CN114491760A - Method and device for calculating installation angle of anchor pull rod - Google Patents

Method and device for calculating installation angle of anchor pull rod Download PDF

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CN114491760A
CN114491760A CN202210111126.0A CN202210111126A CN114491760A CN 114491760 A CN114491760 A CN 114491760A CN 202210111126 A CN202210111126 A CN 202210111126A CN 114491760 A CN114491760 A CN 114491760A
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霍学晋
王东绪
杨明芳
汪珍
陈佳
苗润池
刘芸欣
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China Railway Major Bridge Reconnaissance and Design Institute Co Ltd
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China Railway Major Bridge Reconnaissance and Design Institute Co Ltd
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Abstract

The invention relates to a method and a device for calculating an installation angle of an anchor pull rod, which comprises the steps of obtaining theoretical vertex coordinates of a scattered cable saddle and coordinates of a wire strand anchoring point, and calculating a tangent angle of a flat bending end point of the wire strand and a tangent angle of an initial vertical bending end point of the wire strand according to the theoretical vertex coordinates of the scattered cable saddle and the coordinates of the wire strand anchoring point; acquiring the total balance force of the main side-span cable, and calculating the tension of each strand according to the strand flat-bent end point chamfer, the strand initial vertical-bent end point chamfer and the total balance force of the main side-span cable; traversing each strand, and iteratively calculating the unstressed length of the suspended section of the strand and the coordinates of the upper end part of the anchor pull rod of the strand according to the coordinates of the anchor point of the strand, the tangent angle of the flat bent end point of the strand, the tangent angle of the initial vertical bent end point of the strand, the tension of each strand and the vertical position of the strand in the saddle groove; and calculating the installation angle of the anchor rod according to the iteratively calculated coordinates of the upper end part of the strand anchor rod. Meanwhile, the problem that the stress-free length of the suspension section strand in the related technology is inaccurate to calculate can be solved.

Description

Method and device for calculating installation angle of anchor pull rod
Technical Field
The invention relates to the technical field of suspension bridge design, in particular to a method and a device for calculating an installation angle of an anchor pull rod.
Background
At present, when a suspension bridge is designed, the installation angle of each anchor pull rod needs to be calculated and is reflected on a design drawing. The construction of the suspension bridge anchor span is very complex, and is reflected in the following 3 aspects: 1) due to the anchoring requirement, the cable strand is in a space scattering state in the anchoring span; 2) the cable saddle is a complex space body consisting of a plurality of vertical curved circular arcs and flat curved circular arcs with different radiuses, so that each strand has different vertical curved end points and flat curved end points; 3) the end part of the cable strand is anchored by a steel anchor pull rod, the anchor pull rod is in an inclined state, and the inclined installation angles are different. Due to the complex structure, the accurate analysis of the suspension bridge anchor span is extremely complex, the installation angle of the anchor pull rod, the stress-free length of the suspension section of the wire strand, the positions of the vertical bending end point and the horizontal bending end point of the cable saddle, the tension force of the wire strand and the like are mutually associated and coupled, and any change can cause other changes along with the change.
In the related art, a simplified method is adopted for calculation of the installation angle of the anchor rod, and no accurate analysis method and related research exist. The simplified method is to take the straight line angle of the anchor point (the lower end point of the anchor rod, given by design) of the anchor surface after connecting the IP point of the cable saddle and the strand as the installation angle of the anchor rod, and the simplified method has the following problems:
(1) the state of the suspension section of the wire strand in the anchor span under the action of self weight is a catenary instead of a straight line, so that the tangential direction of the end force of the wire strand is deviated from the installation angle of the anchor pull rod, the steel anchor pull rod generates additional bending moment, the stress is not good, and the catenary is replaced by the straight line, so that the calculation of the stress-free length of the wire strand in the suspension section is inaccurate;
(2) the accurate coordinates of the vertical bending end point and the horizontal bending end point of each strand cannot be obtained, and the stress-free length of the closely-attached section of the strand and the saddle groove in the scattered cable saddle groove cannot be accurately calculated, so that the blanking length of the full-bridge strand has errors;
(3) the sum of the component force of the tension of each wire strand of the anchor span obtained by calculation on the inclined surface of the cable saddle is unequal to the component force of the main cable of the side span, so that the cable saddle still can slide on the inclined surface, the tension of each wire strand of the anchor span can be redistributed after sliding, the tension of each wire strand is finally unequal, and the overall safety coefficient of the anchor span is reduced.
Disclosure of Invention
The embodiment of the invention provides a method and a device for calculating an anchor rod installation angle, which are used for calculating the anchor rod installation angle and solving the problem of inaccurate calculation of the stress-free length of a suspension section strand in the related technology.
The embodiment of the invention provides a method for calculating an installation angle of an anchor pull rod, which is characterized by comprising the following steps:
acquiring theoretical vertex coordinates of the scattered cable saddle and coordinates of a strand anchoring point, and calculating a strand flat bending end point chamfer and a strand initial vertical bending end point chamfer according to the theoretical vertex coordinates of the scattered cable saddle and the coordinates of the strand anchoring point;
acquiring the total balance force of the main side-span cable, and calculating the tension of each strand according to the strand flat-bent end point chamfer, the strand initial vertical-bent end point chamfer and the total balance force of the main side-span cable;
traversing each strand, and iteratively calculating the unstressed length of the suspended section of the strand and the coordinates of the upper end part of the anchor pull rod of the strand according to the coordinates of the anchor point of the strand, the tangent angle of the flat bent end point of the strand, the tangent angle of the initial vertical bent end point of the strand, the tension of each strand and the vertical position of the strand in the saddle groove;
and calculating the installation angle of the anchor rod according to the iteratively calculated coordinates of the upper end part of the strand anchor rod.
In some embodiments, before acquiring the theoretical vertex coordinates of the saddle and the coordinates of the anchor points of the strands, the method further comprises the following steps:
defining a global coordinate system OXYZ, wherein the Y axis of the global coordinate system is vertically upward;
defining a local coordinate system oxyz, wherein the origin of the local coordinate system is an intersection point o of a vertical line and a slip plane when the theoretical vertex of the cable saddle makes the vertical line towards the slip plane, and the y-axis direction of the local coordinate system is the self-weight direction of a catenary cable;
definition of saddle seatMarker system
Figure RE-GDA0003582439680000021
The saddle local coordinate system is obtained by rotating the local coordinate system around the horizontal z-axis of the saddle counterclockwise by an angle beta, and
said local coordinate system oxyz is directed to saddle local coordinate system
Figure RE-GDA0003582439680000031
Is a conversion matrix of
Figure RE-GDA0003582439680000032
Figure RE-GDA0003582439680000033
Defining a local coordinate system of the anchor surface of the strand, and enabling a conversion matrix of the local coordinate system of the anchor surface of the strand and the overall coordinate system OXYZ to be
Figure RE-GDA0003582439680000034
Local coordinate system of saddle
Figure RE-GDA0003582439680000035
The theoretical vertex coordinates of the cable saddle are
Figure RE-GDA0003582439680000036
Figure RE-GDA0003582439680000037
And is
Figure RE-GDA0003582439680000038
Wherein beta is the angle of inclination of the slip plane, (X)ip、 Yip、Zip) The coordinates of the theoretical vertex of the cable saddle are (X) under the overall coordinate system OXYZo、 Yo、Zo) The coordinate of the o point under the overall coordinate system OXYZ is shown;
saddle local coordinate system
Figure RE-GDA0003582439680000039
The coordinates of the anchoring point of the silk strand are
Figure RE-GDA00035824396800000310
And is
Figure RE-GDA00035824396800000311
Wherein (X)0i、Y0i、Z0i) The coordinates of the strand anchoring points under the overall coordinate system OXYZ are adopted, and
Figure RE-GDA00035824396800000312
wherein
Figure RE-GDA00035824396800000313
Is TmTranspose matrix of (x'0i、y′0i、z′0i) For a predetermined strand anchoring point in said strand anchoring surface local coordinate system WmThe lower coordinate, i is 1 to N, N is the total number of strands, (X)m、Ym、Zm) The coordinates of the center of the anchor surface under the overall coordinate system OXYZ are shown.
In some embodiments, the calculating the strand flat bend end point chamfer and the strand initial vertical bend end point chamfer according to the scattered cable saddle theoretical vertex coordinates and the strand anchoring point coordinates comprises the following steps:
establish the equation Ax2+ Bx + C is 0, and
A=1+a2,B=2×(a×b-a×xpc-zpc),
Figure RE-GDA0003582439680000041
Figure RE-GDA0003582439680000042
solving an equation to obtain the flat bent end of each strand at the anchor span sideTransverse coordinate z of pointpiAccording to
Figure RE-GDA0003582439680000043
Solving strand flat-bending end point tangent angle theta of No. i strandiWherein
RhIs the flat bending radius of the cable saddle groove, xpcAnd zpcRespectively the ordinate and abscissa of the circle center of the flat curved arc, z0siThe transverse position of the strand in the saddle groove;
the method for calculating the initial vertical bending end point chamfer angle of the strand according to the theoretical vertex coordinate of the scattered cable saddle and the anchor point coordinate of the strand comprises the following steps:
according to
Figure RE-GDA0003582439680000044
Calculating the initial vertical bending end point cutting angle gamma of the No. i strandi
In some embodiments, obtaining the total balance force of the side span main cable and calculating the tension of each strand according to the tangent angle of the flat bending end point of each strand and the tangent angle of the initial vertical bending end point of each strand comprises the following steps:
step 01, according to FR=FXRcosβ+FYRsinβ、FL=FRAnd
Figure RE-GDA0003582439680000045
calculating the component force F of the main cable force along the sliding surfaceRThe total balance force F of the side span main cableLAnd the tension f of each strandiWherein F isXRLongitudinal component of tension force of main cable across side span, FYRIs the vertical component of the tension force of the side span main cable.
