CN111324985A - Method for evaluating fatigue life of continuous tube containing groove-shaped scratch defects - Google Patents

Method for evaluating fatigue life of continuous tube containing groove-shaped scratch defects Download PDF

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CN111324985A
CN111324985A CN202010261455.4A CN202010261455A CN111324985A CN 111324985 A CN111324985 A CN 111324985A CN 202010261455 A CN202010261455 A CN 202010261455A CN 111324985 A CN111324985 A CN 111324985A
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defect
strain
wall groove
shaped scratch
defects
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CN111324985B (en
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刘少胡
钟虹
周浩
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Yangtze University
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Abstract

The invention relates to an evaluation method for the fatigue life of a continuous pipe containing groove-shaped scratch defects, belonging to the field of safety evaluation of the service life of a pipe column. The method comprises the steps of screening and confirming the outer wall groove-shaped scratch defects and the inner wall groove-shaped scratch defects, detecting the shape geometric parameters of the scratch defects, and calculating the fatigue life of the continuous pipe containing the outer wall groove-shaped scratch defects and the inner wall groove-shaped scratch defects; and the continuous pipe containing the outer wall groove-shaped scratch defects and the inner wall groove-shaped scratch defects is subjected to a three-stage evaluation step, so that the defect of fatigue life evaluation of the conventional continuous pipe containing the groove-shaped defects is overcome, the cost is saved, the economic benefit is increased, the use risk of the continuous pipe is reduced, and the method has great production practice significance.

Description

Method for evaluating fatigue life of continuous tube containing groove-shaped scratch defects
Technical Field
The invention relates to an evaluation method for the fatigue life of a continuous pipe containing groove-shaped scratch defects, belonging to the field of safety evaluation of the service life of a pipe column.
Background
The Continuous Tube (CT) is an endless tube formed by welding a plurality of sections of steel strips, and is wound on a roller with a larger diameter so as to be convenient for transportation and operation. Compared with the traditional drilling and completion mode, the coiled tubing does not need to be additionally erected on a derrick and be broken out, so that the operation period is greatly shortened, the labor intensity is reduced, the exploitation cost is reduced, and the cost can be saved by 25-40%. The continuous pipe technology becomes a new technology which is improved day by day in the field of petroleum and natural gas exploration and development, and is praised as universal operation equipment due to wide application range and convenient use of continuous pipe operation equipment.
The fatigue of coiled tubing falls within the category of typical low cycle fatigue because coiled tubing undergoes 6 alternating bend-straight deformations during one run up and down, forcing it into a plastic state when the deformation far exceeds the elastic limit of the material. Mechanical damage is often unavoidable during the transportation and operation of the continuous pipe, and the damage defect forms of groove-shaped scratches, spherical indentations and the like, wherein the groove-shaped scratches are one of the main defect forms. At present, a perfect method for evaluating the residual life of the groove-shaped scratch defect is not available, and usually, in the field use process, if the scratch defect occurs, the whole disc of continuous pipe is directly scrapped, so that the residual fatigue life of the continuous pipe containing the groove-shaped defect cannot be continuously exerted, the use cost is increased, and the operation risk is increased. Therefore, an evaluation method is urgently needed to make up the deficiency of the conventional fatigue life evaluation of the continuous pipe containing the groove-shaped scratch defects, so that the continuous pipe containing the defects is correctly used, and the use risk is reduced.
Disclosure of Invention
The invention aims to provide a method for evaluating the fatigue life of a continuous pipe containing groove-shaped scratch defects, which can accurately evaluate the fatigue life safety of the continuous pipe containing groove-shaped scratch defects, thereby accurately using the continuous pipe containing the defects and reducing the use risk.
