JPS5960242A - Plastic strain control apparatus - Google Patents

Plastic strain control apparatus

Info

Publication number
JPS5960242A
JPS5960242A JP17014682A JP17014682A JPS5960242A JP S5960242 A JPS5960242 A JP S5960242A JP 17014682 A JP17014682 A JP 17014682A JP 17014682 A JP17014682 A JP 17014682A JP S5960242 A JPS5960242 A JP S5960242A
Authority
JP
Japan
Prior art keywords
strain
waveform
plastic
load
stress
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
JP17014682A
Other languages
Japanese (ja)
Other versions
JPH0221740B2 (en
Inventor
Hironari Mita
裕也 三田
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.)
Shimadzu Corp
Shimazu Seisakusho KK
Original Assignee
Shimadzu Corp
Shimazu Seisakusho KK
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 Shimadzu Corp, Shimazu Seisakusho KK filed Critical Shimadzu Corp
Priority to JP17014682A priority Critical patent/JPS5960242A/en
Publication of JPS5960242A publication Critical patent/JPS5960242A/en
Publication of JPH0221740B2 publication Critical patent/JPH0221740B2/ja
Granted legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N3/00Investigating strength properties of solid materials by application of mechanical stress
    • G01N3/08Investigating strength properties of solid materials by application of mechanical stress by applying steady tensile or compressive forces

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  • Physics & Mathematics (AREA)
  • Health & Medical Sciences (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Chemical & Material Sciences (AREA)
  • Analytical Chemistry (AREA)
  • Biochemistry (AREA)
  • General Health & Medical Sciences (AREA)
  • General Physics & Mathematics (AREA)
  • Immunology (AREA)
  • Pathology (AREA)
  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【発明の詳細な説明】 この発明は、利率1の引張・圧#ii試験にふ−いて1
核(4組の塑性歪j11を制倒lする装着に関する。
Detailed Description of the Invention This invention is based on the tension/pressure #ii test with an interest rate of 1.
Nucleus (related to mounting to suppress the four sets of plastic strains j11).

、−+]■に、A’A’ i’lは引張・圧縮荷重が加
えられることにより歪みがにトじる。この場合、 4A
’;rJlを塑性度?/させたときの歪みには、弾性歪
と塑性歪とが含まれる。ところで、gl性歪みに依存し
た利′A′、−1の特性を調べるには、弾性歪速度が例
えば一定になるJ:うにAA相に引Ill;、・即席1
荷屯を加える場合がある。
, -+] ■, A'A'i'l becomes distorted when tensile and compressive loads are applied. In this case, 4A
'; rJl is the degree of plasticity? / The strain when it is made includes elastic strain and plastic strain. By the way, in order to investigate the characteristics of the profit 'A', -1 that depends on the glastic strain, the elastic strain rate is constant, for example, J: sea urchin is drawn into the AA phase Ill;,・immediate 1
Cargo tonnage may be added.

ところが、利料に荷重を加えると塑性歪のみならず弾性
歪も変化するので、単に荷重を加えただけでb;L塑伐
・11″ミを一定の速度で変化さ萌ることがCきない。
However, when a load is applied to the interest rate, not only the plastic strain but also the elastic strain changes, so simply adding a load causes the B; do not have.

このため、4)J料に加える荷重の大きさを制i卸する
8叔があるが、この制餠を止4ijiに行って塑+’+
 rr〕速度を−・定にすることはヤング率が利、I:
1の物理的性′αに1.トミして刻々と変化J−るので
非常にM7f+シい。
For this reason, there are 4) 8 points to control the magnitude of the load applied to the J material, but this control is stopped at 4 iji and the plastic +'+
rr] Making the velocity constant is Young's modulus, I:
1 for the physical property 'α of 1. It is very M7f+ because it changes every moment.

この発明ば、士、述に鑑み、ヤング率が一1記のように
変化しても塑性歪速度がI91定値になるようにA′A
”ADlに加える荷重の大きさを1確にかつ容易に制g
4+できるようにすることを1」的とする。
In this invention, in view of the above, A′A
``The size of the load applied to the ADl can be precisely and easily controlled.
The goal is to be able to do 4+.

