hex Head Bolt, Stud Bolt

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Model NO.:

Stud Bolts

Material:

Carbon Steel

Type:

Round Head

Connection:

Common Bolt

Head Style:

Round

Standard:

DIN, ANSI, JIS, GOST

Grade:

B6

Application:

Machinery

Finish:

Polishing

Trademark:

C&N

Transport Package:

Plywood Box, Plywood Case, Wooden Pallet

Specification:

ASTM F468 UNS R56400

Origin:

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:

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 Alloys^A
UNS Designation	Alloy	General Name	Aluminum	Carbon	Iron	Titanium	Hydrogen	Nitrogen	Oxygen	Palladium	Vanadium	Chromium	Molybdenum	Zirconium	Tin	Silicon	Residuals^B
Each	Total
R56400	5^C	Titanium grade 5^C	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	Hardness^A	Full Size Tests B	Machined Specimen Tests
Tensile Strength, min, ksi	Yield Strength, min, ksi^C	Tensile Strength, min, ksi	Yield Strength, min, ksi^C	Elongation in 4D, min %^D
Titanium Alloys
Ti 5 Class A^H	F 468DT	all	30 - 39 HRC	130 - 165	125	130	120	10
Ti 5 Class B^H	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 Area^A, in²	Threads / inch	Stress Area^A, in²	Threads / inch	Stress Area^A, 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.