JPH06238387A - Forging of long size steel - Google Patents
Forging of long size steelInfo
- Publication number
- JPH06238387A JPH06238387A JP2663993A JP2663993A JPH06238387A JP H06238387 A JPH06238387 A JP H06238387A JP 2663993 A JP2663993 A JP 2663993A JP 2663993 A JP2663993 A JP 2663993A JP H06238387 A JPH06238387 A JP H06238387A
- Authority
- JP
- Japan
- Prior art keywords
- forging
- upsetting
- ratio
- shaft part
- shaft
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Landscapes
- Forging (AREA)
Abstract
Description
【0001】[0001]
【産業上の利用分野】本発明は、一端にフランジ部を一
体に形成させた航空機用大型エンジンの長尺シャフト等
の製造に好適に適用される長尺鋼材の鍛造方法に関す
る。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a method for forging a long steel material suitably applied to the manufacture of a long shaft of a large-sized aircraft engine having a flange portion integrally formed at one end.
【0002】[0002]
【従来の技術】航空機用大型ファンジェットエンジンに
は、一端に、ファンディスクが取付けられるフランジ
(傘部9を一体に形成させた長尺のシャフト用鍛造材が
使用されている。この様なシャフト素材としては、例え
ばマルエージング鋼が用いられ、素材の歩留りの向上や
靱性や引張強度等の、必要な材料力学的性質を得るため
に、シャフト部を所定の鍛練比で鍛伸させる一方、一端
部を据え込んでフランジ部が一体に形成され、製品形状
に近い形状(ニアネットシェイプ)のシャフト材を得る
ようにしている。この種のシャフト材の従来の製造方法
としては、先ず鍛造機により軸部を鍛伸させた後、プレ
ス機で端部を据え込んでフランジ部を形成させている。2. Description of the Related Art A large fan jet engine for an aircraft uses a long shaft forging material having a flange to which a fan disk is attached at one end (an umbrella portion 9 is integrally formed. As the material, for example, maraging steel is used, and in order to obtain necessary material mechanical properties such as improvement of material yield and toughness and tensile strength, the shaft part is stretched at a predetermined wrench ratio while The flange part is integrally formed by setting up the parts to obtain a shaft material with a shape (near net shape) close to the product shape.The conventional manufacturing method of this kind of shaft material is as follows: After forging the shaft portion, the flange is formed by upsetting the end portion with a pressing machine.
【0003】[0003]
【発明が解決しようとする課題】しかしながら、エンジ
ンの大型化に伴って全長が3000mmにも及ぶ長尺の
シャフト用鍛造材が要請されるようになってきた。この
ようなシャフト材は、軸部の長さが長いので、鍛伸させ
たシャフトを上下方向に立てた状態でプレス機にセット
してその端部の据込加工を行なうことは不可能に近い。However, as the engine becomes larger, there has been a demand for a long shaft forging material having a total length of 3000 mm. Since such a shaft material has a long shaft portion, it is almost impossible to set the end portion of the forged and stretched shaft in a press machine while standing upright. .
【0004】そこで、端部に形成させるフランジ(傘
部)の外径に等しい鋼材を準備し、フランジ部を残して
所望の径に鍛伸させた後、機械加工によりフランジを形
成させると、フランジ部のファイバフローが、このフラ
ンジ部に作用する遠心力の方向と一致せず、強度的要求
を満足しないことになる。本発明は、このような事情に
鑑みてなされたもので、軸部においては鍛伸により結晶
粒の微細化による鋼組織の改善を図り、フランジ部にお
いては所要のファイバフローを有し、且つ、ネットシェ
イプ化を図り、もって高靱性、高強度の、軸部の長さが
2000mm以上の長尺鋼材の鍛造方法を提供すること
を目的とする。Therefore, when a steel material having the same outer diameter as the flange (umbrella) to be formed at the end is prepared, and the flange is left to be forged to a desired diameter and then the flange is formed by machining, the flange is formed. The fiber flow of the portion does not match the direction of the centrifugal force acting on the flange portion, and the strength requirement is not satisfied. The present invention has been made in view of such circumstances, in the shaft portion to improve the steel structure by refining the crystal grains by forging, has a required fiber flow in the flange portion, and, It is an object of the present invention to provide a method for forging a long steel material having a high toughness and high strength and having a shaft portion length of 2000 mm or more by achieving a net shape.
