CN104656674B - Method for adjusting deflexion of cantilever mechanical structure - Google Patents
Method for adjusting deflexion of cantilever mechanical structure Download PDFInfo
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- CN104656674B CN104656674B CN201410818839.6A CN201410818839A CN104656674B CN 104656674 B CN104656674 B CN 104656674B CN 201410818839 A CN201410818839 A CN 201410818839A CN 104656674 B CN104656674 B CN 104656674B
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- adpting flange
- double
- movement
- wedge
- cantilever
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Abstract
The invention provides a method for adjusting deflexion of a cantilever mechanical structure. The method includes the following steps in sequence: calculating to determine the adjusting angle of a double-wedge gasket adjusting mechanism; mounting the double-wedge gasket between connecting flanges of the cantilever mechanical structure; measuring the deflexion of the centers of all connecting flanges of the cantilever mechanical structure, and adjusting the cantilever mechanical structure from the cantilever end again; adjusting the center of the connecting flange: if the center of a connecting flange is below the horizontal line, rotating the wedge-shaped gasket at the position of the previous connecting flange, so as to enlarge the adjusting angle of the double-wedge gasket adjusting mechanism and enable the center of the connecting flange to move upwards, and if the center of a connecting flange is above the horizontal line, rotating the wedge-shaped gasket at the position of the previous connecting flange, so as to reduce the adjusting angle of the double-wedge gasket adjusting mechanism and enable the center of the connecting flange to move downwards. The center of the connecting flange is repeatedly adjusted until the center reaches the horizontal line and meets the straightness requirements of the cantilever mechanical structure. The adjusting method provided by the invention is easy to operate and high in accuracy of adjustment.
Description
Technical field
The present invention relates to a kind of cantilever frame for movement amount of deflection control method, cantilever frame for movement can be adjusted using the present invention
Deflection deformation, change cantilever frame for movement natural bow value, meet cantilever frame for movement physics morpheme size require.
Background technology
In some engineer applied fields, often use large scale cantilever frame for movement.Due to being made by gravity and other external force
With cantilever frame for movement can produce compared with Large deflection it is impossible to reach the linearity index of engine request.At present.Engineering construction
During frequently with increase cantilever frame for movement rigidity method, by from high rigidity, low-density material, subtracting as far as possible
The amount of deflection of few cantilever frame for movement, is required with the physics morpheme size meeting cantilever frame for movement.But, for some large scales
Cantilever frame for movement, after taking said method, the linearity that still can not meet cantilever frame for movement requires.Often adopt at present
With single taperliner, cantilever frame for movement is adjusted.Cantilever frame for movement segmentation manufactures, and is carried out using flange between each section
Connect, between flange, adjust the original shape of cantilever frame for movement using single taperliner, by adjusting, cantilever frame for movement
Original shape be the broken line being upturned, in the presence of the making a concerted effort of gravity and other external force, cantilever frame for movement is tilted upward
The distance rising can be compensated with its amount of deflection, by the taperliner using proper angle, so that each flange connections is located just at
In same horizontal line, thus reaching linearity index.But, single taperliner adjusts the essence that method extremely relies on taperliner angle
Really calculate and Precision Machining, each taperliner angle is different and processes and cannot be carried out Secondary Control after installing, and can only pass through
The adjusting gasket of the different angles of replacing can be only achieved expected linearity and requires repeatedly.
Content of the invention
In order to overcome single taperliner reconcile method excessively rely on the accurate calculating of taperliner angle and Precision Machining and
Need to change the shortcoming that pad just can carry out Secondary Control, the present invention provides a kind of cantilever frame for movement amount of deflection control method.