The technical scheme of the invention is as follows:
a method for evaluating the fatigue life of a continuous tube containing groove-shaped scratch defects is characterized by comprising the following steps: it comprises the following steps:
1) firstly, screening and confirming the outer wall groove-shaped scratch defects and the inner wall groove-shaped scratch defects on a service continuous pipe;
2) the defect parameters of the outer wall groove-shaped scratch defect and the inner wall groove-shaped scratch defect comprise a defect axial angle β, a defect depth a, a defect length c, a defect width b, a blunted fillet R around the scratch, the circumferential distribution of the defect and the circumferential distribution number of the defect, and the ice utilizes defect detection equipment to measure the parameters of the outer wall groove-shaped scratch defect and the inner wall groove-shaped scratch defect;
3) obtaining sensitive parameters which are the defect depth a, the defect width b, the defect axial angle β and the defect length c in sequence from sensitive parameters in the defect axial angle β, the defect depth a, the defect length c, the defect width b, the blunted fillet R around the scratch, the circumferential distribution of the defects and the circumferential distribution number of the defects based on an orthogonal test method;
4) theoretically calculating the fatigue life of the continuous tube containing the outer wall groove-shaped scratch defects and the inner wall groove-shaped scratch defects on the basis of considering the groove-shaped defect sensitive parameters;
5) carrying out three-stage evaluation on the continuous pipe containing the outer wall groove-shaped scratch defects and the inner wall groove-shaped scratch defects; namely, the three-stage evaluation was performed on the continuous pipe containing the groove-shaped scratch defect. Compared with a complete continuous pipe under the same working condition, direct scrapping with fatigue life reduced by 50 percent, fine evaluation with fatigue life reduced by 20-50 percent and rough evaluation with fatigue life reduced by less than 20 percent are carried out;
the method for calculating the fatigue life of the continuous tube containing the outer wall groove-shaped scratch defects and the inner wall groove-shaped scratch defects in the step 4) comprises the following steps:
when the outer surface of the continuous pipe has the outer wall groove-shaped scratch defects and the inner wall groove-shaped scratch defects, the influence of the outer wall groove-shaped scratch defects and the inner wall groove-shaped scratch defects on the fatigue life is considered when the fatigue life model of the continuous pipe is established; obtaining radial stress of continuous tube under internal pressure based on thick-wall cylinder theory
Figure 216931DEST_PATH_IMAGE001
Hoop stress
Figure 134071DEST_PATH_IMAGE002
And axial stress
Figure 569600DEST_PATH_IMAGE003
Figure 964810DEST_PATH_IMAGE004
In the formula:
Figure 779182DEST_PATH_IMAGE005
the outer radius of the continuous tube is mm;
Figure 601644DEST_PATH_IMAGE006
is the inner radius, mm;
Figure 399836DEST_PATH_IMAGE007
is the internal pressure, MPa; r is any radius, mm.
According to the analysis of stress andvon Misesthe criterion, that the critical point for yielding first always is the inner surface of the continuous pipe, in which case
Figure 598736DEST_PATH_IMAGE008
Figure 267615DEST_PATH_IMAGE009
According to the Remberg-Osgood elastic-plastic stress-strain relation, the total strain generated by bending action
Figure 667503DEST_PATH_IMAGE010
Is elastically strained
Figure 421833DEST_PATH_IMAGE011
And plastic strain
Figure 158845DEST_PATH_IMAGE012
And (3) the sum:
Figure 213388DEST_PATH_IMAGE013
in the formula:Dis outside a continuous tubeDiameter, mm;
Figure 643233DEST_PATH_IMAGE014
is the bending radius, mm;Eis the modulus of elasticity, MPa;
Figure 884858DEST_PATH_IMAGE015
