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    • 2. 发明公开
    • PRODUCTION METHOD FOR Ni-BASED SUPER HEAT-RESISTANT ALLOY
    • 镍基超级耐热合金的生产方法
    • EP3287209A1
    • 2018-02-28
    • EP16768885.2
    • 2016-03-24
    • Hitachi Metals, Ltd.
    • KOBAYASHI, ShinichiUENO, TomonoriOHNO, Takehiro
    • B21J5/00B21J1/06B21J13/02C22C19/05C22F1/10C22F1/00
    • C22F1/10B21J1/06B21J5/00B21J13/02C22C19/05C22C19/051C22C19/056C22F1/00
    • Provide is a production method whereby it is possible to obtain a high-strength Ni-based superalloy which is used in an aircraft engine or a gas turbine for power generation and which has good hot workability and a homogeneous microstructure.
      The method is a method of producing a Ni-based superalloy in which a hot working material of a Ni-based superalloy is subjected to hot working with a die heated to a temperature, the hot working material having a composition consisting of, in mass%, 0.001 to 0.050% of C, 1.0% to 4.0% of Al, 3.0% to 7.0% of Ti, 12% to 18% of Cr, 12% to 30% of Co, 1.5% to 5.5% of Mo, 0.5% to 2.5% of W, 0.001% to 0.050% of B, 0.001% to 0.100% of Zr, 0% to 0.01% of Mg, 0% to 5% of Fe, 0% to 3% of Ta, 0% to 3% of Nb, and the remainder of Ni and impurities, the method including: a hot working material heating step of heating and holding the hot working material in a temperature range of 950°C to 1150°C for 1 hour or longer; and a hot working step of performing hot working on the hot working material with the die that is heated to the temperature in a range of 800°C to 1150°C.
    • 提供一种生产方法,其可以获得用于发电的飞机发动机或燃气轮机中并且具有良好热加工性和均匀微观结构的高强度Ni基高温合金。 该方法是一种制造Ni基超级合金的方法,其中Ni基超级合金的热加工材料用加热到一定温度的模具进行热加工,所述热加工材料具有如下组成,以质量% ,C:0.001〜0.050%,Al:1.0〜4.0%,Ti:3.0〜7.0%,Cr:12〜18%,Co:12〜30%,Mo:1.5〜5.5% 至W的2.5%,B的0.001%至0.050%,Zr的0.001%至0.100%,Mg的0%至0.01%,Fe的0%至5%,Ta的0%至3%,0%至3% 所述方法包括:热加工材料加热步骤,将所述热加工材料在950℃至1150℃的温度范围内加热并保持1小时或更长时间; 以及用加热到800℃至1150℃范围内的温度的模具对热加工材料进行热加工的热加工步骤。
    • 5. 发明公开
    • METHOD FOR MANUFACTURING PURE NIOBIUM END GROUP COMPONENTS FOR SUPERCONDUCTING HIGH-FREQUENCY ACCELERATION CAVITY
    • 用于生产纯铌ENDGRUPPENKOMPONENTEN的超导高频加速区
    • EP3167972A1
    • 2017-05-17
    • EP15809895.4
    • 2015-06-15
    • Shinohara Press Service Co., Ltd.Nohara, KiyohikoInter-University Research Institute Corporation High Energy Accelerator Research Organization
    • NOHARA KiyohikoKAWABATA NobuyukiNAKAMURA HideyoshiMIYAJIMA KyoheiSHINOHARA MasayukiHAYANO HitoshiYAMAMOTO AkiraSAEKI TakayukiKATO ShigekiYAMANAKA Masashi
    • B21J5/00B21D28/00B21D28/02B21D28/16B21J1/06B21J13/02B21K25/00B30B15/14
    • B21D28/02B21J1/003B21J1/06B21J5/00B21J13/02H01P1/2082H01P11/001H01P11/007
    • [Problem to be Solved]
      Targeting mass production, the present invention provides an advanced method of manufacturing pure niobium plate end-group components from pure niobium plate material for superconducting high frequency accelerator cavity, wherein the invention is to convert the procedure/production method from the conventional machining or waterjet cutting followed by the conventional cold forging to the whole press-forming.
      [Solution]
      A method of manufacturing pure niobium plate end-group components for superconducting high frequency accelerator cavity used for the acceleration of charged particles, composing of
      (1) shear-blanking procedure of the pure niobium plate different from the conventional fine blanking, wherein the clearance is set to be very small value below 0.5% of pure niobium plate thickness to form a near net shape semi-product free from foreign objects on and below the material surface under the restriction of the material on binding tool to generate counter force, and
      (2) forging procedure at different temperatures from any of the conventional hot or warm or cold forging, wherein press forging is conducted to be free from the occurrence of blue brittleness/necking and to bring about prominent metal-flow, formability, the size accuracy in any portion of a product and the margin of further press-forming by controlling forging temperature to be below 200°C and beyond ambient room temperature,
      and characterized in that
      manufacturing method such as full machining or waterjet cutting followed by cold forging of the pure niobium plate end-group components is converted to the whole press-forming method.