The cantilever frame for movement amount of deflection control method of the present invention, in turn includes the following steps:
A. calculate the regulation angle determining double-wedge pad adjustment mechanism;
B. double-wedge pad is arranged between the adpting flange of cantilever frame for movement;
C. measure the amount of deflection at cantilever frame for movement each adpting flange center, start cantilever frame for movement is carried out from cantilever end
Adjust again;
D., when adpting flange is centrally located at below horizontal line, the taperliner rotating at previous adpting flange is double to increase
The regulation angle of taperliner governor motion, makes adpting flange center move up;
E., when adpting flange is centrally located above the horizon, at the previous adpting flange of rotation, taperliner is to reduce folding wedge
The regulation angle of shape pad adjustment mechanism, makes adpting flange center move down;
F. by this regulation repeatedly until by this adpting flange center adjustment to horizontal line on, reach cantilever machinery knot
The linearity of structure requires.
By two pieces of identical taperliners, connection combines described double-wedge pad adjustment mechanism back-to-back.
Described regulation angle is.
The technical solution adopted for the present invention to solve the technical problems is:Two panels identical taperliner combines back-to-back,
When its I, III rudder face line is all vertical and direction is identical, adjusts angle maximum, be the twice of monolithic taperliner angle;When it
The equal level of I, III rudder face line and in opposite direction when, adjust angle be 0.By rotary wedge pad, double-wedge pad can be made to adjust
The regulation angle of section mechanism consecutive variations between 0 degree to 2 times taperliner inclination angle.Cantilever frame for movement segmentation manufactures, respectively
It is attached by adpting flange between section, between flange, angular adjustment is carried out by double-wedge pad adjustment mechanism.According to outstanding
Version, the density of adopted material and elastic modelling quantity after the installation of arm frame for movement, calculates its sag curve, Ran Hougen
Calculate the double-wedge pad that each adpting flange center adjustment to same horizontal line is needed according to the amount of deflection at each adpting flange center
The regulation angle of governor motion, and then determine the anglec of rotation of pad.According to this theoretical calculation regulation angle value to cantilever machine
Tool structure is assembled.After completing the assembling of cantilever frame for movement, start to measure the position at each adpting flange center from cantilever end,
If adpting flange center, needs to change the tune of double-wedge pad adjustment mechanism according to measurement result not in the same horizontal line
Section angle, is adjusted again to cantilever frame for movement.When adpting flange is centrally located at below horizontal line, rotate previous connection
The taperliner of flange, to increase the regulation angle of double-wedge pad adjustment mechanism, makes adpting flange center move up;When
When adpting flange is centrally located above the horizon, rotates taperliner at previous adpting flange and adjust machine to reduce double-wedge pad
The regulation angle of structure, makes adpting flange center move down.By this regulation repeatedly until adjusting this adpting flange center
Save on horizontal line.It is adjusted to far-end from cantilever end successively, until the center of all of adpting flange is respectively positioned on same water
On horizontal line, the linearity reaching cantilever frame for movement requires.
The invention has the beneficial effects as follows, it is possible to use the double-wedge pad of two panels identical taperliner composition adjusts machine
Structure, by the rotation of taperliner, realizes a range of continuously adjusting angle.First with the regulation angle of theoretical calculation to outstanding
The amount of deflection of arm frame for movement is tentatively adjusted, the position at each adpting flange center then being obtained according to measurement, rotary wedge
Pad changes the regulation angle of double-wedge pad adjustment mechanism, and cantilever frame for movement is adjusted repeatedly, until by each connection
Flange center is adjusted in same horizontal line, reaches expected linearity requirement.
Brief description
Fig. 1 is the lateral view of the taperliner in the embodiment of the present invention;
Fig. 2 is the front view of the taperliner in the present invention;
Fig. 3 is that in the embodiment of the present invention, the adpting flange between double-wedge pad adjustment mechanism and cantilever frame for movement is connected
Schematic diagram;
Fig. 4 is the sectional view of Fig. 3;
Fig. 5 is the overall structure after cantilever frame for movement assembling in the embodiment of the present invention;
In figure;1. taperliner 2. cylinder 3. adpting flange.
Specific embodiment
The present invention is further described with reference to the accompanying drawings and examples.
Embodiment 1
In FIG, taperliner 1 end flat is respectively disc and ellipsoid, and two face angulations are defined as.
