CN116618562A - Free forging preparation method of Ti55531 titanium alloy large-size square billet - Google Patents
Free forging preparation method of Ti55531 titanium alloy large-size square billet Download PDFInfo
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Abstract
本发明公开了Ti55531钛合金大规格方坯自由锻造制备方法,具体为对Ti55531钛合金铸锭依次进行“高‑低‑高”开坯锻造、β温度以下两相区低温锻造、横向展宽、拔扁方成型方坯;经该方法所制备的Ti55531钛合金大规格锻坯重量可达2T,高低倍组织及力学性能良好,可满足各标准规范要求,可以实现制备大规格Ti55531钛合金锻造方坯的目的,能满足批量化生产,具有重要的经济、军事战略意义。
The invention discloses a method for preparing Ti55531 titanium alloy large-scale billet free forging, specifically performing "high-low-high" billet forging on the Ti55531 titanium alloy ingot in sequence, low-temperature forging in the two-phase region below the β temperature, lateral widening, and drawing. Flat square forming billet; the weight of the Ti55531 titanium alloy large-scale forging billet prepared by this method can reach 2T, the structure and mechanical properties of high and low magnification are good, which can meet the requirements of various standards and specifications, and can realize the preparation of large-scale Ti55531 titanium alloy forging billet It can meet the purpose of mass production and has important economic and military strategic significance.
Description
技术领域technical field
本发明属于钛合金材料加工技术领域,涉及Ti55531钛合金大规格方坯自由锻造制备方法。The invention belongs to the technical field of titanium alloy material processing, and relates to a method for preparing Ti55531 titanium alloy large-size billet free forging.
背景技术Background technique
在航空航天工业中,钛合金是飞机和发动机的主要结构材料之一;为适应航空新型结构件对材料性能和工艺性能上的要求,最新的钛合金设计发展趋势是朝着高强高韧的综合方向发展;目前,传统的高强高韧钛合金主要有近β型钛合金Ti-1023和BT22(国内牌号TC18,名义成分为Ti-5Al-5Mo-5V-1Fe-1Cr)等;随着航空航天业的迅速发展,新型的高强高韧钛合金也在不断研制中,其中Ti55531钛合金是由VSMPO公司与空客公司以BT-22为基础所研制的一种高强韧亚稳β型钛合金,其Mo当量为13.1,在退火态状态下的强度水平可达1080MPa,经热处理后,抗拉强度可超过1500MPa;Ti55531钛合金名义成分为Ti-5Al-5V-5Mo-3Cr-1Zr,其化学成分中含有较高质量分数的钼、钒、铬等β相稳定元素,因此该合金在淬火后仍能保持完整的β相,并且具有较低的α/β转变温度(相变点范围约820~860℃);Ti55531合金作为一类高性能轻质高强结构材料与Ti-1023合金相比,其冶炼、加工成本低,不会产生明显的成分偏析,并具有比强度高、抗拉强度高、断裂韧性好、淬透性好(≥250mm)、对偏析不敏感、以及较宽的加工工艺范围等优点,容易实现强度、韧性等指标的匹配性调控,具有优异的综合力学性能;In the aerospace industry, titanium alloy is one of the main structural materials of aircraft and engines; in order to meet the requirements of new aviation structural parts on material performance and process performance, the latest titanium alloy design development trend is towards the comprehensive combination of high strength and high toughness development direction; at present, traditional high-strength and high-toughness titanium alloys mainly include near-β-type titanium alloys Ti-1023 and BT22 (domestic brand TC18, nominal composition is Ti-5Al-5Mo-5V-1Fe-1Cr), etc.; With the rapid development of the industry, new high-strength and high-toughness titanium alloys are also being continuously developed. Among them, Ti55531 titanium alloy is a high-strength, toughness, metastable β-type titanium alloy developed by VSMPO and Airbus based on BT-22. Its Mo equivalent is 13.1, and its strength level in the annealed state can reach 1080MPa. After heat treatment, the tensile strength can exceed 1500MPa; the nominal composition of Ti55531 titanium alloy is Ti-5Al-5V-5Mo-3Cr-1Zr, and its chemical composition Contains a higher mass fraction of β-phase stable elements such as molybdenum, vanadium, chromium, etc., so the alloy can still maintain a complete β-phase after quenching, and has a lower α/β transformation temperature (the phase transition point ranges from about 820 to 