In some embodiments, traversing each strand, and iteratively calculating the unstressed length of the strand suspended section and the coordinates of the upper end of the strand anchor rod according to the coordinates of the strand anchor point, the strand horizontal bend end point cut angle, the strand initial vertical bend end point cut angle, the tension of each strand and the vertical position of the strand in the saddle groove comprises the following steps:
step 02: selecting No. i silk strand, setting the first middleVariables of
Figure RE-GDA0003582439680000046
And an iteration variable γ; cutting the vertical bent end point of the No. i silk strand into an angle gammaiTo the intermediate variable
Figure RE-GDA0003582439680000051
And combining the first intermediate variable
Figure RE-GDA0003582439680000052
To the iteration variable γ;
step 03: according to
Figure RE-GDA0003582439680000053
And
Figure RE-GDA0003582439680000054
and
Figure RE-GDA0003582439680000055
fh=fxl/cos(atan(fzl/fxl) And f) andv=fylcalculating the resultant force f of the selected strand on the horizontal planehAnd resultant force f in the vertical directionvWherein
Figure RE-GDA0003582439680000056
Is TZThe transposed matrix of (2);
step 04: calculating the coordinates of the tail points of the vertical bends of the wire strands according to the vertical bend radius of the cable scattering saddle groove, the central angle corresponding to the circular arc section of the vertical bend line of the saddle groove and the vertical position of the wire strands in the saddle groove;
step 05: iteratively calculating the initial unstressed length S of the suspended section of the strand according to the coordinates of the anchoring point of the strand, the coordinates of the vertical bending end point of the strand, the resultant force of the selected strand on the horizontal plane and the resultant force of the selected strand in the vertical direction0And the current unstressed length S of the strand suspended section;
step 06: judgment of | (S-S)0)/S0If the | meets the preset precision, if so, determining whether the | meets the preset precisionAccording to
Figure RE-GDA0003582439680000057
Calculating a first vertical position difference delta h of the wire strand at the upper end part of the anchor rod1Otherwise, assigning the value of the current unstressed length S to the initial unstressed length S0Then returns to step 02ExecuteStep 02 to step 05;
step 07: setting a second intermediate variable
Figure RE-GDA0003582439680000058
And make
Figure RE-GDA0003582439680000059
And is
Figure RE-GDA00035824396800000510
Then returning to step 02 to execute step 02 to step 06 according to the method
Figure RE-GDA00035824396800000511
Calculating the second vertical position difference delta h of the wire strand at the upper end part of the anchor rod2
And step 08: setting a third intermediate variable
Figure RE-GDA00035824396800000512
And make
Figure RE-GDA00035824396800000513
And is
Figure RE-GDA00035824396800000514
Then returning to step 02 and executing steps 02 to 06, according to
Figure RE-GDA00035824396800000515
Calculating the third vertical position difference delta h of the wire strand at the upper end part of the anchor rod0Wherein y issiIs the vertical coordinate, L, of the end point of the selected vertical bend of the strand in the local coordinate system oxyzmgiIs the anchor rod length;
step 09: judgment of
Figure RE-GDA00035824396800000516
If the preset precision is met, terminating the iteration if the preset precision is met, otherwise, enabling the iteration to be ended
Figure RE-GDA0003582439680000061
Δh1=Δh2And Δ h2=Δh0Then, the step 02 is returned to and the steps 02 to 08 are executed:
step 10: according to xmi=xsi-Lcos(atan((zsi-z0i)/(xsi-x0i)))、ymi=ysi+ H and zmi=zsi+Lsin(atan((zsi-z0i)/(xsi-x0i) )) calculating coordinates (x) of the upper end of the strand anchor rodmi、 ymi、zmi) And taking the current value of the iteration variable gamma as the final vertical bending end point cutting angle of the No. i strand, and taking the current unstressed length S calculated by iteration as the unstressed length of the final strand suspended section of the No. i strand.
In some embodiments, traversing each strand, and iteratively calculating the unstressed length of the strand suspended section and the coordinates of the upper end of the strand anchor rod according to the coordinates of the strand anchor point, the strand horizontal bend end point cut angle, the strand initial vertical bend end point cut angle, the tension of each strand and the vertical position of the strand in the saddle groove comprises the following steps:
updating the final strand vertical bending end point tangent angle value calculated by the current iteration to gammaiAnd will update gammaiSubstitution into
Figure RE-GDA0003582439680000062
Obtaining an iteratively calculated side span main cable total balance force F'L
In | (F'L-FL)/FLIf the | does not meet the preset precision, the updated gamma is usediGo back to step 01 to calculate updated FLAnd fiAnd with said updated gammai、FLAnd fiThe loop from step 02 to step 10 is entered.
In some embodiments, the step 04 comprises the steps of:
supposing that the saddle groove vertical bending line consists of n sections of circular arcs, and enabling the vertical bending radius R of the cable scattering saddle groove corresponding to each section of circular arcvIs represented by RvkWherein k is an integer from 1 to n;
making the R tovkThe corresponding central angle is denoted by phikAnd according to Rki=Rvk+DiCalculating the vertical bending radius R of the No. i strand in the saddle groovekiWherein D isiThe vertical height of the No. i silk strand on the section of the main cable is defined;
when gamma is less than or equal to phi1According to
Figure RE-GDA0003582439680000063
Calculating the ordinate of the end point of the vertical bend of the selected strand
Figure RE-GDA0003582439680000064
And vertical coordinate
Figure RE-GDA0003582439680000065
When phi is1<γ≤φ12According to
Figure RE-GDA0003582439680000071
Calculating the ordinate of the end point of the vertical bend of the selected strand
Figure RE-GDA0003582439680000072
And vertical coordinate
Figure RE-GDA0003582439680000073
When phi is12<γ≤φ123According to
Figure RE-GDA0003582439680000074
Calculating the end point of the vertical bend of the selected strandOrdinate of the curve
Figure RE-GDA0003582439680000075
And vertical coordinate
Figure RE-GDA0003582439680000076
When phi is123When < gamma, according to
Figure RE-GDA0003582439680000077
Calculating the ordinate of the end point of the vertical bend of the selected strand
Figure RE-GDA0003582439680000078
And vertical coordinate
Figure RE-GDA0003582439680000079
According to
Figure RE-GDA00035824396800000710
Calculating the abscissa of the end point of the vertical bend of the selected strand
Figure RE-GDA00035824396800000711
According to
Figure RE-GDA00035824396800000712
Will be in the saddle local coordinate system
Figure RE-GDA00035824396800000713
Coordinates of vertical bending end point of lower selected strand
Figure RE-GDA00035824396800000714
Converting the position of the filament to a local coordinate system oxyz to obtain the coordinates (x) of the end point of the vertical bend of the selected filament under the local coordinate system oxyzsi、ysi、zsi)。
In some embodiments, said step 05 comprises the steps of:
according to
Figure RE-GDA00035824396800000715
Calculating the initial unstressed length S of the suspended section of the strand0Wherein L ismgiFor the anchor rod length, (x)0i、y0i、z0i) Is the coordinate of the lower strand anchoring point of the local coordinate system oxyz, (x)si、ysi、zsi) The coordinates of the vertical bent end points of the lower strands of the local coordinate system oxyz are obtained;
according to f'v=fv-ωS0And f'h=fhCalculating the vertical force f 'of the wire strand at the upper end of the anchor rod'vAnd resultant force in the horizontal plane f'hAccording to
Figure RE-GDA00035824396800000716
Calculating the inclination angle of the upper end of the anchor rod
Figure RE-GDA00035824396800000717
According to
Figure RE-GDA00035824396800000718
Calculating the horizontal projection length L of the silk strands;
according to
Figure RE-GDA0003582439680000081
And calculating the current unstressed length S and the vertical projection length H of the strands, wherein EA is the tensile rigidity of the strands, and omega is the bulk density of the main cable.
In some embodiments, the calculating the anchor rod installation angle from the iteratively calculated upper end coordinates of the strand anchor rod includes the steps of:
according to
Figure RE-GDA0003582439680000082
Converting the coordinates of the upper end part of the strand anchor rod into an integral coordinate system OXYZ, and performing transformation according to lambda on the integral coordinate system OXYZ1=atan((Ymi-Y0i)/Xmi)、λ2=atan((Zmi-Z0i)/Xmi) And λ3=atan(tan(λ1)/cos(λ2) Calculating the anchor rod installation angle, where λ1Is the included angle between the projection of the anchor pull rod on the XY plane and the X axis, lambda2Is the included angle between the projection of the anchor rod on the XZ plane and the X axis, lambda3Is the angle between the anchor rod and the XZ plane.
