JPH01241330A - Blank for superplastic forming - Google Patents
Blank for superplastic formingInfo
- Publication number
- JPH01241330A JPH01241330A JP63067288A JP6728888A JPH01241330A JP H01241330 A JPH01241330 A JP H01241330A JP 63067288 A JP63067288 A JP 63067288A JP 6728888 A JP6728888 A JP 6728888A JP H01241330 A JPH01241330 A JP H01241330A
- Authority
- JP
- Japan
- Prior art keywords
- forming
- blank
- plate
- plate thickness
- thickness
- 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.)
- Pending
Links
- 238000007789 sealing Methods 0.000 claims description 6
- 238000010438 heat treatment Methods 0.000 abstract description 3
- 230000008719 thickening Effects 0.000 abstract 1
- 238000000465 moulding Methods 0.000 description 10
- 238000000034 method Methods 0.000 description 7
- 239000000463 material Substances 0.000 description 6
- 230000000694 effects Effects 0.000 description 3
- 239000002828 fuel tank Substances 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 239000011324 bead Substances 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 238000010894 electron beam technology Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 235000013622 meat product Nutrition 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 230000002028 premature Effects 0.000 description 1
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は人工衛星姿勢制御用燃料タンクの構成部材であ
る球形タンクシェルその他各種航空・宇宙機器部品等の
超塑性成形に適用される被加工素材の改良に関する。[Detailed Description of the Invention] [Field of Industrial Application] The present invention is applied to superplastic forming of spherical tank shells, which are components of fuel tanks for artificial satellite attitude control, and various aerospace equipment parts. Regarding improvement of materials.
従来超塑性成形は、一般に第3図に示すように金型1,
2の間に被加工素板3をセットし、これら全体を超塑性
成形温度に加熱、維持した状態で、上型1から導入され
るガス(例えばArガス)圧力によって被加工素板3を
下型2の内壁面に押しつけ、成形を行う。この際、成形
ガス圧を保持するため、被加工素板3の周囲と下型2と
の間には上型に金型突起ピード5を一体的に設け、これ
を被加工素板3の周囲に喰い込ま・せるガス圧シール機
構を介して上下金型がプレスされている。また他の方法
として第4図に示すように、ワイヤー6を上型1の下面
と被加工素板3の上面周囲部に配設し被加工素板3の周
囲に喰い込ませることによってガス圧シールを行なって
いるものもある。Conventional superplastic forming generally involves a mold 1, as shown in Figure 3.
The blank plate 3 to be machined is set between the molds 1 and 2, and while the whole is heated and maintained at the superplastic forming temperature, the blank plate 3 to be machined is lowered by the pressure of gas (for example, Ar gas) introduced from the upper die 1. It is pressed against the inner wall surface of mold 2 to perform molding. At this time, in order to maintain the molding gas pressure, a mold projection pea 5 is integrally provided on the upper die between the periphery of the blank plate 3 to be processed and the lower die 2, and this is installed around the blank plate 3 to be processed. The upper and lower molds are pressed through a gas pressure seal mechanism. As another method, as shown in FIG. 4, a wire 6 is arranged around the lower surface of the upper mold 1 and the upper surface of the blank plate 3 to be processed, and the wire 6 is inserted around the blank plate 3 to be processed. Some are also doing sealing.
ところで上記のような従来の成形法でのこのシールの主
作用は、前述のよって成形ガス圧を維持することにある
が、もう一つの作用は成形に伴う半径方向の引張力に対
して被加工素板フランジ部の全型内流入を防止すること
にある。By the way, the main function of this seal in the conventional molding method described above is to maintain the molding gas pressure as described above, but another function is to protect the workpiece against the radial tensile force associated with molding. The purpose is to prevent the entire flange part of the blank plate from flowing into the mold.
