CN106202652A - The lightweight topological method of product and shredder cutterhead - Google Patents
The lightweight topological method of product and shredder cutterhead Download PDFInfo
- Publication number
- CN106202652A CN106202652A CN201610503275.6A CN201610503275A CN106202652A CN 106202652 A CN106202652 A CN 106202652A CN 201610503275 A CN201610503275 A CN 201610503275A CN 106202652 A CN106202652 A CN 106202652A
- Authority
- CN
- China
- Prior art keywords
- volume
- percentage
- cutterhead
- shredder
- tool rest
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Classifications
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F30/00—Computer-aided design [CAD]
- G06F30/20—Design optimisation, verification or simulation
- G06F30/23—Design optimisation, verification or simulation using finite element methods [FEM] or finite difference methods [FDM]
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B02—CRUSHING, PULVERISING, OR DISINTEGRATING; PREPARATORY TREATMENT OF GRAIN FOR MILLING
- B02C—CRUSHING, PULVERISING, OR DISINTEGRATING IN GENERAL; MILLING GRAIN
- B02C18/00—Disintegrating by knives or other cutting or tearing members which chop material into fragments
- B02C18/06—Disintegrating by knives or other cutting or tearing members which chop material into fragments with rotating knives
- B02C18/16—Details
- B02C18/18—Knives; Mountings thereof
- B02C18/182—Disc-shaped knives
Abstract
The invention discloses a kind of product light-weighted topological optimization algorithm, The present invention gives a parameters optimization constrained procedure commonly used, rational percentage by volume and iterations rather than artificial trial can be immediately arrived at by theoretical algorithm, shorten the design cycle, advantage for this week method of large and complex structure is more prominent, the method can adjust parameter according to the different of design structure precision, such as initial percentage by volume, percentage by volume increment, and value, institute in this way most of Topology Algorithm are all suitable for.The invention also discloses a kind of shredder cutterhead, sword is torn up including what disk body and fixing with described disk body was connected, described disk body includes that annular connection dish and multiple Yu described connection dish are integrally formed and are distributed on the tool rest connecting disk ring week, and before and after described disk body, two sides are respectively correspondingly provided with groove.
Description
Technical field
The present invention relates to technical field of mechanical design, particularly relate to lightweight topological method and the shredder of a kind of product
Cutterhead.
Background technology
The purpose of structure optimization is to make the structure designed more economical from material, and from structure, the distribution of power is more reasonable.Its
Content contains structural dimension optimization, Shape optimization and topological optimization, and topological optimization is side even more important in structure optimization
Face, the improvement of structural topology can be substantially improved the performance of structure or alleviate the weight of structure, bringing direct economic benefit, because of
This choice structure topology optimization problem, as research direction, has great realistic meaning.At present, Topology Optimization Method has uniformly
Change method (homogenization method), density variable method, Varying-thickness method (variable thickness method), gradually
Enter method (evoluti onary structural optimization (ESO) method) and BESO method etc., wherein BESO side
Method is to be improved on the basis of ESO method, and BESO method can not only delete unit can also recovery unit.ESO method
Proposed by Xie and Steven the earliest, mainly make final remaining material reach set by constantly reducing material
Constraints.BESO method is proposed by Querin et al the earliest, is the improvement to ESO method, by deleting or extensive
Multiple unit makes final volume meet constraints, and it is the unit not having stress less that this method terminates the condition of iteration,
In this way can ensure that the rigidity of structure, and the physical dimension of topologies can clearly be calculated.But
This method is a kind of evolution method, so its iterations is more, computational efficiency is inefficient compared with SIMP method, this
Outward, although Tanskanen discusses the theoretical basis of ESO, but its convergence has not been established, and this also makes
Obtain BESO method instability and mistake easily occurs.
Topological optimization plays an important role in terms of lightweight product, and shredder cutter diameter is 450mm, and thickness is
50mm, carries out topological optimization to it and makes its lightweight can increase whole tearing up in the case of tearing up usefulness not reducing shredder
The life-span of machine, and improve the stress of main shaft, thus reduce the energy consumption of shredder.
