Top Suppliers Titanium alloy 10V-2Fe-3Al UNS R56410 to Brazil Factory
continue to improve, to ensure product quality in line with market and customer standard requirements. Our company has a quality assurance system have been established for Top Suppliers Titanium alloy 10V-2Fe-3Al UNS R56410 to Brazil Factory, We sincerely welcome both foreign and domestic business partners, and hope to work with you in the near future!
HY Titanium 10-2-3 Material grades and equivalents
10-2-3 Titanium, UNS R56410
Introduction
HY Titanium 10-2-3 is a near beta alloy developed as a high strength forging alloy. This grade provides the best combination of strength and toughness of the commercially available titanium alloys. Its strength permits about a 27% weight savings when compared to Ti-6Al-4V. At the 180 ksi tensile strength level, the K1cvalue is 40 ksi-in ½ minimum. Solution treated and aged material possesses excellent resistance to stress corrosion cracking, typically K1scc being greater than 0.8 K1c. Solution treated material should not be subject to long term exposure in the 500-800°F range. This could result in high strength but low ductility.
High strength condition: Solution treat 60-100°F below the beta transus (typically 1460-1480°F), not less than 30 minutes, water quench. Age 900-975°F not less than 8 hours, air cool. For lower strength, overage in the 950-1150°F range. This alloy is deep hardenable, capable of high strengths in sections up to approximately 4″ thick.
This grade is usually supplied as billet or bar, finish rolled or forged in the alpha-beta field. For the high strength condition, the forging is usually given a pre-form forge above the beta transus, followed by 15-25% reduction below the beta transus.
Chemistry Composition
|
|
V |
Al |
Fe |
C |
N |
O |
H |
Y |
Others, |
Others, |
Ti |
|
MIN |
9.0 |
2.6 |
1.6 |
- |
- |
- |
- |
- |
- |
- |
- |
|
MAX |
11.0 |
3.4 |
2.22 |
0.05 |
0.05 |
0.13 |
0.015 |
0.005 |
0.10 |
0.30 |
Balance |
Features
- High strength and toughness
- Weight savings when compared to Ti-6Al-4V
- Excellent resistance to stress corrosion cracking
Applications
- Hand and die forgings
- Aircraft landing gear
- Golf club driver faces
Physical Properties
Density: 0.168 lb/inch³
Nominal Beta Transus: 1470°F
Poisson’s ratio: 0.32
Thermal Expansion: 75-800°F, 5.4×10-6 in/in°F
Tensile Modulus: 15.9×106 psi
Modulus: 16.2×106 psi
* 70°F to indicated temperature.
Mechanical Properties
Minimum Mechanical Properties AMS 4984, solution treated and aged
|
Ultimate Tensile Strength, ksi |
173 |
|
Ultimate Tensile Strength, ksi |
160 |
|
0.2% Yield Strength, ksi |
4 |
|
Reduction of Area, % |
Report |
|
fracture toughness, k1C |
40 ksi |
AMS 4987, single solution heat treat & overage
|
Ultimate Tensile Strength, ksi |
140 |
|
0.2% Yield Strength, ksi |
130 |
|
Elongation, % |
8 |
|
Reduction of Area, % |
20 |
|
fracture toughness, k1C |
80 ksi |
| Regular shape for all kinds of alloys | |||
| Form | Specification | Supply Form | Others |
| Sheet | Thickness：0.40-4.75mm，General Width：1000、1219、1500mm | Whole Coil or piece of it | Cold Annealed，Surface 2B、2E |
| Plate | Thickness：4.76-60mm，Width：1500、2000、2500mm，Length：3000、6000、8000、8500mm（Under 10mm plate can be coiled） | Whole Coil or piece of it | Single hot rolling，Solid solution annealed state，Surface 1D |
| Belt | Thickness：0.10-3.0mm，Width：50-500mm | Whole Coil or Specified size | Cold Annealed，Surface 2B、2E |
| Bar & Rod | Rolled barΦ5-45mm，Length≤1500mm | Polished Bar（circle、Square） | Solution annealing,descaling |
| Forged barΦ26-245mm，Length≤4000mm | |||
| Weld tube | Outer diameterΦ4.76-135mm，Wall Thickness0.25-4.00mm，Length：≤35000 mm | Base on your requirement | |
| Seamless Tube | Outer diameterΦ3-114mm，Wall Thickness0.2-4.5mm | Base on your requirement | |
| Wire | Outer diameterΦ0.1-13mm | Base on your requirement | Ni & Ni alloy, Ti & Ti alloy |
| Forged piece | discs,rings,squares,blocks,slabs | Base on your requirement | Steel, Alloy |
| Flangs | All kinds of Flangs | Base on your requirement | Steel, Alloy |
| Welding Material | Coil wire Φ0.025mm-1.6mm | Base on your requirement | Certificate of Origin：America, Sweden, Britain, Germany, Austria, Italy, France. |
| Straight WireΦ1.6mm-4.0mm | |||
| Welding rodΦ1.2mm-4.0mm | |||
| Tube | Elbow, three links, four links, different diameter size | Base on your requirement | Ni & Ni alloy, Ti & Ti alloy |
| Explosive bonded laminate | Raw Sheet Thickness≥2mm | Base on your requirement | Ni & Ni alloy, Ti & Ti alloy |
Experimentální odlévání monelu na katedře strojírenské technologie při TU v Liberci – Monel je slitina niklu a mědi. Název Monel je registrován jako trademark americké firmy Specific Metals Corporation. Monel vyrobil v roce 1901 Robert Crooks Stanley, slitinu pojmenoval po tehdejším prezidentu firmy Ambrose Monellovi.