860℃); Ti55531 alloy, as a class of high-performance light-weight and high-strength structural material, has lower smelting and processing costs than Ti-1023 alloy, does not produce obvious composition segregation, and has high specific strength, high tensile strength, Good fracture toughness, good hardenability (≥250mm), insensitivity to segregation, and a wide range of processing technology, etc., easy to achieve matching control of strength, toughness and other indicators, and has excellent comprehensive mechanical properties;
Ti55531钛合金作为1类高性能轻质高强结构材料,在航空领域受到极大重视,已大量用于制作大型运输机起落架、机身框架等关键部位的承力构件,如在空客公司A380超大型远程宽体客机的机翼与挂架的连接装置等部位获得应用;Ti55531 titanium alloy, as a class 1 high-performance light-weight and high-strength structural material, has received great attention in the aviation field. The connection device between the wing and the pylon of a large long-range wide-body passenger aircraft has been applied;
发明内容Contents of the invention
本发明的目的是提供Ti55531钛合金大规格方坯自由锻造制备方法,以实现制备2T级大规格Ti55531钛合金方坯,便于后续改锻及机加成型特定形貌规格的异形结构件。The purpose of the present invention is to provide a Ti55531 titanium alloy large-size billet free forging preparation method to realize the preparation of 2T-level large-size Ti55531 titanium alloy billet, which is convenient for subsequent forging and machining to form special-shaped structural parts with specific appearance specifications.
本发明所采用的技术方案是,Ti55531钛合金大规格方坯自由锻造制备方法,具体为对Ti55531钛合金铸锭依次进行“高-低-高”开坯锻造、β温度以下两相区低温锻造、横向展宽、拔扁方成型方坯。The technical solution adopted in the present invention is the preparation method of Ti55531 titanium alloy large-scale billet free forging, specifically performing "high-low-high" billet forging on the Ti55531 titanium alloy ingot in sequence, and low-temperature forging in the two-phase region below the β temperature , Horizontal widening, drawing and flattening square billets.
本发明的特点还在于:The present invention is also characterized in that:
其中Ti55531钛合金大规格方坯自由锻造制备方法,具体按以下步骤实施:Among them, the Ti55531 titanium alloy large-scale billet free forging preparation method is specifically implemented according to the following steps:
步骤1,“高-低-高”开坯锻造:将Ti55531钛合金铸锭在β转变温度以上100℃~300℃进行第一次镦拔锻造,锻造后采用空冷,随后在β转变温度以下30℃~50℃进行第二次镦拔锻造,之后再在β转变温度以上30℃~50℃进行第三次镦拔锻造,锻造后采用空冷;Step 1, "high-low-high" billet forging: the Ti55531 titanium alloy ingot is subjected to the first upsetting and drawing forging at 100 ° C ~ 300 ° C above the β transformation temperature. ℃~50℃ for the second upsetting forging, and then the third upsetting forging at 30℃~50℃ above the β transformation temperature, and air cooling after forging;
步骤2,β温度以下两相区低温锻造:对经过步骤1处理的坯料进行镦拔锻造且加热温度在β转变温度以下30℃~60℃,镦拔锻造后采用空冷;Step 2, low-temperature forging in the two-phase region below the β temperature: perform upsetting forging on the blank processed in step 1, and the heating temperature is 30°C to 60°C below the β transformation temperature, and use air cooling after upsetting forging;
步骤3,横向展宽:对经过步骤2处理的坯料进行横向展宽变形且加热温度在β转变温度以下30℃~60℃,锻后采用空冷;Step 3, transverse widening: the billet processed in step 2 is subjected to transverse widening and deformation, and the heating temperature is 30°C to 60°C below the β transformation temperature, and air cooling is adopted after forging;
步骤4,拔扁方成型:对经过步骤S3处理的坯料进行拔扁方成型且加热温度在β转变温度以下30℃~60℃,锻后采用空冷;Step 4, flattening and square forming: performing flattening and square forming on the blank processed in step S3, and the heating temperature is 30°C to 60°C below the β transformation temperature, and air cooling is adopted after forging;
