• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    The invention relates to a manufacturing process for large annular forgings. The process comprises the following steps: firstly, preparing a prefabricated blank; then preparing a blank from the prefabricated blank through upsetting deformation and inter-forming heat preservation process of a multi-level hourglass-shaped module; and finally, manufacturing and processing the blank into the annular forge piece.
    公开号:EP3682982A1
    申请号:EP17925051.9
    申请日:2017-11-10
    公开日:2020-07-22
    发明作者:Yaping Li；Haitao Xu；Gang Sun；Zhaoyang Liu；Chunguang YAN；Qiang Liu；Mingzheng WANG；Donghui Zhang；Mingyue SUN
    申请人:China Institute of Atomic of Energy；
    IPC主号:B21J1-00
    专利说明:
    [0001] The invention relates to a manufacturing method for metals and alloys, in particular to a manufacturing process for large annular forgings. Background
    [0002] The development history of human kinds is, in a sense, a history of the usage and development of materials. The rapid development of the society has put forward higher requirements on manufacturing and processing of materials. New materials and advantaged manufacturing technologies thereof become the key to upgrading of the national supporting industries. Take the large annular forgings as an example. The large annular forgings are widely applied to large containers of aerospace, petroleum, chemical and nuclear power plants. The manufacturing technology for large annular forgings directly determines the manufacturing level of major equipment.
    [0003] Under the existing industrial level, steel ingots used for the annular forgings are made of die-casting ingots or electroslag ingots. For the large-size annular forgings, an assembly welding type structure is often adopted. The assembly welding process is high in cost and long in manufacturing cycle. In addition, the weld joint position is of a cast-state structure and its performance is much lower than that of base metals, so the reliability of products is affected.
    [0004] In order to meet the requirements of a safe, reliable and economical design, it's necessary to develop a manufacturing process for large annular forgings, which is low in cost and short in construction period. Summary
    [0005] The invention aims to provide a safer, more reliable and more economical manufacturing process for large annular forgings.
    [0006] The technical scheme of the invention is as follows: the manufacturing process for large annular forgings comprises the following steps: (S1) preparing prefabricated blanks; (S2) preparing a level I hourglass-shaped module from the prefabricated blanks; (S3) performing upsetting deformation along the height direction and inter-forging heat preservation after heating the level I hourglass-shaped module to prepare an intermediate blank; (S4) preparing a level II hourglass-shaped module from the intermediate blanks; (S5) performing upsetting deformation along the height direction and inter-forging heat preservation after heating the Level II hourglass-shaped module to prepare a blank; (S6) manufacturing and processing the blank into an annular forge piece.
    [0007] Further, as the above manufacturing process for large annular forgings, steps (S4) to (S5) in the process can be repeated for multiple times, the intermediate blanks are made into a multi-level hourglass-shaped module and then the multi-level hourglass-shaped module is made into the blank.
    [0008] Further, as the above manufacturing process for large annular forgings, the prefabricated blanks in step (S1) are constructed by casting blank, forging blank or rolling blank elements and are formed through seal welding and forging; or the prefabricated blanks in step (S1) are directly prepared from forging blanks by machining.
    [0009] Further, as the above manufacturing process for large annular forgings, in step (S2), the prefabricated blanks are made into frustum-shaped units, the small surfaces of the two frustum-shaped units are stacked together and vacuum electron beam welding is conducted to prepare the level I hourglass-shaped modules; and in step (S4), the intermediate blanks are made into frustum-shaped units, the small surfaces of the two frustum-shaped units are stacked together and vacuum electron beam welding is conducted to prepare the level II hourglass-shaped modules. The frustum-shaped units can be of circular cone frustum shapes or rectangular pyramid frustum shapes, and smooth transition at the intermediate interface position of the two frustum-shaped units should be guaranteed.
    [0010] Further, as the above manufacturing process for large annular forgings, the depth of joints for vacuum electron beam welding is 20 to 50 mm.
    [0011] Further, as the above manufacturing process for large annular forgings, the height-diameter ratio of the hourglass-shaped modules in step(S2) or step(S4) is between 1 and 3.
    [0012] Further, as the above manufacturing process for large annular forgings, the height reduction of implementing upsetting deformation on the hourglass-shaped modules in step(S3) or step(S5) is equal to 30 to 55 percent of the total height of the blanks.
