JPS6276429A - Interlayer tensile test method for laminated plate - Google Patents
Interlayer tensile test method for laminated plateInfo
- Publication number
- JPS6276429A JPS6276429A JP21729985A JP21729985A JPS6276429A JP S6276429 A JPS6276429 A JP S6276429A JP 21729985 A JP21729985 A JP 21729985A JP 21729985 A JP21729985 A JP 21729985A JP S6276429 A JPS6276429 A JP S6276429A
- Authority
- JP
- Japan
- Prior art keywords
- hole
- laminate
- circular hole
- load
- round bar
- 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
Landscapes
- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
Abstract
Description
【発明の詳細な説明】 〔産業上の利用分野〕 本発明は、積層板の層間引張試験法に関する。[Detailed description of the invention] [Industrial application field] The present invention relates to a method for interlaminar tensile testing of laminates.
積層板は異方性板であるために、三次元の機械的物性を
有し、その物性測定には様々な試験が必要である。測定
法の一例として、面内の引張試験、曲げ試験、層間せん
断試験などがあり、これらはすでに日本工業規格(J
I S)で制定されている。Since the laminate is an anisotropic plate, it has three-dimensional mechanical properties, and various tests are required to measure the properties. Examples of measurement methods include in-plane tensile tests, bending tests, and interlaminar shear tests, which are already compliant with the Japanese Industrial Standards (J
IS).
しかし、層間引張試験については積層板の板厚が薄いた
めに適切な試験方法が確立されていなかった。これは引
張試験を行うには試験機のつかみ治具に装着するために
試験片の両端部につかみ部を設けなければならず、試験
片にある程度の長さが必要であるからである。However, an appropriate test method for interlaminar tensile testing has not been established because the thickness of the laminate is thin. This is because, in order to perform a tensile test, gripping parts must be provided at both ends of the test piece in order to attach it to the gripping jig of the testing machine, and the test piece needs to have a certain length.
このような試験片を作成するために考えられる方法とし
ては、積層板の本来の板厚よりかなり厚肉にプレス成形
して試験片とする方法と、正規の板厚をもった積層板を
何枚も重ね、接着剤で接着する方法とがある。Possible methods for creating such a test piece include press-forming the laminate into a test piece much thicker than the original thickness, and using a laminate with the normal thickness to create a test piece. There is also a method of stacking the sheets and gluing them together with adhesive.
しかし、前者の方法では厚肉にするために、プレス成形
時に積層板に熱分布をもち、積層板の各部分で硬化条件
が異なったり、残留応力が生じたりして、同じ材質の積
層板でも板厚の違いで機械的特性がことなる虞があり好
ましくない。また後者の方法では、積層板間の接着力を
層間引張り強度より高めることは難しく、なかなか目的
の測定を達成することはできない。However, in the former method, in order to make the wall thick, the laminate has heat distribution during press forming, the curing conditions differ in each part of the laminate, and residual stress occurs, even if the laminate is made of the same material. This is not preferable since there is a possibility that the mechanical properties will differ due to the difference in plate thickness. Furthermore, in the latter method, it is difficult to increase the adhesive strength between the laminates beyond the interlaminar tensile strength, making it difficult to achieve the desired measurement.
本発明は本来の板厚のままでも積層板の層間引張試験が
できるような方法を提供するものである。The present invention provides a method by which an interlaminar tensile test can be performed on a laminate even when the original thickness remains unchanged.
