
Product Our Products


Aluminium Aluminium Pipe/Tube

Aluminium Aluminium Rod/Bar

Copper Copper Sheet/Plate

Copper Copper Pipe/Tube

Copper Copper Rod/Bar

Stainless Steel Changjin Stainless Steel

Processing Metal Capillary

Aluminium Aluminum Extrusions

Aluminium Aluminium Alloy

Aluminium Aluminium Profile

Aluminium Aluminum Forgings

Copper Copper Forging

Copper Copper Casting

Copper Copper Product

Aluminium Special Aluminum Plate

Copper Copper Profiles

Aluminium Aluminum Fittings

Copper Brass Series

Aluminium Aluminum Structure Welding

Copper Copper Plate Series

Copper Phosphor Copper Series

Copper Red Copper Series

Copper Cupronickel Series

Copper Beryllium Copper Series
TI5.8AL4SN3.5ZR0.7NB TIMETAL 174 834
TI5.8AL4SN3.5ZR0.7NB TIMETAL 174 834 Timetal 834 is a near alpha titanium alloy offering increased tensile strength and creep resistance up to 600 186C 1112 186F together with improved fatigue strength compared with alloys such as 685 and 829. The alloy is weldable and has good forgeability. Composition Ti Rem Al 5.56.1 Sn 3.05.0
TIMET TIMETAL 174 834 Ti5.8Al4Sn3.5Zr0.7Nb0.5Mo0.35Si
TIMET TIMETAL 174 834 Ti5.8Al4Sn3.5Zr0.7Nb0.5Mo0.35Si0.06C Titanium Alloy.pdf: Price: EMAIL US sales look s.com: IN STOCKS: Documents SGS MSDS Factory Documents. Online Service look s 27660005 . Material Notes: HighStrength, High Temperature, Creep Resistant AlloyIndustry Specifi ions: France: TA6EZ r4Nb.Features: TIMETAL 834 is a near alpha titanium : TIMET
Analysis of backs tered ultrasound amplitude of
01/02/2009 0183 32The titanium alloy Ti5.8Al4Sn3.5Zr0.7Nb0.5Mo0.3Si, also called IMI 834, is a near titanium alloy used for rotating engine components. Through processing, it acquires a bimodal microstructure consisting of primary, p, grains and secondary, s, colonies inherited from grains. This bimodal microstructure is designed for improved mechanical properties such as high fatigue and Cited by: 7
On the occurrence of dynamic strain aging in nearalpha alloy Ti
On the occurrence of dynamic strain aging in nearalpha alloy Ti5.8Al4Sn3.5Zr0.7Nb0.5Mo0.35Si. Nidhi Singh 1, Nishtala Prasad 1 and Vakil Singh 1 Metallurgical and Materials Transactions A volume 30, pages 25472549 1999 Cite this article
TIMET TIMETAL 174 834 Ti5.8Al4Sn3.5Zr0.7Nb0.5Mo0.35Si
TIMET TIMETAL 174 834 Ti5.8Al4Sn3.5Zr0.7Nb0.5Mo0.35Si0.06C Titanium Alloy Categories: Metal Nonferrous Metal Titanium Alloy Alpha/Near Alpha Titanium Alloy. Material Notes: HighStrength, High Temperature, Creep Resistant Alloy. Industry Specifi ions: France: TA6EZ r4Nb. Features: TIMETAL 834 is a near alpha titanium alloy offering increased tensile strength and creep resistance
HIGH STRENGTH, HIGH TEMPERATURE, CREEP RESISTANT ALLOY
Ti5.8Al4Sn3.5Zr0.7Nb0.5Mo0.35Si0.06C ELEMENT WEIGHT Aluminum 5.50 6.10 Tin 3.00 5.00 Zirconium 3.00 5.00 Niobium 0.50 1.00 Molybdenum 0.25 0.75 Silicon 0.20 0.60 Carbon 0.04 0.08 Iron 0.05 Oxygen 0.075 0.15 Nitrogen 0.03 Hydrogen 0.006 Residual Elements,each 0.05 Residual Elements,total 0.20 Titanium Remainder CHEMICAL COMPOSITION Table 1 PHYSICAL
Analysis of backs tered ultrasound amplitude of
The amplitudes of backs tered ultrasound were measured at 10 MHz on different samples of the near titanium alloy Ti5.8Al4Sn3.5Zr0.7Nb0.5Mo0.3Si.
Titanium Alloys and Their Characteristics: Part One Total Materia ...
Ti 6Al 4Sn 3.5Zr 0.5Mo 0.35Si 0.7Nb 0.06C. The niobium is added for oxidation resistance and the carbon to allow a greater temperature range over which the alloy is a mixture of , in order to facilitate thermomechanical processing. This particular alloy is used in the manufacture of aero engine discs and has replaced discs ...
NearTi JST
For nearalpha DAT54, Ti5.8Al4Sn3.5Zr2.8Mo0.7Nb0.4Si0.06C, designed as a compressor disk alloy, the optimum primary alpha was defined 17vol. in the transformed beta. The fullscale disks in the alloy were successfully manufactured through the melting by PPCVARVAR and the thermomechanical processing by GFM press die forge. The solution treatment for the above structure, at beta transus
JST
Ti 5.8Al 4Sn 3.5Zr 0.7Nb 0.5Mo 0.35Si 0.06C IMI834 a 5.1 7.7 4.55 LPCHPC, MUT: 863 K 2 A380 6 Materia Japan 558 2016 b b a ab b a ab a b