TA1 TA2 TC4 GR1 High Strength Aerospace Titanium Forged Components 


   1,Titanium Forging Application  1. Aerospace  Aircraft structural components  Jet engine components: fan blades, housings, disks, compressor blades, disks, short shafts, housings  Spacecraft components: blades for fuel tanks, attitude control engine housings, liquid fuel turbopumps  2. Turbine blades for power generation  3. Medical field  Implants: joint replacements (hip and knee implants), spinal implants and fixation devices  Surgical instruments: for the manufacture of surgical tools, forceps and scalpels  4. Automotive  High-performance engine components: connecting rods, crankshafts  Suspension systems  5. High-end equipment manufacturing  High-speed rail and rail transportation  Large machine tools and precision machinery   2.Product Details
   	 		 			 			 Attribute  			 |  			 			 Details  			 |  		
 		 			 			 Alloy  			 |  			 			 TA1, TA2, TA3, TA9, TC4, GR1, GR2, GR5  			 |  		
 		 			 			 Standard  			 |  			 			 GB/T 2965 - 2007, GB/T 13810 - 2007, ASTM B348, ASTM F67, ASTM F136, AMS4928, MIL4911  			 |  		
 		 			 			 Dimensions  			 |  			 			 Diameter: 3.0 - 200mm<br>Length: 1000 - 6000mm<br>Tolerance: H7 - H11  			 |  		
 		 			 			 Applications  			 |  			 			 Metallurgy, Electronics, Medical, Chemical, Petroleum, Pharmaceutical, Aerospace  			 |  		
 		 			 			 Process  			 |  			 			 α+β forging,β machining forging,Multi-directional die forging,Partial die forging,Isothermal die forging  			 |  		
 		 			 			 MOQ  			 |  			 			 1PCS  			 |  		
 		 			 			 Size  			 |  			 			 Customized  			 |  		
 	 
    
   3,Production Photos
   


   4,Product Features  High strength  Corrosion resistance  High fatigue and impact resistance  Thermal Stability. Titanium has a melting point of 1,668°C (3,034°F)   5,Mechanical/Mechanical Properties of Titanium forging
   	 		 			 			 Alloy  			 |  			 			 Condition  			 |  			 			 Thickness Range/mm  			 |  			 			 Tensile Strength (Rm)/MPa  			 |  			 			 Yield Strength (Rp0.2)/MPa  			 |  			 			 Elongation after Fracture /% ≥  			 |  			 			 Bending Radius  			 |  		
 		 			 			 TA2  			 |  			 			 M  			 |  			 			 0.3 - 1.0  			 |  			 			 440 - 620  			 |  			 			 ≥320  			 |  			 			 ≥35  			 |  			 			 ≥100°, 3t  			 |  		
 		 			 			    			 |  			 			    			 |  			 			 > 1.0 - 2.0  			 |  			 			 440 - 620  			 |  			 			 ≥320  			 |  			 			 ≥30  			 |  			 			 ≥100°, 3t  			 |  		
 		 			 			    			 |  			 			    			 |  			 			 > 2 - 5.0  			 |  			 			 440 - 620  			 |  			 			 ≥320  			 |  			 			 ≥25  			 |  			 			 ≥90°, 3t  			 |  		
 		 			 			    			 |  			 			    			 |  			 			 > 5 - 10.0  			 |  			 			 440 - 620  			 |  			 			 ≥320  			 |  			 			 ≥25  			 |  			 			 -  			 |  		
 		 			 			    			 |  			 			    			 |  			 			 > 10.0 - 30  			 |  			 			 440 - 620  			 |  			 			 ≥320  			 |  			 			 ≥18  			 |  			 			 -  			 |  		
 		 			 			 TC4  			 |  			 			 M  			 |  			 			 0.5 - 1.8  			 |  			 			 925 - 1150  			 |  			 			 ≥870  			 |  			 			 ≥12  			 |  			 			 ≥105°, 9t  			 |  		
 		 			 			    			 |  			 			    			 |  			 			 > 1.8 - 4.0  			 |  			 			 925 - 1150  			 |  			 			 ≥870  			 |  			 			 ≥12  			 |  			 			 ≥105°, 10t  			 |  		
 		 			 			    			 |  			 			    			 |  			 			 > 4.0 - 5.0  			 |  			 			 925 - 1150  			 |  			 			 ≥870  			 |  			 			 ≥10  			 |  			 			 ≥105°, 10t  			 |  		
 		 			 			    			 |  			 			    			 |  			 			 > 5.0 - 10.0  			 |  			 			 925 - 1150  			 |  			 			 ≥825  			 |  			 			 ≥10  			 |  			 			 -  			 |  		
 		 			 			    			 |  			 			    			 |  			 			 > 10.0 - 100  			 |  			 			 925 - 1150  			 |  			 			 ≥825  			 |  			 			 ≥9  			 |  			 			 -  			 |