yield limit, MPa;
the axial force generated by bending is the main cause of plastic strain, and the axial stress is generated under the action of internal pressure and bending
Figure 159982DEST_PATH_IMAGE016
Comprises the following steps:
Figure 462175DEST_PATH_IMAGE017
axial stress resulting from bending from the Holomon relationship of stress to plastic strain
Figure 797341DEST_PATH_IMAGE018
Hoop strain, axial strain and radial strain under internal pressure bending coupling load:
Figure 526263DEST_PATH_IMAGE019
in the formula:
Figure 136235DEST_PATH_IMAGE020
is the hoop strain;
Figure 634213DEST_PATH_IMAGE021
is the axial strain;
Figure 405860DEST_PATH_IMAGE022
is the radial strain;
Figure 763023DEST_PATH_IMAGE023
the cyclic strain hardening coefficient is MPa;
Figure 645528DEST_PATH_IMAGE024
is the cyclic strain hardening index;
in the plastic deformation process of the continuous pipe, the volume invariance assumption is adopted, and the equivalent plastic strain is generated under the coupling load
Figure 998012DEST_PATH_IMAGE025
Comprises the following steps:
Figure 471719DEST_PATH_IMAGE026
adopting a Brown-Miller fatigue life theoretical model, and the strain-life formula is as follows:
Figure 909653DEST_PATH_IMAGE027
Figure 330271DEST_PATH_IMAGE028
maximum shear strain:
Figure 458632DEST_PATH_IMAGE029
positive strain at maximum shear strain plane:
Figure 572082DEST_PATH_IMAGE030
in order to consider the influence of other parameters except sensitive parameters on the fatigue life of the continuous tube, a correction coefficient is introduced
Figure 497313DEST_PATH_IMAGE031
Figure 721621DEST_PATH_IMAGE032
In the formula:c 0 the depth of the pit defect;N f the number of fatigue bending times of the continuous tube;
maximum shear strain after introducing correction coefficient and positive strain of maximum shear strain plane:
Figure 314276DEST_PATH_IMAGE033
the final fatigue life calculation model of the continuous pipe containing the defects is as follows:
Figure 598627DEST_PATH_IMAGE034
the invention has the beneficial effects that
Compared with the prior art, the method has the advantages that the fatigue life of the continuous pipe containing the outer wall groove-shaped scratch defects and the inner wall groove-shaped scratch defects is calculated by screening, confirming and detecting the outer wall groove-shaped scratch defects and the inner wall groove-shaped scratch defects, detecting the shape geometric parameters of the scratch defects and calculating the fatigue life of the continuous pipe containing the outer wall groove-shaped scratch defects and the inner wall groove-shaped scratch defects; carrying out three-stage evaluation on the continuous pipe containing the outer wall groove-shaped scratch defects and the inner wall groove-shaped scratch defects; therefore, the method makes up the defect of the fatigue life evaluation of the conventional continuous pipe containing the groove defects, saves the cost, increases the economic benefit, reduces the use risk of the continuous pipe, and has great production practice significance.
Drawings
FIG. 1 is a flow chart of a method for evaluating the fatigue life of a continuous pipe containing groove-shaped scratch defects;
FIG. 2 is a schematic three-dimensional half-section view of a groove-shaped scratch defect;
FIG. 3 is a schematic top view of a groove shaped scratch defect;
FIG. 4 is a schematic view of a coiled tubing bend deformation;
FIG. 5 is a schematic diagram of the cross-sectional force applied to the coiled tubing;
in the figure: 1. 2, continuous pipe, 2, outer wall groove shape scratch defect, and 3, inner wall groove shape scratch defect.
The specific implementation mode is as follows:
in order that those skilled in the art will better understand the technical solution of the present invention, the following detailed description of the present invention is provided in conjunction with the accompanying drawings and embodiments.
