AMS 4928 Gr5 6Al4V Aerospace Titanium Bars

AMS 4928 Gr5 6Al4V Aerospace Titanium Bars

Products Detail of AMS 4928 Titanium Bars

Introduction of AMS 4928 Aerospace Material Specification Ti-6AL-4V

Titanium Alloy Bars, Wire, Forgings, Rings, and Drawn Shapes, 6Al - 4V, Annealed UNS R56400

Alpha-Beta titanium alloy

It is part of the Aerospace Material Standards series from SAE International.

This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, drawn shapes, and stock for forging or flash welded rings.  

Application: These products have been used typically for parts requiring moderate strength with a maximum service temperature in the 750 to 900°F (399 to 510℃) range depending on time at temperature where the product is to be used in the annealed condition, but usage is not limited to such applications.

Bars: Hot finished with or without subsequent cold reduction,annealed,and descaled.Unless prohibited by purchaser,bars may be solution heat treated before annealing.A machined or ground surface is permitterd unless prohibited by the purchaser. Alloy shall be multiple melted. The product shall be processed to the final thickness/diameter by metallurgical working operations prior to any straightening, dimensional sizing or surface finishing operation. Bar shall not cut form plate.

Annealing: Heat to a temperature within the range 1300 to 1450°F (704 to 788℃),hold at the selected temperature within +/-25°F (+/-14℃) for not less than 1 hour, and cool as required.