{"id":574,"date":"2025-06-16T08:58:51","date_gmt":"2025-06-16T08:58:51","guid":{"rendered":"https:\/\/dura-alloy.com\/?post_type=product&#038;p=574"},"modified":"2025-06-16T08:58:51","modified_gmt":"2025-06-16T08:58:51","slug":"30crmnsini2a","status":"publish","type":"product","link":"https:\/\/www.dura-alloy.com\/es\/producto\/30crmnsini2a\/","title":{"rendered":"30CrMnSiNi2A"},"content":{"rendered":"<p style=\"text-align: center;\"><strong><span>Alcance del suministro de Aviation Group:<\/span><\/strong><\/p>\n<p style=\"text-align: center;\"><strong><span>Varillas redondas, chapas de acero, piezas forjadas no est\u00e1ndar, anillos, tubos sin soldadura, personalizaci\u00f3n no est\u00e1ndar, \u00a1bienvenido a preguntar!<\/span><\/strong><\/p>\n<p><strong><span>1.\u00a0<\/span><\/strong><strong><span>Introducci\u00f3n a los materiales 30CrMnSiNi2A<\/span><\/strong><\/p>\n<p><span>\u00a0 \u00a0 \u00a0 Tras el tratamiento t\u00e9rmico, el acero estructural de aleaci\u00f3n 30CrMnSiNi2A puede obtener alta resistencia, buena plasticidad y tenacidad, buena resistencia a la fatiga y tenacidad a la fractura, y baja tasa de propagaci\u00f3n de grietas por fatiga.<\/span><\/p>\n<p><strong><span>2. Composici\u00f3n qu\u00edmica de 30CrMnSiNi2A<\/span><\/strong><\/p>\n<table border=\"-\" width=\"1120\">\n<tbody>\n<tr>\n<td width=\"97\"><span>aleaci\u00f3n<\/span><\/td>\n<td width=\"64\">%<\/td>\n<td width=\"51\"><span>Cromo Cr<\/span><\/td>\n<td width=\"51\"><span>Carbono C<\/span><\/td>\n<td width=\"51\"><span>Manganeso Mn<\/span><\/td>\n<td width=\"51\"><span>Silicio Si<\/span><\/td>\n<td width=\"51\"><span>F\u00f3sforo P<\/span><\/td>\n<td width=\"51\"><span>Azufre S<\/span><\/td>\n<td width=\"51\"><span>Ni<\/span><\/td>\n<\/tr>\n<tr>\n<td rowspan=\"2\" width=\"97\"><span>30crmnsini2a<\/span><\/td>\n<td width=\"64\"><span>Valor m\u00ednimo<\/span><\/td>\n<td width=\"51\">0.90<\/td>\n<td width=\"51\">0.27<\/td>\n<td width=\"51\">1.0<\/td>\n<td width=\"51\">0.9<\/td>\n<td width=\"51\">&#8211;<\/td>\n<td width=\"51\"><span>&#8211;<\/span><\/td>\n<td width=\"51\">1.4<\/td>\n<\/tr>\n<tr>\n<td width=\"64\"><span>Valor m\u00e1ximo<\/span><\/td>\n<td width=\"51\">1.20<\/td>\n<td width=\"51\">0.34<\/td>\n<td width=\"51\">1.3<\/td>\n<td width=\"51\">1.2<\/td>\n<td width=\"51\">0.020<\/td>\n<td width=\"51\"><span>0.020<\/span><\/td>\n<td width=\"51\">1.8<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<p><strong><span>3.<\/span><\/strong><span>\u00a0Propiedades mec\u00e1nicas de 30CrMnSiNi2A<\/span><\/p>\n<p><span>Resistencia a la tracci\u00f3n \u03c3b (MPa): 1)1767; 2)1627<\/span><\/p>\n<p><span>Elongaci\u00f3n \u03b45 (%): 1)12; 2)13<\/span><\/p>\n<p><span>Contracci\u00f3n de secci\u00f3n \u03c8 (%): 50<\/span><\/p>\n<p><span>Valor de la tenacidad al impacto \u03b1ku (J\/cm2): 1)79; 2)90<\/span><\/p>\n<p><span>Tama\u00f1o de la muestra: bar<\/span><\/p>\n<p><strong><span>IV. Propiedades f\u00edsicas