本発明は積層板に上面から貫通しないストレートの円形
穴を開け、下面から該円形穴と穴軸が−敗し、かつ内径
が該円形穴の直径よりも大きい貫通しない円形の溝穴を
開け、互いの穴の深さの合計が積層板の板厚よりも大き
くなるように加工を゛施し、これを試験片として、該溝
穴の外形より大きい穴を開けた支持台の上に、溝穴を設
けた面を下にして、溝穴と支持台の穴の穴軸を一致させ
るように置き、該円形穴に同径の丸棒をさし込み、荷重
を加えることを特徴とする。The present invention involves drilling a non-penetrating straight circular hole in a laminate from the top surface, and drilling a non-penetrating circular slot hole from the bottom surface where the circular hole and the hole axis are connected to each other, and whose inner diameter is larger than the diameter of the circular hole. The holes were processed so that the total depth of each hole was greater than the thickness of the laminate, and this was used as a test piece. It is characterized in that it is placed with the side provided with it facing down so that the hole axes of the slot and the hole in the support stand are aligned, and a round rod of the same diameter is inserted into the circular hole to apply a load.
本発明を図面に従って詳細に説明する。The present invention will be explained in detail with reference to the drawings.
第1図は積層板の層間引張試験法の原理を説明する縦断
面図である。積層板5の一方の面にストレートの円形穴
1とその周りを囲むように他方の面から円形の溝穴かを
設けである。2つの穴はそれぞれ貫通しておらず、その
穴軸は互い一致している。穴の深さはA部のように2つ
の穴が大輪方向に重なった部分が出来るように加工され
ている。FIG. 1 is a longitudinal sectional view illustrating the principle of an interlaminar tensile test method for a laminate. A straight circular hole 1 is provided on one side of the laminated plate 5, and a circular slot hole is provided on the other side so as to surround the straight circular hole 1. The two holes do not pass through each other, and their hole axes coincide with each other. The depth of the holes is machined so that there is a part where two holes overlap in the direction of the large ring, as shown in part A.
すなわち、両穴の深さの合計が積層板の板厚より大きく
なっている。That is, the total depth of both holes is greater than the thickness of the laminate.
次に試験法について説明する。試験片は溝穴2の設けた
面を下にして支持台4に置く。支持台4に予め溝穴2の
外径より大きい穴を開けておき、互いの穴の穴軸を一致
させて、溝穴2の部分が支持台4の面に接触しないよう
にする。円形穴1には丸棒3を挿入し、この丸棒3に荷
重を加える。Next, the test method will be explained. The test piece is placed on the support stand 4 with the side with the slot 2 facing down. A hole larger than the outer diameter of the slot 2 is previously drilled in the support 4, and the axes of the holes are aligned to prevent the part of the slot 2 from contacting the surface of the support 4. A round rod 3 is inserted into the circular hole 1, and a load is applied to this round rod 3.
そうすれば、A部に示す部分に積層板5の層間方向に引
張力が生ずる。この層間に引張破壊が起こるまで丸棒3
に荷重を加え、破壊荷重を第2図のB部の面積で除すれ
ば積層板5の層間引張強度を求めることができる。By doing so, a tensile force is generated in the interlayer direction of the laminate 5 at the portion indicated by A section. Round bar 3 until tensile failure occurs between this layer.
The interlaminar tensile strength of the laminate 5 can be determined by applying a load to the laminate 5 and dividing the breaking load by the area of section B in FIG.
また、負荷時には円形穴1の底部のa部と溝穴2の底部
のb部は応力集中を受けやすくなるために、縁に面とり
または丸め加工をおこなうのが好ましい。また、円形穴
1の外壁と溝穴2の内壁の距離は0,5〜2flの範囲
とするのが好ましい。0゜5fl未満であると加工精度
が悪くなったり、寸法測定が難しくなり、2fl以上を
越えるとA部には眉間引張力よりもむしろ曲げ力がかか
るようになるので好ましくない。Furthermore, since stress concentration is likely to be applied to portion a of the bottom of the circular hole 1 and portion b of the bottom of the slotted hole 2 when a load is applied, it is preferable to chamfer or round the edges. Further, it is preferable that the distance between the outer wall of the circular hole 1 and the inner wall of the slot hole 2 is in the range of 0.5 to 2 fl. If it is less than 0.5 fl, processing accuracy will deteriorate and dimension measurement will become difficult, and if it exceeds 2 fl, bending force will be applied to the part A rather than glabellar tensile force, which is not preferable.