    [0013] Further, as the above manufacturing process for large annular forgings, the blanks after upsetting in step(S3) or step(S5) are subjected to high-temperature diffusion bonding, wherein the heating temperature is not less than 1200 °C and the heat preservation time after temperature reaching stable is not less than 12 hours.
    [0014] Further, as the above manufacturing process for large annular forgings, in step (S6), the blank is manufactured and processed into the annular forge piece through upsetting, punching, reaming and flatting processes.
    [0015] The invention has the following beneficial effects: according to the manufacturing process for large annular forgings, which is provided by the invention, the prefabricated blank is made into the hourglass-shaped module, the hourglass-shaped construction blank can centralize the deformation in the upsetting process around the interface position, and generation of the surface tensile stress is avoided, so that the blank is subjected to big pressure stress uniformly and the surface tensile stress state of the blank is obviously optimized. Meanwhile, the minimum section area of the hourglass-shaped blank is small, so pressure needed by forging can be effectively reduced. Compared with a structure manufactured by an assembly welding process, the large annular forge piece manufactured by the process has the following advantages: materials are saved by about 30 percent, the manufacturing cycle is shortened by about 50 percent and the manufacturing cost is comprehensively reduced by about 15 percent. Furthermore, the annular forge piece manufactured by the process owns small performance fluctuation, wherein the strength fluctuation is 30 to 50 MPa and the impact toughness fluctuation is 50 to 70 J, so that the safety and reliability of the annular forge piece under service are greatly improved. Brief Description of Drawings
    [0016] FIG. 1 is a flow schematic diagram of the manufacturing process for large annular forgings of the invention. FIG. 2 is a flow schematic diagram of the manufacturing process for the annular forge piece in the embodiment 1 of the invention. FIG. 3 is a flow schematic diagram of the manufacturing process for the annular forge piece in the embodiment 2 of the invention.Description of Embodiments
    [0017] The invention is described in details below with reference to the accompanying drawings and embodiments.
    [0018] As shown in FIG. 1, described from the overall technological process, a special-shaped metal construction forming method comprises the following steps: step (1) preparing a prefabricated blank; step (2) preparing a level I special-shaped module (hourglass-shaped module) from the prefabricated blank; step (3) performing upsetting deformation along the height direction and inter-forging heat preservation after heating the level I special-shaped module to prepare an intermediate blank; step (4) preparing a level II special-shaped module (hourglass-shaped module) from the intermediate blank; step (5) performing upsetting deformation along the height direction and inter-forging heat preservation after heating the level II hourglass-shaped module to prepare a blank; and step (6) manufacturing and processing the blank into an annular forge piece.
    [0019] In the process of manufacturing the blank, steps (4) to (5) can be repeated for multiple times, the intermediate blank is made into a multi-level special-shaped module, the advantages of the hourglass-shaped module are completely utilized, the volume and weight of the intermediate blank are continuously enlarged, and the blank is finally prepared.
    [0020] The prefabricated blanks in step (1) can be constructed by casting blank, forging blank or height blank elements and be formed through seal welding and forging (refer to the description of "a homogeneous metal construction forming method" in CN201511026272.X for the method); or the prefabricated blanks are directly prepared from forging blanks by machining.
    [0021] On one hand, one charasteristic of the invention is embodied in the manufacturing process of the blank in steps (2) to (5). The multilevel hourglass-shaped modules are prepared from the prefabricated blanks, the hourglass-shaped construction blanks can centralize the deformation in the upsetting process on the interface position, and generation of the surface tensile stress is avoided, so that the blank is subjected to big pressure stress uniformly and the surface tensile stress state of the blank is obviously improved. Therefore, the prefabricated blanks or the intermediate blanks are made into the frustum-shaped units firstly, and the frustum-shaped units can be prepared through a forging and/or machining mode. The small surfaces of the two frustum-shaped units are stacked together and vacuum electron beam welding is conducted to prepare the hourglass-shaped modules. In the embodiments, the frustum-shaped units can be of circular cone frustum shapes or rectangular pyramid frustum shapes (also can be of other frustum shapes, such as a hexagonal pyramid frustum and an octagonal pyramid frustum). The minimum section area of the hourglass-shaped blank is small, so pressure needed by forging can be effectively reduced. However, when the middle sunken position is narrow, fold defects will occur in the forging process; and when the middle sunken position is wide, the effect of reducing the forging pressure will be weakened. Thus, when the hourglass-shaped blank is designed, the size of the included angle between the lower bottom edge and the waist edge of the longitudinal trapezoid section of each frustum-shaped unit should be taken into consideration so as to be within an ideal range. Meanwhile, smooth transition of the trapezoidal blank is conducted, so that the fact that the trapezoidal blank is folded at the intermediate interface position is avoided and a sharp corner at the junction of the two trapezoidal blanks is avoided. The junction of the two frustum-shaped units is realized by a vacuum electron beam welding mode, a to-be-welded surface is processed and cleaned and then the periphery of the to-be-welded blank in a vacuum chamber is subjected to vacuum electron beam seal welding, wherein the depth of joints for vacuum electron beam welding is 20 to 50 mm. The height-diameter ratio of the hourglass-shaped module formed after welding is between 1 and 3. The height-diameter ratio described here refers to the ratio of the total height of the hourglass-shaped module to the diameter of the bottom surface of the circular cone frustum (or the side length of the bottom surface of the rectangular pyramid frustum).
