JPH1123420A - Method for evaluating life of bolt - Google Patents

Method for evaluating life of bolt

Info

Publication number
JPH1123420A
JPH1123420A JP17573397A JP17573397A JPH1123420A JP H1123420 A JPH1123420 A JP H1123420A JP 17573397 A JP17573397 A JP 17573397A JP 17573397 A JP17573397 A JP 17573397A JP H1123420 A JPH1123420 A JP H1123420A
Authority
JP
Japan
Prior art keywords
threads
bolt
test
creep
engaged
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.)
Withdrawn
Application number
JP17573397A
Other languages
Japanese (ja)
Inventor
Masao Takei
真男 武井
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 JP17573397A priority Critical patent/JPH1123420A/en
Publication of JPH1123420A publication Critical patent/JPH1123420A/en
Withdrawn legal-status Critical Current

Links

Landscapes

  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)

Abstract

PROBLEM TO BE SOLVED: To evaluate a life with high reliability by forming a test piece by retaining several threads of a bolt under test and boring a center portion, and executing a general purpose creep or low cycle fatigue test via a jig to be engaged with the threads. SOLUTION: Several threads of a base end of a bolt under test are retained at an engaging part of a bolt under test with female threads, and cut by retaining a base end side. Thereafter, the treads are bored in an axial hole of a predetermined diameter to form coaxial threaded hole to a test piece 7. The base end side of the piece 7 is engaged with a drug rod 9a of a tester, and a thread side is engaged with a jig 8 having female threads engaged with a drug bar 9b. It is applied to a general purpose creep or low cycle fatigue tester. Thus, the piece 7 is formed, several threads are loaded, and testing load is shared at several threads to a load shared at the several threads in a practical use state. Thus, a stress distribution from the threads to roots of the thread becomes similar to a real bolt to obtain a testing condition near using stress condition of the real bolt, and hence its life evaluation has high reliability.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は高温ボルト等のねじ
底部の経年劣化評価を破壊手法で行なうボルトの寿命評
価方法に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a bolt life evaluation method for evaluating the aging of a screw bottom of a high-temperature bolt or the like by a destruction technique.

【0002】[0002]

【従来の技術】高温ボルトは長期間使用するうちにクリ
ープや低サイクル疲労等の損傷を受けることが知れてお
り、定期的に取り換える部品の1つである。この取替え
時期を的確に把握し、取替えインター・バルを最適化す
るため、通常の開放点検に於いて、ボルトの点検を実施
し、傾向管理を実施したり、精密点検に於いて代表ボル
トを抜き取り、切断調査することにより当該機器に使用
されているボルトの余寿命を把握することも実施されて
いる。またこの代表ボルトを抜き取り、切断調査する場
合、供試ボルトよりクリープ或いは疲労試験用の試験片
を加工し、その試験片にてクリープ或いは低サイクル疲
労試験を実施することも実施されている。
2. Description of the Related Art High temperature bolts are known to suffer damage such as creep and low cycle fatigue during long-term use, and are one of the parts that are regularly replaced. In order to accurately grasp the timing of this replacement and optimize the replacement interval, check the bolts during normal opening inspections, perform trend management, and remove the representative bolts during precision inspection. In addition, it is also practiced to grasp the remaining life of the bolt used in the device by performing a cutting survey. When the representative bolt is extracted and cut and inspected, a test piece for creep or fatigue test is processed from the test bolt, and a creep or low cycle fatigue test is performed on the test piece.

【0003】一般的には、ボルトのクリープ或いは低サ
イクル疲労の損傷はねじ底部より発生し、き裂、破断に
至ることが多く、また強度評価上もねじ底部が応力集中
により高い局部応力を生じることが知られている。
In general, creep or low-cycle fatigue damage of bolts occurs from the bottom of the screw, often leading to cracks and fractures. In addition, from the viewpoint of strength evaluation, the screw bottom generates high local stress due to stress concentration. It is known.