Summary of the invention
It is an object of the invention to for technological deficiency present in prior art, and the lightweight topology of a kind of product is provided
Method.
It is an object of the invention to disclose and a kind of utilize what described product lightweight topological method prepared to tear up machine knife
Dish.
Be the technical scheme is that by realizing the purpose of the present invention
A kind of product light-weighted topology design method, comprises the following steps,
1) to Modeling in Product and by given design section limited grid discretization setup unit property value and initial
Boundary condition and initial load;
2) carry out finite element analysis and obtain unit and the sensitivity data of node;
3) minima a of a percentage by volume is set;
4) at whole design section, node sensitivity data is carried out submissiveization;I.e. the Sensitirity va1ue of each unit again
It is ranked up, determines to delete unit by sensitivity, big not the deleting of sensitivity,
5) according to formulaCalculate current sensitivity degrees of data and the meansigma methods of a upper iteration step sensitivity data,
And preserve to following iteration step use, wherein αiReferring to the sensitivity of i-th unit, k is current iterations;
6) target volume that following iteration walks is determined;An iteration will delete some unit, and successive ignition is close to target
Volume;
7) property value of unit is redefined;Utilize new cell attribute value amendment design having as next step iteration
Finite element analysis model;
8) 2 are repeated)-7) step, until reaching predetermined target volume and meeting convergence criterion, i.e. reach to set
The volume requirement of small size percent a,
9) on the basis of first initial volume percent, increase the percentage by volume that value is m carry out counting for the second time
Calculation repeats 3)-8), until meeting εrLess than 0.1;
10) by step 9) draw topology percentage by volume and iterations input BESO model in and obtain final
Topological structure.
The present invention gives a parameters optimization constrained procedure commonly used, conjunction can be immediately arrived at by theoretical algorithm
The percentage by volume of reason rather than artificial trial, shorten the design cycle, for the advantage of this week method of large and complex structure
More prominent, the method can adjust parameter, such as initial percentage by volume a, volume hundred according to the different of design structure precision
Fractional increments, and εrValue, institute in this way most of Topology Algorithm are all suitable for.
Described step 2)-9) computational methods be:
F=KU (3)
T=r'(6)
V*=fV0 (8)
Wherein r=1,2,3, Λ, N (9)
F=a+rm (10)
F and U represents load vector and displacement vector respectively;C is flexibility;xeBeing the e design variable, solid element is 1,
Dummy cell takes 0.001;N is total number of unit;K is Bulk stiffness matrix;F is percentage by volume;M is that percentage by volume increases
Amount, it is substantially relevant with design accuracy, and precision its value the highest is the least;R is calculation times;εrRepresent be the r time calculating time
The change of two adjacent volume percentage difference values and the ratio of maximum Flexibility Difference;What r' represented is changing when meeting formula (5)
Generation number, t represents the iterations meeting Structural Design Requirement;What k represented is current iterations;I represents element number;
What a represented is an initial minimum volume percent.
Preferably, described product is the cutterhead of shredder, The present invention gives the adjacent body being applicable to shredder cutterhead
The difference of long-pending percent and the ratio 0.1 of maximum Flexibility Difference, at difference and the ratio of maximum Flexibility Difference of adjacent percentage by volume
During less than 0.1, the structure of shredder cutterhead can reduce volume under conditions of meeting rigidity to greatest extent, reaches green raw
The effect produced.
Preferably, in described step 9) in utilize Python program that percentage by volume and iterations are assigned to BESO mould
Type is to improve BESO efficiency.
A kind of shredder cutterhead, including disk body with fix the sword that tears up being connected with described disk body, described disk body includes
Annular connection dish and multiple Yu described connection dish are integrally formed and are distributed on the tool rest connecting disk ring week, described disk body
Front and back two sides are respectively correspondingly provided with groove.
The connection dish that the root of described tool rest is corresponding is formed with through hole.
