C21D1/56

THICK STEEL PLATE FOR HIGH HEAT INPUT WELDING AND HAVING GREAT HEAT-AFFECTED AREA TOUGHNESS AND MANUFACTURING METHOD THEREFOR

A thick steel plate for high heat input welding and having great heat-affected area toughness and a manufacturing method therefor, comprising the steps of smelting, casting, rolling, and cooling. Also, the chemical composition of the steel plate satisfies 1Ti/N6 and (Ca+REM+Zr)/Al0.11, where the effective S content in steel=S-0.8Ca-0.34REM-0.35Zr. and the effective S content in steel: 0.0006-0.005%; finely dispersed inclusions may be formed, and the amount of composite inclusion CaO+Al.sub.2O.sub.3+MnS+TiN in the steel plate is at a proportion of 12%. With respect to welding in which the thickness of the steel plate is 50-70 mm, the tensile strength of a base material is 510 MPa. and welding input energy is 200-400 kJ/cm, the average Charpy impact work of a welding heat-affected area of the steel plate at 40 C. is 100 J or more, and at the same time, the average Charpy aging impact work of the base material of thickness at 40 C. is 46 J or more.

A METHOD OF A HEAT TRANSFER OF A NON-METALLIC OR METALLIC ITEM
20180371304 · 2018-12-27 · ·

A method of heat treatment of a non-metallic or metallic item is provided. The method includes at least one step A) of heat transfer between the item and a heat transfer fluid A including a fluid medium and nanoparticles. The heat transfer fluid has a heat transfer coefficient above the heat transfer coefficient of water. The method also includes at least one step B) of heat transfer between the item and a heat transfer fluid B including a fluid medium and nanoparticles. The heat transfer fluid B has a heat transfer coefficient different from the heat transfer coefficient of A and above the heat transfer coefficient of water. The heat transfer fluids A and B are different.

THICK STEEL PLATE FOR HIGH HEAT INPUT WELDING AND HAVING GREAT HEAT-AFFECTED AREA TOUGHNESS AND MANUFACTURING METHOD THEREFOR

A thick steel plate for high heat input welding and having great heat-affected area toughness and a manufacturing method therefor, comprising the steps of smelting, casting, rolling, and cooling. Chemical composition is properly controlled for the steel plate and satisfies 1Ti/N6 and Mg/Ti>0.017, where effective S content in steel=S1.3 Mg0.8 Ca0.34 REM0.35 Zr, and effective S content in steel: 0.0003-0.003%; finely dispersed inclusions may be formed in the steel plate, and the amount of composite inclusion MgO+Ti.sub.2O.sub.3+MnS in the steel plate is controlled at a proportion greater than or equal to 5%. The tensile strength of a base material so acquired is 510 MPa, insofar as welding input energy is 200400 kJ/cm, the average Charpy impact work of the steel plate at 40 C. is 100 J or more, at the same time, the average Charpy aging impact work of the base material of thickness at 40 C. is 46 J or more.

METHOD FOR PRODUCING 7000-SERIES ALUMINUM ALLOY MEMBER EXCELLENT IN STRESS CORROSION CRACKING RESISTANCE

The stress corrosion cracking resistance of an aluminum alloy member consisting of 7000-series aluminum alloy extruded shape is improved. At least one region of a quenched aluminum alloy extruded shape is subjected to a restoring treatment of heating at a temperature-raising rate of 0.4 C./second or more, holding at a temperature ranging 300 to 590 C. for a time longer than zero second and cooling at a cooling rate of 0.5 C./second or more. A plastic working is applied to the region within 72 hours. The region is subjected to a heat treatment of heating at a temperature-raising rate of 0.4 C./second or more, holding at a temperature ranging 300 to 590 C. for a time longer than zero second and not longer than 300 seconds and cooling at a cooling rate of 2000 C./minute or less. The whole of the aluminum alloy extruded shape is subjected to an artificial aging treatment.

