JPS63210640A - Apparatus for testing twist fatigue of composite material - Google Patents

Apparatus for testing twist fatigue of composite material

Info

Publication number
JPS63210640A
JPS63210640A JP4154687A JP4154687A JPS63210640A JP S63210640 A JPS63210640 A JP S63210640A JP 4154687 A JP4154687 A JP 4154687A JP 4154687 A JP4154687 A JP 4154687A JP S63210640 A JPS63210640 A JP S63210640A
Authority
JP
Japan
Prior art keywords
composite material
torsional fatigue
testing device
gripping
materials according
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
Application number
JP4154687A
Other languages
Japanese (ja)
Other versions
JPH0785049B2 (en
Inventor
Kenhachi Mihashi
健八 三橋
Hiroyuki Kaido
博幸 海藤
Kunihiko Fujimoto
邦彦 藤本
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.)
Yokohama Rubber Co Ltd
Original Assignee
Yokohama Rubber Co 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 Yokohama Rubber Co Ltd filed Critical Yokohama Rubber Co Ltd
Priority to JP4154687A priority Critical patent/JPH0785049B2/en
Publication of JPS63210640A publication Critical patent/JPS63210640A/en
Publication of JPH0785049B2 publication Critical patent/JPH0785049B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

PURPOSE:To detect only pure twist fatigue without acting load other than a twist on a sample, by making one of both grasping parts of a tubular composite material freely movable in the axial direction. CONSTITUTION:Both ends of a tubular composite material S are grasped by grasping parts 5, 6 and twist load within such a range that vibration frequency is 1-4Hz and amplitude is pi/2-pi/3 rad is repeatedly applied to the composite material S while internal pressure of 200-300KPa is applied by a compressor 8. The tubular composite material S generates change such that said material S shrinks in the diameter direction and axial direction thereof and extends to the original state when the load is released. However, the composite material S is held to an almost constant diameter corresponding to extension and shrinkage change so that the generation of collapse is prevented with respect to the shrinkage in the diameter direction by the internal pressure from the compressor 8 and the generation of tensile stress is prevented with respect to the shrinkage in the axial direction by the movement of the grasping part 6 toward the grasping part 5. Therefore, only pure twist fatigue is detected by a torque meter 3.

Description

【発明の詳細な説明】 〔発明の技術分野〕 本発明はプラスチック、ゴム等を主材とする複合材の捩
り疲労を試験する装置に関するものである。
DETAILED DESCRIPTION OF THE INVENTION [Technical Field of the Invention] The present invention relates to an apparatus for testing torsional fatigue of composite materials mainly made of plastic, rubber, etc.

〔従来技術〕[Prior art]

プラスチック、ゴム等の材料は補強コードで補強された
り、或いは性質の異なるプラスチック、ゴム等が互いに
組み合わされて、複合材として使用されることがある。
Materials such as plastics and rubbers may be reinforced with reinforcing cords, or plastics, rubbers, etc. with different properties may be combined with each other to form a composite material.

このような複合材を使用するとき、捩り疲労特性は重要
な評価ファクターの一つになっている。しかし、従来の
複合材の捩り疲労試験装置では測定データにノイズが多
く、信頬性が低いという問題があった。
When using such composite materials, torsional fatigue properties are one of the important evaluation factors. However, conventional torsional fatigue test equipment for composite materials has a problem in that the measurement data contains a lot of noise and has low reliability.

例えば、米国特許第2,412.524号明細書に記載
された捩り疲労試験装置では、チューブ状にしたサンプ
ルの両端を把持し、その一方の端部に捩りを加えるよう
にしたものであるが、この撲りを加えることによって、
サンプルが軸方向(長手方向)に収縮して引張り応力を
発生するため、純粋な捩り疲労だけを測定することがで
きないという問題があるのである。
For example, in the torsional fatigue test device described in U.S. Pat. No. 2,412,524, both ends of a tube-shaped sample are held and one end is twisted. , by adding this distortion,
The problem is that pure torsional fatigue cannot be measured because the sample contracts in the axial direction (longitudinal direction) and generates tensile stress.