    [0022] In the manufacturing process of the blank in steps (2) to (5), another characteristic of the method is that the large forge piece is divided into a plurality of modules to perform construction by a multi-level modular manufacturing process. According to the process method, multiple pieces can be put into production, so that the production efficiency can be effectively improved and the construction period can be effectively guaranteed.
    [0023] In the forging process of the blank in step(3) or step(5), the blank is heated firstly, wherein the highest heating temperature is not less than 1200 °C; then the hourglass-shaped blank is subjected to upsetting deformation along the height direction; and the heated blank is placed on a press operating platform and is subjected to upsetting along the height direction, wherein the height reduction of the upsetting deformation is equal to 30 to 55 percent of the total height of the blank. Then, the blank after upsetting is subjected to high-temperature diffusion bonding and the blank after upsetting is sent back to a heating furnace to perform heating, wherein the heating temperature is not less than 1200 °C and the heat preservation time after temperature reaching stable is not less than 12 hours.
    [0024] On the other hand, another characteristic of the method is embodied in step (6), wherein the blank is manufactured and processed into the annular forge piece by upsetting, punching, reaming and flatting processes. The method has overcome the defects of a higher cost and longer manufacturing cycle of the traditional assembling welding process, and has solved the problems of product reliability caused by the performance of the weld joint position much lower than that of base metals. Embodiment 1
    [0025] The target product of the embodiment is a large annular forge piece.
    [0026] In the first step, steel ingots are obtained by a pouring mode and the steel ingots are heated and are subjected to blooming and forging to form prefabricated blanks, wherein the size of the prefabricated blanks is as follows: 1200 mm in diameter and 1500 mm in height, as shown in FIG. 2(a).
    [0027] In the second step, the prefabricated blanks are heated before being forged, wherein the highest heating temperature is not less than 1200 °C. The prefabricated blanks are subjected to die forging to form level I frustum-shaped units, as shown in FIG. 2(b).
    [0028] In the third step, the level I frustum-shaped units are subjected to vacuum electron beam welding. In a vacuum chamber, the superposed level I frustum-shaped unit blanks are subjected to vacuum electron beam seal welding to form level I hourglass-shaped modules, wherein the welding depth is 20 to 50 mm, as shown in FIG. 2(c).
    [0029] In the fourth step, the welded level I hourglass-shaped modules are heated before being forged, wherein the highest heating temperature is not less than 1200 °C. The heated blanks are placed on a press operating platform, so that the height direction of the blanks is along a vertical direction. Upsetting is implemented along the height direction, wherein the height reduction is equal to 30 to 55 percent of the total height of the blanks. The blanks are subjected to high-temperature diffusion bonding. The blanks after upsetting are sent back to a heating furnace to perform heating, wherein the heating temperature is not less than 1200 °C and the heat preservation time after temperature reaching stable is not less than 12 hours. Then the blanks are subjected to rounding, as shown in FIG. 2(d).
    [0030] In the fifth step, the blanks are heated before being forged, wherein the highest heating temperature is not less than 1200 °C. The blanks are subjected to die forging to form level II frustum-shaped units, as shown in FIG. 2(e).
    [0031] In the sixth step, the level II frustum-shaped units are subjected to vacuum electron beam welding. In the vacuum chamber, the superposed level II frustum-shaped unit blanks are subjected to vacuum electron beam seal welding to form level II hourglass-shaped modules, wherein the welding depth is 20 to 50 mm, as shown in FIG. 2(f).
