JP2580287B2 - How to make a metal San German panel - Google Patents

How to make a metal San German panel

Info

Publication number
JP2580287B2
JP2580287B2 JP63273125A JP27312588A JP2580287B2 JP 2580287 B2 JP2580287 B2 JP 2580287B2 JP 63273125 A JP63273125 A JP 63273125A JP 27312588 A JP27312588 A JP 27312588A JP 2580287 B2 JP2580287 B2 JP 2580287B2
Authority
JP
Japan
Prior art keywords
sheets
thin
core
panel
sheet
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.)
Expired - Fee Related
Application number
JP63273125A
Other languages
Japanese (ja)
Other versions
JPH02121733A (en
Inventor
隆之 都筑
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP63273125A priority Critical patent/JP2580287B2/en
Publication of JPH02121733A publication Critical patent/JPH02121733A/en
Application granted granted Critical
Publication of JP2580287B2 publication Critical patent/JP2580287B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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  • Shaping Metal By Deep-Drawing, Or The Like (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は、航空機,ロケツト、スペースシヤトル等の
各種宇宙往還機に用いられる断熱パネルや人工衛星用に
用いられるアビオニクスパネル等に適用する各種の金属
製サンドイツチパネルの製作方法に関する。
DETAILED DESCRIPTION OF THE INVENTION [Industrial Application Field] The present invention relates to various types of insulation panels used for various spacecraft such as aircraft, rockets, space shuttles, and avionics panels used for artificial satellites. The present invention relates to a method for manufacturing a metal San German panel.

〔従来の技術〕[Conventional technology]

従来航空機宇宙機器等に使用する金属サンドイツチパ
ネルの製造技術としては次に示すような方法が普通に知
られている。
2. Description of the Related Art Conventionally, the following method is generally known as a manufacturing technique of a metal San German panel used for aerospace equipment and the like.

(1) コアを所定の形状に成形し、その後フエースシ
ートを接合してパネルとする方法。
(1) A method in which a core is formed into a predetermined shape and then a face sheet is joined to form a panel.

(2) 3枚以上の板を用いて、対向する板の所定の位
置を選択的に拡散接合した後に超塑性的に板をふくらま
せてパネルとする方法。
(2) A method in which three or more plates are selectively diffusion-bonded to predetermined positions of opposing plates, and then the plates are superplastically inflated into panels.

(3) 所定の位置を選択的に溶接した2枚の板を超塑
性的にふくらませ、その外層に配置した板と拡散接合し
てパネルとする方法。
(3) A method in which two plates having predetermined positions selectively welded are superplastically inflated and diffusion-bonded to a plate disposed on the outer layer to form a panel.

〔発明が解決しようとする課題〕[Problems to be solved by the invention]

ところで、前述の従来の金属サンドイツチパネルの各
製作方法ではそれぞれ次に示すような不具合点がある。
By the way, each of the above-mentioned conventional methods of manufacturing a metal San Germanium panel has the following disadvantages.

(1) 従来方法1ではコアとフエースシートを個別に
成形するため、金型コスト,製作コストが共に高くなる
のと同時に、接合面精度に問題があり、コア形状の複雑
なものや曲面パネルの製作は非常に困難である。
(1) In the conventional method 1, since the core and the face sheet are separately molded, both the mold cost and the manufacturing cost are increased, and at the same time, there is a problem in the joint surface accuracy, and the complicated core shape and the curved panel are not used. Fabrication is very difficult.

(2) 従来方法2では接合防止用マスカット(セラミ
ックの微粒子を主成分としたもの)の接合部への飛散に
より接合不良を生じたり、あるいは接合予定部以外が接
合する可能性があり、品質の安定性に問題があるのと同
時に、適用材料が拡散接合性を有する同種の材料に限ら
れるという問題がある。
(2) In the conventional method 2, there is a possibility that a joint failure may occur due to scattering of the joint-preventing muscat (mainly composed of ceramic fine particles) to the joint portion, or a portion other than the portion to be joined may be joined. At the same time, there is a problem in stability, and there is a problem in that the applied material is limited to the same type of material having diffusion bonding properties.

