Engineering Physics of High-Temperature Materials. Nirmal K. Sinha
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СКАЧАТЬ of glass are unthinkable. Today, superalloys are closely linked to the aerospace industry. In aircraft and land‐based gas turbine engines, superalloys are used extensively. About 60%, by weight, of most modern gas turbine engine structural components, such as blades, vanes, and integral wheels, are made of nickel‐base superalloys. Although air travel by jet aircraft is a common mode of transportation today, how many travelers can imagine that the reliability of modern jet engines based on superalloy technology is connected to the kitchens of the world. The development of nickel‐base superalloys, actually, started almost 100 years ago due to the demands, among others, of the kitchens of the world. It started from the development of 20 wt.% Cr in an 80 wt.% Ni solid solution alloy for electrical heating elements (Betteridge and Heslop 1974; Ross and Sims 1987; Stephens 1989). Chromium was added to nickel to improve its strength and oxidation resistance.

      During the 1940–1960 period, the most widely used precipitation hardened nickel‐base alloys, belonging to the cubic system, were developed in the metallurgical laboratories for the hottest components of jet and rocket engines. In Chapter 2, chemical compositions of a few nickel‐base superalloys are given to provide a quick glance at the world of gas turbine engine materials. During the decade of 1960–1970, directionally solidified (DS) nickel‐base superalloys were developed for fabricating turbine blades used in modern gas turbine engines (Duhl 1987). Directionally solidified polycrystalline superalloys (belonging to the cubic system) are highly anisotropic, strong, and creep resistant. The long axis of turbine blades is parallel to the long axis of the columnar grains with large cross‐sectional areas. The <001> axis is parallel to the long axis of the grains. The Hall–Petch relation for strength giving preference to fine‐grained materials at low homologous temperatures is not applicable at elevated temperatures; large‐grained materials are used at high temperatures. Grain boundaries are the sources of weakness at high temperatures. Single crystals of nickel‐base alloys are now used for manufacturing turbine blades in today’s advanced jet engines (Duhl 1989). Creep, fracture, and creep modeling of nickel‐base single crystals are presented in detail in Chapter 5.

Schematic illustration of melting points of some pure metals and ice.

      The perception of ice as a cryogenic material, i.e. a material at very low temperatures, comes not from the thermodynamic point of view, but from the very fact that the temperatures associated with ice are uncomfortably cold for humans. The notion that ice is cold is enhanced by the very fact that it exists at “negative” temperatures in Celsius. This negativity is deeply rooted even in scientific minds of material scientists even though they are familiar with temperatures in kelvin and thermodynamic “homologous” scale.

      Ice has been continued to be treated as the public enemy and “ice‐rich” oceans in the Arctic and the Antarctic, two of three Earth's cryosphere zones, are often described as “ice‐infested.” This is a misconception: ice is not a cryogenic material. On Earth's surface, as pointed out earlier, ice exists at extremely high homologous temperatures. It is crystalline and transparent. These facts make ice the best analog for studies related to creep, fracture and hence most engineering properties of crystalline materials at high temperatures.

      Geophysics and geology focus on the scientific study of the earth. These fields are in advanced stages of a huge subject dealing with various aspects of the earth. The environment we live in is ever changing as the surface of the earth and its interior are constantly shifting. Geological and geophysical studies are an integral part of physics, chemistry, and mathematics and use the scientific methods developed in general. As in most fields, it is natural that our hypotheses and beliefs СКАЧАТЬ