Feasibility of manufacturing combustion chambers for aeronautical use in Mexico
Tài liệu tham khảo
Al-Jarba, 2004, Carbon containing single-crystal nickel-based superalloys: Segregation behavior and carbide formation, Journal of the Minerals, 56, 50
Allen, 1991, Development of a product manufacturing analysis and costing, International Journal of Advanced Manufacturing Technology, 6, 205, 10.1007/BF02601440
Alniak, 2010, Hot forging behavior of nickel based superalloys under elevated temperatures, Material & Design, 31, 1588, 10.1016/j.matdes.2009.09.020
European Aeronautic Defence and Space Company, 2012
Ashby, 2009, 545
Campbell, 2008, 212
Chryssolouris, 2006, 68
Forbes-Jones, 1999, The structural evolution of superalloy ingots during hot working, Journal of Minerals, 51, 27
Groover, 2007, 215
Ipek, 2012, An expert system based material approach to manufacturing, Material & Design, 47, 331, 10.1016/j.matdes.2012.11.060
Jang, 2011, Oxidation behavior of wrought nickel-based superalloys in various high temperature environments, Transactions of Nonferrous Metals Society of China, 21, 1524, 10.1016/S1003-6326(11)60891-1
Kashyap, 2000, Activation energy for superplastic deformation of IN718, Scripta Materialia, 43, 429, 10.1016/S1359-6462(00)00453-X
Lefebvre, 2010, 351
Mattingly, 2002, 325
Plan de Vuelo Nacional, 2009
Pollock, 2010, New Co-based γ–γ′ high-temperature alloys, Journal of Minerals, 62, 58
Pollock, 2006, Nickel-based superalloys for advanced turbine engines: Chemistry, microstructure, and properties, Journal of Propulsion and Power, 22, 361, 10.2514/1.18239
Pro-Aéreo 2012–2020, 2011
Reed, 2006, 33
Schreiber, K., Floege, H. (2007, July). Method for the Manufacture of a Combustion Chamber of a Gas-Turbine Engine. US Patent No: US 7, 243,426 B2.
Shen, 2000, Manufacturing of aerospace forgings, Journal of Materials Processing Technology, 98, 189, 10.1016/S0924-0136(99)00198-3
Swift, 2003, 1
The Boeing Company 2010 Annual Report. (2011). Chicago, IL: W. James McNerney, Jr.