このため金型突起ビードやワイヤーは必要に応じて数条
設けられるが、加工設備の限界(炉内有効ゾーン)−杯
の製品を成形しようとするようなスペース上余裕がない
場合には、下型肉製品輪郭の肩(R部)近くで7−ルす
る必要が生ずる。For this reason, several mold protruding beads and wires are installed as necessary, but if there is no space available due to the limitations of the processing equipment (effective zone in the furnace), such as when molding a cup product, it is necessary to It becomes necessary to perform a 7-rule near the shoulder (R part) of the profile of the molded meat product.
この場合、第5図に示すように金型突起ピードやワイヤ
の喰い込みの結果被加工素板3の板厚減少が成形部肩部
の近くに生ずるため、成形に伴う半径方向引張力prが
その部分に集中して局部的不均一変形をひき起し、遂に
は破断に至って所定の成形が不可能となる不具合があっ
た。In this case, as shown in FIG. 5, as a result of the mold protrusion speed and biting of the wire, the thickness of the blank plate 3 to be processed is reduced near the shoulder of the forming part, so that the radial tensile force pr accompanying forming is reduced. There was a problem in that local non-uniform deformation was concentrated in that part, which eventually led to breakage, making it impossible to perform the desired molding.
このような不具合を生じたのは、シールの結果被加工素
板のシール部残存板厚1.が、素板初期板厚t。よシも
必然的に小さくなることに起因する。The reason for this problem is that the residual thickness of the seal part of the workpiece blank after sealing is 1. However, the initial thickness of the raw plate is t. This is due to the fact that the size also inevitably becomes smaller.
このため本発明の超塑性成形用ブランクは、超塑性ガス
圧成形を行なう被加工素板(ブランク)に於て、超塑性
成形前の該素板周囲のシール部板厚を、あらかじめ成形
部の初期板厚よシも厚く構成したことを特徴としている
。Therefore, in the blank for superplastic forming of the present invention, in the blank to be processed by superplastic gas pressure forming, the thickness of the sealing part around the blank before superplastic forming is determined in advance of the forming part. It is characterized by a thicker initial board thickness.
上述の本発明の超塑性成形用ブランクは、第1、第2図
に示すようにあらかじめ被加工素板のシール部板厚T。As shown in FIGS. 1 and 2, the above-mentioned superplastic forming blank of the present invention has a thickness T of the sealed portion of the workpiece blank in advance.
を、成形部初期板厚t。よりも意図的に厚くするように
構成した。その板厚設定に当っては、シールの喰い込み
δがあっても、その部分の残存板厚t+=(To−δ)
が、成形部初期板厚toよシも大きくなるようにした。, the initial plate thickness t of the forming part. It was designed to be intentionally thicker than the original. When setting the plate thickness, even if there is a seal bite δ, the remaining plate thickness at that part t + = (To - δ)
However, the initial plate thickness of the molded part was also increased.
上記素板を用いることによって、シール状態でもその部
分の残存板厚t1が成形部板厚toよシも大きくなるた
め、成形に伴う半径方向引張応力の集中が解除され、当
該部での不均一変形や破断が防止でき、良好な成形が可
能となった。By using the above-mentioned blank plate, even in the sealed state, the remaining plate thickness t1 of that part becomes larger than the plate thickness of the molded part, so the concentration of radial tensile stress accompanying molding is released, and unevenness in the part is reduced. Deformation and breakage were prevented, and good molding became possible.
以下図面によシ本発明の一実施例について説明すると、
第1図は本発明を人工衛星用球形燃料タンクに実施した
変肉素板の加工方法を示す。An embodiment of the present invention will be described below with reference to the drawings.
FIG. 1 shows a method of processing a modified wall blank plate in which the present invention is applied to a spherical fuel tank for an artificial satellite.
又第2図は本発明の他の実施例を示している。FIG. 2 also shows another embodiment of the invention.
第1図に於て1は上金型、2は下金型、3は被加工素板
で金型1,2の間に被加工素板3をセットし、これら全
体を超塑性成形温度に加熱。In Figure 1, 1 is the upper mold, 2 is the lower mold, and 3 is the blank plate to be processed. heating.
