| 序号 | 专利名 | 申请号 | 申请日 | 公开(公告)号 | 公开(公告)日 | 发明人 |
|---|---|---|---|---|---|---|
| 1 | 抗锌致裂纹钢板及其制造方法 | CN201310244713.8 | 2013-06-19 | CN103320693B | 2015-11-18 | 刘自成; 吴勇; 李先聚 |
| 本发明公开了一种抗锌致裂纹钢板及其制造方法,采用低C-超低Si-高Mn-低Als-(Ti+Nb)微合金化处理的低合金钢作为基础,适当降低钢中Als的含量,控制Mn/C≥15、[(%Mn)+0.75(%Mo)]×(%C)≤0.16、Nb/Ti≥1.8且Ti/N在1.50~3.40之间、CEZ≤0.44%且B含量≤2ppm、Ni/Cu≥1.50、Ca处理且Ca/S比控制在1.0~3.0,(%Ca)×(%S)0.28≤1.0×10-3,优化TMCP工艺,使成品钢板的显微组织为铁素体+弥散分布细小的贝氏体晶团,平均晶粒尺寸在10μm以下,获得均匀优异的力学性能、优良的焊接性及抗锌致裂纹特性,特别适用于海洋结构用喷锌涂装耐蚀钢板、超高压输电结构用喷锌耐蚀钢板及滨海桥梁结构用喷锌涂装耐蚀钢板等。 | ||||||
| 2 | 固化/模塑由粉末制成的近净成形组件的方法 | CN201380072196.9 | 2013-12-20 | CN104968454A | 2015-10-07 | M·R·马森; M·A·尼格利; R·J·米勒 |
| 一种用于固化由粉末制成的预制件的方法,其包含:(a)将预制件放置在智能感受器之间;(b)通过施加变化的低强度磁场将智能感受器加热到平衡温度,其中低强度磁场具有穿过智能感受器的表面的磁通量;(c)至少在智能感受器的温度达到平衡温度之后的一段时间期间,施加固化压力至预制件;以及(d)当施加固化压力时,施加具有穿过预制件的表面的磁通量的脉冲高强度磁场。高强度磁场的强度和脉冲率被选择,使得预制件的晶体相将在基本恒定的温度下快速振荡。脉冲高强度磁场被施加得足够长,以便在相振荡期间实现预制件的超塑性。 | ||||||
| 3 | 高硬度、高韧性铁基合金和其制备方法 | CN200880109526.6 | 2008-08-01 | CN101809181B | 2013-11-13 | 罗纳德·E·贝利; 托马斯·R·帕拉伊尔; 格兰·J·斯维亚特克 |
| 本文一个方面涉及具有高硬度和有利水平的多重攻击弹道抗性的低合金钢,同时具有最小的裂纹扩展,赋予适用于军事装甲应用的弹道性能水平。本发明的钢的某些实施方案具有的硬度超过550HBN且相对于常规军事规格显示高水平的抗弹道穿透性。 | ||||||
| 4 | 抗锌致裂纹钢板及其制造方法 | CN201310244713.8 | 2013-06-19 | CN103320693A | 2013-09-25 | 刘自成; 吴勇; 李先聚 |
| 本发明公开了一种抗锌致裂纹钢板及其制造方法,采用低C-超低Si-高Mn-低Als-(Ti+Nb)微合金化处理的低合金钢作为基础,适当降低钢中Als的含量,控制Mn/C≥15、[(%Mn)+0.75(%Mo)]×(%C)≤0.16、Nb/Ti≥1.8且Ti/N在1.50~3.40之间、CEZ≤0.44%且B含量≤2ppm、Ni/Cu≥1.50、Ca处理且Ca/S比控制在1.0~3.0,(%Ca)×(%S)0.28≤1.0×10-3,优化TMCP工艺,使成品钢板的显微组织为铁素体+弥散分布细小的贝氏体晶团,平均晶粒尺寸在10μm以下,获得均匀优异的力学性能、优良的焊接性及抗锌致裂纹特性,特别适用于海洋结构用喷锌涂装耐蚀钢板、超高压输电结构用喷锌耐蚀钢板及滨海桥梁结构用喷锌涂装耐蚀钢板等。 | ||||||
| 5 | 固化/模塑由粉末制成的近净成形组件的方法 | CN201380072196.9 | 2013-12-20 | CN104968454B | 2017-07-18 | M·R·马森; M·A·尼格利; R·J·米勒 |
| 一种用于固化由粉末制成的预制件的方法,其包含:(a)将预制件放置在智能感受器之间;(b)通过施加变化的低强度磁场将智能感受器加热到平衡温度,其中低强度磁场具有穿过智能感受器的表面的磁通量;(c)至少在智能感受器的温度达到平衡温度之后的一段时间期间,施加固化压力至预制件;以及(d)当施加固化压力时,施加具有穿过预制件的表面的磁通量的脉冲高强度磁场。高强度磁场的强度和脉冲率被选择,使得预制件的晶体相将在基本恒定的温度下快速振荡。脉冲高强度磁场被施加得足够长,以便在相振荡期间实现预制件的超塑性。 | ||||||
| 6 | 高硬度、高韧性铁基合金和其制备方法 | CN200880109526.6 | 2008-08-01 | CN101809181A | 2010-08-18 | 罗纳德·E·贝利; 托马斯·R·帕拉伊尔; 格兰·J·斯维亚特克 |
| 本文一个方面涉及具有高硬度和有利水平的多重攻击弹道抗性的低合金钢,同时具有最小的裂纹扩展,赋予适用于军事装甲应用的弹道性能水平。本发明的钢的某些实施方案具有的硬度超过550 HBN且相对于常规军事规格显示高水平的抗弹道穿透性。 | ||||||
| 7 | 二重硬度鋼物品および作製方法 | JP2013548422 | 2011-12-22 | JP5834095B2 | 2015-12-16 | ステファンソン,ンジャル; ベイリー,ロナルド・イー; スウィアテク,グレン・ジェイ |
| 8 | 厚鋼板の製造方法 | JP2011523636 | 2011-01-27 | JPWO2011099408A1 | 2013-06-13 | 中島 清孝; 清孝 中島; 学 星野 |
| 厚鋼板の製造方法であって、所定の成分組成を有する鋼片を1000〜1200℃に加熱した後、板厚中心温度950〜1200℃で、累積圧下率50〜95%、パス数4〜16パスの前段圧延を施し、次いで、板厚中心温度850〜950℃で、パス数2〜8パス、各パスでの圧下率10〜25%、パス間時間3〜25秒の後段圧延を施し、その後、板厚中心温度750℃以上から0.5〜8℃/sの冷却速度で630〜700℃まで前段冷却を施し、続いて、10〜50℃/sの冷却速度で550℃以下まで後段冷却を施し、板厚10〜40mm、降伏応力315〜550MPaで、ミクロ組織が軟質相のフェライト、硬質相のパーライト、ベイナイト、マルテンサイトの1種又は2種以上の混合組織であり、かつ、板厚中心部のフェライト面積率が70〜95%、硬質相の平均ビッカース硬さが250〜500、平均結晶粒径が5〜20μmの厚鋼板とすることを特徴とする。 | ||||||
| 9 | High hardness and high toughness steel | JP2002135274 | 2002-05-10 | JP4812220B2 | 2011-11-09 | 武盛 高山 |