Monel vykazuje výborné mechanické vlastnosti a chemickou odolnost v náročném prostředí, např. v dlouhodobém kontaktu se slanou vodou, ale i v chemickém průmyslu. Často bývá využit tam, kde již nedostačují vlastnosti nerezových ocelí.
Monel is a group of nickel alloys, largely composed of nickel (up to sixty seven%) and copper, with tiny quantities of iron, manganese, carbon, and silicon. More powerful than pure nickel, Monel alloys are resistant to corrosion by quite a few agents, like promptly flowing seawater. They can be fabricated quickly by very hot- and chilly-working, machining, and welding.[2]
Monel was made by David H. Browne, main metallurgist for Global Nickel Co. Monel alloy four hundred is a binary alloy of the identical proportions of nickel and copper as is found naturally in the nickel ore from the Sudbury (Ontario) mines and is thus thought of a puritan alloy. Monel was named following business president Ambrose Monell, and patented in 1906.[three] Just one L was dropped, for the reason that loved ones names were being not allowed as trademarks at that time.[one] The title is now a trademark of Specific Metals Corporation.
Visit my site for additional Recommendations, Films, Do it yourself assignments and additional:
http://www.mjlorton.com/
—————————–Click “Display additional”—————————————
A information on making use of the correct applications to crimp connectors, strip wire and implement warmth shrink.
You should guidance my information generation by making use of my Amazon Retail store:
http://astore.amazon.com/m0711-twenty
Purchase these applications and connectors below: http://astore.amazon.com/m0711-twenty?node=ten&site=one
——————— Click “Display additional” ——————————-
My site and forum:- http://www.mjlorton.com
Donations and contributions:- http://www.mjlorton.com
My techie channel MJLorton – Solar Power and Digital Measurement Products – http://www.youtube.com/MJLorton
My Techie Amazon Retail store: http://astore.amazon.com/m0711-twenty
My other channel VBlogMag – For nearly any matter beneath the sun! – http://www.youtube.com/VBlogMag
My VBlogMag Amazon Retail store: http://astore.amazon.com/vblogmag-twenty
———————————————————————–
=================================================
Online video sponsor, Pass Ltd – their internet websites:
http://www.tester.co.united kingdom/?cmid=QmhzQjcxYjVlc1E9&afid=bFcwbzliNzVDc289&ats=K2EyUjZNTDh3UTA9 – Examination Products and Examination-meter suppliers and
http://www.calibrate.co.united kingdom/?cmid=QmhzQjcxYjVlc1E9&afid=bFcwbzliNzVDc289&ats=S3Yxd2tOMjVISzA9 – Calibration and support of exam tools
=================================================
Additional dialogue and link to NASA information below:
http://mjlorton.com/forum/index.php?matter=244.
In this online video:
* Deciding upon the correct wire gauge (AWG – American Wire Gauge) for the crimp connector.
* Employing the correct applications to strip the insulation from the wire.
* The correct way to insert the wire into the crimp connector
* Employing the correct crimp applications to crimp the connector
* How to implement warmth shrink accurately to the wire and crimp connector.