In a second aspect, an embodiment of the present invention provides an apparatus for calculating an installation angle of an anchor rod, where the apparatus includes: the iteration initial value acquisition module is used for acquiring theoretical vertex coordinates of the scattered cable saddle and coordinates of the anchoring points of the strands and calculating tangent angles of the flat bending end points of the strands and the initial vertical bending end points of the strands according to the theoretical vertex coordinates of the scattered cable saddle and the coordinates of the anchoring points of the strands;
an iterative computation module to:
acquiring the total balance force of the main side-span cable, and calculating the tension of each strand according to the strand flat-bent end point chamfer, the strand initial vertical-bent end point chamfer and the total balance force of the main side-span cable;
traversing each strand, and iteratively calculating the unstressed length of the suspended section of the strand and the coordinates of the upper end part of the anchor pull rod of the strand according to the coordinates of the anchor point of the strand, the tangent angle of the flat bent end point of the strand, the tangent angle of the initial vertical bent end point of the strand, the tension of each strand and the vertical position of the strand in the saddle groove;
the mounting angle calculation module is used for calculating the mounting angle of the anchor rod according to the iteratively calculated coordinates of the upper end part of the strand anchor rod;
the iteration initial value obtaining module is further configured to:
defining a global coordinate system OXYZ, wherein the Y axis of the global coordinate system is vertically upward;
defining a local coordinate system oxyz, wherein the origin of the local coordinate system is an intersection point o of a vertical line and a slip plane when the theoretical vertex of the cable saddle makes the vertical line towards the slip plane, and the y-axis direction of the local coordinate system is the self-weight direction of a catenary cable;
defining a saddle local coordinate system
Figure RE-GDA0003582439680000091
The saddle local coordinate system is obtained by rotating the local coordinate system around the horizontal z-axis of the saddle counterclockwise by an angle beta, and
the local coordinate system oxyz is towards saddle local coordinate system
Figure RE-GDA0003582439680000092
Is a conversion matrix of
Figure RE-GDA0003582439680000093
Figure RE-GDA0003582439680000094
Defining a local coordinate system of the anchor surface of the strand, and enabling a conversion matrix of the local coordinate system of the anchor surface of the strand and the overall coordinate system OXYZ to be
Figure RE-GDA0003582439680000095
Local coordinate system of saddle
Figure RE-GDA0003582439680000096
The theoretical vertex coordinates of the scattered cable saddle are
Figure RE-GDA0003582439680000097
Figure RE-GDA0003582439680000098
And is provided with
Figure RE-GDA0003582439680000099
Wherein beta is the angle of inclination of the slip plane, (X)ip、 Yip、Zip) The coordinates of the theoretical vertex of the cable saddle are (X) under the overall coordinate system OXYZo、 Yo、Zo) The coordinate of the o point under the overall coordinate system OXYZ is shown;
saddle local coordinate system
Figure RE-GDA00035824396800000910
The coordinates of the anchoring point of the strand are
Figure RE-GDA00035824396800000911
And is
Figure RE-GDA00035824396800000912
Wherein (X)0i、Y0i、Z0i) The coordinates of the strand anchoring point under the global coordinate system OXYZ, and
Figure RE-GDA0003582439680000101
wherein
Figure RE-GDA0003582439680000102
Is TmTranspose matrix of (x'0i、y′0i、z′0i) For a predetermined strand anchoring point in said strand anchoring surface local coordinate system WmThe lower coordinate, i is 1 to N, N is the total number of strands, (X)m、Ym、 Zm) The coordinates of the center of the anchor surface under the overall coordinate system OXYZ are taken as the coordinates;
establish the equation Ax2+ Bx + C is 0, and
A=1+a2,B=2×(a×b-a×xpc-zpc),
Figure RE-GDA0003582439680000103
Figure RE-GDA0003582439680000104
solving an equation to obtain the transverse coordinate z of each strand flat-bending end point on the anchor span sidepiAnd according to
Figure RE-GDA0003582439680000105
Solving strand flat-bending end point tangent angle theta of No. i strandiWherein
RhIs the flat bending radius of the cable saddle groove, xpcAnd zpcRespectively the ordinate and abscissa of the circle center of the flat curved arc, z0siThe transverse position of the strand in the saddle groove;
according to
Figure RE-GDA0003582439680000106
Calculating the initial vertical bending end point cutting angle gamma of the No. i strandi
The iterative computation module is further configured to: performing the following steps 01 to 10;
the step 01 comprises the following steps: according to FR=FXRcosβ+FYRsinβ、FL=FRAnd
Figure RE-GDA0003582439680000107
calculating the component force F of the main cable force along the sliding surfaceRThe total balance force F of the side span main cableLAnd the tension f of each strandiWherein F isXRLongitudinal component of tension force of main cable across side span, FYRVertical component force of the tension force of the side span main cable;
step 02 includes: selecting No. i silk strand, setting the first intermediate variable
Figure RE-GDA0003582439680000108
And an iteration variable γ; cutting the vertical bent end point of the No. i silk strand into an angle gammaiIs assigned to the intermediate variable
Figure RE-GDA0003582439680000109
And combining the first intermediate variable
Figure RE-GDA00035824396800001010
To the iteration variable γ;
step 03 comprises: according to
Figure RE-GDA0003582439680000111
And
Figure RE-GDA0003582439680000112
and
Figure RE-GDA0003582439680000113
fh=fxl/cos(atan(fzl/fxl) And f) andv=fylcalculating the resultant force f of the selected strand on the horizontal planehAnd resultant force f in the vertical directionvWherein
Figure RE-GDA0003582439680000114
Is TZThe transposed matrix of (2);
step 04 comprises: calculating the coordinates of the tail points of the vertical bends of the strands according to the vertical bend radius of the cable scattering saddle groove, the central angle corresponding to the arc section of the vertical bend line of the saddle groove and the vertical position of the strands in the saddle groove;
step 05 comprises: iteratively calculating the initial unstressed length S of the suspended section of the strand according to the coordinates of the anchoring point of the strand, the coordinates of the vertical bent end point of the strand, the resultant force of the selected strand on the horizontal plane and the resultant force of the selected strand in the vertical direction0And the current unstressed length S of the strand suspended section;
step 06 comprises: judgment of | (S-S)0)/S0If | satisfies the preset precision, if yes, according to
Figure RE-GDA0003582439680000115
Calculating a first vertical position difference delta h of the wire strand at the upper end part of the anchor rod1Otherwise, assigning the value of the current unstressed length S to the initial unstressed length S0Then returns to step 02ExecuteStep 02 to step 05;
step 07 includes: setting a second intermediate variable
Figure RE-GDA0003582439680000116
And make
Figure RE-GDA0003582439680000117
And is
Figure RE-GDA0003582439680000118
Then returning to step 02 to execute step 02 to step 06 according to the method
Figure RE-GDA0003582439680000119
Calculating the second vertical position difference delta h of the wire strand at the upper end part of the anchor rod2
Step 08 comprises: setting a third intermediate variable
Figure RE-GDA00035824396800001110
And make it possible to
Figure RE-GDA00035824396800001111
And is
Figure RE-GDA00035824396800001112
Then returning to step 02 and executing steps 02 to 06, according to
Figure RE-GDA00035824396800001113
Calculating the third vertical position difference delta h of the wire strand at the upper end part of the anchor rod0Wherein y issiIs the vertical coordinate, L, of the end point of the selected vertical bend of the strand in the local coordinate system oxyzmgiIs the anchor rod length;
step 09 includes: judgment of
Figure RE-GDA00035824396800001114
If the preset precision is met, terminating the iteration if the preset precision is met, otherwise, enabling the iteration to be ended
Figure RE-GDA00035824396800001115
Δh1=Δh2And Δ h2=Δh0Then returning to the step 02 and executing the step 02 to the step 08;
the step 10 comprises: according to xmi=xsi-Lcos(atan((zsi-z0i)/(xsi-x0i)))、ymi=ysi+ H and zmi=zsi+Lsin(atan((zsi-z0i)/(xsi-x0i) )) calculating coordinates (x) of the upper end of the strand anchor rodmi、ymi、zmi) Taking the current value of the iteration variable gamma as the final vertical bending end point cutting angle of the No. i strand, and taking the current unstressed length S calculated by iteration as the unstressed length of the final strand suspended section of the No. i strand;
the step 04 comprises the steps of:
supposing that the saddle groove vertical bending line consists of n sections of circular arcs, and enabling the vertical bending radius R of the cable scattering saddle groove corresponding to each section of circular arcvIs represented by RvkWherein k is an integer from 1 to n;
making the R tovkThe corresponding central angle is denoted by phikAnd according to Rki=Rvk+DiCalculating the vertical bending radius R of the No. i strand in the saddle groovekiWherein D isiThe vertical height of the No. i silk strand on the section of the main cable is defined;
when gamma is less than or equal to phi1According to
Figure RE-GDA0003582439680000121
Calculating the ordinate of the end point of the vertical bend of the selected strand
Figure RE-GDA0003582439680000122
And vertical coordinate
Figure RE-GDA0003582439680000123
When phi is1<γ≤φ12According to
Figure RE-GDA0003582439680000124
Calculating the ordinate of the end point of the vertical bend of the selected strand
Figure RE-GDA0003582439680000125
And vertical coordinate
Figure RE-GDA0003582439680000126
When phi is12<γ≤φ123According to
Figure RE-GDA0003582439680000127
Calculating the ordinate of the end point of the vertical bend of the selected strand
Figure RE-GDA0003582439680000128
And vertical coordinate
Figure RE-GDA0003582439680000129
When phi is123When < gamma, according to
Figure RE-GDA00035824396800001210
Calculating the ordinate of the end point of the vertical bend of the selected strand
Figure RE-GDA00035824396800001211
And vertical coordinate
Figure RE-GDA00035824396800001212
According to
Figure RE-GDA00035824396800001213
Calculating the abscissa of the end point of the vertical bend of the selected strand
Figure RE-GDA0003582439680000131
According to
Figure RE-GDA0003582439680000132
Will be in the saddle local coordinate system
Figure RE-GDA0003582439680000133
Coordinates of vertical bending end point of lower selected strand
Figure RE-GDA0003582439680000134
Converting to local coordinate system oxyz to obtain local partCoordinate (x) of selected end point of vertical bending of filament strand under coordinate system oxyzsi、ysi、zsi);
Said step 05 comprises the steps of:
according to
Figure RE-GDA0003582439680000135
Calculating the initial unstressed length S of the suspended section of the strand0Wherein L ismgiFor the anchor rod length, (x)0i、y0i、z0i) Is the coordinate of the lower strand anchoring point of the local coordinate system oxyz, (x)si、ysi、zsi) The coordinates of the vertical bent end points of the lower strands of the local coordinate system oxyz are obtained;
according to f'v=fv-ωS0And f'h=fhCalculating the vertical force f 'of the wire strand at the upper end of the anchor rod'vAnd resultant force in the horizontal plane f'hAccording to
Figure RE-GDA0003582439680000136
Calculating the inclination angle of the upper end of the anchor rod
Figure RE-GDA0003582439680000137
According to
Figure RE-GDA0003582439680000138
Calculating the horizontal projection length L of the silk strands;
according to
Figure RE-GDA0003582439680000139
Calculating the current unstressed length S and the vertical projection length H of the strand, wherein EA is the tensile rigidity of the strand, and omega is the bulk density of the main cable;
the iterative computation module is further configured to:
updating the final strand vertical bending end point tangent angle value calculated by the current iteration to gammaiAnd will updated gammaiSubstitution into
Figure RE-GDA00035824396800001310
Obtaining an iteratively calculated side span main cable total balance force F'L
In | (F'L-FL)/FLIf the | does not meet the preset precision, the updated gamma is usediGo back to step 01 to calculate updated FLAnd fiAnd with said updated gammai、FLAnd fiEntering a loop from step 02 to step 10;
the installation angle calculation module is further configured to:
according to
Figure RE-GDA0003582439680000141
Converting the coordinates of the upper end part of the strand anchor rod into an integral coordinate system OXYZ, and performing transformation according to lambda on the integral coordinate system OXYZ1=atan((Ymi-Y0i)/Xmi)、λ2=atan((Zmi-Z0i)/Xmi) And λ3=atan(tan(λ1)/cos(λ2) Calculating the anchor rod installation angle, where λ1Is the included angle between the projection of the anchor pull rod on the XY plane and the X axis, lambda2Is the included angle between the projection of the anchor rod on the XZ plane and the X axis, lambda3Is the angle between the anchor rod and the XZ plane.