    • [要解决的问题]靶向大量生产,本发明提供了在制造由纯铌板材纯铌板端基组分超导高频加速腔,worin本发明的先进的方法是从转换的程序/制造方法 现有的加工或喷水切割其次是常规冷锻整个压制成形。 [解决方法]制造纯铌板端基组分超导用于带电粒子加速的高频加速腔,(1)剪切冲裁纯铌板的步骤不同于常规的精密冲裁,worin构成的方法 的间隙被设置为低于纯铌板厚度的0.5%非常小的值,以形成接近最终形状的半成品免费从上和材料表面下方的材料的限制下异物对结合工具生成反作用力, 和(2)锻造过程从任何传统的热或热或冷锻造的不同温度下,worin锻压传导到来自蓝色脆性的发生游离/颈缩和带来突出的金属流动性,成型性,尺寸 精度的产品的任何部分和另外的边缘通过控制锻造温度压制成形为低于200℃和超过环境室温 即,特色DASS制造方法:如完整加工或随后将纯铌板端基组分的冷锻水射流切割被转换为整个冲压成形方法。
    • 6. 发明公开
    • MANUFACTURING METHOD FOR CONSTANT VELOCITY UNIVERSAL JOINT OUTER JOINT MEMBER AND OUTER JOINT MEMBER
    • 进程,以追踪外部连接器和接头外部连接器
    • EP3156677A1
    • 2017-04-19
    • EP15810447.1
    • 2015-05-20
    • NTN Corporation
    • NATSUME RenjiHARADA KuniakiMANO YoshiyaSUZUKI KiyohiroTSUBOI ShunichirouNAGATAKE AkiraSUGIYAMA TatsuroKOBAYASHI Masazumi
    • F16D3/20B21J1/06B21J5/08B21J13/02B21K1/14B23K15/00
    • F16D3/22B21J1/06B21J5/08B21J13/02B21K1/14B21K1/765B23K15/00F16D3/20F16D3/205F16D2003/22326
    • Provided is a method of manufacturing an outer joint member of a constant velocity universal joint, which is constructed by forming, through use of separate members, a cup section having track grooves formed at an inner periphery of the cup section and engageable with torque transmitting elements, and a shaft section formed at a bottom portion of the cup section, and by welding a cup member forming the cup section and a shaft member forming the shaft section, the method including: forming the cup member and the shaft member of medium carbon steel; preparing, as the cup member, a cup member having a cylindrical portion and a bottom portion integrally formed by forging, and a joining end surface formed on an outer surface of the bottom portion in a machining step after the forging; preparing, as the shaft member, a shaft member having a joining end surface to be joined to the bottom portion of the cup member, which is formed in the machining step; bringing the joining end surface of the cup member and the joining end surface of the shaft member into abutment against each other; and welding the cup member and the shaft member by radiating a beam from an outer side of the cup member to an abutment portion between the cup member and the shaft member in a radial direction of the cup member, in which the shaft member has a step portion in which the joining end surface is formed and a radially inner side recessed portion formed thereon by forging from a billet cut from a bar material.
    • 提供了一种制造在等速万向接头的外侧接头构件的方法,所有这些都通过形成建造,通过使用单独的构件,一个杯形部分具有轨道槽在形成在所述杯部的内周面并与扭矩传递元件接合 ,并在杯形部的底部形成的轴部,并且通过焊接一个杯形件形成所述杯形部和一个轴部件形成轴部,所述方法包括:形成所述杯形件和中碳钢的轴部件 ; 制备,如杯状部件,其具有筒状部和通过锻造一体形成的底部部分,和形成在在锻造后的加工步骤中,底部部分的外表面上的接合端面的杯构件; 制备,随着轴构件,具有连接端面的轴构件被接合到其在加工步骤中形成的杯状部件的底部,所有; 使杯构件的接合端面和轴构件成相互抵接的接合端面; 和焊接杯构件,并通过在上述杯体和在所述杯状部件的径向方向上的轴构件,其中所述轴部件具有台阶之间抵接部分从所述杯部件的外侧照射光束至该轴构件 这些部分在接合端面形成和径向内侧的凹部通过从棒材料的坯料切锻造形成在其上。
    • 8. 发明授权
    • THERMO-MECHANICAL PROCESSING OF NICKEL-BASE ALLOYS
    • 镍基合金的热机械处理
    • EP2714953B1
    • 2016-03-09
    • EP12722236.2
    • 2012-05-07
    • ATI Properties, Inc.
    • FORBES JONES, Robin M.ROCK, Christopher A.
    • C22C19/05C22F1/10
    • C22C19/058B21D22/022B21J1/06C22C19/05C22F1/10
    • A thermo-mechanical treatment process is disclosed. The process comprises a first heating step comprising heating a nickel-base alloy workpiece to a temperature greater than a M 23 C 6 carbide solvus temperature of the nickel-base alloy; a first working step comprising working the heated nickel-base alloy workpiece to a reduction in area of 20% to 70%, wherein the nickel-base alloy workpiece is at a temperature greater than a M 23 C 6 carbide solvus temperature when the first working step begins; a second heating step comprising heating the worked nickel-base alloy workpiece to a temperature in a range of 927°C (1700°F) to less than the M 23 C 6 carbide solvus temperature of the nickel-base alloy, wherein the as-worked nickel-base alloy workpiece is maintained at elevated temperature and not permitted to cool to ambient temperature between completion of the first working step and beginning of the second heating step; and a second working step comprising working the heated nickel-base alloy workpiece to a second reduction in area of 20% to 70%, wherein the nickel-base alloy workpiece is at a temperature greater than 927°C (1700°F) and less than the M 23 C 6 carbide solvus temperature of the nickel-base alloy when the second working step begins.