For regular polygon hole to be in transmission connection with corresponding polygon shaft in the middle part of described connection dish.
Described through hole is circular.
Described tool rest is 6.
Described tool rest be connected dish arrange in the same plane, described tool rest triangular in shape and with the radial direction being connected dish
Keeping angle, be formed with joint face inside the outer end of tool rest, the back of described tool rest is arc.
Compared with prior art, the invention has the beneficial effects as follows:
The present invention gives a parameters optimization constrained procedure commonly used, conjunction can be immediately arrived at by theoretical algorithm
The percentage by volume of reason rather than artificial trial, shorten the design cycle, for the advantage of this week method of large and complex structure
More prominent, the method can adjust parameter, such as initial percentage by volume a, volume hundred according to the different of design structure precision
Mark increments, and εrValue, institute in this way most of Topology Algorithm are all suitable for.
Accompanying drawing explanation
Fig. 1 show the cutterhead modeling schematic diagram of the present invention;
Fig. 2 show the structural representation after topological optimization;
Fig. 3 show percentage by volume and deformation quantity graph of a relation.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, the present invention is described in further detail.Should be appreciated that described herein
Specific embodiment only in order to explain the present invention, be not intended to limit the present invention.
The present invention will be described further with below equation for detailed description of the invention.
F=KU (3)
T=r'(6)
V*=fV0 (8)
Wherein r=1,2,3, Λ, n (9)
F=a+rm (10)
F and U represents load vector and displacement vector respectively;C is flexibility;xeBeing the e design variable, solid element is 1,
Dummy cell takes 0.001;N is total number of unit;K is Bulk stiffness matrix;F is percentage by volume;M is that percentage by volume increases
Amount, it is relevant with design accuracy, and precision its value the highest is the least;R is calculation times;ε is two adjacent volume percentage difference values
Change and the ratio of maximum Flexibility Difference;εrRepresent be the r time calculate time two adjacent volume percentage difference values change and
The ratio of maximum Flexibility Difference;What r' represented is the iterations when meeting formula (5), and t represents and meets Structural Design Requirement
Iterations;What k represented is current iterations;I represents element number;What a represented is an initial minimum volume hundred
Mark.
Specifically, comprise the following steps
1, utilizing finite element software ABAQUS to be modeled cutterhead, the size of cutterhead is 50mm with reference to the thickness of cutterhead,
The material of cutterhead is that its design parameter of 42CrMo is shown in Table 1,
Table 1 cutterhead material parameter
Constraints is fixation cutter head inner ring, and inside triangle indication part is geometrical constraint part as shown in Figure 1, outward
What portion's arrow represented is loading section, and the size of load draws according to the dynamic analog of shredder, and shredder tears up Automobile Plate
Process, the material of Automobile Plate is 6111 aluminium alloys, and thickness is 8mm, analyze during shredder tears up the stress shape of cutterhead
Condition, selects the load that the every a part of stress of cutterhead is maximum, uses maximum load to load FEM (finite element) model, to guarantee topology
The reliability of optimum results, magnitude of load specifically gives in the following table.
This model is carried out stress and strain model, is 10182 unit by model partition, 13055 nodes, use C3D8R mono-
Element type, 8 node linear hexahedral elements, reduce integration, hourglass control.
2, operation program draws parameters optimization
Execution equation (6)-(8) utilizing Python program constantly to circulate draw one so that constitutionally stable iteration
Number of times, circulation solves (9), and (10) two formulas can draw the percentage by volume of optimization, and shown below is with shredder cutterhead
As a example by draw the data of flexibility, program can stop 65% in percentage by volume, and following data is only for explanation difference rate of change
Start flexibility change to start to diminish less than 0.1, can show that optimum percentage by volume is 65% according to formula (10), i.e. have satisfied
Enough meet volume during rigidity minimum simultaneously, thus reach light-weighted purpose, in order to verification expression (10) correctness we adjust
Go out the value of each percentage by volume deformation quantity, as shown in following table and Fig. 3, find the change of deformation quantity when percentage by volume is 65%
Melting the change beginning to diminish explanation rigidity to reduce, illustrating that percentage by volume is when 65% is suitable.