【0005】[0005]
【課題を解決するための手段および作用】上記した目的
を達成するために、本発明においては、長さL1と外径
Dの比L1/Dが1〜3である一端据込部と軸部とを有
する棒材の前記一端据込部を据込比1/2 u以上に据え込
んだ後、再結晶温度以下に再加熱し、前記軸部を鍛練比
2s以上に鍛伸し、鍛伸した軸部の長さL2が2000
mm以上であることを特徴とする長尺鋼材の鍛造方法が
提供される。In order to achieve the above-mentioned object, in the present invention, one end upsetting portion and shaft portion having a ratio L1 / D of the length L1 to the outer diameter D of 1 to 3 are provided. After setting up the one end upsetting part of the bar material having and with the upsetting ratio of 1/2 u or more, it is reheated to a recrystallization temperature or lower, and the shaft part is forged to a forging ratio of 2 s or more, and forged. The shaft length L2 is 2000
There is provided a method for forging a long steel material, which is characterized in that it is not less than mm.
【0006】この発明の長尺鋼材の鍛造方法は、一端に
傘状のフランジやディスク状の歯車、カウンタウエイト
等を一体に形成させた、製品軸部長さL2が2000m
m以上である、例えば、航空機用エンジンのスタブシャ
フトの製造に好適に適用される。図1ないし図5は、本
発明方法による航空機用エンジンのスタブシャフトの製
造工程を示し、これらの図を参照して本発明方法の詳細
を説明する。In the method for forging a long steel material according to the present invention, the product shaft portion length L2 is 2000 m in which one end is integrally formed with an umbrella-shaped flange, a disk-shaped gear, a counterweight and the like.
m or more, for example, it is suitably applied to the manufacture of stub shafts for aircraft engines. 1 to 5 show steps of manufacturing a stub shaft of an aircraft engine according to the method of the present invention, and the details of the method of the present invention will be described with reference to these drawings.
【0007】先ず、所定形状の素材(ビレット)10を
準備してこれをプレス機の下ダイ12にセットする。素
材10の鋼種としては、鍛伸により鋼組織が改善される
ものであれば特に限定されるものではないが、マルエー
ジング鋼等が好適に適用できる。素材10は、所要の外
径(D)および長さを有する丸棒形状をなし、これを所
定温度に加熱したものである。下ダイ12の上面中央に
は、製品のフランジ部を成形するための型12aが形成
されている。素材10は、その上端10aを型12aの
型底から上方に長さL1だけ突出させており、この突出
させた部分10a(長さL1×外径D)が据込部とな
る。この据込部10aの長さL1と外径Dの比(L1/
D)は1〜3に設定される。据込部10aの形状比(L
1/D)が3より大きいと、据込時に座屈が生じる虞が
あり、逆に1より小さいと、据え込んで形成されるフラ
ンジ部のファイバフローが所要のパターンに形成されな
い。First, a material (billet) 10 having a predetermined shape is prepared and set on the lower die 12 of the press. The steel type of the material 10 is not particularly limited as long as the steel structure can be improved by forging, but maraging steel or the like can be suitably applied. The material 10 has a round bar shape having a required outer diameter (D) and length, and is heated to a predetermined temperature. At the center of the upper surface of the lower die 12, a mold 12a for molding a flange portion of the product is formed. The material 10 has an upper end 10a protruding upward from the mold bottom of the mold 12a by a length L1, and the protruding portion 10a (length L1 × outer diameter D) serves as an upsetting portion. The ratio of the length L1 of the upsetting portion 10a to the outer diameter D (L1 /
D) is set to 1-3. The shape ratio (L
If 1 / D) is larger than 3, buckling may occur at the time of upsetting, and if it is smaller than 1, the fiber flow of the flange portion formed by upsetting is not formed in a required pattern.
【0008】素材10は、プレス機により下ダイ12を
回転させながら平据え込みして、型入れする(図2)。
このときの据込比は1/2 u以上に据え込むのがよく(こ
の明細書全体において、「据込比は1/2 u以上に据え込
む」なる表現は、据込比が1/2u,1/2.5u,1/3u…と、据込
比1/2 uより据込量が大になるように据え込むことを意
味する)、これ以下の場合には所要のファイバフローが
形成されない。次いで、上ダイをポンチ14に代え、据
込部10aを型内12aに押し込み(図3)、製品のフ
ランジ形状に近いニアネットシェイプが得られる。この
ポンチによる型内押込み工程は製品によっては省略する
ことができる。The raw material 10 is flatly set up while the lower die 12 is rotated by a press machine, and put in a mold (FIG. 2).