The technical scheme provided by the invention has the beneficial effects that:
the embodiment of the invention provides a method for accurately calculating the stress-free length of a closely-attached section of a strand in a scattered cable saddle groove and the saddle groove. Through the coordinates of the vertical bending end point and the horizontal bending end point of the wire strand, the unstressed length of the closely-attached section of the wire strand and the saddle groove in the scattered cable saddle groove can be accurately calculated, so that the full-bridge blanking total length of the wire strand is more accurate, and the factory processing and field erection can be accurately controlled; in addition, through the coordinates of the end points of the vertical bending and the end points of the horizontal bending, a designer can easily judge whether the horizontal bending of the strand occurs before the vertical bending, and further determine whether the design parameters of the saddle groove and the design coordinates of the rear anchor point of the strand need to be adjusted.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings needed to be used in the description of the embodiments will be briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings based on these drawings without creative efforts.
Fig. 1 is a schematic flowchart of a method for calculating an anchor rod installation angle according to an embodiment of the present invention;
FIG. 2 is a schematic view of the strand alignment within the saddle slot provided by an embodiment of the present invention;
FIG. 3 is a schematic view of the spreading and anchoring of the anchor cross-filament strands according to an embodiment of the present invention;
FIG. 4 is a schematic diagram of a local coordinate system according to an embodiment of the present invention;
fig. 5 is a schematic vertical and plane view of a cable saddle according to an embodiment of the present invention.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are some, but not all, embodiments of the present invention. All other embodiments, which can be obtained by a person skilled in the art without any inventive step based on the embodiments of the present invention, are within the scope of the present invention.
In one specific embodiment, the anchor rod installation angle is calculated according to the following method steps:
step (1): define 3 coordinate systems (global coordinate system OXYZ, local coordinate system OXYZ and saddle local coordinate system)
Figure RE-GDA0003582439680000151
) And drawing a vertical line from the theoretical top of the cable saddle to the slip plane, and taking the intersection point of the vertical line and the slip plane as a point o.
Wherein, the Y axis of the overall coordinate system OXYZ is vertical upwards; the local coordinate system OXYZ is translated to the origin O of the global coordinate system OXYZObtaining an intersection point o; saddle local coordinate system
Figure RE-GDA0003582439680000152
The local coordinate system oxyz is rotated counterclockwise around the horizontal z-axis by an angle β, which is the inclination angle of the slip plane (given the known conditions of the design).
It follows that the local coordinate system oxyz is directed to the saddle local coordinate system
Figure RE-GDA0003582439680000153
Is converted into a matrix
Figure RE-GDA0003582439680000154
The coordinate of the theoretical vertex of the cable saddle is known as (X) under the overall coordinate system OXYZip、Yip、 Zip) The vertical height from the theoretical vertex to the slip plane is H0(given the known conditions of the design), the coordinate of the o point in the global coordinate system OXYZ is (X)o、Yo、Zo) Wherein X iso=Xip+H0sinβcosβ、Yo=Yip+H0sinβsinβ、Zo=Zip
By setting a local coordinate system oxyz and a saddle local coordinate system
Figure RE-GDA0003582439680000155
The two coordinate systems assist in calculation, and can facilitate solution of a strand catenary equation and saddle related parameters.
Step (2), converting the theoretical vertex coordinates of the cable saddle into a local coordinate system of the cable saddle
Figure RE-GDA0003582439680000161
Then, the theoretical vertex coordinates of the cable saddle are obtained as
Figure RE-GDA0003582439680000162
Step (3), setting a local coordinate system W of the anchor surface of the strandm(the inclination angle alpha is designed by the anchor surface to ensureGiven that α is given by design), then WmThe transformation matrix of the coordinate system and the global coordinate system OXYZ is
Figure RE-GDA0003582439680000163
The coordinate of the center of the anchor surface under the overall coordinate system OXYZ is (X)m、Ym、Zm) (known conditions) in the local coordinate system W of the anchor surface of the strandmNext, the given strand anchor point coordinates are designed to be (x'0i、y′0i、z′0i) (i is 1 to N, N is the total number of strands), and the coordinates are converted to an overall coordinate system oyx, i.e. the system is a system of three dimensional coordinates
Figure RE-GDA0003582439680000164
Then converted into saddle local coordinate system
Figure RE-GDA0003582439680000165
Under the condition that
Figure RE-GDA0003582439680000166
And (4) calculating coordinates of the flat bending end points of all the strands at the anchor span side. Can be in the saddle local coordinate system
Figure RE-GDA0003582439680000167
Calculating the transverse coordinate z of the flat bending end point of each strandpiAnd a flat bend tangent angle thetai(i is 1-N, N is the total number of strands), and establishing an equation according to the geometrical relationship: ax2+ Bx + C ═ 0, where a ═ 1+ a2, B=2×(a×b-a×xpc-zpc),
Figure RE-GDA0003582439680000168
Figure RE-GDA0003582439680000169
The transverse coordinate z can be obtained by solving the equationpiAnd flat bend corner cuts
Figure RE-GDA00035824396800001610
Wherein R ishIs the flat bending radius of the cable saddle groove, xpcAnd zpcRespectively the ordinate and abscissa of the circle center of the flat curved arc, z0siThe transverse position of the strands in the saddle slots, determined by the strand alignment, is given by design and is a known condition.
And (5) calculating an iterative initial value of the tangent angle of the end point of the vertical bend of the strand (the tangent angle of the end point of the initial vertical bend of the strand). According to a local coordinate system of the saddle
Figure RE-GDA0003582439680000171
Lower strand anchor point coordinates
Figure RE-GDA0003582439680000172
Figure RE-GDA0003582439680000173
And cable saddle IP point
Figure RE-GDA0003582439680000174
Calculating iterative initial value of vertical bending end point cutting angle of silk strand
Figure RE-GDA0003582439680000175
(i is 1 to N, N is the total number of strands).
And (6) calculating the total balance force (namely the component force along the slip plane) of the side-span main cable. Let FRIs a side span main cable force along a slip plane (a cable saddle local coordinate system)
Figure RE-GDA0003582439680000176
Shaft) component, from a longitudinal component F of the main cable tensionXRAnd a vertical component force FYRTo obtain i.e. FR=FXRcosβ+FYRsin beta; according to the mechanical equilibrium condition in the direction of the slip plane, i.e. FL=FR (FLFor anchoring across each strand in the local coordinate system of the cable saddle
Figure RE-GDA0003582439680000177
Axial divisionThe sum of the forces).
Step (7) according to the tangent angle theta of the flat bending end pointiAnd initial vertical bend end point tangent angle gammaiAnd formulas
Figure RE-GDA0003582439680000178
The tension of the strand can be obtained
Figure RE-GDA0003582439680000179
This step ensures that each strand has the same safety factor, and that the tensions of the strands are equal.
And (8) entering a strand loop (i is 1-N), and executing the steps from 8-01 to 8-10 until all strands are traversed.
Step 8-01, setting a first intermediate variable aiming at No. i silk strands
Figure RE-GDA00035824396800001710
And an iteration variable γ; cutting the vertical bent end point of the No. i silk strand into an angle gammaiIs assigned to the intermediate variable
Figure RE-GDA00035824396800001711
(i.e. the
Figure RE-GDA00035824396800001712
) And combining the first intermediate variable
Figure RE-GDA00035824396800001713
Is given to the iteration variable gamma (i.e. the value of
Figure RE-GDA00035824396800001714
)。
8-02, in a saddle local coordinate system
Figure RE-GDA00035824396800001715
Then the three-dimensional component force of the strand is obtained,
Figure RE-GDA00035824396800001716
and
Figure RE-GDA00035824396800001717
converting the three-dimensional component force to be under a local coordinate system oxyz (the self-weight direction of the catenary cable is the vertical y direction) to obtain
Figure RE-GDA0003582439680000181
(
Figure RE-GDA0003582439680000182
Is TZTransposed matrix of) and calculates the resultant force f on the horizontal planeh=fxl/cos(atan(fzl/fxl) Resultant force f) in the vertical directionv=fyl
Step 8-03, a saddle local coordinate system is adopted
Figure RE-GDA0003582439680000183
Lower strand anchor point coordinates
Figure RE-GDA0003582439680000184
Figure RE-GDA0003582439680000185
Conversion to local coordinate system oxyz, i.e.
Figure RE-GDA0003582439680000186
Step 8-04, calculating the coordinate (x) of the end point of the vertical bending of the silk strand under the local coordinate system oxyzsi、 ysi、zsi). The vertical radius of curvature of the cable saddle groove is Rvk(assuming that the saddle-groove vertical bending line is composed of n segments of circular arcs, k is an integer from 1 to n), and the corresponding central angle is phik,DiCalculating the vertical bending radius R of the No. i wire strand in the saddle groove for the vertical height of the No. i wire strand on the section of the main cable (taking the saddle groove top as the reference)kiIs Rki=Rvk+Di
In the saddle local coordinate system
Figure RE-GDA0003582439680000187
Next, the coordinates of the end point of the vertical bend of the strand are calculated according to the area where the end point of the vertical bend of the strand is located and the vertical position of the end point in the saddle groove:
when gamma is less than or equal to phi1Sometimes:
Figure RE-GDA0003582439680000188
phi when1<γ≤φ12Sometimes:
Figure RE-GDA0003582439680000189
③ when phi12<γ≤φ123Sometimes:
Figure RE-GDA00035824396800001810
phi when123When < gamma:
Figure RE-GDA00035824396800001811
when k is more than or equal to 4, the longitudinal coordinate of the vertical bending end point of the strand can be obtained by analogy
Figure RE-GDA00035824396800001812
And vertical coordinate
Figure RE-GDA0003582439680000191
And pass through
Figure RE-GDA0003582439680000192
Further calculating the horizontal coordinate of the vertical bending end point of the strand
Figure RE-GDA0003582439680000193
Then coordinate transformation is carried out to obtain a saddle local coordinate system
Figure RE-GDA0003582439680000194
Vertical bending end point coordinate of lower strand
Figure RE-GDA0003582439680000195
Converting the position of the filament into a local coordinate system oxyz to obtain the coordinates (x) of the vertical bending end point of the filament under the local coordinate system oxyzsi、ysi、zsi) Namely that
Figure RE-GDA0003582439680000196
8-05, under a local coordinate system oxyz, according to a basic equation of a catenary cable unit, anchoring point coordinates (x) by the strands0i、y0i、z0i) Strand vertical bend end point coordinate (x)si、ysi、zsi) Length L of anchor rodmgiThe stress-free length of the strand free section and the coordinates of the lower end point of the strand (i.e. the coordinates of the upper end of the anchor rod) are iteratively calculated. The vertical planes defining the strand anchor points and the end points of the vertical bends are strand planes, each strand having a different strand plane.