Referring to fig. 1 to 5, the method for evaluating the fatigue life of the continuous pipe containing the groove-shaped scratch defects, provided by the invention, comprises the following steps:
firstly, screening and confirming an outer wall groove-shaped scratch defect 2 and an inner wall groove-shaped scratch defect 3 on a service continuous pipe 1;
secondly, detecting the shape geometric parameters of the outer wall groove-shaped scratch defect 2 and the inner wall groove-shaped scratch defect 3;
thirdly, sensitive defect parameters of an outer wall groove-shaped scratch defect 2 and an inner wall groove-shaped scratch defect 3 are optimized;
fourthly, theoretically calculating the fatigue life of the continuous pipe 1 containing the outer wall groove-shaped scratch defects 2 and the inner wall groove-shaped scratch defects 3;
fifthly, carrying out three-level evaluation on the continuous pipe 1 containing the outer wall groove-shaped scratch defect 2 and the inner wall groove-shaped scratch defect 3;
in the second step, the defect parameters of the outer wall groove-shaped scratch defect 2 and the inner wall groove-shaped scratch defect 3 comprise a defect axial angle β, a defect depth a, a defect length c, a defect width b, a blunted fillet R around the scratch, the circumferential distribution of the defects and the circumferential distribution number of the defects, and the parameters of the outer wall groove-shaped scratch defect 2 and the inner wall groove-shaped scratch defect 3 are measured by using defect detection equipment;
in the third step, sensitive parameters of the defect axial angle β, the defect depth a, the defect length c, the defect width b, the rounding R around the scratch, the circumferential distribution of the defects and the circumferential distribution number of the defects are obtained on the basis of an orthogonal test method, wherein the sensitive parameters are the defect depth a, the defect width b, the defect axial angle β and the defect length c in sequence;
in the fourth step, on the basis of considering the sensitive parameters of the groove defects, the method for calculating the fatigue life of the continuous pipe 1 containing the groove defects comprises the following steps:
when the inner surface and the outer surface of the continuous pipe 1 have the outer wall groove-shaped scratch defects 2 and the inner wall groove-shaped scratch defects 3, the influence of the outer wall groove-shaped scratch defects 2 and the inner wall groove-shaped scratch defects 3 on the fatigue life is considered when the fatigue life model of the continuous pipe 1 is established. Obtaining radial stress of the coiled tubing 1 under the action of internal pressure based on the thick-wall cylinder theory
Figure 11154DEST_PATH_IMAGE035
Ring ofStress in the direction of
Figure 39152DEST_PATH_IMAGE036
And axial stress
Figure 627260DEST_PATH_IMAGE037
Figure 816933DEST_PATH_IMAGE038
In the formula:
Figure 716755DEST_PATH_IMAGE039
the outer radius of the continuous pipe 1 is mm;
Figure 814024DEST_PATH_IMAGE040
is the inner radius, mm;
Figure 115693DEST_PATH_IMAGE041
is the internal pressure, MPa; r is any radius, mm.
According to the stress analysis and von Mises guidelines, the critical point at which yielding occurs first is always the inner surface of the continuous pipe 1, in which case
Figure 476267DEST_PATH_IMAGE042
Figure 863386DEST_PATH_IMAGE043
According to the Remberg-Osgood elastic-plastic stress-strain relation, the total strain generated by bending action
Figure 888980DEST_PATH_IMAGE044
Is elastically strained
Figure 779575DEST_PATH_IMAGE045
And plastic strain
Figure 576630DEST_PATH_IMAGE046
And (3) the sum:
Figure 185466DEST_PATH_IMAGE047
in the formula:Dthe diameter of the continuous pipe 1 is mm;
Figure 890117DEST_PATH_IMAGE048
is the bending radius, mm;Eis the modulus of elasticity, MPa;
Figure 900798DEST_PATH_IMAGE049
yield limit, MPa.
The axial force generated by bending is the main cause of plastic strain, and the axial stress is generated under the action of internal pressure and bending
Figure 868754DEST_PATH_IMAGE050
Comprises the following steps:
Figure 964886DEST_PATH_IMAGE051
axial stress resulting from bending from the Holomon relationship of stress to plastic strain
Figure 83015DEST_PATH_IMAGE052
Hoop strain, axial strain and radial strain under internal pressure bending coupling load:
Figure 948203DEST_PATH_IMAGE053
in the formula:
Figure 87060DEST_PATH_IMAGE054
is the hoop strain;
Figure 201646DEST_PATH_IMAGE055
is the axial strain;
Figure 451362DEST_PATH_IMAGE056
is the radial strain;
Figure 436636DEST_PATH_IMAGE057
the cyclic strain hardening coefficient is MPa;
Figure 746394DEST_PATH_IMAGE058
is the cyclic strain hardening index.