Taperliner、Rudder face line and、The position of rudder face line is as shown in Figure 2.
In Fig. 3, two pieces of taperliners assembly double-wedge pad adjustment mechanism in the way of disc is to disc, when two pads
I, III rudder face line of piece all straight up when, the regulation angle of double-wedge pad adjustment mechanism is.To cross the disc center of circle
Disc exterior normal is rotary shaft, two pads all rotate counterclockwises, and the regulation angle of double-wedge pad adjustment mechanism can diminish.When two
When pad all ratates 90 degrees, the regulation angle of double-wedge pad adjustment mechanism is 0 degree.By rotating pad, double-wedge pad is adjusted
The regulation angle of section mechanism can beBetween continuously adjust.The regulation angle of double-wedge pad adjustment mechanismWith pad
The anglec of rotationCorresponding relation be.
Fig. 4 is the assembly relation of double-wedge pad adjustment mechanism and adpting flange.Assembling process in cantilever frame for movement
In, obtain the regulation angle of theoretical calculation by rotating the pad of double-wedge pad adjustment mechanism, be arranged on cantilever frame for movement
Adpting flange 3 between.Flange is connected by screw with flange, and double-wedge pad adjustment mechanism is connected flange screw, when even
The screw of acting flange 3 can rotate double-wedge pad adjustment mechanism pad after unclamping changes regulation angle, the cylinder to cantilever
Body 2 is adjusted again.
In embodiment shown in Fig. 5, by calculating the amount of deflection of cantilever frame for movement it is determined that cantilever frame for movement adjacent two
After the regulation angle of the double-wedge pad adjustment mechanism between section, it is arranged between adpting flange.Then measurement cantilever machinery knot
The structure horizontal distance of each adpting flange center deviation under gravity.Start to carry out node location to far-end from cantilever end
Measurement and regulation.If adpting flange center is above the horizon, increase the anglec of rotation of taperliner at previous adpting flange
Degree adjusts angle to reduce double-wedge pad adjustment mechanism, and node can move down;If adpting flange center horizontal line with
Under, then reduce the anglec of rotation of taperliner at the previous adpting flange regulation angle to increase double-wedge pad adjustment mechanism,
Node can move up.By repeatedly adjusting, until the center of all of adpting flange is finally all located in same horizontal line, hang
The linearity of arm cylinder body reaches requirement.
Claims (2)
1. a kind of cantilever frame for movement amount of deflection control method, in turn includes the following steps:
A. calculate the regulation angle determining double-wedge pad adjustment mechanism;
B. double-wedge pad is arranged between the adpting flange of cantilever frame for movement;
C. measure the amount of deflection at cantilever frame for movement each adpting flange center, start cantilever frame for movement is carried out again from cantilever end
Adjust;
D., when adpting flange is centrally located at below horizontal line, the taperliner at the previous adpting flange of rotation is to increase double-wedge
The regulation angle of pad adjustment mechanism, makes adpting flange center move up;
E., when adpting flange is centrally located above the horizon, at the previous adpting flange of rotation, taperliner is to reduce double-wedge pad
The regulation angle of piece governor motion, makes adpting flange center move down;
F. by this regulation repeatedly until by this adpting flange center adjustment to horizontal line on, reach cantilever frame for movement
Linearity requires.
2. cantilever frame for movement amount of deflection control method according to claim 1, is characterized in that:Described double-wedge pad is adjusted
By two pieces of identical taperliners, connection combines back-to-back for mechanism.
