JP5521161B2 - A phase transformation behavior measurement method considering the accommodation behavior of polycrystalline shape memory alloys. - Google Patents
A phase transformation behavior measurement method considering the accommodation behavior of polycrystalline shape memory alloys. Download PDFInfo
- Publication number
- JP5521161B2 JP5521161B2 JP2010243841A JP2010243841A JP5521161B2 JP 5521161 B2 JP5521161 B2 JP 5521161B2 JP 2010243841 A JP2010243841 A JP 2010243841A JP 2010243841 A JP2010243841 A JP 2010243841A JP 5521161 B2 JP5521161 B2 JP 5521161B2
- Authority
- JP
- Japan
- Prior art keywords
- transformation
- strain
- stress
- behavior
- shape memory
- 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.)
- Active
Links
- 230000009466 transformation Effects 0.000 title claims description 98
- 230000006399 behavior Effects 0.000 title claims description 28
- 229910001285 shape-memory alloy Inorganic materials 0.000 title claims description 20
- 230000004308 accommodation Effects 0.000 title claims description 15
- 238000000691 measurement method Methods 0.000 title claims description 5
- 239000013078 crystal Substances 0.000 claims description 28
- 239000000463 material Substances 0.000 claims description 18
- 238000000354 decomposition reaction Methods 0.000 claims description 6
- 238000012935 Averaging Methods 0.000 claims description 2
- 238000000034 method Methods 0.000 description 8
- 230000007246 mechanism Effects 0.000 description 7
- 229910000734 martensite Inorganic materials 0.000 description 5
- 230000008569 process Effects 0.000 description 5
- 229910001566 austenite Inorganic materials 0.000 description 4
- 238000010586 diagram Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000004044 response Effects 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000005489 elastic deformation Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000006870 function Effects 0.000 description 1
- 230000008707 rearrangement Effects 0.000 description 1
- 229920006395 saturated elastomer Polymers 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000001131 transforming effect Effects 0.000 description 1
Landscapes
- Investigating And Analyzing Materials By Characteristic Methods (AREA)
- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
Description
本発明は,多結晶形状記憶合金のアコモデーション挙動を考慮した相変態挙動測定方法に関するものである. The present invention relates to a method for measuring a phase transformation behavior in consideration of the accommodation behavior of a polycrystalline shape memory alloy.
形状記憶合金の相変態挙動を精密に予測するためには相変態挙動がアコモデーション機構のもとで生じることを正確に記述する必要がある.形状記憶合金の相変態を伴う応力・ひずみ挙動を予測する技術は下記のようにいくつか提案されているが,そのいずれもが相変態におけるアコモデーション挙動を正確に記述するものでなく,予測技術としては不完全なものである. In order to accurately predict the phase transformation behavior of shape memory alloys, it is necessary to accurately describe that the phase transformation behavior occurs under the accommodation mechanism. Several techniques have been proposed for predicting stress / strain behavior accompanying phase transformation of shape memory alloys, but none of them describe the accommodation behavior in phase transformation accurately. Is incomplete.
多結晶形状記憶合金は結晶方位の異なる単結晶合金の集合体であり,それぞれの結晶粒は24通りの変態方位をもっている.例えばある結晶のある変態方位において変態が生じたとすると,生じた変態ひずみによって,その変態方位の変態に抵抗するような内部応力が形成され,次の変態は別の結晶粒の別の方位において生じる.このようなメカニズムが次々と働き,変態過程における多結晶体中の内部応力を最小にする. Polycrystalline shape memory alloys are aggregates of single crystal alloys with different crystal orientations, and each crystal grain has 24 transformation orientations. For example, if a transformation occurs in one transformation orientation of a crystal, the transformation strain produced creates internal stress that resists transformation of that transformation orientation, and the next transformation occurs in another orientation of another crystal grain. . These mechanisms work one after another to minimize the internal stress in the polycrystal during the transformation process.