In the plastic deformation process of the continuous pipe 1, the volume invariance assumption is adopted, and the equivalent plastic strain is generated under the coupling load
Figure 472911DEST_PATH_IMAGE059
Comprises the following steps:
Figure 526317DEST_PATH_IMAGE060
adopting a Brown-Miller fatigue life theoretical model, and the strain-life formula is as follows:
Figure 366097DEST_PATH_IMAGE061
Figure 846757DEST_PATH_IMAGE062
Figure 670357DEST_PATH_IMAGE063
Figure 527454DEST_PATH_IMAGE064
in order to consider the influence of other parameters except sensitive parameters on the fatigue life of the continuous tube, a correction coefficient is introduced
Figure 221741DEST_PATH_IMAGE065
Figure 873302DEST_PATH_IMAGE066
In the formula:
Figure 325143DEST_PATH_IMAGE067
the depth of the pit defect;
Figure 720352DEST_PATH_IMAGE068
the number of fatigue bendings for a continuous tube.
Maximum shear strain after introducing correction coefficient and positive strain of maximum shear strain plane:
Figure 269145DEST_PATH_IMAGE069
Figure 888346DEST_PATH_IMAGE071
in the fifth step, the continuous pipe 1 containing the groove-shaped scratch defects is subjected to three-level evaluation. Compared with the complete continuous pipe 1 under the same working condition, the direct scrapping with the fatigue life reduced by 50 percent is realized, the fine evaluation with the fatigue life reduced by 20 to 50 percent is realized, and the rough evaluation with the fatigue life reduced by less than 20 percent is realized.
The following embodiment is a specific example of the life safety evaluation of the continuous pipe containing the groove-shaped scratch defects:
a coil of 50.8mm coiled tubing being serviced by a gas field (drifting) was tested. The coiled continuous pipe has the strength of QT900 and the wall thickness of 3.96mm, is subjected to drilling and plugging operation for many times before, and has the existing length of 5210.86m and the detection length of 4633.25 m. Two groove-shaped scratch defects are detected on the outer wall surface of the continuous pipe, and the depth of the larger groove-shaped scratch defect is 1 mm.
The influence of the 6 defect parameters on the fatigue life of the continuous tube is evaluated by utilizing finite element calculation, as shown in table 1, the influence of the obtained defect depth, defect width, defect angle and defect length on the fatigue life of the continuous tube is obvious in the 6 defect parameters, and the defect depth is reduced by the maximum extent and the reduction extent is 92% in the 4 parameters. The descending amplitude of the annular distribution and the axial distribution is less than 30 percent, so the 2 defect parameters of the annular distribution and the axial distribution are not considered in the subsequent calculation and evaluation;
Figure 155379DEST_PATH_IMAGE073
as shown in Table 2 and FIGS. 2-3, four parameters of depth a of the groove-shaped defect along the outer circumferential surface, axial angle β of the pit along the axial direction, pit length c and pit width b, each of which takes four levels, were selected by the principle of the orthogonal test method16(44) Orthogonal experimental design, 16 groups of experiments are obtained. At different parameters in the tableK i Expressed at a particular leveliThe sum of the results of the following calculations,
Figure 354279DEST_PATH_IMAGE074
to be at a specific leveliThe average value of
Figure 757579DEST_PATH_IMAGE075
(ii) a Extreme difference in the tableRIs the difference between the maximum average and the minimum average of a particular parameter, i.e.
Figure 669384DEST_PATH_IMAGE076
Range of four defect parametersRAs shown in Table 2, the primary and secondary relationship of the effect of the four defect parameters on the fatigue life of the continuous tube is as follows: depth of pit>Width of pit>Pit angle>Pit length. The range of the defect depth is 120.25, and the range of the other three defect parameters is less than 50, namely the defect depth is a main control parameter influencing the fatigue life of the continuous tube.