【0004】図3〜図6に供試ボルト1から標準型のク
リープ試験片(平滑試験片2と切欠試験片3)を採取し
た例を示す。これに対し、ボルト全体の試験を実施する
ことも考えられるが、試験機の能力の問題や試験実施の
困難さから実現していない。このため、図7〜図9に示
すような供試ボルト1のねじ部から部分的にねじ底を含
む曲げ試験片5を切り出し、曲げクリープ試験機6で試
験する方法も提案され、実用化されている。
FIGS. 3 to 6 show examples in which a standard creep test piece (smooth test piece 2 and notch test piece 3) is sampled from a test bolt 1. FIG. On the other hand, it is conceivable to perform a test on the entire bolt, but this has not been realized due to a problem in the capability of the testing machine and difficulty in performing the test. For this reason, a method of cutting out a bending test piece 5 partially including a screw bottom from the thread portion of the test bolt 1 as shown in FIGS. 7 to 9 and testing it with a bending creep tester 6 has also been proposed and put into practical use. ing.

【0005】[0005]

【発明が解決しようとする課題】上記従来技術は次のよ
うな問題点があり正確な余寿命の予測が困難であった。
The above prior art has the following problems and it is difficult to accurately estimate the remaining life.

【0006】(1)標準型のクリープ試験片を採取し、
クリープまたは疲労試験を行う方法では、ボルトの寿命
の最も苛酷な部位での試験ができない。
(1) A standard creep test piece is collected,
The creep or fatigue test method does not allow testing at the severest part of the bolt life.

【0007】(2)曲げ試験片を切り出し、曲げクリー
プ試験を行う方法では、試験荷重の作用力は実ボルトね
じ部の状態と異なる。
(2) In a method in which a bending test piece is cut out and a bending creep test is performed, the acting force of the test load is different from the actual bolt screw state.

【0008】(3)供試ボルト全体を試験する方法で
は、荷重等が大きくなり過ぎ、汎用のクリープ試験機や
疲労試験機が使用できない。(例えば、直径100mm程
度のボルトの場合、50〜100ton の荷重が必要)
(3) In the method of testing the entire test bolt, the load or the like becomes too large, and a general-purpose creep tester or fatigue tester cannot be used. (For example, for a bolt with a diameter of about 100 mm, a load of 50 to 100 tons is required)

【0009】[0009]

【課題を解決するための手段】本発明は上記課題を解決
するため次の手段を講ずる。
The present invention employs the following means to solve the above-mentioned problems.

【0010】すなわち、クリープまたは低サイクル疲労
試験用の供試ボルトから数ねじ山を残しかつ中央部をく
り抜いた試験片を作り、上記ねじ山にら合する治具を介
して汎用のクリープ試験機または汎用の低サイクル疲労
試験機にかけて寿命評価を行う。
That is, a test piece in which a few threads are left and a center portion is cut out from a test bolt for creep or low cycle fatigue test is produced, and a general-purpose creep test machine is passed through a jig which fits the thread. Alternatively, the life is evaluated using a general-purpose low cycle fatigue tester.

【0011】以上において、供試ボルトから数ねじ山を
残し、かつ中央部がくり抜かれた筒形の試験片が作製さ
れる。そして、試験片のねじ山にら合する治具を介して
汎用のクリープ試験機または/および汎用の低サイクル
疲労試験機にかけて、寿命評価が行れる。このとき、試
験荷重はねじ山が数ねじ山となったので、実使用状態で
数ねじ山分が分担する荷重、すなわち小荷重Fとする。
またくり抜き部の径は残り断面Sが、小荷重F時、実使
用状態の応力となるように設定する。
[0011] In the above, a cylindrical test piece having a few threads left from the test bolt and a hollow central portion is produced. Then, the life is evaluated by using a general-purpose creep tester and / or a general-purpose low cycle fatigue tester through a jig that fits into the thread of the test piece. At this time, the test load is a load that is shared by several threads in the actual use state, that is, a small load F, since the threads have several threads.
The diameter of the hollow portion is set so that the remaining cross section S has a stress in an actual use state when the load F is small.