以下、本発明を実施例に基づいて詳細に説明する。 Hereinafter, the present invention will be explained in detail based on examples.
積層板は紙を基材としたフェノール樹脂積層板を用いた
。板厚は1.541mである。第3図に試験片の加工に
使用した工具を示す。(alはヘリカルコンドミルで円
形穴の加工に用いる。直径は1龍で先端エツジに0,1
5tm程度の面とりを行った。(b)は2枚刃のパラレ
ルエンドミルに加工を加えて溝穴加工用にしたものであ
る。全体の直径は3 mmで、刃先に加工を施し、刃幅
0.5鶴の溝切り刃をつけた。溝切り刃の刃先の内側エ
ッヂには0.1’5mm程度の面とりを行った。試験片
の加工はボール盤で行い、両穴とも深さは1flである
。The laminate used was a phenolic resin laminate with a paper base. The plate thickness is 1.541 m. Figure 3 shows the tools used to process the test piece. (Al is a helical condom mill used for machining circular holes.The diameter is 1 dragon and the tip edge is 0,1
A chamfer of approximately 5 tm was chamfered. (b) is a two-blade parallel end mill that has been modified for slotting. The overall diameter is 3 mm, and the cutting edge has been processed to have a groove cutting blade with a blade width of 0.5 mm. The inner edge of the cutting edge of the groove cutting blade was chamfered to a depth of about 0.1'5 mm. The test piece was processed using a drilling machine, and both holes had a depth of 1 fl.
試験状態を第4図に示す。支持台の上に試験片である積
層板をのせ、円形穴に丸棒3をさし込む。The test conditions are shown in Figure 4. A laminate plate, which is a test piece, is placed on a support stand, and a round bar 3 is inserted into the circular hole.
円形穴に挿入する側の丸棒先端には0.150の面とり
を行った。丸棒3は倒れないようにガイド6が設けであ
る。試験機にはモータ駆動式引張試験機を使用し、丸棒
3に圧縮荷重を加える。試験速度は1mm/minであ
る。The tip of the round bar on the side to be inserted into the circular hole was chamfered to 0.150. A guide 6 is provided to prevent the round bar 3 from falling. A motor-driven tensile testing machine is used as the testing machine, and a compressive load is applied to the round bar 3. The test speed is 1 mm/min.
試験結果を第5図に示す。これは層間引張強度の温度推
移を表したものである。The test results are shown in Figure 5. This represents the change in interlaminar tensile strength with temperature.
本発明により、本来の板厚のままで積層板の層間引張強
度の測定が可能となった。According to the present invention, it has become possible to measure the interlaminar tensile strength of a laminate without changing its original thickness.
第1図は積層板の層間引張試験の原理を説明する縦断面
図、第2図は加工を施した積N板の平面図、第3図(a
l (b)はは試験片の加工に用いる工具の正面図で、
第4図は試験時の縦断面説明図、第5図は紙を基材とし
たフェノール樹脂積層板の層間引張強度の測定結果の温
度推移を示すグラフである。
1 円形穴 2 溝穴
3 丸棒 4 支持台
5 積層板 6 ガイド 771
.61.。
代理人 弁理士 若林邦彦1.゛、、”パ□。
!−・51′
第4図
3L 度 (’C)
第5図
手続補正書(自発)
昭和60年巴月11 日
と
1、事件の″表示
昭和60年特許願第217299号
2、発明の名称
積層板の層間引張試験法
3、補正をする者
事件との関係 特許出願人
名 称 +445)日立化成工業株式会社4、代 理
人
6、補正の内容
(1)%許請求の範囲を別紙の通り訂正する。
(2)明細書第6頁第5行目に「・・・試験片を作成す
るために・・・」とあるを「・・・試験片を作表するた
めに・・・」と訂正する。
(5)明al:iF第4頁第7行目に「・・・該溝穴の
外形より大」とあるを「・・・該溝穴の外径より大」と
訂正する。
(4)明細書第6頁第7行目に「(a)はヘリカルコ」
とあるを「(a)はヘリカル王」と訂正する。
(5)明a’l第7頁の下から6行目に「第6図(a)
(bJはは・・・」とあるを[第3図(a)(b)!!