其中步骤1中在β转变温度以上100℃~300℃开坯冷料加热时,先将合金加热至800℃保温120min,再升温至所需温度进行保温;在第一次镦粗时,铸锭锯切面需要进行铆镦镦粗,镦粗时均采用先镦一半,翻面再镦至尺寸的镦粗方式;Among them, in step 1, when the blank is heated at 100°C to 300°C above the β transformation temperature, the alloy is first heated to 800°C and kept for 120 minutes, and then heated to the required temperature for heat preservation; during the first upsetting, the ingot The sawing surface needs to be riveted and upset. When upsetting, the upsetting method is used to upset half, turn over and then upset to size;
其中步骤1中在β转变温度以上100℃~300℃进行2~4火次的镦拔锻造,每火次变形量控制在30~50%之间;β转变温度以下30℃~50℃进行1~2次镦拔锻造,变形量控制在30~50%之间;β转变温度以上30℃~50℃进行1~2火次的镦拔锻造,变形量控制在30~50%之间;Among them, in step 1, the upsetting forging is carried out at 100°C to 300°C above the β transformation temperature for 2 to 4 times, and the deformation of each fire is controlled between 30% and 50%; the temperature below the β transformation temperature is 30°C to 50°C for 1 ~2 times of upsetting forging, the deformation is controlled between 30-50%; 1-2 times of upsetting forging is carried out at 30°C-50°C above the β transformation temperature, and the deformation is controlled between 30-50%;
其中步骤2中对经过步骤1处理的坯料进行3~5火次的镦拔锻造,变形量控制在30~50%之间;Wherein in step 2, the billet processed in step 1 is subjected to upsetting and drawing forging for 3 to 5 times, and the deformation is controlled between 30 and 50%;
其中步骤1和步骤2的镦拔锻造中拔长压速不大于20mm/s,单次压下量不大于100mm;Wherein step 1 and step 2 in the upsetting and drawing forging, the drawing speed is not greater than 20mm/s, and the single reduction is not greater than 100mm;
其中步骤3中对经过步骤2处理的坯料进行1~3火次的横向展宽变形,变形量控制在20~50%之间;Wherein, in step 3, the blank processed in step 2 is subjected to lateral widening and deformation for 1 to 3 times, and the deformation is controlled between 20 and 50%;
其中步骤2和步骤3中坯料从加热炉到快锻机的转移时间不大于40S,终锻温度不小于800℃;The transfer time of the billet from the heating furnace to the fast forging machine in step 2 and step 3 shall not exceed 40 seconds, and the final forging temperature shall not be less than 800°C;
其中步骤4中对经过步骤3处理的坯料进行拔扁方成型,变形量控制在15~40%之间;Wherein in step 4, the billet processed in step 3 is flattened and square-shaped, and the amount of deformation is controlled between 15% and 40%;
其中步骤4中拔扁方成型火次数不大于2火次。Wherein in the step 4, the number of times of flattening and forming fires is no more than 2 fire times.
本发明的有益效果是:The beneficial effects of the present invention are:
本发明的Ti55531钛合金大规格方坯自由锻造制备方法,与常规锻造锻坯相比,利用10000T大吨位快锻机的锻造压力优势提供锻坯展宽变形时的大变形量,可有效减少火次,提高生产效率,所成型的大规格方坯可后续继续进行改锻与机加成特定尺寸要求的异形件。因此本发明所提供的一种Ti55531钛合金大规格方坯自由锻造制备方法,可以实现制备2T级大规格Ti55531钛合金方坯,具有重要的经济、军事战略意义。Compared with the conventional forging billet, the method for preparing Ti55531 titanium alloy large-size square billet free forging of the present invention utilizes the forging pressure advantage of the 10000T large-tonnage fast forging machine to provide a large amount of deformation when the forging billet is widened and deformed, which can effectively reduce the number of fires , to improve production efficiency, the formed large-size billet can be subsequently modified for forging and machining to add special-shaped parts with specific size requirements. Therefore, the free forging preparation method of a Ti55531 titanium alloy large-size billet provided by the present invention can realize the preparation of a 2T-level large-size Ti55531 titanium alloy billet, which has important economic and military strategic significance.