de 30CrMnSiNi2A<\/span><\/strong><\/p>\n<p><strong><span>\u00a0 \u00a0 \u00a0 30CrMnSiNi2A\u00a0<\/span><\/strong><strong><span>especificaciones de tratamiento t\u00e9rmico y estructura metalogr\u00e1fica:<\/span><\/strong><\/p>\n<p><span>\u00a0 \u00a0 \u00a0 Especificaciones del tratamiento t\u00e9rmico: 1) Enfriamiento en aceite a 890-900\u2103, templado a 200-300\u2103, enfriamiento al aire; 2) Calentamiento a 890-900\u2103, templado en un tanque de sal nitrificante a temperatura media de 210-280\u2103 durante 1 hora, enfriamiento al aire y, a continuaci\u00f3n, enfriamiento posterior a 200-300\u2103, enfriamiento al aire.<\/span><\/p>\n<p><span>Estructura metalogr\u00e1fica: 1) Revenido a alta temperatura despu\u00e9s de laminaci\u00f3n en caliente o laminaci\u00f3n en fr\u00edo es perlita; 2) Normalizado y revenido a alta temperatura es cortexita revenida; 3) Recocido isot\u00e9rmico es perlita y ferrita de chapa; 4) Estado normalizado es martensita y bainita; 5) Estado usado es martensita revenida.<\/span><\/p>\n<p><strong>\u00a0<\/strong><strong><span>\u00a0 \u00a0 \u00a0 Temperatura cr\u00edtica de 30CrMnSiNi2A\u00a0<\/span><\/strong><strong><span>acero<\/span><\/strong><\/p>\n<table border=\"-\">\n<tbody>\n<tr>\n<td width=\"164\"><span>Punto cr\u00edtico<\/span><\/td>\n<td width=\"164\"><span>Ac1<\/span><\/td>\n<td width=\"164\"><span>AC3<\/span><\/td>\n<td width=\"82\">Sra.<\/td>\n<td width=\"82\"><span>Observaci\u00f3n<\/span><\/td>\n<\/tr>\n<tr>\n<td width=\"164\"><span>Temperatura (valor aproximado)\/\u2103<\/span><\/td>\n<td width=\"164\">705\u00a0 705<\/td>\n<td width=\"164\">800\u00a0 815<\/td>\n<td width=\"82\">321\u00a0 \u00a0314<\/td>\n<td width=\"82\">1\u00a0 \u00a02<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<p><span>Nota: 1. Composici\u00f3n del acero (%) utilizado: 0,27C, 1,05Si, 1,06Mn, 1,05Cr, 1,66Ni, 0,013P, 0,005S;<\/span><\/p>\n<p><span>\u00a0 \u00a0 \u00a0 \u00a02. Composici\u00f3n del acero (%) utilizado: 0,30C, 1,10Si, 1,07Mn, 1,06Cr, 1,50Ni, 0,014P, 0,005S.\u00a0<\/span><\/p>\n<p><strong><span>V.\u00a0<\/span><\/strong><strong><span>Caracter\u00edsticas y \u00e1mbito de aplicaci\u00f3n de 30CrMnSiNi2A<\/span><\/strong><\/p>\n<p><span>\u00a0 \u00a0 \u00a0 El 30CrMnSiNi2A tiene una alta templabilidad y buenas propiedades de mecanizado y soldadura, pero es m\u00e1s sensible a la entalla y a la fragilizaci\u00f3n por hidr\u00f3geno (incluida la fragilizaci\u00f3n por hidr\u00f3geno ambiental).<\/span><\/p>\n<p><span>\u00a0 \u00a0 \u00a0 30CrMnSiNi2A es adecuado como importante componente estructural portante de tensiones, como conectores de alta resistencia y piezas de ejes.<\/span><\/p>\n<p>&nbsp;<\/p>","protected":false},"excerpt":{"rendered":"<p>Scope of supply of Aviation Group: Round rods, steel plates, non-standard forgings, rings, seamless pipes, non-standard customization, welcome to inquire! 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