Priority Applications (1)
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CN201410818839.6A CN104656674B (en) | 2014-12-25 | 2014-12-25 | Method for adjusting deflexion of cantilever mechanical structure |
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CN201410818839.6A CN104656674B (en) | 2014-12-25 | 2014-12-25 | Method for adjusting deflexion of cantilever mechanical structure |
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CN104656674A CN104656674A (en) | 2015-05-27 |
CN104656674B true CN104656674B (en) | 2017-02-22 |
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Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN201067780Y (en) * | 2007-05-23 | 2008-06-04 | 天水锻压机床有限公司 | Suspension arm slide rod for steel pipe expanding machine |
CN101417400A (en) * | 2008-12-22 | 2009-04-29 | 齐齐哈尔二机床(集团)有限责任公司 | Large-size CNC horizontal milling and boring machine ram movable inclined guide-rail compensation method and device |
CN201351804Y (en) * | 2009-02-12 | 2009-11-25 | 杨泰 | Household wedge-shaped gasket |
CN102357842A (en) * | 2011-10-19 | 2012-02-22 | 上海三一精机有限公司 | Double compensation method and device for moving tilt of numerical control floor type boring-milling machine ram |
CN102528566A (en) * | 2011-12-14 | 2012-07-04 | 中捷机床有限公司 | Ram flexibility compensation mechanism of heavy numerical control floor type milling and boring machine |
CN102581687A (en) * | 2011-11-30 | 2012-07-18 | 威海华东数控股份有限公司 | Guide track unloading device for crossbeam of large-sized machine tool and deflection compensation method |
CN202356986U (en) * | 2011-11-03 | 2012-08-01 | 芜湖恒升重型机床股份有限公司 | Ram deflection deformation compensation device |
CN202389991U (en) * | 2011-12-14 | 2012-08-22 | 中冶陕压重工设备有限公司 | Movable supporting device of end part of cantilever winding drum of reeling machine |
CN202925724U (en) * | 2012-11-20 | 2013-05-08 | 北京金易格新能源科技发展有限公司 | Bracket gravity members for curtain bracket and curtain bracket |
CN202945799U (en) * | 2012-12-03 | 2013-05-22 | 张若美 | Adjustable wall connecting rod of steel pipe scaffold |
CN203908516U (en) * | 2013-08-27 | 2014-10-29 | 徐州重型机械有限公司 | Crane suspension arm linearity automatic detection device |
-
2014
- 2014-12-25 CN CN201410818839.6A patent/CN104656674B/en active Active
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN201067780Y (en) * | 2007-05-23 | 2008-06-04 | 天水锻压机床有限公司 | Suspension arm slide rod for steel pipe expanding machine |
CN101417400A (en) * | 2008-12-22 | 2009-04-29 | 齐齐哈尔二机床(集团)有限责任公司 | Large-size CNC horizontal milling and boring machine ram movable inclined guide-rail compensation method and device |
CN201351804Y (en) * | 2009-02-12 | 2009-11-25 | 杨泰 | Household wedge-shaped gasket |
CN102357842A (en) * | 2011-10-19 | 2012-02-22 | 上海三一精机有限公司 | Double compensation method and device for moving tilt of numerical control floor type boring-milling machine ram |
CN202356986U (en) * | 2011-11-03 | 2012-08-01 | 芜湖恒升重型机床股份有限公司 | Ram deflection deformation compensation device |
CN102581687A (en) * | 2011-11-30 | 2012-07-18 | 威海华东数控股份有限公司 | Guide track unloading device for crossbeam of large-sized machine tool and deflection compensation method |
CN102528566A (en) * | 2011-12-14 | 2012-07-04 | 中捷机床有限公司 | Ram flexibility compensation mechanism of heavy numerical control floor type milling and boring machine |
CN202389991U (en) * | 2011-12-14 | 2012-08-22 | 中冶陕压重工设备有限公司 | Movable supporting device of end part of cantilever winding drum of reeling machine |
CN202925724U (en) * | 2012-11-20 | 2013-05-08 | 北京金易格新能源科技发展有限公司 | Bracket gravity members for curtain bracket and curtain bracket |
CN202945799U (en) * | 2012-12-03 | 2013-05-22 | 张若美 | Adjustable wall connecting rod of steel pipe scaffold |
CN203908516U (en) * | 2013-08-27 | 2014-10-29 | 徐州重型机械有限公司 | Crane suspension arm linearity automatic detection device |
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