このメカニズムによる変態ひずみ生成過程をアコモデーションと呼び,アコモデーションを生じさせるメカニズムをアコモデーション機構と呼ぶ.本発明はこのメカニズムのもとで生じる変態ひずみの挙動,すなわち,変態ひずみのアコモデーション挙動を精密に計算することを可能にする技術に関するものである. The transformation strain generation process by this mechanism is called accommodation, and the mechanism that causes accommodation is called accommodation mechanism. The present invention relates to a technology that makes it possible to accurately calculate the behavior of transformation strain generated under this mechanism, that is, the accommodation behavior of transformation strain.
本発明の特徴とする技術条件は次の通りである。
多結晶形状記憶合金を結晶方位の異なる結晶粒の並列結合により示し,各結晶粒をさらに部分要素に分割し.部分要素の変態ひずみの平均を結晶粒の変態ひずみとし,これから結晶粒の弾性ひずみおよび応力を求めると共に各結晶粒の各変態面における分解せん断応力を求め、その値の大きい順に変態は生じるとして変態が起きるごとに応力分布の再分布を計算して最大の分解せん断応力を発生する部分要素を求め,最大せん断応力が変態条件を満足する時、変態ひずみを当該部分要素に与えると共に変態ひずみの値を更新し、更新した変態ひずみの値を用いて弾性ひずみを更新しこの弾性ひずみを用いてミクロ応力の値を更新し、このミクロ応力を座標変換してマクロ座標でのマクロ応力に変換し、この応力を部分要素を含む材料構造にわたって平均し,これをマクロ応力とすることを特徴とする多結晶形状記憶合金のアコモデーション挙動を考慮した相変態挙動測定方法.
The technical conditions characterized by the present invention are as follows.
A polycrystalline shape memory alloy is shown by parallel connection of grains with different crystal orientations, and each grain is further divided into sub-elements. The average transformation strain of the sub-elements is taken as the transformation strain of the crystal grains. From this, the elastic strain and stress of the grains are obtained, and the decomposition shear stress at each transformation surface of each grain is obtained. When the maximum shear stress satisfies the transformation condition, the transformation strain is given to the subelement and the value of the transformation strain is calculated. , Update the elastic strain using the updated transformation strain value, update the microstress value using this elastic strain, convert the microstress to the macrostress in the macro coordinate, Considering the accommodation behavior of polycrystalline shape memory alloy, which is characterized by averaging this stress over the material structure including the subelements and making this a macro stress Phase transformation behavior measurement methods.
外部ひずみ増分を与え,各結晶粒の応力を計算し,変態条件を満足する場合変態ひずみを計算し,変態ひずみの発生による応力の再分布を計算する.各結晶粒の応力の平均を微視材料全体の応力とする.こうすることにより変態を考慮した形状記憶合金の応力・ひずみ関係が求められる.また,温度増分を与え,それに伴う変態ひずみを計算することにより,温度変化の影響を考慮した応力・ひずみ関係が求められる. Given the external strain increment, calculate the stress of each grain, calculate the transformation strain if the transformation condition is satisfied, and calculate the stress redistribution due to the occurrence of transformation strain. The average stress of each crystal grain is the stress of the entire microscopic material. In this way, the stress / strain relationship of the shape memory alloy considering the transformation is obtained. In addition, the stress-strain relationship considering the effect of temperature change can be obtained by giving the temperature increment and calculating the accompanying transformation strain.
以下に本発明の実施するための形態を説明する。
材料の応力とひずみの関係を構成式という.この構成式を導くときに用いられる材料の物理的なモデルを構成式モデルという.物理的なモデルは,材料のすべての挙動を精密に表現するものではないが,要求される材料応答を妥当に表現でき,かつその応答を定式化する場合に必要な簡略化されたモデルである必要がある.また,この物理的なモデルとその帰結である構成式を合わせたものも構成式モデルと呼ばれる.この発明は,形状記憶合金の変態挙動に対して,そのアコモデーション挙動を考慮した構成式モデルを与えるものである.以下では構成式モデルのことを単にモデルと呼ぶ.