The iterative process is 8-05-a to 8-05-f.
8-05-a, according to
Figure RE-GDA0003582439680000197
Calculating the initial unstressed length, the vertical force f 'of the wire strand at the upper end of the anchor rod'v=fv-ωS0Resultant force in the horizontal plane f'h=fh
8-05-b, the end of the strand suspension section in the strand plane is tangent to the anchor rod, so that the angle of inclination of the upper end of the anchor rod
Figure RE-GDA0003582439680000198
Should be equal to the tangent angle of the strand ends, i.e.
Figure RE-GDA0003582439680000199
The anchor rod can be ensured not to generate additional bending moment.
8-05-c, according to
Figure RE-GDA00035824396800001910
Calculating the horizontal projection length L of the silk strands;
8-05-d, iteratively calculating the current unstressed length S and the vertical projection length H of the strand according to a basic equation of a catenary unit, wherein the basic equation of the catenary unit is as follows:
Figure RE-GDA00035824396800001911
Figure RE-GDA00035824396800001912
wherein EA is the tensile stiffness of the strands and omega is the bulk density of the main cable.
8-05-e, performing precision judgment on the unstressed length calculated by current iteration: if (S-S)0)/S0| is less than the preset precision (the preset precision can be set to 10)-6And | (S-S)0)/S0The smaller the value of | can make the precision of the calculation result higher), then enter 8-05-f, otherwise make S0Return 8-05-a, and execute 8-05-a through 8-05-e.
8-05-f, according to
Figure RE-GDA0003582439680000201
Calculating a first vertical position difference delta h of the wire strand at the upper end part of the anchor rod1
Step 8-06, let
Figure RE-GDA0003582439680000202
Returning to the step 8-01, and substituting the updated parameter values into the parameter values after the step 8-01 to the step 8-05
Figure RE-GDA0003582439680000203
Calculate Δ h2
Step 8-07, order
Figure RE-GDA0003582439680000204
Returning to the step 8-01, and substituting the updated parameter values into the parameter values after the step 8-01 to the step 8-05
Figure RE-GDA0003582439680000205
Calculate Δ h0
Step 8-08, judgment
Figure RE-GDA0003582439680000206
Whether or not it is less than a preset accuracy (the preset accuracy may be set to 10)-6And is and
Figure RE-GDA0003582439680000207
smaller values may result in higher accuracy of the calculated results); if so, terminating the iteration, otherwise, order
Figure RE-GDA0003582439680000208
Δh1=Δh2,Δh2=Δh0. And 8-01, and executing the steps 8-01 to 8-08 until the preset precision is met, and then terminating the iteration.
Step 8-09, according to the formula xmi=xsi-Lcos(atan((zsi-z0i)/(xsi-x0i)))、 ymi=ysi+ H and zmi=zsi+Lsin(atan((zsi-z0i)/(xsi-x0i) )) calculates the upper end coordinates (x) of the strand anchor rod in the local coordinate system oxyzmi、ymi、zmi)。
Step 8-10, taking the iteration final value gamma as the final vertical bending cutting angle of the No. i silk strand, namely gammaiTaking the updated unstressed length S as the final unstressed length S of the strandiI.e. Si=S。
And 8-11, returning to the step 8-01, and recycling the step 8-01 to the step 8-10 until all the strands are calculated. To this end, the end points of the vertical bends of all strands are obtainedVertical bending cutting angle gammaiAnd the unstressed length S of the suspended section (the part between the end point of the vertical bend and the upper end part of the anchor rod) of the anchor cross inner wire strandi
Step (9), the tangent angle theta of the flat bending end point obtained by current iterative computation is usediAnd vertical bend end point tangent angle gammaiSubstitution into
Figure RE-GDA0003582439680000209
Calculating a new local coordinate system of each strand of the anchor span side on the scattered cable saddle
Figure RE-GDA0003582439680000211
Sum of axial component forces F'LAnd judging | (F'L-FL)/FLWhether | is smaller than a preset precision (the preset precision can be set to 10)-6And | (F'L-FL)/FLThe smaller the | value is, the higher the precision of the calculation result is, if yes, the calculation is terminated, otherwise, the vertical bending end point tangent angle gamma is updatediAnd returning to the step (7).
Step (10), transforming the coordinates of the upper end part of each strand anchor rod under the local coordinate system OXYZ to the coordinates under the integral coordinate system OXYZ,
Figure RE-GDA0003582439680000212
calculating the installation angle of each anchor rod under an overall coordinate system OXYZ, wherein the included angle between the projection of the anchor rod on the XY plane and the X axis is lambda1=atan((Ymi-Y0i)/Xmi) The included angle between the projection of the anchor pull rod on the XZ plane and the X axis is lambda2=atan((Zmi-Z0i)/Xmi) Angle lambda between anchor rod and XZ plane3=atan(tan(λ1)/cos(λ2))。
Therefore, the accurate anchor rod installation angle of each strand and the accurate stress-free length of each strand suspension section can be obtained, and the vertical bending tangent point and the horizontal bending tangent point coordinates of each strand in the scattered cable saddle groove are determined.
Compared with the related art, the design and installation angle of the anchor rod is calculated by obtaining the coordinates of the upper end part of the strand anchor rod through iteration and then calculating the design and installation angle of the anchor rod according to the coordinates of the upper end part and the lower end part. The beneficial effects include: the method is a completely accurate method without any simplification, the installation angle of the anchor rod, the unstressed length of the suspension section of the wire strand, the positions of the vertical bending end point and the horizontal bending end point of the cable saddle and the tension of the wire strand are simultaneously obtained through coupling iteration, so that the result simultaneously meets a plurality of conditions, including: the tension of the wire strand does not generate additional bending moment at the end part of the anchor pull rod; the sum of the inclined plane component forces of the strand pulling force at the end point of the vertical bend is completely equal to the side span main cable component force; the upper end of the suspension section wire strand is accurately tangent to the cable saddle groove at the end point of the vertical bend; the stress-free length of the strand and the tension of the strand satisfy the catenary equation. Meanwhile, the stress-free length of the closely-attached section of the strand and the saddle groove in the scattered cable saddle groove can be accurately calculated according to the coordinates of the vertical bending end point and the horizontal bending end point of the strand, so that the full-bridge blanking total length of the strand is more accurate, and the factory processing and field erection can be accurately controlled; in addition, through the coordinates of the end points of the vertical bending and the end points of the horizontal bending, a designer can easily judge whether the horizontal bending of the strand occurs before the vertical bending, and further determine whether the design parameters of the saddle groove and the design coordinates of the rear anchor point of the strand need to be adjusted. In addition, the tension of each strand is completely equal, the saddle does not slide any more, the internal force is not redistributed any more, the safety factors of the strands are ensured to be the same, and the durability of the strands can be improved; the end part of the anchor rod does not generate additional bending moment, and only receives the axial tension, so that the durability of the anchor rod can be improved.
In a specific process of calculating the installation angle of the anchor rod, known conditions are as follows: the elastic modulus E of the main cable strand is 1.973E8kPa, the bulk weight omega is 76.917kN/m3, the cross section area A of the strand is 0.003017m2 (the product EA of the elastic modulus E and the cross section area A of the strand is the tensile rigidity of the strand), as shown in figure 5, the IP point coordinate of the cable saddle is (-895.994, 49.876, 0), the inclination angle beta of the sliding surface of the cable saddle is 28.77 degrees, and the component force F of the side-span main cable on the sliding surfaceR699212.27kN, height D of strand in saddle groovei0.063m, the included angle between the normal line of the anchor surface and the horizontal line (the designed inclination angle alpha of the anchor surface) is 36 degrees, and the radius R of the flat bending of the saddle groove of the cable saddlehIs 18m, the vertical bend consists of 4 sections of circular arcs, and the radius R of the vertical bendkiAre respectively 12.5m, 9.5m, 6m and 3.5m, and the included angle phikRespectively 8 degrees, 7 degrees and 7 degrees.
As shown in FIG. 2, the main cable is composed of 352 strands, and for example, the calculation is performed by taking No. 1 strand at the lowest end of the middle and No. 56 strand with a larger installation angle of the anchor rod as an example, the vertical distances from the centers of the two strands to the top of the saddle groove are respectively 0.0315 and 0.3465m, the transverse distances from the center line of the saddle groove are respectively 0m and 0.66m, the anchoring center coordinates of the anchoring surface are (-921.887, 31.073 and 0), the coordinates of the No. 1 strand are (-7.875 and 0), the coordinates of the No. 56 strand are (-4.5 and-6.15) in the local coordinate system of the anchoring surface, and the length L of the anchor rod is LmgiAre all 1.78 m.
The method comprises the following specific steps:
1) as shown in fig. 3 and 4, a local coordinate system oxyz and a saddle local coordinate system are established
Figure RE-GDA0003582439680000221
And coordinate transformation is carried out on the basic parameters, and the method comprises the following steps: theoretical vertex coordinates of the cable saddle, coordinates of anchoring points of the strands and the like;
2) calculating the coordinates of the flat bending end points of the strands to obtain the coordinates of the flat bending end points of No. 1 strand of (0,0.231, 0) and the flat bending cutting angle thetai0 DEG, the coordinates of the flat bending end point of the No. 56 silk strand are (-1.545, 0.429, -0.933), and the flat bending cutting angle thetai9.984 degrees;
3) calculating iterative initial values of the vertical bending end point cutting angles to obtain No. 1 and No. 56 strand vertical bending end point cutting angles gamma1And gamma56Corresponding to 19.784 ° and 14.950 °.