〔発明の目的〕[Purpose of the invention]

本発明の目的は、上述のような従来の試験装置の欠点を
解消し、サンプルに涙り以外の負荷が作用せず、純粋な
捩り疲労のみを測定することができる複合材の捩り疲労
試験装置を提供することにある。
The purpose of the present invention is to provide a torsional fatigue testing device for composite materials that can eliminate the drawbacks of conventional testing devices as described above, and can measure only pure torsional fatigue without applying any load other than tearing to the sample. Our goal is to provide the following.

〔発明の構成〕[Structure of the invention]

上記目的を達成するための本発明の装置は、測定サンプ
ルのチューブ状複合材両端を把持する把持部とそのチュ
ーブ状複合材に内圧を加える加圧部とを設け、前記両把
持部の一方を往復回転駆動部に連結するとともに、他方
を涙り疲労検出部に連結し、かつ両把持部のいずれか一
方を前記チューブ状複合材の軸方向に移動自在にしたこ
とを特徴とするものである。
The apparatus of the present invention for achieving the above object is provided with a gripping part that grips both ends of a tubular composite material of a measurement sample, and a pressurizing part that applies internal pressure to the tubular composite material, and a pressure part that applies internal pressure to the tubular composite material. The gripping portion is connected to a reciprocating rotation drive portion, and the other is connected to a tear fatigue detection portion, and one of the gripping portions is movable in the axial direction of the tubular composite material. .

本発明において、複合材の測定サンプルはチューブ状に
形成されている。さらに好ましくは、少なくとも2枚の
カレンダー材が互いに異なる角度をなして貼り合わされ
ることにより構成される。第5図はその一例を示したも
ので、それぞれコードa、bで補強されたプラスチック
In the present invention, the composite material measurement sample is formed into a tube shape. More preferably, at least two sheets of calendar material are pasted together at different angles. Figure 5 shows an example of this, where plastic is reinforced with cords a and b, respectively.

ゴム等のシート層A、Bが積層されてチューブ状複合材
Sを構成している。
Sheet layers A and B made of rubber or the like are laminated to form a tubular composite material S.

本発明の捩り疲労試験装置は、このようなチューブ状複
合材の一端を往復回転駆動部に連結した把持部で把持す
る一方、他端を捩り疲労検出部に連結した把持部で把持
し、加圧部によって内圧を負荷しつつ前者の往復回転駆
動部により往復捩り荷重をサンプルに負荷するようにす
るが、このとき両把持部のいずれか一方をチューブ状複
合材の軸方向に移動自在にするものである。移動自在に
する側は、後述する実施例のように捩り疲労検出部側の
把持部が好ましいが、往復回転駆動部側の把持部を移動
自在にしてもよい。往復回転駆動部が負荷する捩り荷重
は、振動数が1〜4Hzの範囲で、振幅がπ/2〜π/
3radの範囲が好ましく、また加圧部で負荷する内圧
としては200〜300KPaの範囲が好ましい。
The torsional fatigue testing device of the present invention grips one end of such a tubular composite material with a gripping section connected to a reciprocating rotation drive section, while gripping the other end with a gripping section connected to a torsional fatigue detection section. While internal pressure is applied by the pressure part, a reciprocating torsional load is applied to the sample by the former reciprocating rotation drive part, and at this time, one of the gripping parts is made freely movable in the axial direction of the tubular composite material. It is something. The movable side is preferably the gripping part on the torsional fatigue detection part side as in the embodiment described later, but the gripping part on the reciprocating rotation driving part side may be made movable. The torsional load applied by the reciprocating rotation drive unit has a frequency of 1 to 4 Hz and an amplitude of π/2 to π/
A range of 3 rad is preferable, and a range of 200 to 300 KPa is preferable as the internal pressure applied in the pressurizing section.