The upsetting ratio at this time is preferably set to 1/2 u or more (in the entire specification, the expression "the upsetting ratio is set to 1/2 u or more" means that the upsetting ratio is 1 / 2u. , 1 / 2.5u, 1 / 3u, etc., which means that the installation amount is larger than the installation ratio of 1/2 u). In the case of less than this, the required fiber flow is not formed. . Then, the upper die is replaced with the punch 14, and the upsetting portion 10a is pushed into the mold 12a (FIG. 3), and a near net shape close to the flange shape of the product is obtained. Depending on the product, the in-mold pushing step using the punch can be omitted.
【0009】次に、軸部10bの鍛伸工程に入るが、鍛
伸前に、フランジ部を成形した素材10を、再結晶温度
以下(例えば、上述したマルエージング鋼では1100
℃以下)に再加熱しておく。そして、4面鍛造機により
シャフト素材10の軸部10bを、鍛練比1.5s以上
で鍛伸する(図4)。4面鍛造機の詳細な構成は図示さ
れていないけれども、この鍛造機は、マニピュレータ装
置により被鍛造材を把持し、被鍛造材をその軸方向に対
し直交する4方向から4個の金敷16により同時に圧下
し、被鍛造材をスエージングにより鍛伸(細径化、テー
パ化等)する装置であり、この装置は公知である。金敷
16としては、端部のフランジ肩部形状に適合する形状
を備えたものが使用される。鍛伸時における鍛練比が
1.5sより小さいと組織の改善(結晶粒の微細化)が
得られない。好ましい鍛練比としては2s以上である。
この鍛伸工程により鍛伸部、すなわち軸部10bが20
00mm以上の長さL2に鍛伸される(図5)。なお、
鍛伸されたシャフト素材10は、その後必要な熱処理や
機械加工が施される。Next, in the forging step of the shaft portion 10b, before the forging, the material 10 having the flange portion formed is cooled to a temperature not higher than the recrystallization temperature (for example, 1100 in the above-mentioned maraging steel).
Reheat to below (° C). Then, the shaft portion 10b of the shaft material 10 is forged by a four-sided forging machine at a forging ratio of 1.5 s or more (FIG. 4). Although the detailed structure of the four-sided forging machine is not shown, this forging machine grips the material to be forged by the manipulator device, and uses four anvils 16 from four directions orthogonal to the axial direction of the material to be forged. It is a device for simultaneously pressing and forging (for example, reducing the diameter and tapering) the material to be forged by swaging, and this device is known. As the anvil 16, one having a shape that conforms to the flange shoulder shape of the end is used. If the forging ratio during forging is less than 1.5 s, the improvement of the structure (fine graining) cannot be obtained. The preferred training ratio is 2 s or more.
By this forging step, the forged portion, that is, the shaft portion 10b is 20
It is stretched to a length L2 of 00 mm or more (Fig. 5). In addition,
The forged shaft material 10 is then subjected to necessary heat treatment and machining.
【0010】[0010]
【実施例】本発明の製造方法を航空機用大型エンジンの
スタブシャフトの製造に適用した。先ず、外径(D)3
50mm×長さ1600mmの丸棒形状をなすビレット10
を準備してこれをプレス機の下ダイ12にセットする。
ビレット10は、前述したマルエージング鋼であり、所
定温度(例えば、970℃)に加熱してある。下ダイ1
2の上面中央には、製品のフランジ部を成形するための
型12aが形成されており、ビレット10は、その上端
10aを型12aの型底から上方に長さ(L1)530
mmだけ突出させてセットされ、この突出させた部分、
すなわち据込部10aの長さL1と外径Dの比(L1/
D)は1.5である。EXAMPLES The manufacturing method of the present invention was applied to the manufacturing of stub shafts for large aircraft engines. First, the outer diameter (D) 3
Billet 10 with a round bar shape of 50 mm x length 1600 mm
Is prepared and set on the lower die 12 of the press.