4) And (5) performing iterative calculation from the step (8) to the step (10) to obtain the results of the installation angle of each wire strand anchor rod, the unstressed length of the suspended section, the coordinates of the end point of the vertical bend, the tension force and the like.
According to the traditional method, the angle of a straight line connected between the IP point of the strand saddle and the anchor point of the strand is used as the installation angle of the anchor pull rod of the corresponding strand, so that the spatial distribution of the strand around the curved surface of the strand saddle cannot be considered, and the condition that the anchor span strand is in a catenary state rather than a straight line under the action of self weight is ignored. Because the traditional method simplifies the processing excessively, certain errors exist in the calculation of the installation angle. Table 1 shows the results of comparing the installation angles of the No. 1 and No. 56 strand anchor rods calculated by the present invention and the conventional method.
TABLE 1 Anchor brace installation Angle results
Figure RE-GDA0003582439680000231
As can be seen from Table 1, for the No. 1 strand located at the center line, the error is relatively small, and the included angle lambda between the projection of the anchor rod on the XY plane and the X axis1The error of (2.84%) is larger for No. 56 strands far from the central line, and the included angle lambda between the projection of the anchor rod on the XY plane and the X axis1The error of the anchor rod in the X-axis.
In addition, the method can accurately calculate the unstressed length of the suspension section of the wire strand, the coordinates of the flat bending end point and the vertical bending end point of the wire strand and the cable saddle and the tension of each wire strand, and accurately ensure that the installation angle of the anchor rod is equal to the tangent angle at the lower end of the wire strand, so that the anchor rod cannot generate additional bending moment, and other results such as the unstressed length of the suspension section are shown in a table 2.
TABLE 2 other results
Figure RE-GDA0003582439680000232
An embodiment of the present invention further provides a computer storage medium, where a computer program is stored on the computer storage medium, where the computer program, when executed by a processor, implements the steps of the method for calculating the installation angle of the anchor rod according to any one of claims 1 to 9.
It will be understood by those of ordinary skill in the art that functional modules/units in all or some of the steps of the methods disclosed above may be implemented as software, firmware, hardware, and suitable combinations thereof. In a hardware implementation, the division between functional modules/units mentioned in the above description does not necessarily correspond to the division of physical components; for example, one physical component may have multiple functions, or one function or step may be performed by several physical components in cooperation. Some or all of the physical components may be implemented as software executed by a processor, such as a central processing unit, digital signal processor, or microprocessor, or as hardware, or as an integrated circuit, such as an application specific integrated circuit. Such software may be distributed on computer readable storage media, which may include computer readable storage media (or non-transitory media) and communication media (or transitory media).
The above embodiments are only specific embodiments of the present invention, but the scope of the embodiments of the present invention is not limited thereto, and any person skilled in the art can easily think of various equivalent modifications or substitutions within the technical scope of the embodiments of the present invention, and these modifications or substitutions should be covered by the scope of the embodiments of the present invention. Therefore, the protection scope of the embodiments of the present invention shall be subject to the protection scope of the claims.

Claims (10)

1. A method for calculating the installation angle of an anchor rod is characterized by comprising the following steps:
acquiring theoretical vertex coordinates of the scattered cable saddle and coordinates of a strand anchoring point, and calculating a strand flat bending end point chamfer and a strand initial vertical bending end point chamfer according to the theoretical vertex coordinates of the scattered cable saddle and the coordinates of the strand anchoring point;
acquiring the total balance force of the main side-span cable, and calculating the tension of each strand according to the strand flat-bent end point chamfer, the strand initial vertical-bent end point chamfer and the total balance force of the main side-span cable;
traversing each strand, and iteratively calculating the unstressed length of the suspended section of the strand and the coordinates of the upper end part of the anchor pull rod of the strand according to the coordinates of the anchor point of the strand, the tangent angle of the flat bent end point of the strand, the tangent angle of the initial vertical bent end point of the strand, the tension of each strand and the vertical position of the strand in the saddle groove;
and calculating the installation angle of the anchor rod according to the iteratively calculated coordinates of the upper end part of the strand anchor rod.
2. The method of calculating an anchor rod installation angle of claim 1,
before acquiring the theoretical vertex coordinates of the cable saddle and the coordinates of the anchor points of the strands, the method further comprises the following steps:
defining a global coordinate system OXYZ, wherein the Y axis of the global coordinate system is vertically upward;
defining a local coordinate system oxyz, wherein the origin of the local coordinate system is an intersection point o of a vertical line and a slip plane when the theoretical vertex of the cable saddle makes the vertical line towards the slip plane, and the y-axis direction of the local coordinate system is the self-weight direction of a catenary cable;
defining a saddle local coordinate system
Figure RE-FDA0003582439670000011
The saddle local coordinate system is obtained by rotating the local coordinate system around the horizontal z-axis of the saddle counterclockwise by an angle beta, and
the local coordinate system oxyz is towards saddle local coordinate system
Figure RE-FDA0003582439670000012
Is a conversion matrix of
Figure RE-FDA0003582439670000013
Figure RE-FDA0003582439670000014
Defining a local coordinate system of the anchor surface of the strand, and enabling a conversion matrix of the local coordinate system of the anchor surface of the strand and the overall coordinate system OXYZ to be
Figure RE-FDA0003582439670000021
Local coordinate system of saddle
Figure RE-FDA0003582439670000022
The theoretical vertex coordinates of the cable saddle are
Figure RE-FDA0003582439670000023
Figure RE-FDA0003582439670000024
And is
Figure RE-FDA0003582439670000025
Wherein beta is the angle of inclination of the slip plane, (X)ip、Yip、Zip) The coordinates of the theoretical vertex of the cable saddle are (X) under the overall coordinate system OXYZo、Yo、Zo) The coordinate of the o point under the overall coordinate system OXYZ is shown;
saddle local coordinate system
Figure RE-FDA0003582439670000026
The coordinates of the anchoring point of the silk strand are
Figure RE-FDA0003582439670000027
And is
Figure RE-FDA0003582439670000028
Wherein (X)0i、Y0i、Z0i) The coordinates of the strand anchoring points under the overall coordinate system OXYZ are adopted, and
Figure RE-FDA0003582439670000029
wherein
Figure RE-FDA00035824396700000210
Is TmTranspose matrix of (x'0i、y′0i、z′0i) For a predetermined strand anchoring point in said strand anchoring surface local coordinate system WmThe lower coordinate, i is 1 to N, N is the total number of strands, (X)m、Ym、Zm) The coordinates of the center of the anchor surface under the overall coordinate system OXYZ are shown.
3. The method of calculating an anchor rod installation angle of claim 2,
the method for calculating the tangent angle of the flat bent end point of the strand and the tangent angle of the initial vertical bent end point of the strand according to the theoretical vertex coordinate of the scattered cable saddle and the anchoring point coordinate of the strand comprises the following steps:
establish the equation Ax2+ Bx + C is 0, and
A=1+a2,B=2×(a×b-a×xpc-zpc),
Figure RE-FDA0003582439670000031
Figure RE-FDA0003582439670000032
solving an equation to obtain the transverse coordinate z of each strand flat-bending end point on the anchor span sidepiAccording to
Figure RE-FDA0003582439670000033
Solving strand flat-bending end point tangent angle theta of No. i strandiWherein
RhIs the flat bending radius of the cable saddle groove, xpcAnd zpcRespectively the ordinate and abscissa of the circle center of the flat curved arc, z0siThe transverse position of the strand in the saddle groove;
the method for calculating the initial vertical bending end point chamfer angle of the strand according to the theoretical vertex coordinate of the scattered cable saddle and the anchor point coordinate of the strand comprises the following steps:
according to
Figure RE-FDA0003582439670000034
Calculating the initial vertical bending end point cutting angle gamma of the No. i strandi
4. The method of calculating an anchor rod installation angle of claim 3,
acquiring the total balance force of the side span main cable and calculating the tension of each strand according to the strand flat bending end point chamfer and the strand initial vertical bending end point chamfer, wherein the method comprises the following steps:
step 01, according to FR=FXRcosβ+FYRsinβ、FL=FRAnd
Figure RE-FDA0003582439670000035
calculating the component force F of the main cable force along the sliding surfaceRThe total balance force F of the side span main cableLAnd the tension f of each strandiWherein F isXRLongitudinal component of tension force of main cable across side span, FYRIs a vertical component of the side span main cable tension force.