The form for implementing this invention is demonstrated below.
The relation between stress and strain of material is called constitutive equation. The physical model of the material used to derive this constitutive equation is called the constitutive equation model. The physical model is not a precise representation of all the behavior of the material, but is a simplified model that can reasonably represent the required material response and is necessary to formulate the response. There is a need. A combination of this physical model and the resulting constitutive equation is also called a constitutive equation model. This invention provides a constitutive model that takes into account the accommodation behavior of the transformation behavior of shape memory alloys. In the following, a constitutive model is simply called a model.
形状記憶合金の変態におけるアコモデーション挙動を記述するため,多結晶形状記憶合金を結晶方位の異なる結晶粒の集合体として表現する.それら集合体によって表現される材料の微視要素が巨視的材料中に埋め込まれるとする時,微視要素中のそれぞれの方位の結晶粒は周りの材料からの変位拘束により自由に変形できない.これを表現するため,それぞれの方位の結晶粒のひずみが,外部ひずみ(材料の微視要素に与えられるひずみ:結晶粒の集合体の外部から与えられるひずみ)と等しくなるモデルを考える.このモデルは,材料の微視要素を図1に模式的に示されるように方位の異なる結晶粒の並列結合で表していることになる.またこのモデルにおいては各結晶粒のひずみは外部ひずみに等しくなるので等ひずみモデルとも呼ばれる. In order to describe the accommodation behavior in the transformation of shape memory alloys, polycrystalline shape memory alloys are expressed as aggregates of grains with different crystal orientations. When the microscopic elements of the material expressed by these aggregates are embedded in the macroscopic material, the crystal grains in each orientation in the microscopic element cannot be freely deformed due to displacement constraints from surrounding materials. In order to express this, we consider a model in which the strain of crystal grains in each orientation is equal to the external strain (strain applied to the microscopic element of the material: strain applied from outside the aggregate of crystal grains). In this model, the microscopic elements of the material are represented by parallel coupling of grains with different orientations as schematically shown in Fig. 1. In this model, the strain of each grain is equal to the external strain, so it is also called an equistrained model.
このモデルにおいていずれかの結晶粒で変態が生じたとすると,その結晶粒においては変態ひずみが生じることにより,弾性ひずみが減少し,応力が減少することになる.したがって次の変態は,他の結晶粒で生じることになり,さらにすでに生じた変態ひずみの方向に対し,それを打ち消す方向の変態が生じることとなる.このようにして,変態ひずみのアコモデーション挙動が記述されることになる. If a transformation occurs in any of the grains in this model, the transformation strain occurs in that grain, resulting in a decrease in elastic strain and a decrease in stress. Therefore, the next transformation will occur in other grains, and a transformation in the direction that cancels the transformation strain that has already occurred will occur. In this way, the accommodation behavior of the transformation strain is described.
一つの結晶粒のひずみを考える場合,結晶粒全体に一時に変態ひずみが生じるとすると,変態固有ひずみは10%程度とかなり大きいので,変態ひずみ発生に伴う応力変動の程度が大きすぎて計算モデルが不安定になる.
図2に示すように,一つの結晶粒をさらに細分化して結晶粒と同じ結晶方位をもつN個の部分要素に分け,それぞれの部分要素に対して異なる変態限界応力を与えることにより,変態ひずみが部分要素ごとに起こるとすることができる.このとき,結晶粒の変態ひずみは,N個の部分要素の変態ひずみの平均であり,一つの部分要素の変態によって生じる変態固有ひずみの1/Nが,一回の変態により生じる結晶粒の変態ひずみとなる.Nに対して大きな値を与えることにより,結晶粒における一回あたり生じる変態ひずみを小さくすることができ,計算の不安定化を防ぐことができる.
When considering the strain of a single crystal grain, if the transformation strain is generated in the entire crystal grain at one time, the transformation inherent strain is as large as 10%. Becomes unstable.