| 10 | Process for the production of thick armour plates | US152034 | 1993-11-12 | US5458704A | 1995-10-17 | Jochen Bobbert; Rudolf Kawalla; Hans Pircher; Gerd Sussek; Gunter Weihrauch |
| The invention relates to a process for the production of very hard armour plates from steel slabs, wherein the slabs are hot rolled to a final thickness above 50 mm and then hardened and possibly tempered. The characterizing feature of the invention is that a continuously cast slab is produced from a steel having0.25 to 0.32% C0.05 to 0 75% Si0.10 to 1.50% Mn0.90 to 2.00% Cr0.10 to 0.70% Mo1 20 to 4 50% Ni0.01 to 0.08% Almax 0.015% Pmax 0.005% Smax 0.012% Nresidue Fe, including usual impurities,the slab then being heated to a temperature of 1150.degree. C. or higher and heated through, whereafter following cooling in air and by the spraying of its two wide sides with pressurized water, the slab is hot rolled with a surface temperature in the range of 1050.degree. to 900.degree. C. in shaping passes having an individual deformation of .epsilon..sub.h >0.1 and with a shape factor SF>0.40 to the final thickness. | ||||||
| 11 | Case-Hardened plate armor and method of making | US162558 | 1988-03-01 | US4857119A | 1989-08-15 | David A. Karst; Felix R. Pawlowski; William A. Potrafke; Harold E. Schuneman |
| Case-hardened plate armor disclosed includes a steel plate (14,18) that is heat treated to provide carbonitride surfaces and a tough, ductile core, with the carbonitride surfaces having a toughness of at least 66, and preferably at least 67, on the Rockwell C scale to prevent surface penetration, and with the tough, ductile core being softer than the carbonitride surfaces to prevent brittle fracture. The steel plate (14,18) may be made from either rolled homogenous armor which has a final core hardness in the range of 45 to 50 on the Rockwell C scale, or from high-hard armor which has a final core hardness in the range of 52 to 54 on the Rockwell C scale. The steel plate may be made with holes or may be imperforate depending upon weight requirements. The case-hardening of the steel plate is performed by heating in an atmosphere of nitrogen and carbon, quenching of the heated steel plate, thereafter tempering the quenched steel plate, deep freezing of the tempered steel plate, and subsequently again tempering the steel plate after the deep freezing to provide the hard carbonitride surfaces and the softer but tougher and more ductile core. | ||||||
| 12 | Method for making armor plate | US244004 | 1981-03-16 | US4431466A | 1984-02-14 | Donald F. MeLampy |
| A method for making armor plate which comprises commencing with a homogeneous metal plate that has been hardened. Then moving the plate into a liquid bath while applying heat to one surface of the plate. The plate is progressively moved into the bath at an angle while the heat is applied at or near the point of intersection of the plate with the bath and on a surface of the plate which is opposite that which is in contact with the bath. | ||||||