METHOD FOR PRODUCING 7000-SERIES ALUMINUM ALLOY MEMBER EXCELLENT IN STRESS CORROSION CRACKING RESISTANCE

The stress corrosion cracking resistance of an aluminum alloy member consisting of 7000-series aluminum alloy extruded shape is improved. At least one region of a quenched aluminum alloy extruded shape is subjected to a restoring treatment of heating at a temperature-raising rate of 0.4 C./second or more, holding at a temperature ranging 300 to 590 C. for a time longer than zero second and cooling at a cooling rate of 0.5 C./second or more. A plastic working is applied to the region within 72 hours. The region is subjected to a heat treatment of heating at a temperature-raising rate of 0.4 C./second or more, holding at a temperature ranging 300 to 590 C. for a time longer than zero second and not longer than 300 seconds and cooling at a cooling rate of 2000 C./minute or less. The whole of the aluminum alloy extruded shape is subjected to an artificial aging treatment.

Low alloy oil well steel pipe and method for manufacturing same

Low-alloy oil-well steel pipe includes a composition consisting, in mass %, of C: 0.40 to 0.65%, Si: 0.05 to 0.50%, Mn: 0.10 to 1.00%, P: 0.020% or less, S: 0.0020% or less, Cu: 0.15% or less, Cr: 0.40 to 1.50%, Mo: 0.50 to 2.50%, V: 0.05 to 0.25%, Ti: 0 to less than 0.01%, Nb: 0.01 to 0.2%, sol. Al: 0.010 to 0.100%, N: 0.006% or less, B: 0 to 0.0015%, and Ca: 0 to 0.003%, the balance being Fe and impurities. The structure has tempered martensite and 0 to less than 2% volume ratio of retained austenite. A grain size number of prior-austenite grain in the structure is 9.0 or more. An equivalent circular diameter of a sub-structure surrounded by a boundary having a crystal orientation difference of 15 or more from a packet boundary, a block boundary and a lath boundary is 3 m or less for the tempered martensite.

Low alloy oil well steel pipe and method for manufacturing same

Low-alloy oil-well steel pipe includes a composition consisting, in mass %, of C: 0.40 to 0.65%, Si: 0.05 to 0.50%, Mn: 0.10 to 1.00%, P: 0.020% or less, S: 0.0020% or less, Cu: 0.15% or less, Cr: 0.40 to 1.50%, Mo: 0.50 to 2.50%, V: 0.05 to 0.25%, Ti: 0 to less than 0.01%, Nb: 0.01 to 0.2%, sol. Al: 0.010 to 0.100%, N: 0.006% or less, B: 0 to 0.0015%, and Ca: 0 to 0.003%, the balance being Fe and impurities. The structure has tempered martensite and 0 to less than 2% volume ratio of retained austenite. A grain size number of prior-austenite grain in the structure is 9.0 or more. An equivalent circular diameter of a sub-structure surrounded by a boundary having a crystal orientation difference of 15 or more from a packet boundary, a block boundary and a lath boundary is 3 m or less for the tempered martensite.

Method of making an endoprosthesis containing multi-phase stainless steel
09987121 · 2018-06-05 · ·

An endoprosthesis fabricated from multi-phase ferrous steel. Endoprostheses can include a variety of devices such as staples, orthodontic wires, heart valves, filter devices, and stents, many of which devices are diametrically expandable devices. Multi-phase ferrous steels include dual phase steels and transformation induced plasticity steels (TRIP steels).

Method of making an endoprosthesis containing multi-phase stainless steel
09987121 · 2018-06-05 · ·

An endoprosthesis fabricated from multi-phase ferrous steel. Endoprostheses can include a variety of devices such as staples, orthodontic wires, heart valves, filter devices, and stents, many of which devices are diametrically expandable devices. Multi-phase ferrous steels include dual phase steels and transformation induced plasticity steels (TRIP steels).

Methods for making high hardness, high toughness iron-base alloys

One aspect of the present disclosure is directed to low-alloy steels exhibiting high hardness and an advantageous level of multi-hit ballistic resistance with minimal crack propagation imparting a level of ballistic performance suitable for military armor applications. Certain embodiments of the steels according to the present disclosure have hardness in excess of 550 HBN and demonstrate a high level of ballistic penetration resistance relative to conventional military specifications.