As shown in Fig. 2, a single crystal grain is further subdivided into N sub-elements having the same crystal orientation as the crystal grains, and different transformation limit stresses are applied to each sub-element, thereby transforming the transformation strain. Can occur for each subelement. At this time, the transformation strain of the grain is the average of the transformation strains of the N subelements, and 1 / N of the transformation inherent strain caused by the transformation of one subelement is the transformation of the grain caused by one transformation. Strain. By giving a large value to N, the transformation strain that occurs in each crystal grain can be reduced, and instability of the calculation can be prevented.
結晶粒の変態ひずみはこれら部分要素の変態ひずみの平均となる.結晶粒の弾性ひずみは外部ひずみの値からこの平均変態ひずみを差し引くことによって求められ,これから結晶粒の応力が計算できる. The transformation strain of the grains is the average of the transformation strains of these subelements. The elastic strain of a crystal grain is obtained by subtracting this average transformation strain from the value of the external strain, and from this, the stress of the crystal grain can be calculated.
部分要素の応力は,このように求められた結晶粒の応力に等しいとする.すなわち,結晶粒内では部分要素は直列結合で表される.これを図2に示す. The stress of the subelement is assumed to be equal to the stress of the crystal grain thus obtained. In other words, the subelements are represented by series connection within the crystal grains. This is shown in Fig.2.
1個の結晶粒には24通りの変態の方向が存在するので,上記のようにして求められた応力から,それぞれの変態面上に働く分解せん断応力を計算し,その最大値が限界値を超過する場合,変態が生じるとする. Since one crystal grain has 24 transformation directions, the decomposition shear stress acting on each transformation plane is calculated from the stress obtained as described above, and the maximum value is the limit value. If it exceeds, the transformation will occur.
変態面上に働く垂直応力の作用も考慮することも可能である.変態駆動応力τDRは具体的にτDR=τ+ασで表される.
但し、τ:分解せん断応力, σ:変態面に働く垂直応力, α:材料定数
変態駆動応力の大小で変態ひずみの発生を評価する.
It is also possible to consider the effect of normal stress acting on the transformation surface. The transformation driving stress τ DR is specifically expressed by τ DR = τ + ασ.
However, τ is the decomposition shear stress, σ is the normal stress acting on the transformation surface, α is the material constant transformation driving stress, and the occurrence of transformation strain is evaluated.
変態の限界値は,それを越すと変態が起こる限界値と,すでに変態が起きてしまった要素において,それ以下になると変態が元に復する,すなわち,逆変態に対する限界値を設定することができる.また,その限界値を超すと変態の方向が変化する変態再配列の限界値を設定することができる. For the limit value of transformation, the limit value at which transformation will occur and the element that has already undergone transformation will be restored to its original value when it is less than that, that is, the limit value for reverse transformation may be set. it can. Moreover, the limit value of transformation rearrangement in which the transformation direction changes when the limit value is exceeded can be set.
上記限界値を温度の関数として設定することにより,機械的負荷のみならず温度変化に対する形状記憶合金の変態挙動を記述することができる. By setting the above limit values as a function of temperature, it is possible to describe not only the mechanical load but also the transformation behavior of shape memory alloys with respect to temperature changes.
微視材料要素の応力は各結晶粒の応力の平均となる. The stress of the microscopic material element is the average of the stress of each crystal grain.
上記の一連の計算は,材料座標,結晶粒座標(部分要素座標),変態面座標における物理量の座標変換に注意しながら進める.
計算手続きを図3に示す.すなわち,
ステップ1: ひずみεの微小増分dεをあたえる.この時ひずみはε+dεとなる.
ステップ2: 各結晶粒中の部分要素のひずみを求める.一定ひずみの仮定により,この値はε+dεに等しい.ただし,このひずみは材料のマクロ座標で定義されているので,座標変換により,部分要素のミクロ座標でのひずみに変換しておく.部分要素の変態ひずみを差し引いて弾性ひずみを求める.