5. The method of calculating an anchor rod installation angle of claim 4,
traversing each strand, and iteratively calculating the unstressed length of the suspended section of the strand and the coordinates of the upper end part of the anchor pull rod of the strand according to the coordinates of the anchor point of the strand, the tangent angle of the flat bent end point of the strand, the tangent angle of the initial vertical bent end point of the strand, the tension of each strand and the vertical position of the strand in the saddle groove, wherein the method comprises the following steps:
step 02: selecting No. i silk strand, setting the first intermediate variable
Figure RE-FDA0003582439670000041
And an iteration variable γ; cutting the vertical bent end point of the No. i silk strand into an angle gammaiIs assigned to the intermediate variable
Figure RE-FDA0003582439670000042
And combining the first intermediate variable
Figure RE-FDA0003582439670000043
To the iteration variable γ;
step 03: according to
Figure RE-FDA0003582439670000044
And
Figure RE-FDA0003582439670000045
and
Figure RE-FDA0003582439670000046
fh=fxl/cos(atan(fzl/fxl) And f) andv=fylcalculating the resultant force f of the selected strand on the horizontal planehAnd resultant force f in the vertical directionvWherein
Figure RE-FDA0003582439670000047
Is TZThe transposed matrix of (2);
step 04: calculating the coordinates of the tail points of the vertical bends of the strands according to the vertical bend radius of the cable scattering saddle groove, the central angle corresponding to the arc section of the vertical bend line of the saddle groove and the vertical position of the strands in the saddle groove;
step 05: iteratively calculating the initial unstressed length S of the suspended section of the strand according to the coordinates of the anchoring point of the strand, the coordinates of the vertical bending end point of the strand, the resultant force of the selected strand on the horizontal plane and the resultant force of the selected strand in the vertical direction0And the current unstressed length S of the strand suspended section;
step 06: judgment of | (S-S)0)/S0If | satisfies the preset precision, if yes, according to
Figure RE-FDA0003582439670000048
Calculating a first vertical position difference delta h of the wire strand at the upper end part of the anchor rod1Otherwise, assigning the value of the current unstressed length S to the initial unstressed length S0Then returns to step 02ExecuteStep 02 to step 05;
step 07: setting a second intermediate variable
Figure RE-FDA0003582439670000049
And make
Figure RE-FDA00035824396700000410
And is
Figure RE-FDA00035824396700000411
Then returning to step 02 to execute step 02 to step 06 according to the method
Figure RE-FDA00035824396700000416
Calculating the second vertical position difference delta h of the wire strand at the upper end part of the anchor rod2
Step 08: setting a third intermediate variable
Figure RE-FDA00035824396700000412
And make
Figure RE-FDA00035824396700000413
And is
Figure RE-FDA00035824396700000414
Then returning to step 02 and executing steps 02 to 06, according to
Figure RE-FDA00035824396700000415
Calculating the third vertical position difference delta h of the wire strand at the upper end part of the anchor rod0Wherein y issiIs the vertical coordinate, L, of the end point of the selected vertical bend of the strand in the local coordinate system oxyzmgiIs the anchor rod length;
step 09: judgment of
Figure RE-FDA0003582439670000051
If the preset precision is met, terminating the iteration if the preset precision is met, otherwise, enabling the iteration to be ended
Figure RE-FDA0003582439670000052
Δh1=Δh2And Δ h2=Δh0Then, the step 02 is returned to and the steps 02 to 08 are executed:
step 10: according to xmi=xsi-Lcos(atan((zsi-z0i)/(xsi-x0i)))、ymi=ysi+ H and zmi=zsi+Lsin(atan((zsi-z0i)/(xsi-x0i) )) calculating coordinates (x) of the upper end of the strand anchor rodmi、ymi、zmi) And taking the current value of the iteration variable gamma as the final vertical bending end point cutting angle of the No. i silk strand, and taking the current stress-free length S calculated by iteration as the stress-free length of the final silk strand suspension section of the No. i silk strand.
6. The method of calculating an anchor rod installation angle of claim 5,
traversing each strand, and iteratively calculating the unstressed length of the suspended section of the strand and the coordinates of the upper end part of the anchor pull rod of the strand according to the coordinates of the anchor point of the strand, the tangent angle of the flat bent end point of the strand, the tangent angle of the initial vertical bent end point of the strand, the tension of each strand and the vertical position of the strand in the saddle groove, wherein the method comprises the following steps:
updating the final strand vertical bending end point tangent angle value calculated by the current iteration to gammaiAnd will update gammaiSubstitution into
Figure RE-FDA0003582439670000053
Obtaining an iteratively calculated side span main cable total balance force F'L
In | (F'L-FL)/FLIf the | does not meet the preset precision, the updated gamma is usediGo back to step 01 to calculate updated FLAnd fiAnd with said updated gammai、FLAnd fiThe loop from step 02 to step 10 is entered.
7. The method of calculating an anchor rod installation angle of claim 5, wherein said step 04 comprises the steps of:
supposing that the saddle groove vertical bending line consists of n sections of circular arcs, and enabling the vertical bending radius R of the cable scattering saddle groove corresponding to each section of circular arcvIs represented by RvkWherein k is an integer from 1 to n;
making the R tovkCorrespond toThe central angle of (a) is expressed as phikAnd according to Rki=Rvk+DiCalculating the vertical bending radius R of the No. i strand in the saddle groovekiWherein D isiThe vertical height of the No. i silk strand on the section of the main cable is defined;
when gamma is less than or equal to phi1According to
Figure RE-FDA0003582439670000061
Calculating the ordinate of the end point of the vertical bend of the selected strand
Figure RE-FDA0003582439670000062
And vertical coordinate
Figure RE-FDA0003582439670000063
When phi is1<γ≤φ12According to
Figure RE-FDA0003582439670000064
Calculating the ordinate of the end point of the vertical bend of the selected strand
Figure RE-FDA0003582439670000065
And vertical coordinate
Figure RE-FDA0003582439670000066
When phi is12<γ≤φ123According to
Figure RE-FDA0003582439670000067
Calculating the ordinate of the end point of the vertical bend of the selected strand
Figure RE-FDA0003582439670000068
And vertical coordinate
Figure RE-FDA0003582439670000069
When phi is123When < gamma, according to
Figure RE-FDA00035824396700000610
Calculating the ordinate of the end point of the vertical bend of the selected strand
Figure RE-FDA00035824396700000611
And vertical coordinate
Figure RE-FDA00035824396700000612
According to
Figure RE-FDA00035824396700000613
Calculating the abscissa of the end point of the vertical bend of the selected strand
Figure RE-FDA00035824396700000614
According to
Figure RE-FDA00035824396700000615
Will be in the saddle local coordinate system
Figure RE-FDA00035824396700000616
Vertical bending end point coordinate of lower selected strand
Figure RE-FDA00035824396700000617
Converting the position of the filament into a local coordinate system oxyz to obtain the coordinates (x) of the end point of the vertical bend of the selected filament under the local coordinate system oxyzsi、ysi、zsi)。
8. The method of calculating an anchor rod installation angle of claim 5,
the step 05 comprises the steps of:
according to
Figure RE-FDA00035824396700000618
Calculating the initial unstressed length S of the suspended section of the strand0Wherein, LmgiFor the anchor rod length, (x)0i、y0i、z0i) Is the coordinate of the lower strand anchoring point of the local coordinate system oxyz, (x)si、ysi、zsi) The coordinates of the vertical bent end points of the lower strands of the local coordinate system oxyz are obtained;
according to f'v=fv-ωS0And f'h=fhCalculating the vertical force f 'of the wire strand at the upper end of the anchor rod'vAnd resultant force in the horizontal plane f'hAccording to
Figure RE-FDA0003582439670000071
Calculating the inclination angle of the upper end of the anchor rod
Figure RE-FDA0003582439670000072
According to
Figure RE-FDA0003582439670000073
Calculating the horizontal projection length L of the silk strands;
according to
Figure RE-FDA0003582439670000074
And calculating the current unstressed length S and the vertical projection length H of the strand, wherein EA is the tensile rigidity of the strand, and omega is the bulk density of the main cable.
9. The method of calculating an anchor rod installation angle of claim 5,
the anchor rod installation angle is calculated according to the iteratively calculated upper end coordinates of the strand anchor rod, and the method comprises the following steps:
according to
Figure RE-FDA0003582439670000075
Converting the coordinates of the upper end part of the strand anchor rod into an integral coordinate system OXYZ, and performing transformation according to lambda on the integral coordinate system OXYZ1=atan((Ymi-Y0i)/Xmi)、λ2=atan((Zmi-Z0i)/Xmi) And λ3=atan(tan(λ1)/cos(λ2) Calculating the anchor rod installation angle, where λ1Is the included angle between the projection of the anchor pull rod on the XY plane and the X axis, lambda2Is the included angle between the projection of the anchor pull rod on the XZ plane and the X axis, lambda3Is the angle between the anchor rod and the XZ plane.