3 topological optimizations realize
This algorithm adds the constraint to parameters optimization based on BESO Topology Optimization Method, and this algorithm is easy to write journey
Sequence, and have the good compatibility with ABAQUS software, utilize Python program to realize this calculating, wherein volume constraint letter
VolFrac, iterations iter represent, import this program in ABAQUS/CAE module, i.e. obtain final optimization topology
Structure.
The invention provides a kind of new topological optimization algorithm, this algorithm adds based on BESO Topology Optimization Method
Constraint to parameter, reduces blindness and the error manually taking Selection parameter, thus improves the efficiency of topological optimization, accelerates to optimize
Process, and reduce the mistake occurred during optimization, increase the reliability of design.
Simultaneously as its a kind of concrete application, devising a kind of new car shredder cutterhead, it is than the body of original cutterhead
Long-pending reduce 23%, and demonstrate its rigidity and intensity theoretically all in tolerance band.
As in figure 2 it is shown, the cutterhead of the present invention includes that what annular disk body 1 and fixing with described disk body was connected tears up sword,
Described disk body 1 includes that annular connection dish 10 and multiple Yu described connection dish are integrally formed and are distributed on connection disk ring week
Tool rest 11, before and after described disk body, two sides are respectively correspondingly provided with groove 12, corresponding at the root of described tool rest 11
Connection dish on be formed with circular through hole 13.
The cutterhead of the present invention, front and back, two sides are respectively arranged with the groove of the formula of emptying, i.e. shape on connection dish and tool rest
Become a communication type groove, be effectively reduced overall volume, and combine force analysis, tool rest root less for stress is corresponding
Connection dish on offer through hole, reduce further cutterhead weight, and arranging of through hole facilitate locating and machining, effectively prevents
The appearance of unbalance dynamic phenomenon occurs.
Specifically, described tool rest is to be that regular polygon hole is with corresponding in the middle part of 6 described connection dishes
Polygon shaft, as hexagonal shaft is in transmission connection, uses tool rest and axle sleeve to set formula mode, and stable transmission is reliable and keeps in repair
Maintenance is convenient.
Wherein, tearing up the more preferable cutting angle of sword for ease of providing, described tool rest is arranged on same plane with being connected dish
In, described tool rest is triangular in shape and keeps angle with the radial direction being connected dish, i.e. tool rest is obliquely installed the most in one direction,
Being formed with joint face 14 inside the outer end of tool rest, the described sword that tears up is fixedly installed on joint face, utilizes the most inside
Sword is torn up in the joint face fixed installation tilted, and when tearing up sword stress, radial shape diminishes, and is effectively improved service life.
The above is only the preferred embodiment of the present invention, it is noted that for the common skill of the art
For art personnel, under the premise without departing from the principles of the invention, it is also possible to make some improvements and modifications, these improvements and modifications
Also should be regarded as protection scope of the present invention.
Claims (9)
1. a product light-weighted topology design method, it is characterised in that comprise the following steps,
1) to Modeling in Product and by given design section limited grid discretization setup unit property value and initial boundary
Condition and initial load;
2) carry out finite element analysis and obtain unit and the sensitivity data of node;
3) minima a of a percentage by volume is set;
4) at whole design section, node sensitivity data is carried out submissiveization;
5) according to formulaCalculate current sensitivity degrees of data and the meansigma methods of a upper iteration step sensitivity data, and preserve
Use to following iteration step, wherein αiReferring to the sensitivity of i-th unit, k is current iterations;
6) target volume that following iteration walks is determined;
7) property value of unit is redefined;Utilize new cell attribute value amendment design the finite element as next step iteration
Analyze model;
8) 2 are repeated)-7) step, until reaching predetermined target volume and meeting convergence criterion;
9) increase on the basis of a upper percentage by volume value m carry out calculating for the second time as new percentage by volume
Repeat 3)-8), until meeting εrLess than 0.1, m is the percentage by volume increment set;
10) by step 9) percentage by volume of topology that draws and iterations again input in BESO in mastery routine and obtain
Whole topological structure.
