The principles of alloying Ni heat resistant alloys, possessing high-temperature corrosion resistance

被引:0
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作者
Koval', A.D. [1 ]
Belikov, S.B. [1 ]
Sanchugov, E.L. [1 ]
机构
[1] Zaporozhskij Natsional'nyj TU, Zaporozh'e, Ukraine
关键词
Aircraft materials - Alloying - Aluminum - Chromium - Composition effects - Corrosion resistance - Heat resistance - Kerosene - Nickel alloys - Rare earth elements - Refractory metals - Titanium;
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摘要
An influence of Cr additives (1.5-27.6%) on high-temperature corrosion processes in alloys is investigated. The alloys of Ni-Cr, Ni-Cr-Al, Ni-Cr-(Al+Ti), Ni-Cr-Co-W-Mo-(Al+Ti) systems are tested in the combustion products of aviation kerosene, containing 1% Si, with addition of Na salt water solution. The class of heat-and-corrosion resistant alloys (ChS70VI, 3MI-3, SNL-1, ChS91VI, 3MI-11) with moderate or high (30%) content of Cr, Ti/Al more than 1, and balanced content of refractory and rare earth elements is created.
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页码:5 / 9
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