Technical Data Sheet Alloy 230 is a nickel-chromium-tungsten-molybdenum alloy that combines excellent high temperature strength, outstanding resistance to nitriding environments and excellent long term thermal stability. Alloy 230 is easily fabricated and has very good forming and welding characteristics. Due to Alloy 230 combined properties it is very well suited to a wide variety of component applications in the aerospace …
Technical Data Sheet Haynes 188 / Udimet alloy 188 is a cobalt based nickel-chromium-tungsten alloy with a small addition of lanthanum to give a very protective scale. Alloy 188 combines excellent high-temperature strength with good resistance to both oxidizing environments up to 2000°F and to sulfate deposit hot corrosion. Alloy 188 has good forming characteristics and is capable of being …
Technical Data Sheet Alloy PK33 is a nickel- chromium – cobalt precipitation hardenable alloy but the addition of Molybdenum makes Alloy PK33 solid-solution strengthened. PK33 is commonly used in gas turbines as flame tubes because of its high temperature strength, creep resistance and welded sheet structures. Chemical Composition Limits Weight% Ni Cr Mo Fe Al Ti C PK33 Bal 16-20 …
Technical Data Sheet Alloy PE16 is a precipitation-hardenable nickel-iron-chromium alloy with an addition of molybdenum for solid-solution strengthening. PE16 has good strength and oxidation resistance at temperature to about 1380ºF (750ºC). Alloy PE16 is designed to provide a precipitation-hardened material having excellent hot-working, cold-working and welding characteristics. PE16 is commonly used in gas-turbines components and in nuclear reactors. Chemical Composition …
Technical Data Sheet Alloy PE11 (UNS N09901) main elements are nickel, iron and chromium, but the additions of Aluminium, Titanium and Molybdenum makes the PE11 both precipitation hardened and solid-solution strengthened. PE11 is commonly used in gas turbines because of its high tensile ductility strength and as it was developed for use at 550°C (1020°F). Chemical Composition Limits Weight% Ni …
Technical Data Sheet Alloy 105 is a wrought nickel-colbalt-chromium base alloy which also contains molybdenum, aluminium and titanium which results in a high strength alloy that can be used in conditions up to 950°C with good creep resistance. Alloy 105 is used for turbine blades, discs, forgings, ring sections, bolts and fasteners. Chemical Composition Limits Weight% C Si Cu Fe …
Technical Data Sheet Alloy 201 (UNS N02201) is a commercially pure wrought nickel, with good mechanical properties and an excellent resistance to many corrosives. Nickel 201 has low carbon (0.02% max) for applications over 315°C it is mainly used for food processing equipment, chemical shipping drums, caustic handling equipment and piping, electronic parts, aerospace and missile components, rocket motor cases, …
Technical Data Sheet Alloy 200 (UNS N02200) is a commercially pure wrought nickel, with good mechanical properties and an excellent resistance to many corrosive environments. Alloy 200 has good thermal, electrical and magnetostrictive properties. Alloy 201 is exactly the same but with less carbon for hotter applications. Both Alloy 200 and Alloy 201 are generally used in food processing equipment, …
Aluminium Alloy 1050A (Alloy 1050) is a popular grade of Aluminium. 1050A Aluminium Alloy is known for its excellent corrosion resistance, high ductility and highly reflective finish. Alloy 1050A (Alloy 1050) is typically used for chemical process plant equipment, food industry containers, pyrotechnic powder, architectural flashings, lamp reflectors, cable sheathing. Chemical Composition Limits Weight% Si Fe Cu Mn Mg Zn …
The AD700 project was launched in 1998 with the goal of establishing a demonstration power station with steam parameters of 700℃/720℃/35 MPa and a unit efficiency of more than 50%. The United States and Japan also carried out research on the A-USC project in 2001 and 2008. 1-2] 617 Nickel-based alloy is a Cr-Co-Mo type nickel-based high-temperature alloy mainly based …
