Technical Data Sheet Titanium Grades 1-4 are unalloyed and generally known as CP (Commercially Pure). The tensile and yield strength of titanium generally increases with the grade number. Titanium is 30% stronger than Steel but nearly 50% lighter and although Aluminium is lighter, Titanium is stronger and has excellent strength retention. Due to Titanium\’s weight, strength and high corrosion resistance …
Technical Data Sheet Titanium Grades 1-4 are unalloyed and generally known as CP (Commercially Pure). The tensile and yield strength of titanium generally increases with the grade number. Titanium is 30% stronger than Steel but nearly 50% lighter and although Aluminium is lighter, Titanium is stronger and has excellent strength retention. Due to Titanium\’s weight, strength and high corrosion resistance …
Technical Data Sheet Chemical Composition Limits Weight% C Mn Si P S Ni Fe Nickel Iron 4750 0.035 max 0.8 max 0.5 max 0.02 max 0.008 max 47.0-50.0 Bal As per MIL-N-14411 Comp 3 and 4 Alloy 4750/ High Perm 49® is a 48% nickel-iron alloy which combines a high saturation flux density (approx. 16000 gauss / 1.6 tesla) …
Technical Data Sheet Chemical Composition Limits Weight% C Si Co Mn Ni Fe Super Invar 32-5 0.02 0.25 5.50 0.40 32 Bal Super Invar 32-5 is a magnetic, austenitic, solid solution alloy containing iron, nickel and cobalt. 32-5 was originally designed to provide minimum thermal expansion at room temperatures. It has the austenite stability to service temperatures at least …
Technical Data Sheet Chemical Composition Limits Weight% C Si Mn P+S Cr Ni Others AFNOR Z10CNW17 0.07-0.12 1.00 max 1.00 max 0.040 P 0.030S 16.0-18.0 12.0-14.0 W 2.5-4.00 Ti 4X C / 0.80 B 0.001 – 0.006 AFNOR Z10CNWT17-13B 0.07-0.12 1.00 max 1.00 max 0.040 P 0.030S 16.0-18.0 12.0-14.0 W 2.5-4.00 Ti 4X C / 0.80 B 0.001 – …
Technical Data Sheet 35NCD16 is a low alloy steel which combines high strength and hardenability with good dimensional stability, making it an excellent alloy for large section mechanical parts or tooling of complex shapes subject to high stressses. In addition to aerospace structural applications, it is also suitable for mould for manufacturing plastic materials and bolster for drop stamps. 35NCD16 …
Technical Data Sheet Alloy 15CDV6 is a low carbon steel which combines a high yield strength (superior to SAE 4130) with good toughness and weldability. 15CDV6 can be readily welded with very little loss of properties during welding and without the need for further heat treatment. This alloy finds many applications in the aerospace and motorsports industries in such components …
Technical Data Sheet Alloy Steel 300M VAR is similar to 4340 with the addition of vanadium and a higher silicon content. Alloy 300M offers a combination of toughness and ductility at high strength levels without an increased carbon content. Alloy 300M VAR is Vacuum arc-remelted for excellent purity. 300M can also be supplied dual certified to the British aerospace standard …
Aircraft Alloy Steel 300M / AISI E4340 Mod (AMS 6417 / AMS 6419) Read More »
Technical Data Sheet NITRALLOY 135™Modified VAC-ARC is a low alloy nitriding grade of steel with moderate hardenability. As will all nitriding steels NITRALLOY 135™Modified VAC-ARC provides a high case hardness without affecting the core properties of the metal. NITRALLOY 135™Modified VAC-ARC is generally used for aircraft gears, shafts, pinions, crankshafts, cams, camshafts and bolts. Chemical Composition Limits Weight% C Mn …
Aircraft Steel 135 Mod / Nitriding (AMS 6470 / AMS 6472 / AMS 6471) Read More »
Technical Data Sheet LESCALLOY HY-TUF VAC ARC® is a high strength low alloy steel. within the tensile range 220/240 ksi (1517/1655MPa) LESCALLOY HY-TUF VAC ARC has good ductility, fracture toughness and impact strength. HY-TUF is most commonly used for aircraft landing gear, flap tracks and other structural applications. Chemical Composition Limits Weight% C Mn Si Ni Cr Mo LESCALLOY HY-TUF …
Aircraft Steel HY-TUF Vac Melt (AMS 6418 / AMS 6425) Read More »