    [0032] In the seventh step, the welded level II hourglass-shaped modules are heated before being forged, wherein the highest heating temperature is not less than 1200 °C. The heated blanks are placed on a press operating platform, so that the height direction of the blanks is along the vertical direction. Upsetting is implemented along the height direction, wherein the height reduction is equal to 30 to 55 percent of the total height of the blanks. The blanks are subjected to high-temperature diffusion bonding. The blanks after upsetting are sent back to the heating furnace to perform heating, wherein the heating temperature is not less than 1200 °C and the heat preservation time after temperature reaching stable is not less than 12 hours. Then the blanks are subjected to rounding to prepare a blank, as shown in FIG. 2(g).
    [0033] In the eighth step, the blank is subjected to upsetting, punching, reaming and flatting. The blanks are processed on a 16-m ring rolling mill to obtain the final size, as shown in FIG. 2(h).
    [0034] In the embodiment, the fifth step to the seventh step can be repeatedly conducted, the intermediate blanks are made into multilevel hourglass-shaped modules and the multilevel hourglass-shaped modules are made into the blank. Embodiment 2
    [0035] The target product of the embodiment is a large annular forge piece.
    [0036] In the first step, a stainless steel continuous casting plate blank prepared by a continuous casting mode is cut into 11 blanks with the specifications of 1500 mm ∗ 1500 mm ∗ 200 mm. The six surfaces of each continuous casting blank are machined and to-be-welded surfaces are cleaned, so that fresh metal surfaces are exposed.
    [0037] In the second step, the blanks are subjected to vacuum electron beam welding. In a vacuum chamber, the peripheries of the superposed blanks are subjected to vacuum electron beam seal welding, wherein the welding depth is 20 to 50 mm and the size after welding is 1500 mm in width, 1500 mm in length and 2200 mm in height, as shown in FIG. 3(a).
    [0038] In the third step, the welded blanks are heated before being forged, wherein the highest heating temperature is not less than 1200 °C and the heating speed is required to be less than 100 °C/h. The heated blanks are placed on a press operating platform, so that the height direction of the blanks is along a vertical direction. Upsetting is implemented along the height direction, wherein the height reduction is equal to 30 to 55 percent of the total height of the blanks. The blanks are subjected to high-temperature diffusion bonding. The blanks after upsetting are sent back to a heating furnace to perform heating, wherein the heating temperature is not less than 1200 °C and the heat preservation time after temperature reaching stable is not less than 12 hours.
    [0039] In the fourth step, the blanks are subjected to upsetting in three directions and are subjected to edge chamfering, chamfering and machining to form prefabricated blanks, as shown in FIG. 3 (b).
    [0040] In the fifth step, the prefabricated blanks are heated before being forged, wherein the highest heating temperature is not less than 1200 °C. The prefabricated blanks are subjected to die forging to form level I frustum-shaped units, as shown in FIG. 3(c).
    [0041] In the sixth step, the level I frustum-shaped units are subjected to vacuum electron beam welding. In a vacuum chamber, the superposed level I frustum-shaped unit blanks are subjected to vacuum electron beam seal welding to form level I hourglass-shaped modules, wherein the welding depth is 20 to 50 mm, as shown in FIG. 3(d).
    [0042] In the seventh step, the welded special-shaped modules are heated before being forged, wherein the highest heating temperature is not less than 1200 °C. The heated blanks are placed on a press operating platform, so that the height direction of the blanks is along a vertical direction. Upsetting is implemented along the height direction, wherein the height reduction is equal to 30 to 55 percent of the total height of the blanks. The blanks are subjected to high-temperature diffusion bonding. The blanks after upsetting are sent back to a heating furnace to perform heating, wherein the heating temperature is not less than 1200 °C and the heat preservation time after temperature reaching stable is not less than 12 hours. Then the blanks are subjected to rounding, as shown in FIG. 3(e).
    [0043] In the eight step, the blanks are heated before being forged, wherein the highest heating temperature is not less than 1200 °C. The blanks are subjected to die forging to form level II frustum-shaped units, as shown in FIG. 3(f).