(3) 従来方法3では、超塑性成形中の接合面汚染に
よるコアとフエースシートの拡散接合不良が生ずる可能
性があり、品質の安定性に問題があるのと同時に適用材
料が拡散接合性を有する同種の材料に限られ、更に4層
をこえる多層パネルの製作は不可能である。
(3) In the conventional method 3, there is a possibility that the diffusion bonding failure between the core and the face sheet may occur due to contamination of the bonding surface during the superplastic forming. It is not possible to manufacture a multilayer panel having more than four layers, limited to the same kind of material.

本発明は上記各不具合点を解決した新たな金属サンド
イツチパネルの製作方法を提供しようとするものであ
る。
An object of the present invention is to provide a new method for manufacturing a metal San Grenchi panel that has solved the above-mentioned disadvantages.

〔課題を解決するための手段〕[Means for solving the problem]

このため本発明の金属サンドイッチパネルの製作方法
は、サンドイッチパネルのコアシート部構成用部材と、
フェースシート構成部材である2枚もしくは3枚の薄板
の任意の位置を適宜溶接手段等により接合した薄板の組
を2組以上コアシート同志が重なり合うよう積層し、更
にこれら各薄板の各組の積層時対向する各組最外層とな
るコアシート構成部材を超塑性特性を有する材料製とす
ると共に該板同志を薄板外側端部で接合もしくは機械的
にクランプ又は板間を真空引きして密接保持するよう形
成して被加工体を一体に構成し、該被加工体を上下の金
型間に位置決め配置して金型によりクランプし、次いで
超塑性成形温度に加熱して前記各薄板を膨らませ、所定
の形状を有す該金型に密着させることにより超塑性成形
を行うことを特徴としている。
For this reason, the method for manufacturing a metal sandwich panel of the present invention includes a member for forming a core sheet portion of the sandwich panel,
Two or more sets of thin sheets in which arbitrary positions of two or three thin sheets as face sheet constituent members are appropriately joined by welding means or the like are stacked so that two or more sets of core sheets overlap each other, and further, each set of these thin sheets is stacked. The core sheet constituting member which is the outermost layer of each pair is made of a material having superplastic properties, and the plates are joined at the outer ends of the thin plates or mechanically clamped or vacuumed between the plates to hold them tightly. The workpiece is integrally formed, the workpiece is positioned between the upper and lower molds, clamped by the molds, and then heated to a superplastic forming temperature to expand each of the thin sheets, and It is characterized in that superplastic forming is performed by bringing the mold into close contact with the mold having the following shape.

〔作用〕[Action]

前述の本発明金属サンドイツチパネルの製作方法によ
れば、2枚もしくは3枚づつを所定の(任意の)位置で
接合した薄板の組を積層して、金型内で超塑性成形温度
に加熱して各薄板の組の板の隙間内部に流体圧を負荷し
超塑性成形することにより、対向する各薄板組の最外層
の板同志は互いに密着したまゝ同一形状に成形されあた
かも一枚の板のように扱うことが可能となる。これによ
りコアとフエースシートの接合品質が安定するのと同時
に、拡散接合性を有しない材料や異種材料の組合せに対
しても適用可能であり、更に曲面パネル,多層パネルも
製作できるという特徴を有している。
According to the above-described method of manufacturing a metal San Germanium panel of the present invention, two or three sheets are joined at predetermined (arbitrary) positions, and a set of thin plates is laminated and heated to a superplastic forming temperature in a mold. By applying a fluid pressure inside the gap between the plates of each set of thin plates and performing superplastic forming, the outermost plates of each of the opposed sets of thin plates are formed into the same shape while being in close contact with each other, as if one sheet It can be handled like a board. This stabilizes the bonding quality between the core and the face sheet, and at the same time, is applicable to materials that do not have diffusion bonding properties or a combination of different materials, and can also produce curved panels and multilayer panels. doing.

〔実施例〕〔Example〕

以下図面により本発明の一実施例方法について説明す
ると、第1図は本発明の第1の実施例を示す作用説明
図、第2図は第2の実施例を示す作用説明図である。
The method of one embodiment of the present invention will be described below with reference to the drawings. FIG. 1 is an operation explanatory view showing a first embodiment of the present invention, and FIG. 2 is an operation explanatory view showing a second embodiment.