TABLE 2 orthogonal test Table
Figure 423714DEST_PATH_IMAGE078
According to the finite element calculation result, based on a conservative algorithm, when mechanical analysis and fatigue life prediction of the continuous pipe containing the defects are carried out, the angle of the pit defects is 90 degrees. Fig. 4 is a schematic diagram of a deformation of a small section of coiled tubing containing a dimple defect, and fig. 5 is a schematic cross-sectional view thereof.MBending moment, cross-section, to which the coiled tubing is subjectedP 1Is the external pressure to which the coiled tubing is subjected,P 2is connected toThe internal pressure to which the extension pipe is subjected,r 1in order to continue the inner radius of the tube,r 2is the outer radius of the continuous tube,c i andc 0 the thickness of the defects inside and outside the continuous tube,θthe central angle of the pit defect corresponding to the cross section of the continuous tube.
As can be seen from the finite element calculation and the orthogonal experiment, the depth of the groove defect is the most sensitive parameter influencing the fatigue life of the continuous pipe. When the inner surface and the outer surface of the continuous pipe are provided with the groove-shaped defects, the influence of the groove-shaped defects on the fatigue life is considered during the establishment of the fatigue life model of the continuous pipe. Obtaining radial stress of continuous tube under internal pressure based on thick-wall cylinder theory
Figure 160725DEST_PATH_IMAGE079
Hoop stress
Figure 684111DEST_PATH_IMAGE080
And axial stress
Figure 645113DEST_PATH_IMAGE081
Figure 621160DEST_PATH_IMAGE082
In the formula:
Figure 161862DEST_PATH_IMAGE083
the outer radius of the continuous tube is mm;
Figure 805333DEST_PATH_IMAGE084
is the inner radius, mm;
Figure 547024DEST_PATH_IMAGE085
is the internal pressure, MPa; r is any radius, mm.
According to the stress analysis and von Mises guidelines, the critical point for initial yielding is always the inner surface of the coiled tubing, in which case
Figure 275946DEST_PATH_IMAGE086
Figure 354760DEST_PATH_IMAGE087
According to the Remberg-Osgood elastic-plastic stress-strain relation, the total strain generated by bending action
Figure 383896DEST_PATH_IMAGE088
Is elastically strained
Figure 889964DEST_PATH_IMAGE089
And plastic strain
Figure 106182DEST_PATH_IMAGE090
And (3) the sum:
Figure 988687DEST_PATH_IMAGE091
in the formula:Dis the outer diameter of the continuous tube, mm;
Figure 996963DEST_PATH_IMAGE092
is the bending radius, mm;Eis the modulus of elasticity, MPa;
Figure 939511DEST_PATH_IMAGE093
yield limit, MPa.
The axial force generated by bending is the main cause of plastic strain, and the axial stress is generated under the action of internal pressure and bending
Figure 377446DEST_PATH_IMAGE094
Comprises the following steps:
Figure 798063DEST_PATH_IMAGE095
axial stress resulting from bending from the Holomon relationship of stress to plastic strain
Figure 801791DEST_PATH_IMAGE096
Hoop strain under bending coupling load under internal pressureAxial strain and radial strain:
Figure 649661DEST_PATH_IMAGE097
in the formula:
Figure 574892DEST_PATH_IMAGE098
is the hoop strain;
Figure 799200DEST_PATH_IMAGE099
is the axial strain;
Figure 532801DEST_PATH_IMAGE100
is the radial strain;
Figure 817152DEST_PATH_IMAGE101
the cyclic strain hardening coefficient is MPa;
Figure 229678DEST_PATH_IMAGE102
is the cyclic strain hardening index.
In the plastic deformation process of the continuous pipe, the volume invariance assumption is adopted, and the equivalent plastic strain is generated under the coupling load
Figure 523257DEST_PATH_IMAGE103
Comprises the following steps:
Figure 704839DEST_PATH_IMAGE104
adopting a Brown-Miller fatigue life theoretical model, and the strain-life formula is as follows:
Figure 160091DEST_PATH_IMAGE105
Figure 59914DEST_PATH_IMAGE106
maximum shear strain:
Figure 281817DEST_PATH_IMAGE107
positive strain at maximum shear strain plane:
Figure 317906DEST_PATH_IMAGE108
on one hand, during theoretical calculation, the fatigue life of the groove-shaped defect of the continuous pipe is only calculated based on a conservative algorithm, and on the other hand, the lowest yield strength (the yield strength of the continuous pipe in engineering practice is higher than the minimum value) is selected during calculation, so that the predicted value of the fatigue life of the groove-shaped defect of the continuous pipe is smaller than an experimental value, and in order to enable the calculation result of a theoretical model to be more accurate, a correction coefficient is obtained by comparing and regressing the experimental value and the theoretical calculation result
Figure 944059DEST_PATH_IMAGE109
Figure 331178DEST_PATH_IMAGE110
In the formula:c 0 the depth of the pit defect;N f the number of fatigue bendings for a continuous tube.