The billet 10 is the above-mentioned maraging steel and is heated to a predetermined temperature (for example, 970 ° C.). Lower die 1
A mold 12a for molding a flange portion of the product is formed at the center of the upper surface of the bill 2, and the billet 10 has an upper end 10a extending upward from the mold bottom of the mold 12a by a length (L1) 530.
It is set by protruding only mm, and this protruding part,
That is, the ratio of the length L1 of the upsetting portion 10a to the outer diameter D (L1 /
D) is 1.5.
【0011】ビレット10は、プレス機により下ダイ1
2を回転させながら平据え込みして、型入された(図
2)。次いで、上ダイをポンチ14に代え、据込部10
aを型内12aに完全に押し込み(図3)、製品のフラ
ンジ形状に近いニアネットシェイプを得た。次に、フラ
ンジ部を成形した素材10を、再結晶温度以下である1
100℃に再加熱し、4面鍛造機によりシャフト素材1
0の軸部10bを鍛練比3sで、長さ(L2)3000
mm、軸径(D2)200mmに鍛伸した(図4,図
5)。得られたシャフト素材10の金属組織を顕微鏡で
観察した結果、平均結晶粒径は#8.3であった。The billet 10 is formed by pressing the lower die 1 with a press machine.
It was flatly set up while rotating 2 and was set in a mold (Fig. 2). Then, the upper die is replaced with the punch 14, and the upsetting unit 10 is replaced.
a was completely pushed into the mold 12a (FIG. 3), and a near net shape close to the flange shape of the product was obtained. Next, the material 10 in which the flange portion is molded is at a recrystallization temperature or lower 1
Reheat to 100 ° C, and shaft material 1 with a four-sided forging machine
0 shaft part 10b with a training ratio of 3s, length (L2) 3000
mm and shaft diameter (D2) 200 mm (FIGS. 4 and 5). As a result of observing the metal structure of the obtained shaft material 10 with a microscope, the average crystal grain size was # 8.3.
【0012】図6は、本発明方法により製造されるシャ
フト素材10のフランジ部(傘部)10aにおけるファ
イバフローの変化を模式的に示し、図6(A)は、図1
に示す素材10の未加工時のフローを、図6(B)は、
図2に示す平据込後のフローを、図6(C)は、図3に
示すポンチ後のフローをそれぞれ示す。一方、図7は、
比較方法によりシャフト素材を製造した場合のフランジ
部のファイバフローを模式的に示す。この比較方法で
は、図7(A)に示すように、製品時のフランジ部の外
径に相当する大きさのビレットを準備し、この端部に形
成させるフランジ部分を残して鍛伸した後、機械加工
(切削加工)により所要のフランジを形成させたもので
ある。図7(B)の破線は機械加工により形成させるフ
ランジの外形形状を示す。本発明方法によるシャフト素
材10のファイバフローは、径方向に沿って延びてお
り、本発明方法に依れば、遠心力が作用するフランジ部
のファイバフローを、比較方法のフローと比較して、好
ましいパターンに形成させることができる。FIG. 6 schematically shows a change in fiber flow in the flange portion (umbrella portion) 10a of the shaft material 10 manufactured by the method of the present invention, and FIG.
6B shows a flow of the raw material 10 shown in FIG.
FIG. 6C shows the flow after the flat installation shown in FIG. 2, and FIG. 6C shows the flow after the punch shown in FIG. On the other hand, in FIG.
The fiber flow of the flange part when a shaft material is manufactured by the comparison method is schematically shown. In this comparison method, as shown in FIG. 7 (A), a billet having a size corresponding to the outer diameter of the flange portion at the time of production is prepared, and after the flange portion to be formed at this end is forged and stretched, The required flange is formed by machining (cutting). The broken line in FIG. 7B shows the outer shape of the flange formed by machining. The fiber flow of the shaft material 10 according to the method of the present invention extends along the radial direction, and according to the method of the present invention, the fiber flow of the flange portion on which the centrifugal force acts is compared with the flow of the comparison method, It can be formed into a preferable pattern.