| 13 | Homogeneous armor plate | US63988132 | 1932-10-27 | US2059746A | 1936-11-03 | FRITZ RITTERSHAUSEN |
| 14 | Process of manufacture of armor plate | US49075121 | 1921-08-08 | US1563420A | 1925-12-01 | JOHNSON JOHN B; SAMUEL DANIELS |
| 15 | Age hardenable alloy with a unique combination of very high strength and good toughness | US706745 | 1996-09-09 | US5866066A | 1999-02-02 | Raymond M. Hemphill; David E. Wert; Paul M. Novotny; Michael L. Schmidt |
| An age hardenable martensitic steel alloy having a unique combination of very high strength and good toughness consists essentially of, in weight percent, about______________________________________ C 0.21-0.34 Mn 0.20 max. Si 0.10 max. P 0.008 max. S 0.003 max. Cr 1.5-2.80 Mo 0.90-1.80 Ni 10-13 Co 14.0-22.0 Al 0.1 max. Ti 0.05 max. Ce 0.030 max. La 0.010 max.______________________________________the balance essentially iron. In addition, cerium and sulfur are balanced so that the ratio Ce/S is at least about 2 and not more than about 15. A small but effective amount of calcium can be present in place of some or all of the cerium and lanthanum. | ||||||
| 16 | Armor plate quenching | US48727643 | 1943-05-17 | US2378044A | 1945-06-12 | SORENSEN CHARLES E; MCCARROLL RUSSELL H; ROTHENTHALER NICHOLAS E |
| 17 | Armor plate | US64353732 | 1932-11-19 | US1995484A | 1935-03-26 | SULLIVAN ROBERT J |
| 18 | Armor plate and process of making same | US57130322 | 1922-06-27 | US1457103A | 1923-05-29 | FRANCIS BRADLEY; FREVERT HARRY L |
| 19 | Armor plate and process of making same | US57130222 | 1922-06-27 | US1457102A | 1923-05-29 | FRANCIS BRADLEY; FREVERT HARRY L |
| 20 | Armour-plate and process for its manufacture | US667037 | 1984-11-01 | US4645720A | 1987-02-24 | Hans Pircher; Werner Bentz; Alfred Tegethoff |
| Armour-plate comprising a two layer bonded subsequently heat-treated clad steel comprising an upper layer and a base layer wherein:(a) the upper layer contains (in percent by weight)______________________________________ 0.30 to 0.80% carbon 0.10 to 0.80% silicon 0.40 to 1.20% manganese up to 0.015% phosphorus up to 0.015% sulfur 0.20 to 2.80% chromium 0.05 to 1.00% molybdenum 0.01 to 0.05% aluminum up to 0.40% nickel ______________________________________ remainder iron including unavoidable impurities;(b) said base layer contains (in percent by weight)______________________________________ 0.17 to 0.40% carbon 0.10 to 0.80% silicon 0.40 to 2.00% manganese up to 0.025% phosphorus up to 0.025% sulfur 0.10 to 1.50% chromium 0.05 to 1.50% molybdenum 0.01 to 0.05% aluminum ______________________________________ remainder iron including unavoidable impurities the carbon content of said upper layer being substantially higher than the carbon content of said base material. The armour-plate is useful in vehicles such as tanks, personnel carriers, jeeps, ships and planes. | ||||||
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