この発明は、上記目的をJ3U成するために、彎約して
言えば利料に引張・圧路j荷・1i′を加えている間に
利料の歪はと応力とから見掛けのヤング率(コンプライ
アンス)を求め、このヤング率に基づいて弾性矛を計”
j:’ L、所望する塑性歪とこの弾性歪とから全歪波
形を決定し、この全歪波形に対応して利料(1て荷重を
加えることにより、塑性歪量を制御するようにtIjI
ff成されている。
In order to achieve the above object, the present invention has been developed to calculate the apparent Young's modulus from the strain and stress while adding tension, pressure path load, and 1i' to the interest. (compliance) and calculate the elastic rod based on this Young's modulus.”
j:'L, determine the total strain waveform from the desired plastic strain and this elastic strain, and apply a load (tIjI) corresponding to this total strain waveform to control the amount of plastic strain.
ff has been created.

以下、この発明の構成を実施例について図面に基づき具
体的に説明する。
EMBODIMENT OF THE INVENTION Hereinafter, the structure of this invention will be specifically explained about an Example based on drawing.

第1図はこの発明の実施例のブロック回路図である。応
力測定手段(1)は利料(試験片)が第2図の応力−歪
線図に示すように弾性領域(ト)を1匹え更に塑性領域
(ト)における最大引張応力σmaxに全る壕での引張
荷重を受け:lk後、除荷重されて静荷重領域0にある
ときに、この静荷重領域C)における桐斜の応力Δσを
6(11定する。歪測定手段り2)ケよこの静荷重領域
0における4シ泊1の歪み△εを測定する。見掛けのヤ
ング率の計算手段(3)は、応力測定手段(1)からの
応力測定信号と、歪測定手段(2)からの歪測定信号と
により見用けのヤング率E(−J−σ/Δε)を計算し
、その計:i;tl’、結果をヤング率計算信号として
弾性歪計算手段(4)に送出する。ここで、第1図の応
力−歪線図において、静荷重領域(Qをあられす線は弾
性領域囚をあられす線と勾配が同じである。しだがって
、静荷重領域0をあられす線と横軸の歪をあられす線と
の交点位置については、前記最大引張応力輻axの値と
、前記見掛けのヤング率E、つ1す、除荷重1」」1域
0をあられす線の勾P記の値とにより決定することがで
きる。しだがって、前記交点位1市の歪値と、最大引張
応力C1maxでの横軸上の歪値とから弾性歪ε、を計
算することができる。
FIG. 1 is a block circuit diagram of an embodiment of the invention. Stress measuring means (1) is based on the test piece (test piece) having one elastic region (G) and a plastic region (G) with the maximum tensile stress σmax as shown in the stress-strain diagram in Figure 2. After receiving a tensile load in the trench, when the load is removed and it is in the static load region 0, the stress Δσ of the paulownia slope in this static load region C) is determined to be 6 (11). The strain △ε of 4 sheets and 1 in the horizontal static load area 0 is measured. The apparent Young's modulus calculation means (3) calculates the apparent Young's modulus E(-J-σ /Δε), the sum: i; tl', and the result is sent to the elastic strain calculation means (4) as a Young's modulus calculation signal. Here, in the stress-strain diagram in Figure 1, the line representing the static load region (Q) has the same slope as the line representing the elastic region. Regarding the intersection position of the line and the strain line on the horizontal axis, the value of the maximum tensile stress radiation ax and the line that expresses the apparent Young's modulus E, Therefore, the elastic strain ε is calculated from the strain value at the intersection point 1 and the strain value on the horizontal axis at the maximum tensile stress C1max. be able to.

弾性歪計算手段(4)は、この計鈷に従って、最大引張
応力測定手段(5)からの最大引張応力I7maxにつ
いての信号と、児掛けのヤング率についての計算信号と
から弾性歪ε1を計算するようになっている。
According to this calculation, the elastic strain calculation means (4) calculates the elastic strain ε1 from the signal about the maximum tensile stress I7max from the maximum tensile stress measurement means (5) and the calculation signal about the Young's modulus of the child support. It looks like this.