ステップ3: 弾性ひずみに弾性係数を乗じて部分要素の応力(ミクロ応力)を求める.部分要素には24通りの変態システムがあるので,そのそれぞれに対して変態面の方位を考慮した分解せん断応力を求める.
ステップ4: 最大の分解せん断応力を発生する部分要素を求め,最大せん断応力が変態条件を満足する場合は,変態ひずみをこの部分要素に与え,変態ひずみの値を更新する.更新された変態ひずみの値を用い弾性ひずみを更新する.これを用いてミクロ応力の値を更新する.
ステップ5: 座標変換によりミクロ座標での応力をマクロ座標での応力に変換する.この応力を図2に示す構造にわたって平均し,これをマクロ応力とする.このプロセスにより各増分段階においてマクロひずみを与えた時のマクロ応力が与えられる.初期値を与えて温度・負荷条件に沿った温度および負荷の増分計算を繰り返し行うことにより与えられた温度・負荷条件における応力・ひずみの履歴が計算できる.
The above series of calculations proceeds with careful attention to the transformation of physical quantities in material coordinates, crystal grain coordinates (sub-element coordinates), and transformation plane coordinates.
Figure 3 shows the calculation procedure. That is,
Step 1: Give a small increment dε of strain ε. At this time, the strain is ε + dε.
Step 2: Obtain the strain of the subelements in each crystal grain. Due to the assumption of constant strain, this value is equal to ε + dε. However, since this strain is defined by the macro coordinates of the material, it is converted to the strain in the micro coordinates of the subelement by coordinate transformation. The elastic strain is obtained by subtracting the transformation strain of the subelement.
Step 3: Multiply the elastic strain by the elastic modulus to obtain the stress of the subelement (micro stress). Since there are 24 transformation systems for subelements, the decomposition shear stress considering the orientation of the transformation plane is obtained for each of them.
Step 4: Find the subelement that generates the maximum decomposition shear stress. If the maximum shear stress satisfies the transformation condition, give the transformation strain to this subelement and update the transformation strain value. The elastic strain is updated using the updated transformation strain value. The microstress value is updated using this.
Step 5: Convert stress in micro coordinates to stress in macro coordinates by coordinate transformation. This stress is averaged over the structure shown in Fig. 2, and this is the macro stress. This process gives the macro stress when the macro strain is applied at each incremental stage. By giving initial values and repeatedly calculating temperature and load increments according to the temperature and load conditions, the history of stress and strain at the given temperature and load conditions can be calculated.
上記計算の具体例として,形状記憶合金の超弾性挙動の計算例を図4に示す.
図4は、形状記憶合金の超弾性挙動の計算例である.オーステナイト状態にある(Af点以上の温度領域)形状記憶合金に単軸引張り応力を負荷すると,応力の増加に伴いマルテンサイト変態が生じ,応力・ひずみ曲線の勾配が緩くなる.さらに変形が進みマルテンサイト変態が飽和するとマルテンサイトの弾性変形により,応力・ひずみ曲線が立ち上がる.次いで除荷過程においては,ある応力以下になるとオーステナイト逆変態が起こり,オーステナイト逆変態の飽和を経て,応力・ひずみの原点に復帰する.この一連の応力・ひずみ挙動が示されている.
As a specific example of the above calculation, Fig. 4 shows a calculation example of the superelastic behavior of a shape memory alloy.
Fig. 4 is an example of calculation of the superelastic behavior of a shape memory alloy. When uniaxial tensile stress is applied to a shape memory alloy in the austenite state (temperature range above the Af point), martensitic transformation occurs as the stress increases, and the gradient of the stress-strain curve becomes gentle. As the deformation further progresses and the martensitic transformation is saturated, the stress-strain curve rises due to the elastic deformation of the martensite. Next, in the unloading process, the austenite reverse transformation occurs when the stress falls below a certain stress, and after the saturation of the austenite reverse transformation, it returns to the origin of stress and strain. This series of stress / strain behavior is shown.