先ず第1図に於いて、サンドイッチパネルのコアシー
ト構成部材となる2枚の薄板2、3を所定の接合位置1
においてサンドイッチパネルのフェースシート構成部材
と適宜溶接手段により接合した2つの薄板の組を、該コ
アシート部を構成する薄板2、3同志が重なり合うよう
2組重ね合わせ、対向する各組の最外層の板同志すなわ
ちコアシート構成部材同志をその板外側端5で溶接又は
機械的にクランプして接合して被加工体6を構成する。
薄板最外層部の対向する各組外側端部5での接合は2枚
の板(2、3)の間を真空引きし、超塑性成形中2枚の
板を密着させておくためのものであり、密着性,気密性
が維持できれば特に必要ではない。次に被加工体6を上
型7及び下型8の間に位置決めして周囲をクランプし、
超塑性成形温度に加熱して、薄板の組2,3の各々の板隙
間内部に流体圧を負荷してふくらませ、型に密着させる
ことにより、金属サンドイツチパネル9を製作する。こ
のとき、対向する各組の最外層の板(2、3)は互いに
密着したまま同一形状に成形され、成形温度にて拡散接
合性を有する材料であれば成形中に接合して一体の板10
となる。また拡散接合性を有しない材料の場合は、最外
層板間にフイラーメタルを挿入しておいて成形中あるい
はその前後にろう付けしても良い。第2図の実施例の場
合は、4枚の薄板2、3、4を含む3つの薄板の組を第
1図の場合と同様に接合して積層した場合を示してい
る。その他の製作工程は第1図の場合と同様であるので
説明を省略する。
First, in FIG. 1, two thin plates 2 and 3 serving as core sheet constituent members of a sandwich panel are joined at a predetermined joining position 1.
In the above, two sets of thin plates joined to the face sheet constituting member of the sandwich panel by welding means are overlapped with two sets of thin plates 2 and 3 constituting the core sheet portion so as to overlap each other, and the outermost layer of each of the opposing sets is overlapped. The workpieces 6 are formed by welding or mechanically clamping the plates, that is, the core sheet components, at the outer ends 5 of the plates.
The joining of the outermost layer portion of the thin plate at the opposing outer end portions 5 of each pair is for evacuating the two plates (2, 3) to keep the two plates in close contact during superplastic forming. Yes, it is not particularly necessary if the adhesion and airtightness can be maintained. Next, the workpiece 6 is positioned between the upper mold 7 and the lower mold 8 and the periphery thereof is clamped.
By heating to the superplastic forming temperature and applying fluid pressure to the inside of the gap between each of the sets of thin plates 2 and 3 to inflate them, and bringing them into close contact with the mold, the metal sanctuary panel 9 is manufactured. At this time, the opposing outermost plates (2, 3) of each set are formed into the same shape while being in close contact with each other, and if a material having diffusion bonding property at the forming temperature is bonded during the forming, an integrated plate is formed. Ten
Becomes In the case of a material having no diffusion bonding property, a filler metal may be inserted between the outermost layer plates and brazed during or before and after molding. The embodiment of FIG. 2 shows a case where three thin plate sets including four thin plates 2, 3, and 4 are joined and laminated in the same manner as in the case of FIG. Other manufacturing steps are the same as those in FIG.

なお、各薄板組の接合方法としてはスポツト溶接,シ
ーム溶接など各種接合方法が適用可能である。
Various joining methods such as spot welding and seam welding can be applied as the joining method of each thin plate set.

〔発明の効果〕〔The invention's effect〕

以上述べたように本発明の効果を前述の従来方法との
比較で述べると次の通りである。
As described above, the effects of the present invention are described below in comparison with the above-described conventional method.

(1) 従来方法1に比較してコア形状,パネル曲率の
自由度の大幅向上,コストの大幅低減等の効果を有す
る。
(1) Compared to the conventional method 1, there are effects such as a significant improvement in the degree of freedom of the core shape and the panel curvature, a significant reduction in cost, and the like.

(2) 従来方法2,3に比較して接合品質の向上,適用
可能材料の拡大,パネルの多層化に対する自由度の拡大
等の効果を有する。
(2) Compared to the conventional methods 2 and 3, it has the effects of improving the joining quality, expanding the applicable materials, and increasing the degree of freedom for multi-layer panels.