一方、この実施例では、第3図の塑性歪一時間線[羽に
示すように拐訓に与える塑性歪としては三角波のように
歪速度が一定の塑性歪を与えるようにしている。このた
め、塑性歪波形出力手段(6)は、第3図に示す波形の
信号を全歪波形決定手段(7)に送出する。全歪波形決
定手段(7)は、全歪二弾性歪+塑性歪であることから
、弾性歪計算手段(4)からの弾性歪信号と、塑性歪波
形出力手段(6)からの塑性歪波形ja−号とにより、
第4図の全歪一時間線図の実線に示すような波形を決定
してこれを全歪信号として試1倹片歪制1311手段(
8)に送出する。
On the other hand, in this embodiment, as shown in the plastic strain one-time line of FIG. Therefore, the plastic strain waveform output means (6) sends a signal having the waveform shown in FIG. 3 to the total strain waveform determination means (7). Since the total strain waveform determining means (7) is a total strain of two elastic strain + plastic strain, the elastic strain signal from the elastic strain calculation means (4) and the plastic strain waveform from the plastic strain waveform output means (6) By the ja- issue,
A waveform as shown in the solid line in the total distortion one-time diagram in FIG.
8).

試験片歪制可1手段(8)は、入力されてきた全歪信号
に基づいて試験片としての利判に荷重を加える。
The test piece strain control means 1 (8) applies a load to the test piece based on the input total strain signal.

従って、利、41には第4図の波形(実線)に従って変
化する引張・圧希1荷重が加えられることになシ、との
引張・圧縮荷重による利料の全歪において塑1生歪は第
3図の実線、第4図の破線に示すような波形変化に対応
して変化制菌さぜられる。
Therefore, a tensile/compression 1 load that changes according to the waveform (solid line) in Figure 4 is applied to 41, and the plastic 1 raw strain is Sterilization changes occur in response to waveform changes as shown by the solid line in FIG. 3 and the broken line in FIG. 4.

第5図は第1図を(マイクロ)コンピュータに適用した
場合の構成図であシ、第6図はその動作;況明のだめの
プログラムフロー1ヤ−1・である。
FIG. 5 is a block diagram when FIG. 1 is applied to a (micro)computer, and FIG. 6 is its operation; a program flow 1-1 of the situation.

第5図において、試験機(10には応力測定手段として
のロー ドセルと、歪測定手段としての:rTi ;t
lチill罰と、試験片荷重制御手段の一部としてのサ
ーボパルプブとが含′止れる。制御装f1t(II)は
ロードセルや歪計測)1gからの応力や歪に関する信号
を増幅するための増幅器や、サーボパルプに対1〜て荷
重制御信号を加える制御ユニットを備えている。側部1
装置(11)の増幅器からの出力信号はインターフェー
ス回路(121を介して見掛けのヤング率計算手段(3
)等としテ(7)マイクロコンピュータ(13)に入力
される一力、マイクロコンピュータ(13)からの制御
指定信号はインターフェース回路(12)を介して制御
装置(11)に加えられるとともに、この制御装置(I
f)の制御ユニットから試験機00のサーボパルプに送
られる。このような構成の動作を第6図に従って説明す
る。先ず、マイクロコンピュータ(13)により弾性歪
測定周期であるか否かが判断される〔ステップ(n工)
〕。弾性歪測定周期でない(No)ときは、塑性歪制御
で〔ステップ(n+、)]、逆(YES)のときは全歪
制御で〔ステップ(n3)〕、材料を引張・圧縮して試
験を行う。
In Fig. 5, a testing machine (10 includes a load cell as a stress measuring means and a strain measuring means as a
1 illumination and a servo pulp as part of the specimen load control means. The control device f1t (II) is equipped with an amplifier for amplifying signals related to stress and strain from the load cell and strain measurement) 1g, and a control unit that applies a load control signal to the servo pulp. Side part 1
The output signal from the amplifier of the device (11) is passed through the interface circuit (121) to the apparent Young's modulus calculation means (3).
), etc. (7) A control designation signal from the microcomputer (13) is applied to the control device (11) via the interface circuit (12), and this control Equipment (I
f) is sent from the control unit to the servo pulp of testing machine 00. The operation of such a configuration will be explained with reference to FIG. First, the microcomputer (13) determines whether or not it is the elastic strain measurement cycle [step (n)].
]. If it is not the elastic strain measurement period (No), perform the test with plastic strain control [step (n+, )], and if the opposite (YES), perform the test with total strain control [step (n3)], by tensioning and compressing the material. conduct.