【0013】[0013]
【発明の効果】以上の説明で明らかなように、本発明の
長尺鋼材の鍛造方法に依れば、軸部を鍛伸する前に、一
端据込部の据込加工が実行されるために、製品時の軸部
の長さが2000mm以上のものでも、据込機(プレス
機)による据込加工ができる。そして、長さL1と外径
Dの比L1/Dが1〜3である一端据込部を、据込比1/
2 u以上に据え込むので、このように据え込んだ一端据
込部には、好ましいファイバフローを形成させることが
できる。一方、軸部は鍛練比1.5s以上に鍛伸される
ので、この部分の結晶粒が微細化し、所要の材料力学的
性能、すなわち、靱性に優れ、高強度の長尺鋼材を得る
ことができる。As is apparent from the above description, according to the method for forging a long steel material of the present invention, upsetting of the upsetting portion is performed before the shaft portion is forged. In addition, even when the length of the shaft portion of the product is 2000 mm or more, upsetting can be performed by the upsetting machine (press machine). Then, one end swaged portion having a ratio L1 / D of the length L1 and the outer diameter D of 1 to 3 is
Since it is set up to 2 u or more, a preferable fiber flow can be formed at the one end set-up portion thus set up. On the other hand, since the shaft portion is forged and stretched at a wrought ratio of 1.5 s or more, the crystal grains in this portion are refined, and it is possible to obtain a long steel material having a required material mechanical performance, that is, excellent toughness and high strength. it can.
【図1】本発明に係る長尺鋼材の鍛造方法の製造工程を
示し、素材をダイにセットした状態の断面図である。FIG. 1 is a cross-sectional view showing a manufacturing process of a method for forging a long steel material according to the present invention, in which a raw material is set in a die.
【図2】本発明の製造方法により素材の一端を平据込し
た状態の断面図である。FIG. 2 is a cross-sectional view showing a state in which one end of a raw material is flatly set up by the manufacturing method of the present invention.
【図3】図2に示す平据込加工後に、ポンチにより型内
に押込加工を行なった状態の断面図である。FIG. 3 is a cross-sectional view showing a state in which, after the flat upsetting process shown in FIG. 2, the punching process is performed into the mold.
【図4】本発明の製造方法により素材軸部の鍛伸加工状
態を示す側面図である。FIG. 4 is a side view showing a state in which a material shaft portion is forged by the manufacturing method of the present invention.
【図5】本発明の製造方法による素材の鍛伸加工を終え
た状態を示す側面図である。FIG. 5 is a side view showing a state in which the forging process of the material by the manufacturing method of the present invention is finished.
【図6】本発明の製造方法により製造される鋼材の一端
据込部のファイバフローの形成過程を示す図である。FIG. 6 is a diagram showing a process of forming a fiber flow at an upset portion of a steel material manufactured by the manufacturing method of the present invention.
【図7】比較方法により製造される鋼材の一端部のファ
イバフローの形成過程を示す図である。FIG. 7 is a diagram showing a process of forming a fiber flow at one end of a steel material manufactured by a comparative method.
10 素材(ビレット) 10a 一端据込部 12 下ダイス 12a 型 14 ポンチ 16 金敷 10 Material (billet) 10a One end upsetting part 12 Lower die 12a type 14 Punch 16 Anvil
Claims (1)
である一端据込部と軸部とを有する棒材の前記一端据込
部を据込比1/2 u以上に据え込んだ後、再結晶温度以下
に再加熱し、前記軸部を鍛練比2s以上に鍛伸し、鍛伸
した軸部の長さL2が2000mm以上であることを特
徴とする長尺鋼材の鍛造方法。1. The ratio L1 / D of the length L1 and the outer diameter D is 1 to 3.