本発明はこの形状記憶合金の相変態を伴う応力・ひずみ挙動を正確に予測するため、当該相変態挙動をアコモデーション機構のもとで生じることを取り入れた測定方法で実現させたものである。
即ち、本発明の測定方法により、形状記憶合金の超弾性挙動の応力―ひずみ関係を計算すると、応力誘起によるマルテンサイト変態開始応力(ひずみ)とその変態終了応力(ひずみ)、及び除荷過程におけるマルテンサイト相からオーステナイト相に逆変態開始応力(ひずみ)とその逆変態終了応力(ひずみ)を明瞭にすることを可能ならしめたものであり、従来の変態及び逆変態の開始・終了応力(ひずみ)の考え方を一新するものである。しかも実験的に変態および逆変態の開始および終了を正確に求めることは不可能であり、学術的に及び産業的に意義の大きなものである。
In the present invention, in order to accurately predict the stress / strain behavior accompanying the phase transformation of the shape memory alloy, the present invention is realized by a measurement method that incorporates the occurrence of the phase transformation behavior under the accommodation mechanism.
That is, when the stress-strain relationship of the superelastic behavior of the shape memory alloy is calculated by the measurement method of the present invention, the stress-induced martensite transformation start stress (strain), the transformation end stress (strain), and the unloading process This makes it possible to clarify the reverse transformation start stress (strain) and the reverse transformation end stress (strain) from the martensite phase to the austenite phase. ). Moreover, it is impossible to accurately determine the start and end of transformation and reverse transformation experimentally, which is of great academic and industrial significance.
Claims (1)
A polycrystalline shape memory alloy is shown by parallel connection of grains with different crystal orientations, and each grain is further divided into sub-elements. The average transformation strain of the sub-elements is taken as the transformation strain of the crystal grains. From this, the elastic strain and stress of the grains are obtained, and the decomposition shear stress at each transformation surface of each grain is obtained. When the maximum shear stress satisfies the transformation condition, the transformation strain is given to the subelement and the value of the transformation strain is calculated. , Update the elastic strain using the updated transformation strain value, update the microstress value using this elastic strain, convert the microstress to the macrostress in the macro coordinate, Considering the accommodation behavior of polycrystalline shape memory alloy, which is characterized by averaging this stress over the material structure including the subelements and making this a macro stress Phase transformation behavior measurement methods.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2010243841A JP5521161B2 (en) | 2010-10-29 | 2010-10-29 | A phase transformation behavior measurement method considering the accommodation behavior of polycrystalline shape memory alloys. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2010243841A JP5521161B2 (en) | 2010-10-29 | 2010-10-29 | A phase transformation behavior measurement method considering the accommodation behavior of polycrystalline shape memory alloys. |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JP2012098064A JP2012098064A (en) | 2012-05-24 |
| JP5521161B2 true JP5521161B2 (en) | 2014-06-11 |
Family
ID=46390159
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2010243841A Active JP5521161B2 (en) | 2010-10-29 | 2010-10-29 | A phase transformation behavior measurement method considering the accommodation behavior of polycrystalline shape memory alloys. |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP5521161B2 (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP5521162B2 (en) * | 2010-11-01 | 2014-06-11 | 国立大学法人 大分大学 | Phase transformation behavior measurement method considering accommodation behavior of polycrystalline shape memory alloy. |
| CN103499599A (en) * | 2013-10-11 | 2014-01-08 | 南京航空航天大学 | Memory alloy phase-change temperature measuring method and measuring system for implementing same |
| JP6562395B2 (en) * | 2015-06-24 | 2019-08-21 | 国立大学法人 大分大学 | Method for estimating phase transformation behavior of polycrystalline shape memory alloys |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP5417736B2 (en) * | 2008-04-21 | 2014-02-19 | 新日鐵住金株式会社 | Polycrystalline solid material property analysis system, polycrystalline solid material property analysis method, polycrystalline solid material property analysis program, and recording medium |
