The book Metals in Aircraft Construction was written by author Wilfred Hanby Here you can read free online of Metals in Aircraft Construction book, rate and share your impressions in comments. If you don't know what to write, just answer the question: Why is Metals in Aircraft Construction a good or bad book?
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* R. A. * IZOD* BRINELLNo. * 35 48 16% 35% 70 192 62. Steel having Good Wearing Surface and Gore resisting large Crushing Load. A 0. 25 per cent, carbon steel is used for parts which demand a good wearing surface and a core capable of withstanding heavy crushing loads. This steel is fairly brittle, and will not stand working under conditions of shock. After normalizing at 870 degrees C. , the following minimum mechanical test results should be obtained : Y. S. * M. S. * E. * R. A. * IZOD* BRINE...LLNo. * 23 38 30% 50% 15 167 After annealing at 780 degrees C. , it should give : Y. S. * M. S. * E. * R. A. * IZOD* BRINELL No. * 22 32 36% 63% 60 134 CARBURIZING TREATMENT : Carburize at 950 degrees C. For 5 hours. Reheat parts to 870 degrees C. , and quench in water. Reheat to 770 degrees C. , and quench in water. After this treatment the mechanical tests on the core should be not less than : Y. S. * M. S. * E. * R. A. * IZOD* BRINELLNo. * 40 55 10% 20% 30 248 63. Low Carbon 3 per cent. Nickel Steel for Parts demand- ing Tough Core.
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