・・・」と訂正する。
(別紙)
特許請求の範囲
1、積層板に上面から貫通しないストレートの円形穴を
開け、下面から該円形穴と太軸が一致し、かつ内径が該
円形穴の直径よシも大きい貫通しない円形の溝穴を開け
、互いの穴の深さの合計が積層板の板厚よりも大きくな
るように加工音節し、こn’t”試験片として、該溝穴
の外径より大きい穴を開けt支持台の上に、溝穴を設け
た面を下にして、溝穴と支持台の穴の太軸を一致させる
ように置き、該円形穴に同径の丸棒をさし込み、荷重を
加えることを特徴とする積層板の層間引張試験法。
2、試験片のストレートの円形穴底面の縁と円形の溝穴
の底面内縁とが面とシまたは丸め加工されている特許請
求の範囲第1項記載の積層板の層間引張試験法。
五 試験片のストレートの円形穴の外壁と円形の溝穴の
内壁の距離が0.5〜2.0111ffl(1)範囲に
加工されている特許請求の範囲第1項または第2項記載
の積層板の層間引張試験法。Figure 1 is a longitudinal cross-sectional view explaining the principle of interlaminar tensile testing of laminated plates, Figure 2 is a plan view of processed N-laminated plates, and Figure 3 (a
l (b) is a front view of the tool used to process the specimen;
FIG. 4 is an explanatory longitudinal cross-sectional view during the test, and FIG. 5 is a graph showing the temperature change of the measurement results of the interlaminar tensile strength of the phenolic resin laminate using paper as the base material. 1 Circular hole 2 Slot 3 Round bar 4 Support stand 5 Laminated plate 6 Guide 771
.. 61. . Agent Patent Attorney Kunihiko Wakabayashi 1.゛、、"Pa□.!-・51' Figure 4 3L Degree ('C) Figure 5 Procedural Amendment (Spontaneous) 11th and 1st Tomoe, 1985, 1985 Patent Application No. No. 217299 2, Name of the invention Interlaminar tensile test method for laminates 3, Relationship with the case of the person making the amendment Patent applicant name +445) Hitachi Chemical Co., Ltd. 4, Agent
Person 6, Contents of amendment (1) The scope of the % claim is corrected as shown in the attached sheet. (2) In the 5th line of page 6 of the specification, the phrase "...to prepare test pieces..." is corrected to "...to tabulate test pieces..." . (5) Clarification: In the 7th line of page 4 of iF, the phrase "...larger than the outer diameter of the slot" is corrected to "...larger than the outer diameter of the slot." (4) “(a) is helicalco” on page 6, line 7 of the specification.
Correct the statement to read, ``(a) is King Helical.'' (5) In the 6th line from the bottom of the 7th page of the clear page ``Figure 6 (a)
(bJ Haha...”) [Figure 3 (a) (b)!!
"..." I corrected myself. (Attachment) Claim 1: A straight circular hole that does not penetrate from the top surface of the laminate, and a circular hole that does not penetrate from the bottom surface, whose thick axis coincides with the circular hole, and whose inner diameter is larger than the diameter of the circular hole. Drill a slotted hole, process the holes so that the total depth of each hole is greater than the thickness of the laminate, and use this as a test specimen to drill a hole larger than the outer diameter of the slotted hole. t Place the slotted side on the support base so that the thick axes of the slots and the holes in the support base are aligned, insert a round bar with the same diameter into the circular hole, and apply the load. An interlaminar tensile test method for a laminate, characterized in that the edge of the bottom of the straight circular hole of the test specimen and the inner edge of the bottom of the circular slot are rounded or rounded. Interlaminar tensile testing method for laminates according to paragraph 1. 5. A patent in which the distance between the outer wall of the straight circular hole of the test piece and the inner wall of the circular slot is in the range of 0.5 to 2.0111ffl (1). An interlaminar tensile test method for a laminate according to claim 1 or 2.