附图说明Description of drawings
图1为本发明的Ti55531钛合金大规格方坯自由锻造制备方法的流程图;Fig. 1 is the flow chart of Ti55531 titanium alloy large size billet free forging preparation method of the present invention;
图2为本发明的Ti55531钛合金大规格方坯自由锻造制备方法中Ti55531钛合金大规格方坯R态锻坯宏观形貌;Fig. 2 is the Ti55531 titanium alloy large-size square billet R-state macroscopic appearance in the Ti55531 titanium alloy large-size square billet free forging preparation method of the present invention;
图3为本发明的Ti55531钛合金大规格方坯自由锻造制备方法中Ti55531钛合金大规格方坯成品形貌;Fig. 3 is Ti55531 titanium alloy large-scale billet finished product morphology in the Ti55531 titanium alloy large-scale square billet free forging preparation method of the present invention;
图4为本发明的Ti55531钛合金大规格方坯自由锻造制备方法中Ti55531钛合金大规格方坯显微组织;Fig. 4 is the Ti55531 titanium alloy large-scale billet microstructure in the Ti55531 titanium alloy large-scale square billet free forging preparation method of the present invention;
图5为本发明的Ti55531钛合金大规格方坯自由锻造制备方法中Ti55531钛合金大规格方坯固溶时效态室温力学性能。Fig. 5 is the room temperature mechanical properties of Ti55531 titanium alloy large-size billet in solid solution aging state in the preparation method of Ti55531 titanium alloy large-size billet free forging of the present invention.
具体实施方式Detailed ways
下面结合附图和具体实施方式对本发明进行详细说明。The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.
本发明提供了Ti55531钛合金大规格方坯自由锻造制备方法,具体按以下步骤实施:如图1所示,通过对Ti55531钛合金铸锭依次进行“高-低-高”开坯锻造、β温度以下两相区低温锻造、横向展宽、拔扁方成型方坯;The invention provides a Ti55531 titanium alloy large-scale billet free forging preparation method, which is specifically implemented according to the following steps: as shown in Figure 1, the Ti55531 titanium alloy ingot is sequentially subjected to "high-low-high" billet forging, β temperature Low-temperature forging, lateral widening, and flattening of square billets in the following two-phase areas;
实施例1Example 1
Ti55531钛合金大规格方坯自由锻造制备方法,具体包括以下步骤:The method for preparing Ti55531 titanium alloy large-scale billet free forging specifically includes the following steps:
步骤1,“高-低-高”开坯锻造:将Ti55531钛合金铸锭在β转变温度以上100℃~300℃进行3火次的镦拔锻造,每火次变形量控制在30~50%之间,锻后均采用空冷,随后在β转变温度以下30℃~50℃进行2次镦拔锻造,变形量控制在30~50%之间,之后再在β转变温度以上30℃~50℃进行2火次的镦拔锻造,变形量控制在30~50%之间,锻后采用空冷;Step 1, "high-low-high" blank forging: the Ti55531 titanium alloy ingot is subjected to upsetting and drawing forging at 100°C to 300°C above the β transformation temperature for 3 times, and the deformation of each fire is controlled at 30% to 50%. In between, air cooling is used after forging, followed by two upsetting forgings at 30°C to 50°C below the β transformation temperature, and the deformation is controlled between 30% and 50%, and then at 30°C to 50°C above the β transformation temperature Carry out 2 times of upsetting and drawing forging, the amount of deformation is controlled between 30% and 50%, and air cooling is used after forging;
步骤2,β温度以下两相区低温锻造:对经过步骤S1处理的坯料进行4火次的镦拔锻造且加热温度在β转变温度以下30℃~60℃,变形量控制在30~50%之间,镦拔锻造后均采用空冷;Step 2, low-temperature forging in the two-phase region below the β temperature: Carry out 4 times of upsetting and drawing forging on the billet processed in step S1, and the heating temperature is 30°C to 60°C below the β transformation temperature, and the deformation is controlled between 30% and 50%. After upsetting and forging, air cooling is adopted;