全歪制御のときは静荷重領域における見掛けのヤング率
(コンプライアンス)からすlP性歪を*l’ 4’l
’−する〔ステップ(+14))。この計算は試験機0
0のロードセルと、歪計測器とから応力と歪みとに関す
る信号を制御装置(11)、インターフェース(1りを
介して取り込んだマイクロコンピュータ(13)によシ
行われる。
When controlling the total strain, the apparent Young's modulus (compliance) in the static load region is calculated from the lP strain *l'4'l
'-Do (step (+14)). This calculation is for test machine 0
This is carried out by a microcomputer (13) which receives signals regarding stress and strain from a load cell and a strain measuring device via a control device (11) and an interface (1).

この計[(1:の後、塑性歪を第3図に示すような波形
で変化さぜるための全歪の出力波形〔第4図の実線〕の
決、ノrに関する計算もマイクロコンピュータ(1:→
により11われる〔ステップ(n5)工こうして」二;
己訓”!’:’に閂ず乙イ1、ジノ)・マイクロコンピ
ュータ(l:l) カラ。
After this calculation, the output waveform of the total strain [solid line in Fig. 4] for changing the plastic strain in the waveform shown in Fig. 3 is calculated using a microcomputer. 1:→
11 [step (n5) thus"2;
Self-discipline"!':'Nibaruzuotii 1, Jino)・Microcomputer (l:l) Kara.

インターフェイス(12)、制御装置(+++の制御ユ
ニットを介して、試」険1ハ=のザーボバルプに与えら
れる。
The interface (12) is applied to the servo valve of the test system via the control unit of the control device (+++).

ザーボバルプは、第4図の実線に示す波形便化に応答し
て月利に荷重を加える。このようにして、月1,1にお
けるI)、V2性歪は第3図のように一定の速度で変化
することになる。
The servo valve applies a load to the monthly interest rate in response to the waveform adjustment shown by the solid line in FIG. In this way, the I) and V2 distortions in Months 1 and 1 will change at a constant speed as shown in FIG.

なお、上述の実施例においては引張荷重についてjjs
a明したが、圧縮荷重と利用に加える場合にも同(、]
2に適用できる。また、上述の実施例において試、験機
の性能の点から、第3図のような塑性歪制御計を行うこ
とができない場合には、・塑性歪のビータイ117ε捷
たば一ε1.のみを全歪で制i卸してもよい。
In addition, in the above-mentioned embodiment, the tensile load is jjs
As explained above, the same applies when applying compressive load and usage.
Applicable to 2. In addition, in the above-described embodiment, if it is not possible to perform a plastic strain control meter as shown in FIG. 3 due to the performance of the testing machine, the following may be used: It is also possible to control only the total distortion.

以−1のように、この発明によれば、塑性領域に至るま
で拐制に引1〕ト2・圧縮荷重を加えて後の静荷重領域
に2ける拐渭1の歪みと厖力とから見]1[けのヤング
率を求め、このヤング率に基づいて弾性歪を計′見し、
この計算値から例えば一定速度で塑性歪が変化する尤う
に全歪波形を決定し、これに対応して利用に荷重を加え
るようにしたので、所望する!II/l性J3が1Fj
られろように利71′lに11゛確にかつ容易に荷11
文を加えることができ、例えばA−Aれ1の残留応力粋
よび異方性が疲労に及ぼす影響の)(ラメータとして塑
性歪に限定する場合に、この塑性歪の制御を容易に行う
ことができる。
As described above-1, according to the present invention, the distortion and displacement force of the suspension 1 in the static load region after applying a compressive load 1) to the plastic region are ] 1 [Find the Young's modulus of the equation, calculate the elastic strain based on this Young's modulus,
From this calculated value, for example, the total strain waveform in which the plastic strain changes at a constant speed is determined, and a load is applied accordingly, so that the desired result can be obtained! II/l sex J3 is 1Fj
Load 11 accurately and easily so that the load 71'l is
For example, when limiting the parameter to plastic strain, it is easy to control this plastic strain. can.