(3)フェースシートとコアシートのセットをコアシー
ト同志が重なるよう積層し、しかも重なり合うコアシー
トとコアシートを超塑性成形以前に密着保持したまま同
一形状に成形したことにより、コアシートとコアシート
の接合品質の確保と、コアシートの板厚分布に均一化を
図ることができる効果を有する。
(3) The core sheet and the core sheet are formed by laminating a set of the face sheet and the core sheet so that the core sheets overlap each other, and forming the overlapping core sheet and the core sheet into the same shape while keeping the core sheet and the core sheet in close contact with each other before superplastic forming. This has the effect that the bonding quality of the core sheet can be ensured and the thickness distribution of the core sheet can be made uniform.

【図面の簡単な説明】[Brief description of the drawings]

第1図は本発明の第1の実施例を示す作用説明図、第2
図は第2の実施例の作用説明図である。 1……接合部、2,3,4……薄板、5……接合部、6……
被加工体、7……上型、8……下型、9……金属サンド
イツチパネル、10……一体接合板
FIG. 1 is an operation explanatory view showing a first embodiment of the present invention, and FIG.
The figure is a diagram for explaining the operation of the second embodiment. 1 ... joint, 2, 3, 4 ... thin plate, 5 ... joint, 6 ...
Workpiece, 7: Upper die, 8: Lower die, 9: Metallic San German panel, 10: Integrated plate

Claims (1)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】サンドイッチパネルのコアシート部構成用
部材と、フェースシート構成部材である2枚もしくは3
枚の薄板の任意の位置を適宜溶接手段等により接合した
薄板の組を2組以上コアシート同志が重なり合うよう積
層し、更にこれら各薄板の各組の積層時対向する各組最
外層となるコアシート構成部材を超塑性特性を有する材
料製とすると共に該板同志を薄板外側端部で接合もしく
は機械的にクランプ又は板間を真空引きして密着保持す
るよう形成して被加工体を一体に構成し、該被加工体を
上下の金型間に位置決め配置して金型によりクランプ
し、次いで超塑性成形温度に加熱して前記各薄板を膨ら
ませ、所定の形状を有す該金型に密着させることにより
超塑性成形を行うことを特徴とする金属サンドイッチパ
ネルの製作方法。
1. A member for constituting a core sheet portion of a sandwich panel, and two or three members constituting a face sheet.
At least two sets of thin sheets in which arbitrary positions of the thin sheets are appropriately joined by welding means or the like are laminated so that the core sheets overlap each other, and furthermore, the core which becomes the outermost layer of each set facing each other when the respective sets of these thin sheets are laminated. The sheet members are made of a material having superplastic properties, and the sheets are joined together at the outer end of the thin sheet or mechanically clamped or vacuum-formed between the sheets so that the sheets are held in close contact with each other to integrally form the workpiece. The workpiece is positioned between the upper and lower dies, clamped by the dies, and then heated to a superplastic forming temperature to expand each of the thin plates and adhere to the dies having a predetermined shape. A method for manufacturing a metal sandwich panel, comprising:
JP63273125A 1988-10-31 1988-10-31 How to make a metal San German panel Expired - Fee Related JP2580287B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP63273125A JP2580287B2 (en) 1988-10-31 1988-10-31 How to make a metal San German panel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP63273125A JP2580287B2 (en) 1988-10-31 1988-10-31 How to make a metal San German panel

Publications (2)

Publication Number Publication Date
JPH02121733A JPH02121733A (en) 1990-05-09
JP2580287B2 true JP2580287B2 (en) 1997-02-12

Family

ID=17523476

Family Applications (1)

Application Number Title Priority Date Filing Date
JP63273125A Expired - Fee Related JP2580287B2 (en) 1988-10-31 1988-10-31 How to make a metal San German panel

Country Status (1)

Country Link
JP (1) JP2580287B2 (en)

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4304821A (en) 1978-04-18 1981-12-08 Mcdonnell Douglas Corporation Method of fabricating metallic sandwich structure

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4304821A (en) 1978-04-18 1981-12-08 Mcdonnell Douglas Corporation Method of fabricating metallic sandwich structure

Also Published As

Publication number Publication date
JPH02121733A (en) 1990-05-09

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