【0012】以上により、汎用のクリープ試験機や低サ
イクル疲労試験機が使用でき、かつ、実使用状態に近似
した状態で試験される。そして寿命評価が行れる。した
がって、信頼性の高い寿命評価が、可能となる。
As described above, a general-purpose creep tester and a low cycle fatigue tester can be used, and the test is performed in a state similar to the actual use state. Then, the life evaluation is performed. Therefore, highly reliable life evaluation can be performed.

【0013】[0013]

【発明の実施の形態】本発明の実施の形態を図1と図2
により説明する。
1 and 2 show an embodiment of the present invention.
This will be described below.

【0014】供試ボルト1から、めねじとの噛合部aに
対し、その基端部のねじ山を数山(図では2山)残す加
工をするとともに先端側を軸に垂直に切断する。また基
端側を小し残して垂直に切断する。そしてねじ山部を所
定径Dの同軸穴でくり抜く。さらに基端側に同軸のねじ
穴bを形成する。これが試験片7となる。
From the test bolt 1, the threaded portion at the base end of the meshing portion a with the female thread is processed to leave several threads (two threads in the figure), and the tip side is cut perpendicularly to the axis. Also, cut vertically, leaving the base end small. Then, the thread portion is cut out with a coaxial hole having a predetermined diameter D. Further, a coaxial screw hole b is formed on the base end side. This becomes the test piece 7.

【0015】この試験片7は基端側が試験機の引棒9a
にら合される。またねじ山側が引棒9bにら合しためす
ねじを持つ治具8にら合される。そして、汎用のクリー
プ試験機や低サイクル疲労試験機にかけられる。
The test piece 7 has a draw bar 9a of the test machine at the base end side.
It is glared. Further, the thread side is engaged with a jig 8 having a female screw for engaging with the pull rod 9b. Then, it is applied to a general-purpose creep tester and a low cycle fatigue tester.

【0016】以上のように試験片7を形成することによ
り、試験荷重はねじ山が数ねじ山となったので、実使用
状態で数ねじ山分が分担する荷重とする。例えば噛合い
部aのねじ山が30山、試験片7のねじ山が2山とすれ
ば、実負荷の1/15程度の小荷重Fでよい。またくり
抜き部の径Dは残り断面Sが、小荷重F時、実使用状態
の応力となるように設定する。
By forming the test piece 7 as described above, the test load is set to a load which is shared by several threads in the actual use state since the threads have several threads. For example, if the thread of the engagement portion a has 30 threads and the thread of the test piece 7 has two threads, a small load F of about 1/15 of the actual load may be used. The diameter D of the hollow portion is set so that the remaining cross section S has a stress in an actual use state at a small load F.

【0017】このようにすることにより、ねじ山からね
じ底に到る応力分布および応力は実ボルトのそれと同様
となり、実ボルトの使用応力条件に近い試験条件を得る
ことができる。したがって、汎用のクリープ試験機や低
サイクル疲労試験機が使用でき、かつ、実使用状態に近
似した状態で試験される。そして寿命評価が行れるの
で、信頼性の高い寿命評価が可能となる。
In this way, the stress distribution and the stress from the screw thread to the screw bottom are the same as those of the actual bolt, and it is possible to obtain a test condition close to the working stress condition of the actual bolt. Therefore, a general-purpose creep tester or a low cycle fatigue tester can be used, and the test is performed in a state similar to an actual use state. Since the life evaluation is performed, highly reliable life evaluation can be performed.