維持した状態で、上型1から導入されるガス(例えばA
rガス)圧力によって被加工素板3を下型2の内壁面に
押しつけ加圧して所望の形状に成形を行なう点は前述の
従来技術と同じ手段を用いるので、詳細は省略する。本
発明の特徴としている点は、あらかじめ超塑性成形前の
被加工素板3の周囲のシール部板厚T0を、成形部初期
板厚t。よシも意図的に厚くした点にある。While maintaining the gas (for example, A) introduced from the upper mold 1,
Since the same means as in the prior art described above is used in that the blank plate 3 to be processed is pressed against the inner wall surface of the lower die 2 and molded into a desired shape using pressure (r gas), the details will be omitted. The feature of the present invention is that the thickness T0 of the sealing part around the blank plate 3 to be processed before superplastic forming is set in advance by the initial thickness t of the forming part. Yoshi is also intentionally made thicker.
変肉素板の加工法としては、切削加工による 4方法が
代表的である。There are four typical cutting methods for processing bare plates with altered thickness.
第2図に示す本発明の他の実施例では、平板の被加工素
板3と、その周囲部のシール部にこれと別体の枠板4と
を用意し、これを拡散接合法、シーム溶接法、電子ビー
ム溶接法などであらかじめ金属接合する方法が考えられ
る。この場合、周囲の枠材は(変形させないので)超塑
性材料である必要はなく、従って材料費低減には有効と
考えられる。In another embodiment of the present invention shown in FIG. 2, a flat blank plate 3 and a separate frame plate 4 are prepared in a sealed area around the flat plate, and these are bonded using a diffusion bonding method and a seam bonding method. Possible methods include welding, electron beam welding, etc. to join metals in advance. In this case, the surrounding frame material does not need to be a superplastic material (since it is not deformed), and is therefore considered effective in reducing material costs.
以上述べたように本発明の超塑性成形用ブランクによれ
ば、次に示す効果が得られる。As described above, according to the superplastic forming blank of the present invention, the following effects can be obtained.
(1)被加工素板シール部の早期破断、成形不能の不具
合が解決できるようになシ、加工設備の限界−杯の大型
部品生産が可能となった。(1) Problems such as premature breakage of the seal portion of the blank plate to be processed and inability to form can be solved, and it has become possible to produce large parts that are at the limit of processing equipment.
(2)既存設備有効活用のほか、コンパクトな金型設計
が可能となシ金型材料・製作費の低減、素材歩溜シの改
善などの効果も期得できる。(2) In addition to effective use of existing equipment, it is possible to design compact molds, reduce mold material and manufacturing costs, and improve material yield.
第1図は本発明の一実施例の加工状態を示す側断面図、
第2図は別の一実施例の側断面図、第3図〜第5図は従
来のガス圧成形の側断面図を示す。
1・・・上型、2・・・下型、3・・・被加工素板、4
・・・枠板、To・・・シール部板厚、to・・・成形
部初期板厚。
第1図
第2図FIG. 1 is a side sectional view showing the processing state of an embodiment of the present invention;
FIG. 2 is a side sectional view of another embodiment, and FIGS. 3 to 5 are side sectional views of conventional gas pressure forming. 1... Upper die, 2... Lower die, 3... Raw plate to be processed, 4
... Frame plate, To... Sealing part plate thickness, to... Initial plate thickness of molding part. Figure 1 Figure 2
Claims (1)
)に於て、超塑性成形前の該素板周囲部のシール部板厚
をあらかじめ成形部の初期板厚よりも厚く構成したこと
を特徴とする超塑性成形用ブランク。(1) In the blank to be processed by superplastic gas pressure forming, the thickness of the sealing part around the blank before superplastic forming is configured to be thicker than the initial thickness of the forming part. A superplastic forming blank featuring:
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP63067288A JPH01241330A (en) | 1988-03-23 | 1988-03-23 | Blank for superplastic forming |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP63067288A JPH01241330A (en) | 1988-03-23 | 1988-03-23 | Blank for superplastic forming |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH01241330A true JPH01241330A (en) | 1989-09-26 |
Family
ID=13340645
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP63067288A Pending JPH01241330A (en) | 1988-03-23 | 1988-03-23 | Blank for superplastic forming |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH01241330A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH03230822A (en) * | 1990-02-02 | 1991-10-14 | Mitsubishi Heavy Ind Ltd | Method for sealing gas pressure in forming using dies |