Corrected maximum shear strain and positive strain of the maximum shear strain plane:
Figure 966559DEST_PATH_IMAGE111
the fatigue life model after correction is:
Figure 122734DEST_PATH_IMAGE112
the model calculation results for different defect depths are shown in table 3:
TABLE 3 model calculation results at different defect depths
Figure 919789DEST_PATH_IMAGE113
In the fifth step, the continuous pipe 1 containing the groove-shaped scratch defects is subjected to three-level evaluation. Compared with the complete continuous pipe 1 under the same working condition, the direct scrapping with the fatigue life reduced by 50 percent is realized, the fine evaluation with the fatigue life reduced by 20 to 50 percent is realized, and the rough evaluation with the fatigue life reduced by less than 20 percent is realized.
TABLE 4 evaluation ratings at different defect depths
Figure 528625DEST_PATH_IMAGE115
The foregoing is only a preferred embodiment of the present invention, and it should be noted that, for those skilled in the art, various modifications and decorations can be made without departing from the principle of the present invention, and these modifications and decorations should also be regarded as the protection scope of the present invention.

Claims (2)

1. A method for evaluating the fatigue life of a continuous tube containing groove-shaped scratch defects is characterized by comprising the following steps:
1) screening and confirming the outer wall groove-shaped scratch defects (2) and the inner wall groove-shaped scratch defects (3) in the service continuous pipe (1);
2) detecting the shape and geometric parameters of the outer wall groove-shaped scratch defect (2) and the inner wall groove-shaped scratch defect (3), wherein the defect parameters of the outer wall groove-shaped scratch defect (2) and the inner wall groove-shaped scratch defect (3) comprise a defect axial angle β, a defect depth a, a defect length c, a defect width b, a blunted fillet R around the scratch, the circumferential distribution of the defects and the circumferential distribution number of the defects, and the parameters of the outer wall groove-shaped scratch defect (2) and the inner wall groove-shaped scratch defect (3) are measured by using defect detection equipment;
3) sensitive defect parameters of the outer wall groove-shaped scratch defect (2) and the inner wall groove-shaped scratch defect (3) are preferably selected, and the sensitive parameters are obtained from sensitive parameters in defect axial angle β, defect depth a, defect length c, defect width b, blunt fillet R around the scratch, circumferential distribution of the defects and the circumferential distribution number of the defects based on an orthogonal test method, wherein the sensitive parameters are the defect depth a, the defect width b, the defect axial angle β and the defect length c in sequence;
4) theoretically calculating the fatigue life of a continuous tube (1) containing an outer wall groove-shaped scratch defect (2) and an inner wall groove-shaped scratch defect (3) on the basis of referring to groove-shaped defect sensitive parameters;
5) carrying out three-level evaluation on the continuous pipe (1) containing the outer wall groove-shaped scratch defect (2) and the inner wall groove-shaped scratch defect (3); namely, carrying out three-stage evaluation on the continuous pipe containing the groove-shaped scratch defects; compared with a complete continuous pipe under the same working condition, the direct scrapping of the pipe with the fatigue life reduced by 50 percent is realized, the fine evaluation of the reduction of the fatigue life by 20 to 50 percent is realized, and the rough evaluation of the reduction of the fatigue life by less than 20 percent is realized.