10. An apparatus for calculating an installation angle of an anchor rod, comprising: the iteration initial value acquisition module is used for acquiring theoretical vertex coordinates of the scattered cable saddle and coordinates of the anchoring points of the strands and calculating tangent angles of the flat bending end points of the strands and the initial vertical bending end points of the strands according to the theoretical vertex coordinates of the scattered cable saddle and the coordinates of the anchoring points of the strands;
an iterative computation module to:
acquiring the total balance force of the main side-span cable, and calculating the tension of each strand according to the strand flat-bent end point chamfer, the strand initial vertical-bent end point chamfer and the total balance force of the main side-span cable;
traversing each strand, and iteratively calculating the unstressed length of the suspended section of the strand and the coordinates of the upper end part of the anchor pull rod of the strand according to the coordinates of the anchor point of the strand, the tangent angle of the flat bent end point of the strand, the tangent angle of the initial vertical bent end point of the strand, the tension of each strand and the vertical position of the strand in the saddle groove;
the mounting angle calculation module is used for calculating the mounting angle of the anchor rod according to the iteratively calculated coordinates of the upper end part of the strand anchor rod;
the iteration initial value obtaining module is further configured to:
defining a global coordinate system OXYZ, wherein the Y axis of the global coordinate system is vertically upward;
defining a local coordinate system oxyz, wherein the origin of the local coordinate system is an intersection point o of a vertical line and a slip plane when the theoretical vertex of the cable saddle makes the vertical line towards the slip plane, and the y-axis direction of the local coordinate system is the self-weight direction of a catenary cable;
defining a saddle local coordinate system
Figure RE-FDA0003582439670000081
The saddle local coordinate system is obtained by rotating the local coordinate system around the horizontal z-axis of the saddle counterclockwise by an angle beta, and
the local coordinate system oxyz is towards saddle local coordinate system
Figure RE-FDA0003582439670000082
Is a conversion matrix of
Figure RE-FDA0003582439670000083
Figure RE-FDA0003582439670000084
Defining a local coordinate system of the anchor surface of the strand, and enabling a conversion matrix of the local coordinate system of the anchor surface of the strand and the overall coordinate system OXYZ to be
Figure RE-FDA0003582439670000085
Local coordinate system of saddle
Figure RE-FDA0003582439670000086
The theoretical vertex coordinates of the cable saddle are
Figure RE-FDA0003582439670000087
Figure RE-FDA0003582439670000088
And is
Figure RE-FDA0003582439670000091
Wherein beta is the angle of inclination of the slip plane, (X)ip、Yip、Zip) The coordinates of the theoretical vertex of the cable saddle are (X) under the overall coordinate system OXYZo、Yo、Zo) The coordinate of the o point under the overall coordinate system OXYZ is shown;
saddle local coordinate system
Figure RE-FDA0003582439670000092
The coordinates of the anchoring point of the silk strand are
Figure RE-FDA0003582439670000093
And is provided with
Figure RE-FDA0003582439670000094
Wherein (X)0i、Y0i、Z0i) The coordinates of the strand anchoring point under the global coordinate system OXYZ, and
Figure RE-FDA0003582439670000095
wherein
Figure RE-FDA0003582439670000096
Is TmTranspose matrix of (x'0i、y′0i、z′0i) For a predetermined strand anchoring point in said strand anchoring surface local coordinate system WmThe lower coordinate, i is 1 to N, N is the total number of strands, (X)m、Ym、Zm) The coordinates of the center of the anchor surface under the overall coordinate system OXYZ are taken as the coordinates;
establish the equation Ax2+ Bx + C is 0, and
A=1+a2,B=2×(a×b-a×xpc-zpc),
Figure RE-FDA0003582439670000097
Figure RE-FDA0003582439670000098
solving an equation to obtain the transverse coordinate z of each strand flat-bending end point on the anchor span sidepiAccording to
Figure RE-FDA0003582439670000099
Solving strand flat-bending end point tangent angle theta of No. i strandiWherein
RhIs the flat bending radius of the cable saddle groove, xpcAnd zpcRespectively the ordinate and abscissa of the circle center of the flat curved arc, z0siThe transverse position of the strand in the saddle groove;
according to
Figure RE-FDA00035824396700000910
Calculating the initial vertical bending end point cutting angle gamma of the No. i strandi
The iterative computation module is further configured to: performing the following steps 01 to 10;
the step 01 comprises the following steps: according to FR=FXRcosβ+FYRsinβ、FL=FRAnd
Figure RE-FDA0003582439670000101
calculating the component force F of the main cable force along the sliding surfaceRThe total balance force F of the side span main cableLAnd the tension f of each strandiWherein F isXRLongitudinal component of tension force of main cable across side span, FYRVertical component force of the tension force of the side span main cable;
step 02 includes: selecting No. i silk strand, setting the first intermediate variable
Figure RE-FDA0003582439670000102
And an iteration variable γ; cutting the vertical bent end point of the No. i silk strand into an angle gammaiIs assigned to the intermediate variable
Figure RE-FDA0003582439670000103
And combining the first intermediate variable
Figure RE-FDA0003582439670000104
To the iteration variable γ;
step 03 comprises: according to
Figure RE-FDA0003582439670000105
And
Figure RE-FDA0003582439670000106
and
Figure RE-FDA0003582439670000107
fh=fxl/cos(atan(fzl/fxl) And f) andv=fylcalculating the resultant force f of the selected strand on the horizontal planehAnd resultant force f in the vertical directionvWherein
Figure RE-FDA0003582439670000108
Is TZThe transposed matrix of (2);
the step 04 comprises the following steps: calculating the coordinates of the tail points of the vertical bends of the strands according to the vertical bend radius of the cable scattering saddle groove, the central angle corresponding to the arc section of the vertical bend line of the saddle groove and the vertical position of the strands in the saddle groove;
step 05 comprises: iteratively calculating the initial unstressed length S of the suspended section of the strand according to the coordinates of the anchoring point of the strand, the coordinates of the vertical bending end point of the strand, the resultant force of the selected strand on the horizontal plane and the resultant force of the selected strand in the vertical direction0And the current unstressed length S of the strand suspended section;
step 06 comprises: judgment of | (S-S)0)/S0If | satisfies the preset precision, if yes, according to
Figure RE-FDA0003582439670000109
Calculating a first vertical position difference delta h of the wire strand at the upper end part of the anchor rod1Otherwise, assigning the value of the current unstressed length S to the initial unstressed length S0Then returns to step 02ExecuteStep 02 to step 05;
step 07 includes: setting a second intermediate variable
Figure RE-FDA00035824396700001010
And make it possible to
Figure RE-FDA00035824396700001011
And is
Figure RE-FDA00035824396700001012
Then returning to step 02 to execute step 02 to step 06 according to the method
Figure RE-FDA0003582439670000111
Calculating the second vertical position difference delta h of the wire strand at the upper end part of the anchor rod2
Step 08 comprises: setting a third intermediate variable
Figure RE-FDA0003582439670000112
And make
Figure RE-FDA0003582439670000113
And is
Figure RE-FDA0003582439670000114
Then returning to step 02 and executing steps 02 to 06, according to
Figure RE-FDA0003582439670000115
Calculating the third vertical position difference delta h of the wire strand at the upper end part of the anchor rod0Wherein y issiIs the vertical coordinate, L, of the end point of the selected vertical bend of the strand in the local coordinate system oxyzmgiIs the anchor rod length;
step 09 includes: judgment of
Figure RE-FDA0003582439670000116
If the preset precision is met, terminating the iteration if the preset precision is met, otherwise, enabling the iteration to be ended
Figure RE-FDA0003582439670000117
Δh1=Δh2And Δ h2=Δh0Then returning to the step 02 and executing the step 02 to the step 08;
the step 10 comprises: according to xmi=xsi-Lcos(atan((zsi-z0i)/(xsi-x0i)))、ymi=ysi+ H and zmi=zsi+Lsin(atan((zsi-z0i)/(xsi-x0i) )) calculating coordinates (x) of the upper end of the strand anchor rodmi、ymi、zmi) Taking the current value of the iteration variable gamma as the final vertical bending end point cutting angle of the No. i strand, and taking the current unstressed length S calculated by iteration as the unstressed length of the final strand suspended section of the No. i strand;
the step 04 comprises the steps of:
supposing that the saddle groove vertical bending line consists of n sections of circular arcs, and enabling the vertical bending radius R of the cable scattering saddle groove corresponding to each section of circular arcvIs represented by RvkWherein k is an integer from 1 to n;
making the R tovkThe corresponding central angle is denoted by phikAnd according to Rki=Rvk+DiCalculating the vertical bending radius R of the No. i strand in the saddle groovekiWherein D isiThe vertical height of the No. i silk strand on the section of the main cable is defined;
when gamma is less than or equal to phi1According to
Figure RE-FDA0003582439670000118
Calculating the ordinate of the end point of the vertical bend of the selected strand
Figure RE-FDA0003582439670000119
And vertical coordinate
Figure RE-FDA00035824396700001110
When phi is1<γ≤φ12According to
Figure RE-FDA00035824396700001111
Calculating the ordinate of the end point of the vertical bend of the selected strand
Figure RE-FDA00035824396700001112
And vertical coordinate
Figure RE-FDA00035824396700001113
When phi is12<γ≤φ123According to
Figure RE-FDA0003582439670000121
Calculating the ordinate of the end point of the vertical bend of the selected strand
Figure RE-FDA0003582439670000122
And vertical coordinate
Figure RE-FDA0003582439670000123
When phi is123When < gamma, according to
Figure RE-FDA0003582439670000124
Calculating the ordinate of the end point of the vertical bend of the selected strand
Figure RE-FDA0003582439670000125
And vertical coordinate
Figure RE-FDA0003582439670000126
According to
Figure RE-FDA0003582439670000127
Calculating the abscissa of the end point of the vertical bend of the selected strand
Figure RE-FDA0003582439670000128
According to
Figure RE-FDA0003582439670000129
Will be in the saddle local coordinate system
Figure RE-FDA00035824396700001210
Coordinates of vertical bending end point of lower selected strand
Figure RE-FDA00035824396700001211
Converting the position of the filament to a local coordinate system oxyz to obtain the coordinates (x) of the end point of the vertical bend of the selected filament under the local coordinate system oxyzsi、ysi、zsi);
The step 05 comprises the steps of:
according to
Figure RE-FDA00035824396700001212
Calculating the initial unstressed length S of the suspended section of the strand0Wherein L ismgiAnchor pull rod length, (x)0i、y0i、z0i) Is the coordinate of the lower strand anchoring point of the local coordinate system oxyz, (x)si、ysi、zsi) The coordinates of the vertical bent end points of the lower strands of the local coordinate system oxyz are obtained;
according to f'v=fv-ωS0And f'h=fhCalculating the vertical force f 'of the wire strand at the upper end of the anchor rod'vAnd resultant force in the horizontal plane f'hAccording to
Figure RE-FDA00035824396700001213
Calculating the inclination angle of the upper end of the anchor rod
Figure RE-FDA00035824396700001214
According to
Figure RE-FDA00035824396700001215
Calculating the horizontal projection length L of the silk strands;
according to
Figure RE-FDA0003582439670000131
Calculating the current unstressed length S and the vertical projection length H of the strand, wherein EA is the tensile rigidity of the strand, and omega is the bulk density of the main cable;
the iterative computation module is further configured to:
updating the final strand vertical bending end point tangent angle value calculated by the current iteration to gammaiAnd will update gammaiSubstitution into
Figure RE-FDA0003582439670000132
Obtaining an iteratively calculated side span main cable total balance force F'L
In | (F'L-FL)/FLIf the | does not meet the preset precision, the updated gamma is usediGo back to step 01 to calculate updated FLAnd fiAnd with said updated gammai、FLAnd fiEntering a loop from step 02 to step 10;
the installation angle calculation module is further configured to:
according to
Figure RE-FDA0003582439670000133
Converting the coordinates of the upper end part of the strand anchor rod into an integral coordinate system OXYZ, and performing transformation according to lambda on the integral coordinate system OXYZ1=atan((Ymi-Y0i)/Xmi)、λ2=atan((Zmi-Z0i)/Xmi) And λ3=atan(tan(λ1)/cos(λ2) Calculating the anchor rod installation angle, where λ1Is the included angle between the projection of the anchor pull rod on the XY plane and the X axis, lambda2For anchoringThe angle between the projection of the rod in the XZ plane and the X axis, λ3Is the angle between the anchor rod and the XZ plane.
CN202210111126.0A 2022-01-24 2022-01-24 Method and device for calculating installation angle of anchor pull rod Pending CN114491760A (en)

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CN202416178U (en) * 2011-12-27 2012-09-05 中铁大桥(郑州)缆索有限公司 Large-specification unit wire strand for main cable of suspension bridge
CN110939066A (en) * 2019-12-06 2020-03-31 中铁大桥勘测设计院集团有限公司 Method for determining tension of anchor cross-wire strand

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