    [0044] In the ninth step, the level II frustum-shaped units are subjected to vacuum electron beam welding. In the vacuum chamber, the superposed level II frustum-shaped unit blanks are subjected to vacuum electron beam seal welding to form level II hourglass-shaped modules, wherein the welding depth is 20 to 50 mm, as shown in FIG. 3(g).
    [0045] In the tenth step, the welded level II hourglass-shaped modules are heated before being forged, wherein the highest heating temperature is not less than 1200 °C. The heated blanks are placed on a press operating platform, so that the height direction of the blanks is along the vertical direction. Upsetting is implemented along the height direction, wherein the height reduction is equal to 30 to 55 percent of the total height of the blanks. The blanks are subjected to high-temperature diffusion bonding. The blanks after upsetting are sent back to a heating furnace to perform heating, wherein the heating temperature is not less than 1200 °C and the heat preservation time after temperature reaching stable is not less than 12 hours. Then the blanks are subjected to rounding to prepare a blank, as shown in FIG. 3(h).
    [0046] In the eleventh step, the blank is subjected to upsetting, punching, reaming and flatting. The blank is processed on a 16-m ring rolling mill to obtain the final size, as shown in FIG. 3(i).
    [0047] In the embodiment, the eighth step to the tenth step can be repeatedly conducted, the intermediate blanks are made into multilevel hourglass-shaped modules and the multilevel hourglass-shaped modules are made into the blank.
    [0048] Obviously, those skilled in the art can perform modifications and variations on the invention without departing from the scope of the invention. Thus, the invention is also intended to include the modifications and variations if the variations and modifications on the invention belong to the range of the claims of the invention as well as the equivalent technologies thereof.
    权利要求:
    Claims (10)
    [0001] a manufacturing process for large annular forgings comprises the following steps:
    (S1) preparing prefabricated blanks;
    (S2) preparing a level I hourglass-shaped module from the prefabricated blanks;
    (S3) performing upsetting deformation along the height direction and inter-forging heat preservation after heating the level I hourglass-shaped module to prepare an intermediate blank;
    (S4) preparing a level II hourglass-shaped module from the intermediate blanks;
    (S5) performing upsetting deformation along the height direction and inter-forging heat preservation after heating the level II hourglass-shaped module to prepare a blank;
    (S6) manufacturing and processing the blank into an annular forge piece.
    [0002] The manufacturing process for large annular forgings as claimed in claim 1, wherein steps (S4) to (S5) in the process can be repeated for multiple times, the intermediate blanks are made into a multi-level hourglass-shaped module and the multi-level hourglass-shaped module is made into the blank.
    [0003] The manufacturing process for large annular forgings as claimed in claim 1 or 2, wherein the prefabricated blanks in step (S1) are constructed by casting blank, forging blank or rolling blank elements and are formed through seal welding and forging; or the prefabricated blanks in step (SI) are directly prepared from forging blanks by machining.
    [0004] The manufacturing process for large annular forgings as claimed in claim 1 or 2, wherein in step (S2), the prefabricated blanks are made into frustum-shaped units, the small surfaces of the two frustum-shaped units are stacked together and vacuum electron beam welding is conducted to prepare the level I hourglass-shaped modules; and in step (S4), the intermediate blanks are made into frustum-shaped units, the small surfaces of the two frustum-shaped units are stacked together and vacuum electron beam welding is conducted to prepare the level II hourglass-shaped modules.
    [0005] The manufacturing process for large annular forgings as claimed in claim 4, wherein the frustum-shaped units can be of circular cone frustum shapes or rectangular pyramid frustum shapes, and smooth transition at the intermediate interface position of the two frustum-shaped units should be guaranteed.
    [0006] The manufacturing process for large annular forgings as claimed in claim 4, wherein the depth of joints for vacuum electron beam welding is 20 to 50 mm.
    [0007] The manufacturing process for large annular forgings as claimed in claim 1 or 2, wherein the height-diameter ratio of the hourglass-shaped modules in step(S2) or step(S4) is between 1 and 3.
    [0008] The manufacturing process for large annular forgings as claimed in claim 1 or 2, wherein the height reduction of implementing upsetting deformation on the hourglass-shaped modules in step(S3) or step (S5) is equal to 30 to 55 percent of the total height of the blanks.
    [0009] The manufacturing process for large annular forgings as claimed in claim 1 or 2, wherein the blanks after upsetting in step(S3) or step(S5) are subjected to high-temperature diffusion bonding, wherein the heating temperature is not less than 1200 °C and the heat preservation time after temperature reaching stable is not less than 12 hours.