| JP5009222B2 (en) * | 2008-04-22 | 2012-08-22 | 新日本製鐵株式会社 | Method and apparatus for predicting deformation characteristics of polycrystalline material, program and recording medium |
| JP5521162B2 (en) * | 2010-11-01 | 2014-06-11 | 国立大学法人 大分大学 | Phase transformation behavior measurement method considering accommodation behavior of polycrystalline shape memory alloy. |
-
2010
- 2010-10-29 JP JP2010243841A patent/JP5521161B2/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| JP2012098064A (en) | 2012-05-24 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Chung et al. | Implementation strategy for the dual transformation region in the Brinson SMA constitutive model | |
| Qidwai et al. | On thermomechanics and transformation surfaces of polycrystalline NiTi shape memory alloy material | |
| Yu et al. | Modeling the martensite reorientation and resulting zero/negative thermal expansion of shape memory alloys | |
| JP5521161B2 (en) | A phase transformation behavior measurement method considering the accommodation behavior of polycrystalline shape memory alloys. | |
| Liu et al. | Mean-field polycrystal plasticity modeling with grain size and shape effects for laser additive manufactured FCC metals | |
| Jape et al. | Stable crack growth during thermal actuation of shape memory alloys | |
| Liu et al. | Modeling damage evolution of graphene/aluminum composites considering crystal cracking and interface failure | |
| Tokuda et al. | Thermomechanical behavior of shape memory alloy under complex loading conditions | |
| CN107563005A (en) | An Instantaneous Optimal Control Method for Vibration of Structures with Different Stiffness in Tension and Compression | |
| Ahadi et al. | Size dependence of the Poisson’s ratio in single-crystal fcc copper nanobeams | |
| Moore et al. | Effects of martensitic phase transformation on fatigue indicator parameters determined by a crystal plasticity model | |
| JP5521162B2 (en) | Phase transformation behavior measurement method considering accommodation behavior of polycrystalline shape memory alloy. | |
| Gilat et al. | Dynamic response of active composite plates: shape memory alloy fibers in polymeric/metallic matrices | |
| Barbera et al. | On the creep fatigue behavior of metal matrix composites | |
| CN116013434A (en) | Simulation Method of Regular Lattice Spring Model for Deformation and Fracture of Anisotropic Materials | |
| Ikeda | Modeling of ferroelastic behavior of shape-memory alloys | |
| Amarante dos Santos et al. | Semi‐active vibration control device based on superelastic NiTi wires | |
| Choudhry et al. | A General Thermo‐Mechanical Shape Memory Alloy Model: Formulation and Applications | |
| Hashiguchi | Indispensability of Subloading Surface Model with Overstress Model for Descriptions of Irreversible Mechanical Phenomena of Solids | |
| Saether et al. | A statistical approach for the concurrent coupling of molecular dynamics and finite element methods | |
| Gilat et al. | Thermal buckling of activated shape memory reinforced laminated plates | |
| Shanthraj et al. | Microstructural modeling of failure modes in martensitic steel alloys | |
| Law et al. | Incorporation of Load Induced Thermal Strain in Finite Element Models | |
| Mondal et al. | Size Effects on Overall Deformation Behavior of SAC Samples | |
| Kim | Predictions of tensile creep behavior of a PZT wafer by a normally distributed free energy model |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| A621 | Written request for application examination |
Free format text: JAPANESE INTERMEDIATE CODE: A621 Effective date: 20130703 |
|
| A521 | Written amendment |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20130704 |
|
| A01 | Written decision to grant a patent or to grant a registration (utility model) |
Free format text: JAPANESE INTERMEDIATE CODE: A01 Effective date: 20140218 |
|
| A61 | First payment of annual fees (during grant procedure) |
Free format text: JAPANESE INTERMEDIATE CODE: A61 Effective date: 20140311 |
|
| R150 | Certificate of patent or registration of utility model |
Ref document number: 5521161 Country of ref document: JP Free format text: JAPANESE INTERMEDIATE CODE: R150 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |