JPS63231240A - Method for detecting crack generation limit strain of thin film coating - Google Patents

Method for detecting crack generation limit strain of thin film coating

Info

Publication number
JPS63231240A
JPS63231240A JP6270087A JP6270087A JPS63231240A JP S63231240 A JPS63231240 A JP S63231240A JP 6270087 A JP6270087 A JP 6270087A JP 6270087 A JP6270087 A JP 6270087A JP S63231240 A JPS63231240 A JP S63231240A
Authority
JP
Japan
Prior art keywords
strain
thin film
test piece
crack generation
crack
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
Application number
JP6270087A
Other languages
Japanese (ja)
Inventor
Masaharu Fujiwara
昌晴 藤原
Eiichiro Otsuka
大塚 英一郎
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 JP6270087A priority Critical patent/JPS63231240A/en
Publication of JPS63231240A publication Critical patent/JPS63231240A/en
Pending legal-status Critical Current

Links

Landscapes

  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)

Abstract

PURPOSE:To easily and accurately the limit strain of crack generation at low cost by placing a bending load on a metallic test-piece which is coated with a thin film and has a strain gauge stuck, and checking the coating surface. CONSTITUTION:A base material 1 is coated 2 and the strain gauge 3 is stuck on the surface to obtain the test-piece, which is strained by applying pressure at the positions of loading means 4 and 5. The strain is measured by the strain gauge 3 and recorded. The test-piece is checked through a microscope after the load is removed to find a range where a crack 7 exists and the minimum strain where the crack 7 exits. In this case, a% and a'% indicate the limit strain.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明はセラミックス等のコーテイング膜のクラツク発
生限界歪の検出法に関する。
DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a method for detecting the critical strain for crack generation in coating films such as ceramics.

〔従来の技術〕[Conventional technology]

金属の表面にコーティングされたセラミックス等の被膜
にクランクが生じる限界の歪金実験的に求める場合、従
来は引張試験片(第4図の符号6)に段階的な歪を与え
て、それぞれの試験片を顕微鏡によシフラック(第4図
の符号7)の有無を調べていfc(第5図)。
To experimentally determine the strain limit at which cranking occurs in a coating such as ceramics coated on the surface of a metal, conventionally a tensile test piece (reference numeral 6 in Figure 4) is subjected to gradual strain, and each test is The piece was examined under a microscope for the presence or absence of siflac (numeral 7 in Fig. 4) (Fig. 5).

〔発明が解決しようとする問題点〕[Problem that the invention seeks to solve]

前述のような従来の方法で1は、−試験片に一条件の歪
しか与えられない為 (1)  クラックが発生する歪の限界値を正しく求め
られない。
In the conventional method as described above, (1) the limit value of strain at which cracks occur cannot be accurately determined because only one condition of strain is applied to the test piece;

(2)条件数に応じた数の試験片が必要となる。(2) A number of test pieces are required according to the number of conditions.

という欠点があった。There was a drawback.

また−試験片で歪を少しずつ増しながらクシツクの調査
をする方法では、試験片を試験機に取付は取外す手間が
かかっていた。
Furthermore, in the method of investigating the stiffness while gradually increasing the strain on the test piece, it was time-consuming to attach and remove the test piece from the testing machine.

〔問題点全解決するための手段〕[Means to solve all problems]

曲げ試験片を用いて歪分布がOからある一定値まで連続
的に負荷し、同時に歪ゲージにより試験片の歪分布を求
めておく。除荷後に試験片の歪ゲージ貼付側のコーテイ
ング面を顕微鏡で調ベクラックが発生している位置を求
める。
Using a bending test piece, a strain distribution is continuously applied from O to a certain constant value, and at the same time, the strain distribution of the test piece is determined using a strain gauge. After unloading, examine the coated surface of the test piece on the side where the strain gauge is attached using a microscope to determine the location where cracks have occurred.

〔作用〕[Effect]

クラックが発生している領域と発生していない領域の境
界の位置の歪の値が、゛クラック発生の限界歪として、
短時間でかつ段階的でなく求められる。
The strain value at the boundary between the cracked area and the non-cracked area is defined as the critical strain for crack generation.
Required in a short period of time and in a non-stepwise manner.

〔実施例〕〔Example〕

第1図に示すように、試験片は母材1(本実施例では4
g×10mm×(イ)囚〕にコーティング2(Cr02
.Cr3O2等)ヲ施シ、表iにq間隔に歪ゲージ3全
貼付したものを用いる。第1図の載荷手段4及び5の位
置に圧力を加え、試験片に第2図(イ)に示すような分
布の歪を与え、歪ゲージ3によシ歪を計測記録する。
As shown in Fig. 1, the test piece was made of base material 1 (4
Coating 2 (Cr02
.. Cr3O2, etc.), and use one in which all three strain gauges are pasted at q intervals in Table i. Pressure is applied to the positions of the loading means 4 and 5 shown in FIG. 1 to give the test piece a strain with a distribution as shown in FIG. 2 (a), and the strain is measured and recorded by the strain gauge 3.

除荷後試験片を顕微鏡により調べ、第2図(ロ)に示す
ようシで、クラック7が存在する範囲を求める。
After unloading, the test piece is examined under a microscope, and the range in which the crack 7 exists is determined as shown in FIG. 2 (b).

クラックが存在する最小の歪が第2図に示すように(イ
)と(ロ)の関係から求める。即ち、第2図(イ)のa
%及び47%が限界歪である。
The minimum strain at which a crack exists is determined from the relationship between (a) and (b) as shown in Figure 2. That is, a in Figure 2 (a)
% and 47% are critical strains.

本試験は第3図に示すように片持梁型の試験片又は構造
でも実施が可能であろう 〔発明の効果〕 従来金属等の表面にコーティングされたセラミック等の
クラック発生の限界は多数の試験片を用いて段階的に求
める等の方法によっていたが、本発明によれば1個の試
験片によりかつ段階的でなく求められる。
This test may also be carried out with a cantilever type test piece or structure as shown in Figure 3. [Effects of the Invention] Conventionally, there are many limitations on the occurrence of cracks in ceramics coated on the surface of metals, etc. Previously, it was determined stepwise using a test piece, but according to the present invention, it is determined using a single test piece without stepwise steps.

従って、セラミックコーティング等の強度の比較を容易
かつ安価に精度よく行うことが出来る。
Therefore, the strength of ceramic coatings and the like can be compared easily, inexpensively, and accurately.

セラミックコーティング等の開発における試駆手段とし
て極めて有効であると考えられる。
It is considered to be extremely effective as a trial method in the development of ceramic coatings, etc.

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

第1図は本発明薄膜コーティングのクラック発生限界歪
検出法の実施例を示す。第2図(イ)(ロ)は第1図の
歪検出法によシ試験片に発生する歪分布とクラックを示
し、第3図は片持梁を用いる本発明の他の実施例を示す
。第4図は従来の試験片と試験方法を示し、第5図は従
来のクラック限界歪の求め方を示す。 1.1′・・・試験片母材   2・・・コーティング
層3・・・歪ゲージ      4,5.5’・・・載
荷点7・・・クラック 代 理 人 弁理士 岡 本 重 又 外2名 第3図 第4図 第5図 歪
FIG. 1 shows an embodiment of the method for detecting the critical strain for crack generation in a thin film coating according to the present invention. Figures 2 (a) and (b) show the strain distribution and cracks that occur in the specimen using the strain detection method shown in Figure 1, and Figure 3 shows another embodiment of the present invention using a cantilever beam. . FIG. 4 shows a conventional test piece and a test method, and FIG. 5 shows a conventional method for determining the crack critical strain. 1.1'...Test piece base material 2...Coating layer 3...Strain gauge 4,5.5'...Loading point 7...Crack agent Patent attorney Shige Okamoto Matato 2 Figure 3 Figure 4 Figure 5 Distortion

Claims (1)

【特許請求の範囲】[Claims] セラミック等の薄膜コーティングを施行し、更に歪ゲー
ジを貼付した金属試験片に曲げ力を負荷し、コーティン
グ層が破損しクラックが発生する限界の歪を検出するこ
とを特徴とする薄膜コーティングのクラック発生限界歪
検出法。
Crack generation in thin film coatings is characterized by applying bending force to a metal test piece coated with a thin film of ceramic, etc., and then applying a bending force to a metal test piece to which a strain gauge is attached, and detecting the limit strain at which the coating layer breaks and cracks occur. Limit strain detection method.
JP6270087A 1987-03-19 1987-03-19 Method for detecting crack generation limit strain of thin film coating Pending JPS63231240A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP6270087A JPS63231240A (en) 1987-03-19 1987-03-19 Method for detecting crack generation limit strain of thin film coating

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP6270087A JPS63231240A (en) 1987-03-19 1987-03-19 Method for detecting crack generation limit strain of thin film coating

Publications (1)

Publication Number Publication Date
JPS63231240A true JPS63231240A (en) 1988-09-27

Family

ID=13207839

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6270087A Pending JPS63231240A (en) 1987-03-19 1987-03-19 Method for detecting crack generation limit strain of thin film coating

Country Status (1)

Country Link
JP (1) JPS63231240A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH085530A (en) * 1994-06-14 1996-01-12 Agency Of Ind Science & Technol Method for measuring critical strain amount of coating film and coating film destroyed position detector used for the method
JP2008292331A (en) * 2007-05-25 2008-12-04 Toshiba Corp Stress corrosion cracking test method
WO2013049252A1 (en) * 2011-09-26 2013-04-04 Fmc Technologies, Inc. Apparatus and method for detecting cracks in flow pipes

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH085530A (en) * 1994-06-14 1996-01-12 Agency Of Ind Science & Technol Method for measuring critical strain amount of coating film and coating film destroyed position detector used for the method
JP2008292331A (en) * 2007-05-25 2008-12-04 Toshiba Corp Stress corrosion cracking test method
WO2013049252A1 (en) * 2011-09-26 2013-04-04 Fmc Technologies, Inc. Apparatus and method for detecting cracks in flow pipes

Similar Documents

Publication Publication Date Title
Read et al. Fatigue of microlithographically-patterned free-standing aluminum thin film under axial stresses
CN110487643B (en) Method for testing shear strength of micron-sized fibers
US5598738A (en) Load apparatus and method for bolt-loaded compact tension test specimen
US4939496A (en) Regulatable creep strain gauges and process for obtaining such gauges
Jin et al. A new driving force parameter for fatigue growth of multiple cracks
US4953973A (en) Detection of compressive residual stresses using the method of caustics
JP3300810B2 (en) Non-destructive method for measuring the aging of the strength of ferromagnetic structural materials
Dawicke et al. Three-dimensional crack closure behavior
JPS63231240A (en) Method for detecting crack generation limit strain of thin film coating
Panin et al. Staging of a localized deformation during tension of specimens of a carbon-carbon composite material with holes of different diameters according to acoustic-emission, surface-deformation mapping, and strain-gauging data
JPS6381244A (en) Fatigue testing method
Stille et al. Very high cycle fatigue behavior of riblet structured Alclad 2024 thin sheets
SU1714357A1 (en) Method of determining deformation of article
US2984101A (en) Tape method for detecting fatigue cracks
RU2229696C2 (en) Process testing sheet materials for double-axes tension
JPS6350737A (en) Method for testing restraint joint
RU2226682C2 (en) Process testing sheet materials for tension
JP3528160B2 (en) Scratch-type material surface film strength test apparatus and test method
Pitt et al. Compliance measurements for assessing structural integrity
Blumenthal High strain rate compression testing of ceramics and ceramic composites
Kukla et al. Assessment of fatigue resistance of aluminide layers on MAR 247 nickel super alloy with full-field optical strain measurements
Seidt et al. Influence of fabrication method on tensile response of split Hopkinson bar-sized specimens
SU888658A1 (en) Method of determining plastic deformation of metal
JP3335770B2 (en) Evaluation method of scale peelability
JPS6126015B2 (en)