步骤3,横向展宽:对经过步骤S2处理的坯料进行2火次的横向展宽变形且加热温度在β转变温度以下30℃~60℃,变形量控制在20~50%之间,锻后采用空冷;Step 3, transverse widening: carry out two times of transverse widening deformation on the billet processed in step S2, and the heating temperature is 30°C-60°C below the β transformation temperature, the deformation is controlled between 20-50%, and air cooling is used after forging ;
步骤4,拔扁方成型:对经过步骤S3处理的坯料进行1火次的拔扁方成型且加热温度在β转变温度以下30℃~60℃,变形量控制在15~40%之间,锻后采用空冷。Step 4, flattening and square forming: the billet processed in step S3 is subjected to flattening and square forming for one heat, and the heating temperature is 30°C to 60°C below the β transformation temperature, and the deformation is controlled between 15% and 40%. Then use air cooling.
实施例2Example 2
优选地,在步骤1中,在β转变温度以上100℃~300℃开坯冷料加热时,先加热至800℃保温120min,再升温至所需温度进行保温。Preferably, in step 1, when heating the cold blank at 100°C to 300°C above the β-transition temperature, it is first heated to 800°C and kept for 120 minutes, and then heated to the required temperature for heat preservation.
优选地,在步骤1中,在首次镦粗时,铸锭锯切面需要进行铆镦镦粗,镦粗时均采用先镦一半,翻面再镦至尺寸的镦粗方式。Preferably, in step 1, when upsetting for the first time, the sawn surface of the ingot needs to be riveted and upset, and the upsetting method is first half upset, turned over and then upset to size.
优选地,在步骤1、步骤2中,拔长压速≤20mm/s,单次压下量≤100mm。Preferably, in step 1 and step 2, the drawing speed is ≤20mm/s, and the single reduction is ≤100mm.
优选地,在步骤2、步骤3中,坯料从加热炉到快锻机的转移时间≤40S,终锻温度≥800℃。Preferably, in step 2 and step 3, the transfer time of the billet from the heating furnace to the fast forging machine is ≤40S, and the final forging temperature is ≥800°C.
优选地,在步骤S4中,拔扁方成型火次数不大于2火。Preferably, in step S4, the number of flattening and square forming fires is not more than 2 fires.
实施例3Example 3
实验结果Experimental results
如图2和图3所示,通过本发明的一种Ti55531钛合金大规格方坯自由锻造制备方法所生产的Ti55531钛合金大规格方坯,低倍组织正常,未见冶金缺陷,如图4所示,显微组织均为β转变基体上的等轴α组织,如图5所示,整体组织性能均匀,能够满足批产要求,具有重要的经济、军事战略意义。As shown in Figure 2 and Figure 3, the Ti55531 titanium alloy large-scale square billet produced by a kind of Ti55531 titanium alloy large-scale square billet free forging preparation method of the present invention has a normal low-magnification structure and no metallurgical defects, as shown in Figure 4 As shown, the microstructures are all equiaxed α-structures on the β-transformation matrix. As shown in Figure 5, the overall structure performance is uniform, which can meet the requirements of batch production and has important economic and military strategic significance.
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| CN119608819A (en) * | 2024-11-22 | 2025-03-14 | 陕西天成航空材料股份有限公司 | Forging-rolling combined preparation method for small-size high-strength and high-toughness titanium alloy bars for machining |
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| CN119794236A (en) * | 2025-01-03 | 2025-04-11 | 陕西天成航空材料股份有限公司 | A method for preparing TC4 titanium alloy fine-grained rods with high efficiency and low cost |
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