2. The method for evaluating the fatigue life of the continuous tube containing the groove-shaped scratch defects according to claim 1, wherein: the method for calculating the fatigue life of the continuous tube (1) containing the outer wall groove-shaped scratch defects (2) and the inner wall groove-shaped scratch defects (3) comprises the following steps:
when the inner surface and the outer surface of the continuous pipe (1) are provided with the outer wall groove-shaped scratch defects (2) and the inner wall groove-shaped scratch defects (3), when a fatigue life model of the continuous pipe (1) is established, the influence of the outer wall groove-shaped scratch defects (2) and the inner wall groove-shaped scratch defects (3) on the fatigue life is considered, and the radial stress of the continuous pipe (1) under the action of internal pressure is obtained based on the thick-wall cylinder theory
Figure 236426DEST_PATH_IMAGE001
Hoop stress
Figure 478051DEST_PATH_IMAGE002
And axial stress
Figure 549912DEST_PATH_IMAGE003
Figure 927804DEST_PATH_IMAGE004
In the formula:
Figure 528550DEST_PATH_IMAGE005
the outer radius of the continuous pipe (1) is mm;
Figure 991892DEST_PATH_IMAGE006
is the inner radius, mm;
Figure 742810DEST_PATH_IMAGE007
is the internal pressure, MPa; r is any radius, mm;
according to the analysis of stress andvon Misesthe criterion is that the critical point for yielding first always is the inner surface of the continuous pipe (1), in which case
Figure 240788DEST_PATH_IMAGE008
Figure 746856DEST_PATH_IMAGE009
According to the Remberg-Osgood elastic-plastic stress-strain relation, the total strain generated by bending action
Figure 963073DEST_PATH_IMAGE010
Is elastically strained
Figure 376737DEST_PATH_IMAGE011
And plastic strain
Figure 729221DEST_PATH_IMAGE012
And (3) the sum:
Figure 406190DEST_PATH_IMAGE013
in the formula:Dthe diameter of the outer diameter of the continuous pipe (1) is mm;
Figure 844125DEST_PATH_IMAGE014
is the bending radius, mm;Eis the modulus of elasticity, MPa;
Figure 183183DEST_PATH_IMAGE015
yield limit, MPa;
the axial force generated by bending is the main cause of plastic strain, and the axial stress is generated under the action of internal pressure and bending
Figure 390174DEST_PATH_IMAGE016
Comprises the following steps:
Figure 503623DEST_PATH_IMAGE017
axial stress resulting from bending from the Holomon relationship of stress to plastic strain
Figure 960012DEST_PATH_IMAGE018
Hoop strain, axial strain and radial strain under internal pressure bending coupling load:
Figure 184320DEST_PATH_IMAGE019
in the formula:
Figure 511397DEST_PATH_IMAGE020
is the hoop strain;
Figure 795747DEST_PATH_IMAGE021
is the axial strain;
Figure 349220DEST_PATH_IMAGE022
is the radial strain;
Figure 377218DEST_PATH_IMAGE023
the cyclic strain hardening coefficient is MPa; is the cyclic strain hardening index;
in the plastic deformation process of the continuous pipe (1), the equivalent plastic strain under the coupling load is adopted on the assumption of constant volume
Figure 558801DEST_PATH_IMAGE024
Comprises the following steps:
Figure 14053DEST_PATH_IMAGE025
adopting a Brown-Miller fatigue life theoretical model, and the strain-life formula is as follows:
Figure 445035DEST_PATH_IMAGE026
Figure 11145DEST_PATH_IMAGE027
maximum shear strain:
Figure 47234DEST_PATH_IMAGE028
positive strain at maximum shear strain plane:
Figure 673388DEST_PATH_IMAGE029
in order to consider the influence of other parameters except sensitive parameters on the fatigue life of the continuous tube, a correction coefficient is introduced
Figure 450720DEST_PATH_IMAGE030
Figure 820521DEST_PATH_IMAGE031
In the formula:c 0 the depth of the pit defect;N f the number of fatigue bending times of the continuous tube;
maximum shear strain after introducing correction coefficient and positive strain of maximum shear strain plane:
Figure 976696DEST_PATH_IMAGE032
the final fatigue life calculation model of the continuous pipe (1) containing the defects is as follows:
Figure 304909DEST_PATH_IMAGE033
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