Selection of High Nickel Super Alloys or aircraft gas applications
Advancements in the materials have contributed in diverse ways in manufacturing gas turbine engines with higher power ratings and efficiency. Improvements in the gas turbine engine design with the passage of time have significantly been possible by the introduction of materials having considerable performance capability. Gas turbines are widely used in the aircraft and land based engines for power production. These materials have played a crucial role- higher capability of the materials to serve at the high temperatures, larger the engine efficiency.
A wide range of high strength materials such as stainless steels and super alloys are used for manufacturing gas turbines. Production of these materials usually involves advanced techniques. The materials used for gas turbine engine applications have high temperature strength as the prime criterion. Other essential factors are stress rupture life, creep properties. low fatigue life, high creep strength etc.
Titanium
Titanium for its high strength to weight ratio, is a commonly used for compressors in aeroengines. Forgings are usually used for the rotating components. For instance, the titanium based alloys are used for fan disc and low pressure compressor discs and blades. The maximum temperature limit for the high temperature applications is 540oC that limits the use of titanium alloys. Here using Nickel based alloys is recommended.
Nickel based super alloys
Considering the increased firing temperatures of the gas turbines and enhanced emission control, use of nickel base super alloys such as Hastelloy X which has high creep strength is recommended. Inconel 617 also finds applications in combustor components. Combustion liners and transition pieces of advanced and uprated machines operating at higher firing temperatures demand high strength materials.
Inconel 718 is used in the production of discs in aircraft engines. Turbine discs of single shaft heavy duty gas turbines are made from chromium-molybdneum-vanadium steel in hardened and tempered condition. With the introduction of advanced gas turbine engines with quite higher firing temperature and compressor ratios, it became crucial to use nickel base super alloy. Inconel 718 is also used for rotors in aircraft engines and aircraft gas turbines.
Identification of creep strength of a material as an essential factor for the gas turbine engines, needs of age hardening, creep and gamma prime volume fraction and consistently increasing service temperature requirements for the aircraft engine resulted in the development of wrought alloys comprising higher aluminum concentration with titanium. Casting compositions can be made for higher temperature strength as it does not require forging. Additionally cast components are intrinsically more durable than forging at high temperatures resulted by the coarse grain size of castings.
Inconel 600 for Rotating airfoils should withstand vigorous temperature, stress and conditions. An essential design factor for the nozzle materials is that they possess high temperature oxidation and corrosion resistance. Nickel base super alloys have an excellent combination of high temperature strength and resistance to hot corrosion which make them a suitable material for heavy duty gas turbine applications. So for your aircraft base industrial applications, you should choose heavy application materials, Nickel base super alloys.