2. lightweight topological method as claimed in claim 1, it is characterised in that described step 2)-9) computational methods be:
F=KU (3)
T=r'(6)
Wherein r=1,2,3, Λ, N (9)
F=a+rm (10)
F and U represents load vector and displacement vector respectively;C is flexibility;xeBeing the e design variable, solid element is 1, empty single
Unit takes 0.001;N is total number of unit;K is Bulk stiffness matrix;F is percentage by volume;M is that the percentage by volume set increases
Amount;R is calculation times;εrRepresent is the change of two adjacent volume percentage difference values during the r time calculating and maximum flexibility
The ratio of difference;What r' represented is the iterations when meeting formula (5), and t represents the iterations meeting Structural Design Requirement;
What k represented is current iterations;I represents element number;What a represented is an initial minimum volume percent, wherein
Volume constraint equation is (4) formula;Object function (1) ensure that the balance of total;(6) formula calculates and meets the iteration time required
Number, the iteration time when its value is that the percentage by volume infinite approach target of structure amasss percent after iteration;(7) formula is convergence standard
Then;(8)-(10) constrain percentage by volume.
3. lightweight topological method as claimed in claim 1, it is characterised in that utilize in described step (6)-(10)
Percentage by volume and iterations are assigned to BESO model to improve BESO efficiency by Python program.
4. the shredder cutterhead obtained by the lightweight topological method described in any one of claim 1-3, it is characterised in that
Including disk body with fix the sword that tears up being connected with described disk body, described disk body includes annular connection dish and multiple and institute
The connection dish stated is integrally formed and is distributed on the tool rest connecting disk ring week, and before and after described disk body, two sides are respectively correspondingly arranged
Fluted.
5. shredder cutterhead as claimed in claim 4, it is characterised in that on the connection dish that the root of described tool rest is corresponding
It is formed with through hole.
6. shredder cutterhead as claimed in claim 4, it is characterised in that be regular polygon hole in the middle part of described connection dish with
Corresponding polygon shaft is in transmission connection.
7. shredder cutterhead as claimed in claim 5, it is characterised in that described through hole is circular.
8. shredder cutterhead as claimed in claim 4, it is characterised in that described tool rest is 6.
9. shredder cutterhead as claimed in claim 4, it is characterised in that described tool rest is arranged on same plane with being connected dish
In, described tool rest is triangular in shape and keeps angle with the radial direction being connected dish, is formed with joint face inside the outer end of tool rest,
The back of described tool rest is arc.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610503275.6A CN106202652A (en) | 2016-06-28 | 2016-06-28 | The lightweight topological method of product and shredder cutterhead |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610503275.6A CN106202652A (en) | 2016-06-28 | 2016-06-28 | The lightweight topological method of product and shredder cutterhead |
Publications (1)
Publication Number | Publication Date |
---|---|
CN106202652A true CN106202652A (en) | 2016-12-07 |
Family
ID=57464256
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201610503275.6A Pending CN106202652A (en) | 2016-06-28 | 2016-06-28 | The lightweight topological method of product and shredder cutterhead |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN106202652A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107423512A (en) * | 2017-07-28 | 2017-12-01 | 广东省智能制造研究所 | A kind of light-weight design method of large-scale die-casting machine tailgate |
CN110414044A (en) * | 2019-05-29 | 2019-11-05 | 中国海洋大学 | The light-weight design method of approach on offshore jacket platforms |
CN114547800A (en) * | 2022-02-25 | 2022-05-27 | 大连理工大学 | Torsion bar lightweight design method based on topological optimization |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102043883A (en) * | 2010-12-29 | 2011-05-04 | 长沙理工大学 | Material breakage constraint-based continuum structure topology design modeling and optimization design method |