After setting up the one end upsetting part of the bar material having one end upsetting part and the shaft part to an upsetting ratio of 1/2 u or more, it is reheated to a temperature lower than the recrystallization temperature, and the shaft part is forged to a training ratio. A forging method for a long steel material, which is forged for 2 seconds or more, and a length L2 of the forged shaft portion is 2000 mm or more.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP02663993A JP3256885B2 (en) | 1993-02-16 | 1993-02-16 | Long steel forging method |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP02663993A JP3256885B2 (en) | 1993-02-16 | 1993-02-16 | Long steel forging method |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH06238387A true JPH06238387A (en) | 1994-08-30 |
JP3256885B2 JP3256885B2 (en) | 2002-02-18 |
Family
ID=12199023
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP02663993A Expired - Fee Related JP3256885B2 (en) | 1993-02-16 | 1993-02-16 | Long steel forging method |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP3256885B2 (en) |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH07171650A (en) * | 1993-12-17 | 1995-07-11 | Kobe Steel Ltd | Hot swaging forging method |
US6144367A (en) * | 1997-03-26 | 2000-11-07 | International Business Machines Corporation | Method and system for simultaneous operation of multiple handheld control devices in a data processing system |
JP2006181577A (en) * | 2004-12-24 | 2006-07-13 | Denso Corp | Method for producing piping parts for high pressure and piping parts for high pressure |
CN102836941A (en) * | 2011-06-20 | 2012-12-26 | 日立金属株式会社 | Production method of forging piece |
CN105689611A (en) * | 2016-03-06 | 2016-06-22 | 江苏海宇机械有限公司 | Machining technology for single-end spline shaft sleeve |
CN106238660A (en) * | 2016-10-28 | 2016-12-21 | 河北科技大学 | A kind of motor shaft compound molding device and method |
CN106363117A (en) * | 2016-11-17 | 2017-02-01 | 攀钢集团攀枝花钢铁研究院有限公司 | Forging method for large-specification GH1016 round alloy rods |
CN109604510A (en) * | 2018-11-29 | 2019-04-12 | 攀枝花市科发机械制造有限公司 | A kind of truck semiaxis forging technology |
CN110695304A (en) * | 2019-10-17 | 2020-01-17 | 浙江凯名瑞汽车部件有限公司 | Spherical shell for automobile, spherical shell forging and machining method of spherical shell forging |
CN110744001A (en) * | 2019-12-09 | 2020-02-04 | 海安金锻工业有限公司 | Forging process of long shaft |
CN114309410A (en) * | 2021-12-30 | 2022-04-12 | 湖南中创空天新材料股份有限公司 | Method for upsetting aluminum alloy blank with ultra-limit height-diameter ratio |
-
1993
- 1993-02-16 JP JP02663993A patent/JP3256885B2/en not_active Expired - Fee Related
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH07171650A (en) * | 1993-12-17 | 1995-07-11 | Kobe Steel Ltd | Hot swaging forging method |
US6144367A (en) * | 1997-03-26 | 2000-11-07 | International Business Machines Corporation | Method and system for simultaneous operation of multiple handheld control devices in a data processing system |
JP2006181577A (en) * | 2004-12-24 | 2006-07-13 | Denso Corp | Method for producing piping parts for high pressure and piping parts for high pressure |
CN102836941A (en) * | 2011-06-20 | 2012-12-26 | 日立金属株式会社 | Production method of forging piece |
CN102836941B (en) * | 2011-06-20 | 2015-05-20 | 日立金属株式会社 | Production method of forging piece |
CN105689611A (en) * | 2016-03-06 | 2016-06-22 | 江苏海宇机械有限公司 | Machining technology for single-end spline shaft sleeve |
CN106238660A (en) * | 2016-10-28 | 2016-12-21 | 河北科技大学 | A kind of motor shaft compound molding device and method |
CN106363117A (en) * | 2016-11-17 | 2017-02-01 | 攀钢集团攀枝花钢铁研究院有限公司 | Forging method for large-specification GH1016 round alloy rods |
CN109604510A (en) * | 2018-11-29 | 2019-04-12 | 攀枝花市科发机械制造有限公司 | A kind of truck semiaxis forging technology |
CN110695304A (en) * | 2019-10-17 | 2020-01-17 | 浙江凯名瑞汽车部件有限公司 | Spherical shell for automobile, spherical shell forging and machining method of spherical shell forging |
CN110695304B (en) * | 2019-10-17 | 2021-01-05 | 浙江凯名瑞汽车部件股份有限公司 | Machining method for spherical shell forging of automobile |
CN110744001A (en) * | 2019-12-09 | 2020-02-04 | 海安金锻工业有限公司 | Forging process of long shaft |
CN114309410A (en) * | 2021-12-30 | 2022-04-12 | 湖南中创空天新材料股份有限公司 | Method for upsetting aluminum alloy blank with ultra-limit height-diameter ratio |
CN114309410B (en) * | 2021-12-30 | 2024-04-16 | 湖南中创空天新材料股份有限公司 | Upsetting method for ultra-limit height-diameter ratio aluminum alloy blank |
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