本発明において、上記往復回転駆動部としてはサーボモ
ータの使用が好ましく、捩り疲労検出部にはトルクメー
タの使用が好ましく、また内圧負荷を行う加圧部にはニ
アコンプレッサが好ましい。また、把持部を移動自在に
するための機構としては出来るだけ摩擦抵抗を発生せず
、円滑な移動ができるものがよく、後述の実施例のよう
に把持部の支持台をベアリングを介してレール上に載せ
、そのレールに沿ってスライドできるようにしたものが
好ましい。
In the present invention, it is preferable to use a servo motor as the reciprocating rotation drive section, a torque meter is preferably used as the torsional fatigue detection section, and a near compressor is preferable as the pressurization section that applies internal pressure load. In addition, as a mechanism for making the grip part movable, it is preferable to use a mechanism that allows for smooth movement without generating frictional resistance as much as possible. It is preferable to place it on top and be able to slide it along the rail.

また、把持部はチューブ状複合材をすべりを生じないよ
うに確実に固定できるものが好ましく、このような把持
部として後述の実施例のようなテーパ型締付はチャック
が優れている。このテーパ型締付はチャックの使用によ
ってチューブ状複合材に正確な捩り角を与えることがで
き、正確な捩り疲労の測定を可能にする。
Further, it is preferable that the gripping part is capable of reliably fixing the tubular composite material without slipping, and a chuck is excellent for such a gripping part in the case of tapered clamping as in the embodiments described below. This tapered clamping can provide an accurate twist angle to the tubular composite material by using a chuck, allowing accurate torsional fatigue measurements.

第1図は本発明の実施例からなる換り疲労試験装置を概
略的に示すものである。1は装置全体を支持するベース
であり、このベース1上の一方の端部に往復回転駆動部
としてサーボモータ2が設置され、また他方の端部に涙
り疲労検出部としてトルクメータ3が設置されている。
FIG. 1 schematically shows an alternative fatigue testing apparatus according to an embodiment of the present invention. Reference numeral 1 denotes a base that supports the entire device, and a servo motor 2 is installed at one end of the base 1 as a reciprocating rotation drive unit, and a torque meter 3 is installed at the other end as a tear fatigue detection unit. has been done.

サーボモータ2は駆動ユニット7により制御され、振動
数1〜4Hz、振幅π/2〜π/3radの範囲で往復
回転ができるようになっている。
The servo motor 2 is controlled by a drive unit 7 and is capable of reciprocating rotation within a frequency range of 1 to 4 Hz and an amplitude of π/2 to π/3 rad.

また、トルクメータ3には記録計11が接続され、検出
したトルク変化を捩じれ疲労として出力するようになっ
ている。
Further, a recorder 11 is connected to the torque meter 3, and the detected torque change is outputted as torsional fatigue.

上記サーボモータ2はヘース1上に固定されているが、
トルクメータ3の方は左右一対のレール4.4上にベア
リングを介して支持され、矢印E方向に移動自在になっ
ている。すなわち、この移動自在の機構は、第2図およ
び第3図A。
The servo motor 2 is fixed on the heath 1,
The torque meter 3 is supported on a pair of left and right rails 4.4 via bearings, and is movable in the direction of arrow E. That is, this movable mechanism is shown in FIGS. 2 and 3A.

Bに示すように、トルクメータ3の下面に左右一対のス
ライダ12.12が固定され、このスライダ12.12
とレール4,4との間にそれぞれスラストベアリング1
3.13が介在し、摩擦抵抗を著しく小さくするように
なっている。
As shown in B, a pair of left and right sliders 12.12 is fixed to the bottom surface of the torque meter 3.
A thrust bearing 1 is installed between the rails 4 and 4, respectively.
3.13 is interposed to significantly reduce frictional resistance.