    [0010] The manufacturing process for large annular forgings as claimed in claim 1 or 2, wherein in step (S6), the blank is manufactured and processed into the annular forge piece through upsetting, punching, reaming and flatting processes.
    类似技术:
    公开号 | 公开日 | 专利标题
    US10953486B2|2021-03-23|Additive forging method for preparing homogenized forged pieces
    CN100467156C|2009-03-11|Method for smithing GH4169 alloy plate shaped forgeable piece in air at an approximately equal temperature
    US8414267B2|2013-04-09|Multiple alloy turbine rotor section, welded turbine rotor incorporating the same and methods of their manufacture
    CN102240774B|2013-07-24|Fine forging forming method of spiral bevel gears
    Allwood et al.2005|The development of ring rolling technology
    US7416105B2|2008-08-26|Superplastically forming of friction welded structural assemblies
    CN102181793B|2012-05-30|Process for manufacturing steel forge piece of vertical conveying pipe of deep sea oil extraction equipment
    CN106583491B|2018-12-04|A kind of manufacturing method of Cr-Ni-Mo-Nb nickel-base alloy seamless pipe
    CN105328020B|2017-09-29|Front ring punch forming frock and its method of work in burner inner liner
    CN101376204B|2010-07-28|Novel technique for producing seamless steel pipe
    US20140102164A1|2014-04-17|Method and apparatus related to joining dissimilar metal
    CN101224484B|2010-11-10|Large-scale forging dies for near-isothermally forging disc forgeable piece
    CN101530898B|2010-10-13|Corrosion-resistant dual metal clad tube blank and manufacturing method thereof
    CN102513799A|2012-06-27|Ring rolling method for flange of megawatt wind generation set tower
    CN103691860B|2015-10-07|The processing method of effective raising Quality of Large Forgings
    CN102764891A|2012-11-07|Method of controlling grain size in forged precipitation-strengthened alloys and components formed thereby
    CN105170853B|2017-05-17|Integral forging forming method for ultra-large type hollow disc forgings
    CN1880175B|2012-07-04|Metal blank for hot dilation forming
    CA2009649A1|1991-01-10|Dual-alloy disk system
    CN101157175A|2008-04-09|A processing method of titanium alloy closing end
    CN104190840B|2016-07-20|A kind of hot upset forging mould structure of stainless steel bolt
    CN103143659B|2015-03-04|Hollow forging method of nuclear power main pipeline
    CN104259357B|2016-05-25|The production method of large-scale steel ingot
    US20170056961A1|2017-03-02|Method of manufacturing multi-material gears
    US3936920A|1976-02-10|Aerodynamic shell structure with fittings and method for fabricating same
    同族专利:
    公开号 | 公开日
    KR20200052922A|2020-05-15|
    CN107626880A|2018-01-26|
    CN107626880B|2020-10-09|
    WO2019051980A1|2019-03-21|
    JP2020533179A|2020-11-19|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    法律状态:
    2019-03-22| STAA| Information on the status of an ep patent application or granted ep patent|Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE |
    2020-06-19| STAA| Information on the status of an ep patent application or granted ep patent|Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE |
    2020-06-19| PUAI| Public reference made under article 153(3) epc to a published international application that has entered the european phase|Free format text: ORIGINAL CODE: 0009012 |
    2020-07-22| 17P| Request for examination filed|Effective date: 20200402 |
    2020-07-22| AK| Designated contracting states|Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
    2020-07-22| AX| Request for extension of the european patent|Extension state: BA ME |
    2020-12-23| DAV| Request for validation of the european patent (deleted)|
    2020-12-23| DAX| Request for extension of the european patent (deleted)|
    2021-06-16| A4| Supplementary search report drawn up and despatched|Effective date: 20210514 |
    2021-06-16| RIC1| Information provided on ipc code assigned before grant|Ipc: B21J5/08 20060101AFI20210508BHEP Ipc: B21J1/04 20060101ALI20210508BHEP Ipc: B21H1/06 20060101ALI20210508BHEP Ipc: B21K1/76 20060101ALI20210508BHEP Ipc: B23K 15/00 20060101ALI20210508BHEP Ipc: B21J5/00 20060101ALI20210508BHEP |
    优先权:
    申请号 | 申请日 | 专利标题
    [返回顶部]