Claims (1)
開け、下面から該円形穴と穴軸が一致し、かつ内径が該
円形穴の直径よりも大きい貫通しない円形の溝穴を開け
、互いの穴の深さの合計が積層板の板厚よりも大きくな
るように加工を施し、これを試験片として、該溝穴の外
形より大きい穴を開けた支持台の上に、溝穴を設けた面
を下にして、溝穴と支持台の穴の穴軸を一致させるよう
に置き、該円形穴に同径の丸棒をさし込み、荷重を加え
ることを特徴とする積層板の層間引張試験法。 2、試験片のストレートの円形穴底面の縁と円形の溝穴
の底面内縁とが面とりまたは丸め加工されている特許請
求の範囲第1項記載の積層板の層間引張試験法。 3、試験片のストレートの円形穴の外壁と円形の溝穴の
内壁の距離が0.5〜2.0mmの範囲に加工されてい
る特許請求の範囲第1項または第2項記載の積層板の層
間引張試験法。[Scope of Claims] 1. A straight circular hole that does not penetrate from the top surface of the laminate, and a circular groove that does not penetrate from the bottom surface and whose hole axis coincides with the circular hole and whose inner diameter is larger than the diameter of the circular hole. Holes were drilled and processed so that the total depth of each hole was greater than the thickness of the laminate, and this was used as a test piece and placed on a support stand with a hole larger than the outer diameter of the slot. , with the side with the slotted hole facing down, the hole axes of the slotted hole and the hole of the support stand are aligned, and a round rod of the same diameter is inserted into the circular hole to apply a load. Interlaminar tensile test method for laminates. 2. The interlaminar tensile test method for a laminate according to claim 1, wherein the edge of the bottom of the straight circular hole of the test piece and the inner edge of the bottom of the circular slot are chamfered or rounded. 3. The laminate according to claim 1 or 2, wherein the distance between the outer wall of the straight circular hole and the inner wall of the circular slot of the test piece is in the range of 0.5 to 2.0 mm. Interlaminar tensile test method.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP21729985A JPS6276429A (en) | 1985-09-30 | 1985-09-30 | Interlayer tensile test method for laminated plate |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP21729985A JPS6276429A (en) | 1985-09-30 | 1985-09-30 | Interlayer tensile test method for laminated plate |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS6276429A true JPS6276429A (en) | 1987-04-08 |
Family
ID=16701960
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP21729985A Pending JPS6276429A (en) | 1985-09-30 | 1985-09-30 | Interlayer tensile test method for laminated plate |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS6276429A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH01196537A (en) * | 1988-02-01 | 1989-08-08 | Agency Of Ind Science & Technol | Method and apparatus for evaluating adhesion strength of film |
KR100994933B1 (en) | 2008-07-21 | 2010-11-19 | 한국과학기술원 | Indentation-driven tensile test specimen with single test section and manufacturing method thereof |
JP2015003409A (en) * | 2013-06-19 | 2015-01-08 | 住友ベークライト株式会社 | Method for measuring adhesion strength against peeling |
-
1985
- 1985-09-30 JP JP21729985A patent/JPS6276429A/en active Pending
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH01196537A (en) * | 1988-02-01 | 1989-08-08 | Agency Of Ind Science & Technol | Method and apparatus for evaluating adhesion strength of film |
KR100994933B1 (en) | 2008-07-21 | 2010-11-19 | 한국과학기술원 | Indentation-driven tensile test specimen with single test section and manufacturing method thereof |
JP2015003409A (en) * | 2013-06-19 | 2015-01-08 | 住友ベークライト株式会社 | Method for measuring adhesion strength against peeling |
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