CN103065015A (en) * | 2013-01-04 | 2013-04-24 | 西安交通大学 | Internal force path geometrical morphology based low-carbon material-saving bearing structure design method |
US20160140269A1 (en) * | 2014-11-14 | 2016-05-19 | Industrial Technology Research Institute | Structural topology optimization design method |
-
2016
- 2016-06-28 CN CN201610503275.6A patent/CN106202652A/en active Pending
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102043883A (en) * | 2010-12-29 | 2011-05-04 | 长沙理工大学 | Material breakage constraint-based continuum structure topology design modeling and optimization design method |
CN103065015A (en) * | 2013-01-04 | 2013-04-24 | 西安交通大学 | Internal force path geometrical morphology based low-carbon material-saving bearing structure design method |
US20160140269A1 (en) * | 2014-11-14 | 2016-05-19 | Industrial Technology Research Institute | Structural topology optimization design method |
Non-Patent Citations (2)
Title |
---|
何智成等: "基于面光滑有限元的复杂三维结构拓扑优化", 《中国机械工程》 * |
焦洪宇等: "基于变密度法的周期性拓扑优化", 《机械工程学报》 * |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107423512A (en) * | 2017-07-28 | 2017-12-01 | 广东省智能制造研究所 | A kind of light-weight design method of large-scale die-casting machine tailgate |
CN110414044A (en) * | 2019-05-29 | 2019-11-05 | 中国海洋大学 | The light-weight design method of approach on offshore jacket platforms |
CN114547800A (en) * | 2022-02-25 | 2022-05-27 | 大连理工大学 | Torsion bar lightweight design method based on topological optimization |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN102063540B (en) | Method for optimally designing machine tool body structure | |
CN106202652A (en) | The lightweight topological method of product and shredder cutterhead | |
CN107391891A (en) | A kind of high aspect ratio wing Optimization Design based on Model Fusion method | |
CN102750410B (en) | Optimization design method for blade layering of wind turbine with horizontal shaft | |
CN102262692B (en) | Method for optimizing skins of airplane airfoil by subsonic flutter | |
Bir | Computerized method for preliminary structural design of composite wind turbine blades | |
CN103294898A (en) | Method for calculating single rod power of overall reactor core | |
CN107220404A (en) | Composite material automobile accumulator housing design method based on multi-stage optimization | |
CN105975706A (en) | Scheme stage wing parameter estimation method | |
CN106126860A (en) | A kind of hypersonic wing Robust Optimal Design considering mismachining tolerance | |
Li et al. | Cross‐Sectional Design of Composite Rotor Blades | |
CN104978450A (en) | Position optimal selection method for active vibration control of helicopter | |
CN104750948A (en) | Optimization method for processing multiple extreme values and multiple restricted problems in flight vehicle design | |
CN113742846A (en) | Optimization method, system and equipment for propelling optimal power unit of near space aircraft | |
CN103678763A (en) | Method for aeroelastic tailoring of composite wing and genetic/sensitivity-based hybrid optimization method of composite wing | |
CN106202841A (en) | A kind of Optimization Design of bed piece supported at three point position | |
CN109271722A (en) | The design method and equipment of the wall thickness of the pylon of wind power generating set | |
Pirrera et al. | Optimization of wind turbine blade spars | |
Bortolotti et al. | An efficient approach to explore the solution space of a wind turbine rotor design process | |
CN104899456A (en) | Real-time correction method for on-orbit spacecraft model | |
Caprace et al. | Incorporating High-Fidelity Aerostructural Analyses in Wind Turbine Rotor Optimization | |
CN113496060A (en) | Pneumatic and structure integrated design method for composite material blade | |
CN105956318A (en) | Improved splitting H-K clustering method-based wind power plant fleet division method | |
CN107104429A (en) | A kind of power system load dispatching method of meter and distributed energy storage system | |
CN108197353A (en) | A kind of solid propellant rocket Fixture Design method of the APDL language based on ANSYS |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
AD01 | Patent right deemed abandoned |
Effective date of abandoning: 20230602 |
|
AD01 | Patent right deemed abandoned |