このような移動自在の機構は、前述したようにトルクメ
ータ3側に設けないで、サーボモータ2側に設けるよう
にしてもよい。また、移動自在の機構にはスラストベア
リングを設けて摩擦抵抗を小さくすることが好ましいが
、このスラストベアリングに代えてスプライン嵌合にし
てもよい。
Such a movable mechanism may not be provided on the torque meter 3 side as described above, but may be provided on the servo motor 2 side. Further, although it is preferable to provide a thrust bearing in the movable mechanism to reduce frictional resistance, a spline fitting may be used instead of the thrust bearing.

5.6はサンプルであるチューブ状複合材Sの両端を着
脱自在に固定するための把持部である。このうち、把持
部5は上記サーボモータ2に連結され、把持部6はトル
クメータ3に連結されている。また、把持部6にはパル
プ9を介してコンブL/、す8が接続され、チューブ状
複合材Sの中に圧縮空気を供給するようになっている。
Reference numeral 5.6 denotes gripping parts for removably fixing both ends of the tubular composite material S, which is a sample. Of these, the grip portion 5 is connected to the servo motor 2, and the grip portion 6 is connected to the torque meter 3. Further, a kelp L/, 8 is connected to the gripping portion 6 via a pulp 9, and is configured to supply compressed air into the tubular composite material S.

10は圧力計である。もちろん、上記コンプレッサ8の
接続は把持部5の方に行ってもよい。
10 is a pressure gauge. Of course, the compressor 8 may be connected to the grip portion 5.

上記把持部5.6は、前述したようにそれぞれテーパ型
締付はチャックから構成されていることが好ましい。第
4図は把持部6の方を代表して図示したもので、このテ
ーパ型締付はチャックは、環状テーパ面15aを有する
オス型15と環状テーパ面16aを有するメス型16と
を互いに嵌合し、周方向に配置した複数本のボルト17
.・−117により締め付けるようにしたものである。
Preferably, each of the gripping parts 5.6 comprises a tapered chuck, as described above. FIG. 4 shows the holding part 6 as a representative, and this tapered mold tightening is performed by fitting a male mold 15 having an annular tapered surface 15a and a female mold 16 having an annular tapered surface 16a into each other. A plurality of bolts 17 arranged together and circumferentially
..・It is designed to be tightened by -117.

この締め付けのとき、環状テーパ面15a、16aの間
にチューブ状複合材Sの端部が内外面から挟持されて固
定されるようになっている。オス型15に設けたエア通
路18は、ニアコンプレッサ8に接続させるためのもの
である。
During this tightening, the ends of the tubular composite material S are clamped and fixed from the inner and outer surfaces between the annular tapered surfaces 15a and 16a. The air passage 18 provided in the male mold 15 is for connecting to the near compressor 8.

上述した涙り疲労試験装置により、チューブ状複合材S
の槻り疲労を測定するときは、そのチューブ状複合材S
の両端を把持部5,6に把持し、コンプレッサ8により
200〜300KPaの内圧を加えつつ、サーボモータ
2によって振動数1〜4Hz、振幅π/2〜π/3ra
dの範囲の捩り荷重を繰り返し負荷するようにする。
Using the tear fatigue test device described above, the tubular composite material S
When measuring the crushing fatigue of the tubular composite material S
is held at both ends by the gripping parts 5 and 6, and while an internal pressure of 200 to 300 KPa is applied by the compressor 8, the servo motor 2 is used to generate vibrations at a frequency of 1 to 4 Hz and an amplitude of π/2 to π/3 ra.
A torsional load within the range of d is applied repeatedly.

そして、捩り荷重が負荷されるとき、チューブ状複合材
Sは径方向と軸方向とに収縮し、解除されると元の状態
に伸びる変化を繰り返す。しかし、本発明の試験装置で
は、上記サンプルの伸縮変化に対応して、径方向の収縮
にはコンプレッサからの内圧によって潰れを生じないよ
うに略一定の径に維持し、また軸方向の収縮には把持部
6が把持部5側に移動することにより、引張応力を発生
しないようにする。したがって、トルクメータ3には純
粋な涙り疲労だけが検出されることになる。
Then, when a torsional load is applied, the tubular composite material S contracts in the radial direction and axial direction, and when the torsional load is released, it repeats a change in which it stretches back to its original state. However, in the testing device of the present invention, in response to the changes in the expansion and contraction of the sample, the diameter is maintained at a substantially constant value for radial contraction so as not to collapse due to the internal pressure from the compressor, and the diameter for axial contraction is maintained at a substantially constant value. By moving the gripping part 6 toward the gripping part 5 side, tensile stress is prevented from being generated. Therefore, the torque meter 3 detects only pure tear fatigue.

