Metals in Aircraft Construction
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In our eReader you can find the full English version of the book. Read Metals in Aircraft Construction Online - link to read the book on full screen. Our eReader also allows you to upload and read Pdf, Txt, ePub and fb2 books. In the Mini eReder on the page below you can quickly view all pages of the book - Read Book Metals in Aircraft Construction
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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.
What to read after Metals in Aircraft Construction?
You can find similar books in the "Read Also" column, or choose other free books by Wilfred Hanby to read onlineMoreLess
To quickly assess the difficulty of the text, read a short excerpt:
* 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.
What to read after Metals in Aircraft Construction?
You can find similar books in the "Read Also" column, or choose other free books by Wilfred Hanby to read onlineMoreLess
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