Results 101 to 110 of about 3,572 (225)
Silicon-slurry/aluminide coating [PDF]
, 1983 A low cost coating protects metallic base system substrates from high temperatures, high gas velocity ovidation, thermal fatigue and hot corrosion and is particularly useful fo protecting vanes and blades in aircraft and land based gas turbine engines. A
Deadmore, D. L., Young, S. G.
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Environmental protection of titanium alloys at high temperatures [PDF]
Various concepts were evaluated for protecting titanium alloys from oxygen contamination at 922 K (1200 F) and from hot-salt stress-corrosion at 755 K (900 F).
Seltzer, M. S. +2 more
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High integrity titanium aluminide compacts
Metal Powder Report, 1991 Abstract Titanium aluminide alloys are important candidates for applications in advanced gas turbine engines and high mach airframes. Compared with conventional titanium alloys, the aluminides are lower in density, higher in modulus, and have better high temperature oxidation and creep resistance.
W. John Porter +2 more
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Special Issue "Lightweight Structural Materials for Automotive and Aerospace". [PDF]
Materials (Basel), 2022 Czerwinski F.
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Materials and structures for hypersonic vehicles [PDF]
Hypersonic vehicles are envisioned to require, in addition to carbon-carbon and ceramic-matrix composities for leading edges heated to above 2000 F, such 600 to 1800 F operating temperature materials as advanced Ti alloys, nickel aluminides, and metal ...
Dixon, Sidney C. +2 more
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Effect of a High-Temperature Treatment on Structural-Phase State and Mechanical Properties of IMC of the Ti-25Al-25Nb at.% System. [PDF]
Materials (Basel), 2022 Skakov M +7 more
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Structures and materials technology for hypersonic aerospacecraft [PDF]
Major considerations in structural design of a transatmospheric aerospacecraft are discussed. The general direction of progress in structures and materials technology is indicated, and technical areas in structures and materials where further research ...
Card, Michael F. +2 more
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Some Aspects of Oxidation and Reduction Processes in Ti-Al and Ti-Al-Nb Systems. [PDF]
Materials (Basel), 2022 Mitoraj-Królikowska M, Drożdż E.
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Optimization of the Dry Turning Process of Ti48Al2Cr2Nb Aluminide Based on the Cutting Tool Configuration. [PDF]
Materials (Basel), 2022 García-Martínez E +5 more
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Titanium Aluminides for Aerospace Applications
Superalloys 1992 (Seventh International Symposium), 1992 The U. S. aircraft industry has realized much of its success because of the steady improvements in specific thrust (thrust/weight) and in specific fuel consumption (fuel used/unit of thrust). The desire to further improve specific thrust both for IHPTET (Integrated High Performance Turbine Engine Technology) and NASP (National Aerospace Plane) programs
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