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

第1図はこの発明の実施例のブロック構成図、第2図は
応力−歪線図、第3図は塑性歪一時間線図、第4図は全
歪一時間線図、第5図は上記実施例もマイクロコンピュ
ータに適用した場合のブロック構成図、第6図はその動
作説明に供するプログラムフローチャー1−である。 (1)・・・応力測定手段、(2)・・・歪測定手段、
(3)・・見掛けのヤング率計算手段、(4)・・・弾
性歪計11ニ手段、(5)・・・最大引張・圧縮応力測
定手段、(6)・・・塑性歪波形出力手段、(7)・・
全歪波形決定手段、(8)・・・試験片歪制御手段 出に11人  株式会社  島津製作所代理人 力゛埋
士 岡田和秀 20
Fig. 1 is a block diagram of an embodiment of the present invention, Fig. 2 is a stress-strain diagram, Fig. 3 is a plastic strain versus time diagram, Fig. 4 is a total strain versus time diagram, and Fig. 5 is a time diagram of total strain. FIG. 6 is a block configuration diagram when the above embodiment is also applied to a microcomputer, and FIG. 6 is a program flowchart 1- for explaining its operation. (1)... Stress measuring means, (2)... Strain measuring means,
(3) Apparent Young's modulus calculation means, (4) Elastic strain meter 11 means, (5) Maximum tensile/compressive stress measurement means, (6) Plastic strain waveform output means , (7)...
Total strain waveform determining means, (8)... 11 people involved in test piece strain control means Shimadzu Corporation Representative Kazuhide Okada 20

Claims (1)

【特許請求の範囲】[Claims] (1)塑・171領域に′1・る」でH料に引張・圧縮
荷重を加えて後のI:仝荷重領域における利材の歪みと
応力とをそれぞれ測定する応力測定手段と歪測定手段と
、1)il +ib両丁段からの各測定イハシじにより
lJl川けの一\・ンク率を1;1坤するヤング早計[
(11手段と、ヤング・t、;;+l↓:1丁段からの
へ・ング率J1埠倍号に基づいて弾性□r′:、を計〕
ンする弾性歪ii’l’ :G?:手段と、予め設定さ
れた塑性歪波形に刈応する信号を出J)する塑性歪波1
[a出力手段と、伸性歪計算手段と塑性歪波形出、/J
丁段と7からの出力により一令歪波形をぜ定しこの全4
f波形にkl応する13号を出力する全歪波形出力手段
とからなるI)ν1性歪制御装;110
(1) A stress measuring means and a strain measuring means for measuring the strain and stress of the material in the I: after applying a tensile/compressive load to the H material in the plastic 171 region in the '1.ru' region and the strain measuring means, respectively. And, 1) Young's quick estimate of 1; 1 kon by each measurement from il + ib both sides.
(Calculate the elasticity □r': based on 11 means and Young's t, ;;+l↓: 1-stage Heng modulus J1 bu number)]
Elastic strain ii'l' :G? : means and a plastic strain wave 1 that outputs a signal responsive to a preset plastic strain waveform.
[a Output means, elastic strain calculation means, and plastic strain waveform output, /J
The first order distortion waveform is determined by the output from Ding stage and 7.
I) ν1 distortion control device consisting of a total distortion waveform output means that outputs No. 13 corresponding to kl to the f waveform; 110
JP17014682A 1982-09-29 1982-09-29 Plastic strain control apparatus Granted JPS5960242A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP17014682A JPS5960242A (en) 1982-09-29 1982-09-29 Plastic strain control apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP17014682A JPS5960242A (en) 1982-09-29 1982-09-29 Plastic strain control apparatus

Publications (2)

Publication Number Publication Date
JPS5960242A true JPS5960242A (en) 1984-04-06
JPH0221740B2 JPH0221740B2 (en) 1990-05-16

Family

ID=15899520

Family Applications (1)

Application Number Title Priority Date Filing Date
JP17014682A Granted JPS5960242A (en) 1982-09-29 1982-09-29 Plastic strain control apparatus

Country Status (1)

Country Link
JP (1) JPS5960242A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS617442A (en) * 1984-06-21 1986-01-14 Saginomiya Seisakusho Inc Plastic strain controlling apparatus

Cited By (1)

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Publication number Priority date Publication date Assignee Title
JPS617442A (en) * 1984-06-21 1986-01-14 Saginomiya Seisakusho Inc Plastic strain controlling apparatus

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JPH0221740B2 (en) 1990-05-16

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