【0018】[0018]

【発明の効果】以上に説明したように、本発明によれ
ば、供試ボルトから数ねじ山を残しかつ中央部をくり抜
いた試験片を作り汎用のクリープ試験機または疲労試験
機にて試験するので、試験荷重を適切に選ぶことによ
り、試験片のねじ底部の応力分布は実機のボルトのそれ
に近い条件を実現できる。
As described above, according to the present invention, a test piece having a few threads left from the test bolt and a central portion cut out is prepared and tested using a general-purpose creep tester or fatigue tester. Therefore, by appropriately selecting the test load, it is possible to realize a condition in which the stress distribution at the screw bottom of the test piece is close to that of the bolt of the actual machine.

【0019】このため正確なクリープまたは低サイクル
疲労試験をすることとなり、正確な余寿命の評価が可能
となる。
For this reason, an accurate creep or low cycle fatigue test is performed, and an accurate evaluation of the remaining life becomes possible.

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

【図1】本発明の実施の一形態の断面図である。FIG. 1 is a sectional view of an embodiment of the present invention.

【図2】上記一形態の試験片の断面図である。FIG. 2 is a cross-sectional view of the test piece of one embodiment.

【図3】従来の一例の説明用側面図である。FIG. 3 is a side view for explaining an example of the related art.

【図4】同従来の一例の説明用正面図である。FIG. 4 is an explanatory front view of the example of the conventional art.

【図5】同従来の一例の平滑クリープ試験片の図であ
る。
FIG. 5 is a view of a smooth creep test piece of the conventional example.

【図6】同従来の一例の環状切欠クリープ試験片の図で
ある。
FIG. 6 is a view of an example of an annular notched creep test piece of the related art.

【図7】同従来の他例の説明用側面図である。FIG. 7 is an explanatory side view of another example of the conventional art.

【図8】同従来の他例の説明用正面図である。FIG. 8 is an explanatory front view of another example of the conventional art.

【図9】同従来の他例の説明図である。FIG. 9 is an explanatory diagram of another example of the related art.

【符号の説明】[Explanation of symbols]

1 供試ボルト 2 平滑試験片 3 切欠試験片 5 試験片 6 曲げクリープ試験機 7 試験片 8 治具 9a,9b 引棒 DESCRIPTION OF SYMBOLS 1 Test bolt 2 Smooth test piece 3 Notch test piece 5 Test piece 6 Bending creep tester 7 Test piece 8 Jig 9a, 9b Pull rod

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 クリープまたは低サイクル疲労試験用の
供試ボルトから数ねじ山を残しかつ中央部をくり抜いた
試験片を作り、上記ねじ山にら合する治具を介して汎用
のクリープ試験機または汎用の低サイクル疲労試験機に
かけて寿命評価を行うことを特徴とするボルトの寿命評
価方法。
1. A creep or low cycle fatigue test bolt is formed with a test piece having several threads left and a central portion cut out from a test bolt, and a general-purpose creep test machine is passed through a jig mating with the thread. Alternatively, a method for evaluating the life of a bolt, wherein the life is evaluated using a general-purpose low-cycle fatigue tester.
JP17573397A 1997-07-01 1997-07-01 Method for evaluating life of bolt Withdrawn JPH1123420A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP17573397A JPH1123420A (en) 1997-07-01 1997-07-01 Method for evaluating life of bolt

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP17573397A JPH1123420A (en) 1997-07-01 1997-07-01 Method for evaluating life of bolt

Publications (1)

Publication Number Publication Date
JPH1123420A true JPH1123420A (en) 1999-01-29

Family

ID=16001296

Family Applications (1)

Application Number Title Priority Date Filing Date
JP17573397A Withdrawn JPH1123420A (en) 1997-07-01 1997-07-01 Method for evaluating life of bolt

Country Status (1)