また、上記実施例の把持部5.6はテーパ型締付はチャ
ックであるので、チューブ状複合材Sをすべりのないよ
うに確実に固定することができ、それによってチューブ
状複合材Sに正確な捩り角度を加えることができる。
In addition, since the gripping portion 5.6 of the above embodiment is a tapered type clamping chuck, it is possible to securely fix the tubular composite material S without slipping, thereby accurately fixing the tubular composite material S. It is possible to add a twist angle.

〔発明の効果〕〔Effect of the invention〕

上述したように、本発明の捩り疲労試験装置は、チュー
ブ状複合材の両端を把持する両把持部のいずれか一方を
、そのチューブ状複合材の軸方向に移動自在にしたので
、サンプルに対し捩り以外の負荷を作用させることがな
(、純粋な捩り疲労のみを検出することができる。
As described above, in the torsional fatigue testing device of the present invention, one of the gripping parts that grip both ends of the tubular composite material is made movable in the axial direction of the tubular composite material, so that No load other than torsion is applied (only pure torsional fatigue can be detected).

また、実施例のように、把持部をテーパ型締付はチャッ
クにすれば、サンプルに正確な捩り角度を加えることが
でき、より一層正確な捩り疲労の測定を可能にする。
Furthermore, if the gripping part is a tapered chuck as in the embodiment, it is possible to apply an accurate torsion angle to the sample, making it possible to measure torsional fatigue even more accurately.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本発明による捩り疲労試験装置の概略図、第2
図は第1図の■矢視図、第3図A。 Bはそれぞれ移動機構の詳細を−示す縦断面図および正
面図、第4図は把持部の縦断面図、第5図はサンプルの
チューブ状複合材を一部破断して示す斜視図である。 2・・・サーボモータ(往復回転駆動部)、3・・・ト
ルクメータ(捩り疲労検出部)、4・・・レール、5.
6・・・把持部、8・・・ニアコンプレッサ、12・・
・スライダ、13・・・スラストベアリング。
Fig. 1 is a schematic diagram of the torsional fatigue testing apparatus according to the present invention;
The figure is a view from the ■ arrow in Figure 1, and Figure 3 A. B is a vertical cross-sectional view and a front view showing details of the moving mechanism, FIG. 4 is a vertical cross-sectional view of the gripping part, and FIG. 5 is a partially cutaway perspective view of the sample tubular composite material. 2... Servo motor (reciprocating rotation drive unit), 3... Torque meter (torsional fatigue detection unit), 4... Rail, 5.
6... Gripping part, 8... Near compressor, 12...
・Slider, 13...Thrust bearing.

Claims (8)