KR100868021B1 (en) * | 2008-06-02 | 2008-11-11 | 서번산업엔지니어링주식회사 | Forming device for embossing part of plate heat exchange |
CN109622719A (en) * | 2018-12-25 | 2019-04-16 | 安徽工业大学 | Multiple groups part pressure medium plate liquid filling deep-drawing forming method |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS53109563A (en) * | 1977-03-04 | 1978-09-25 | Matsushita Refrigeration | Production of synthetic resin box |
JPS56139917A (en) * | 1980-04-03 | 1981-10-31 | Asahi Chem Ind Co Ltd | Manufacture of synthetic resin product |
JPH01150419A (en) * | 1987-12-09 | 1989-06-13 | Natl Space Dev Agency Japan<Nasda> | Superplastic forming method for metallic foil |
-
1988
- 1988-03-23 JP JP63067288A patent/JPH01241330A/en active Pending
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS53109563A (en) * | 1977-03-04 | 1978-09-25 | Matsushita Refrigeration | Production of synthetic resin box |
JPS56139917A (en) * | 1980-04-03 | 1981-10-31 | Asahi Chem Ind Co Ltd | Manufacture of synthetic resin product |
JPH01150419A (en) * | 1987-12-09 | 1989-06-13 | Natl Space Dev Agency Japan<Nasda> | Superplastic forming method for metallic foil |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH03230822A (en) * | 1990-02-02 | 1991-10-14 | Mitsubishi Heavy Ind Ltd | Method for sealing gas pressure in forming using dies |
KR100868021B1 (en) * | 2008-06-02 | 2008-11-11 | 서번산업엔지니어링주식회사 | Forming device for embossing part of plate heat exchange |
CN109622719A (en) * | 2018-12-25 | 2019-04-16 | 安徽工业大学 | Multiple groups part pressure medium plate liquid filling deep-drawing forming method |
CN109622719B (en) * | 2018-12-25 | 2019-12-31 | 安徽工业大学 | Hydro-mechanical deep drawing forming method for multi-component pressure medium plate |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4882823A (en) | Superplastic forming diffusion bonding process | |
US4988037A (en) | Method and apparatus for superplastic forming and diffusion bonding of hollow parts | |
US8464566B2 (en) | Method of manufacturing a valve housing | |
EP0928234A1 (en) | Diffusion bonding of metals | |
JPS61238423A (en) | Forming method for ultraplastic metallic plate | |
US4509671A (en) | Method of producing diffusion bonded superplastically formed structures | |
US4113522A (en) | Method of making a metallic structure by combined superplastic forming and forging | |
US5449109A (en) | Method for superplastic forming by internal pressure | |
JPH01241330A (en) | Blank for superplastic forming | |
JPH0236330B2 (en) | ||
US6510601B1 (en) | Invar forming method for making tooling | |
US3351691A (en) | Nozzle assembly and method of molding same | |
JPH0469009B2 (en) | ||
US4467953A (en) | Cold pressing method | |
JPH04187325A (en) | Superplastically formed goods and its working method | |
JPS62114743A (en) | One-body forming method for nozzle | |
US3206963A (en) | Method and apparatus for explosive forming of metal articles | |
RU2086337C1 (en) | Method of making article of two cemented parts | |
US4101065A (en) | Method of manufacturing multilayer convex collared covers and bottoms for pressure vessels | |
JPH0985385A (en) | Production of bevel gear and sizing die thereof | |
US20040172998A1 (en) | Sealing system for super-plastic gas-pressure forming of aluminum sheets | |
RU2047408C1 (en) | Method for manufacture of enclosures from sheet billets | |
JPS609547A (en) | Manufacture of roughly formed material of connecting rod bolt | |
JP3293962B2 (en) | Manufacturing method of thin hemisphere | |
JPS61273222A (en) | Method and device for manufacturing container of superplastic material |