Country Link
JP (1) JPH1123420A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102854010A (en) * 2012-10-10 2013-01-02 湖南奔腾动力科技有限公司 Fatigue life calculation method for engine parts based on road cycle working condition
CN103983446A (en) * 2014-05-23 2014-08-13 天润曲轴股份有限公司 Crankshaft fatigue bending test calibration device
CN105300673A (en) * 2015-10-10 2016-02-03 中国空间技术研究院 Reliability determination method based on compression spring stress relaxation testing data
CN108982076A (en) * 2018-04-11 2018-12-11 中国石油天然气集团有限公司 A kind of gas well at HTHP oil pipe hermetic seal screw thread assay method
CN110672443A (en) * 2019-10-30 2020-01-10 北京科技大学 Testing device and method suitable for thread missing tooth fatigue of threaded connecting piece

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102854010A (en) * 2012-10-10 2013-01-02 湖南奔腾动力科技有限公司 Fatigue life calculation method for engine parts based on road cycle working condition
CN102854010B (en) * 2012-10-10 2015-10-07 湖南奔腾动力科技有限公司 A kind of engine part fatigue life calculation method based on road state of cyclic operation
CN103983446A (en) * 2014-05-23 2014-08-13 天润曲轴股份有限公司 Crankshaft fatigue bending test calibration device
CN105300673A (en) * 2015-10-10 2016-02-03 中国空间技术研究院 Reliability determination method based on compression spring stress relaxation testing data
CN105300673B (en) * 2015-10-10 2017-07-28 中国空间技术研究院 A kind of reliability based on stage clip stress relaxation test data determines method
CN108982076A (en) * 2018-04-11 2018-12-11 中国石油天然气集团有限公司 A kind of gas well at HTHP oil pipe hermetic seal screw thread assay method
CN108982076B (en) * 2018-04-11 2020-03-10 中国石油天然气集团有限公司 Analysis and evaluation method for gas sealing threads of oil pipe of high-temperature and high-pressure gas well
CN110672443A (en) * 2019-10-30 2020-01-10 北京科技大学 Testing device and method suitable for thread missing tooth fatigue of threaded connecting piece

Similar Documents

Publication Publication Date Title
DE3029957C2 (en) Device for determining the wear on cutting tools by evaluating the vibrations occurring on the cutting tool
JPH1123420A (en) Method for evaluating life of bolt
US6598305B1 (en) Spline gage system and method
BRPI0708031A2 (en) engine block durability test
JP2017020289A (en) Anchor bolt driving jig, anchor bolt driving method, and anchor bolt fixing strength inspection method
DE102018209609A1 (en) Inspection procedure and system
KR101291881B1 (en) Jig for tensile test
US2454159A (en) Guide sleeve construction for plug gauges
US5792960A (en) Tool for measuring decay in wood
CN106839960A (en) It is a kind of for timber structure Tenon node size and the lossless detection method of internal flaw
JP3631946B2 (en) Fatigue crack measuring method and displacement crack measuring instrument
JP2002039885A (en) Bolt fastener with inspection function
CN104977107B (en) Method for the clamping force for determining riveting
Pártl et al. Reconstitution of crack growth from fractographic observations after flight simulation loading
JP3206482B2 (en) Wood diagnosis method and wood connection material
CN215524548U (en) Device for auxiliary measurement of broken sample of tensile test
Sandoz et al. Wood poles ageing and non destructive testing tool
JP2021131357A (en) Method for evaluating fatigue strength of composite material
CN113297538B (en) Non-ferromagnetic material stress damage monitoring method and device and computer equipment
DE102018210463A1 (en) Method for checking at least a partial area of a component and testing device for checking at least a partial area of a component
CN218211044U (en) Go-no go gauge for checking thread
DE2941776A1 (en) Test gauge for holes drilled through coal seam - uses inserted tube to measure longitudinal and cross-sectional alterations caused by roof pressure
JPH0349549A (en) Inspecting method for air gap
JP4296418B2 (en) Axial force securing bolt inspection system
JPH07151662A (en) Creep life evaluation through temperature acceleration test

Legal Events

Date Code Title Description
A300 Withdrawal of application because of no request for examination

Free format text: JAPANESE INTERMEDIATE CODE: A300

Effective date: 20040907