【特許請求の範囲】[Claims] (1)測定サンプルのチューブ状複合材両端を把持する
把持部とそのチューブ状複合材に内圧を加える加圧部と
を設け、前記両把持部の一方を往復回転駆動部に連結す
るとともに、他方を捩り疲労検出部に連結し、かつ両把
持部のいずれか一方を前記チューブ状複合材の軸方向に
移動自在にしたことを特徴とする複合材の捩り疲労試験
装置。
(1) A gripping section that grips both ends of the tubular composite material of the measurement sample and a pressurizing section that applies internal pressure to the tubular composite material are provided, one of the gripping sections is connected to a reciprocating rotation drive section, and the other A torsional fatigue testing device for a composite material, characterized in that the gripping portion is connected to a torsional fatigue detection portion, and either one of the gripping portions is movable in the axial direction of the tubular composite material.
(2)移動自在の把持部が捩り疲労検出部側である特許
請求の範囲第1項記載の複合材の捩り疲労試験装置。
(2) The torsional fatigue testing device for composite materials according to claim 1, wherein the movable gripping section is on the side of the torsional fatigue detection section.
(3)移動自在側の把持部を連結する支持台がベアリン
グを介してレールに支持され、そのレール上を移動自在
にした特許請求の範囲第1項記載の複合材の捩り疲労試
験装置。
(3) The torsional fatigue testing device for composite materials according to claim 1, wherein the support base connecting the movable gripping portion is supported by a rail via a bearing, and is movable on the rail.
(4)往復回転駆動部による往復捩り荷重が振動数1〜
4Hz、振幅π/2〜π/3radの範囲である特許請
求の範囲第1項記載の複合材の捩り疲労試験装置。
(4) The reciprocating torsional load due to the reciprocating rotation drive unit has a frequency of 1 to
4 Hz and an amplitude in the range of π/2 to π/3 rad. The torsional fatigue testing device for composite materials according to claim 1.
(5)往復回転駆動部がサーボモータである特許請求の
範囲第1項記載の複合材の捩り疲労試験装置。
(5) The torsional fatigue testing device for composite materials according to claim 1, wherein the reciprocating rotation drive unit is a servo motor.
(6)捩り疲労検出部がトルクメータである特許請求の
範囲第1項記載の複合材の捩り疲労試験装置。
(6) The torsional fatigue testing device for composite materials according to claim 1, wherein the torsional fatigue detection section is a torque meter.
(7)チューブ状複合材に加える内圧が200〜300
KPaである特許請求の範囲第1項記載の複合材の捩り
疲労試験装置。
(7) The internal pressure applied to the tubular composite material is 200 to 300
The torsional fatigue testing device for composite materials according to claim 1, wherein the test device is KPa.
(8)把持部がテーパ型締付けチャックである特許請求
の範囲第1項記載の複合材の捩り疲労試験装置。
(8) The torsional fatigue testing device for composite materials according to claim 1, wherein the gripping portion is a tapered clamping chuck.
JP4154687A 1987-02-26 1987-02-26 Torsion fatigue test equipment for composite materials Expired - Fee Related JPH0785049B2 (en)

Priority Applications (1)

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JP4154687A JPH0785049B2 (en) 1987-02-26 1987-02-26 Torsion fatigue test equipment for composite materials

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Application Number Priority Date Filing Date Title
JP4154687A JPH0785049B2 (en) 1987-02-26 1987-02-26 Torsion fatigue test equipment for composite materials

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JPS63210640A true JPS63210640A (en) 1988-09-01
JPH0785049B2 JPH0785049B2 (en) 1995-09-13

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104132854A (en) * 2014-07-28 2014-11-05 河海大学 Member pure-torsion experimental device and member pure-torsion experimental method
CN104990805A (en) * 2015-06-26 2015-10-21 上海交通大学 Portable tester for static indentation damage prefabricating of large-scaled composite material structure
CN109668797A (en) * 2018-03-12 2019-04-23 西南交通大学 A kind of reverse micro move fatigue experimental device and test method based on synchrotron radiation

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104132854A (en) * 2014-07-28 2014-11-05 河海大学 Member pure-torsion experimental device and member pure-torsion experimental method
CN104990805A (en) * 2015-06-26 2015-10-21 上海交通大学 Portable tester for static indentation damage prefabricating of large-scaled composite material structure
CN104990805B (en) * 2015-06-26 2017-12-29 上海交通大学 A kind of prefabricated portable testing machine of large-scale composite material Structural Static Indentation Damage
CN109668797A (en) * 2018-03-12 2019-04-23 西南交通大学 A kind of reverse micro move fatigue experimental device and test method based on synchrotron radiation
CN109668797B (en) * 2018-03-12 2023-09-22 西南交通大学 Torsional fretting fatigue test device and method based on synchronous radiation

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