CN109522665A - A kind of Multipurpose Optimal Method of single flow gas-liquid cyclone separator guide vane - Google Patents

A kind of Multipurpose Optimal Method of single flow gas-liquid cyclone separator guide vane Download PDF

Info

Publication number
CN109522665A
CN109522665A CN201811426191.2A CN201811426191A CN109522665A CN 109522665 A CN109522665 A CN 109522665A CN 201811426191 A CN201811426191 A CN 201811426191A CN 109522665 A CN109522665 A CN 109522665A
Authority
CN
China
Prior art keywords
individual
blade
guide vane
matrix
dominated
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
Application number
CN201811426191.2A
Other languages
Chinese (zh)
Inventor
邓雅军
张琳
李国龙
宇波
孙东亮
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Beijing Institute of Petrochemical Technology
Original Assignee
Beijing Institute of Petrochemical Technology
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Beijing Institute of Petrochemical Technology filed Critical Beijing Institute of Petrochemical Technology
Priority to CN201811426191.2A priority Critical patent/CN109522665A/en
Publication of CN109522665A publication Critical patent/CN109522665A/en
Pending legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/10Geometric CAD
    • G06F30/17Mechanical parametric or variational design
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F2111/00Details relating to CAD techniques
    • G06F2111/06Multi-objective optimisation, e.g. Pareto optimisation using simulated annealing [SA], ant colony algorithms or genetic algorithms [GA]

Landscapes

  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Pure & Applied Mathematics (AREA)
  • Mathematical Optimization (AREA)
  • Mathematical Analysis (AREA)
  • Computer Hardware Design (AREA)
  • Evolutionary Computation (AREA)
  • General Engineering & Computer Science (AREA)
  • Computational Mathematics (AREA)
  • Cyclones (AREA)

Abstract

The invention discloses a kind of Multipurpose Optimal Methods of single flow gas-liquid cyclone separator guide vane, initially set up the Model for Multi-Objective Optimization of single flow gas-liquid cyclone separator guide vane, the Model for Multi-Objective Optimization established is to maximize separative efficiency and minimize pressure drop as optimization aim, using blade number, outlet blade angle, width of blade and subtended angle of blade this four blade construction parameters as design variable;The Model for Multi-Objective Optimization established is optimized using second generation non-dominated sorted genetic algorithm, obtains Pareto optimal solution set;According to the actual situation, selection maximizes separative efficiency and minimizes the scheme of pressure drop from the Pareto optimal solution set, and obtains corresponding guide vane structural parameters.This method can conveniently and efficiently obtain the Pareto optimal solution set of cyclone separating property, to select suitable guide vane parameter according to the actual situation for policymaker.

Description

A kind of Multipurpose Optimal Method of single flow gas-liquid cyclone separator guide vane
Technical field
The present invention relates to petroleum gas technical field more particularly to a kind of single flow gas-liquid cyclone separator guide vanes Multipurpose Optimal Method.
Background technique
China deep-sea natural gas resource is extremely abundant, and deep-sea natural gas extraction has important war to guarantee Chinese energy safety Slightly meaning, but deep-sea natural gas extraction difficulty is very big, and harvesting scheme also has very big difference with shallow sea not only different from land.It is international Mainstream recovery method is using underwater multiphase production system, and underwater gas-liquid separator is its key equipment.Single flow gas-liquid eddy flow It is smaller, compact-sized and be easy to parallel connection that separator has many advantages, such as pressure drop, therefore has wide answer in gas-liquid separation under water Use prospect.
Guide vane is the key structure of single flow gas-liquid cyclone separator, due to the presence of guide vane, gas-liquid mixed After object enters axially into cyclone, it is changed into high speed rotation air-flow from axial movement, forms centrifugal field, in the effect of centrifugal force Under, liquid is separated.The structural parameters of guide vane have significant impact, guide vane to the separating property of cyclone Optimization design to improve cyclone separating property have great significance.The core of cyclone guide vane optimization design is thought Want the best match sought between cyclone separating property and guide vane structure, that is, with certain guide vane structure Parameter obtains optimal separating property, but the multi-objective optimization design of power about single flow gas-liquid cyclone separator in the prior art It has not been reported.
Summary of the invention
The object of the present invention is to provide a kind of Multipurpose Optimal Methods of single flow gas-liquid cyclone separator guide vane, should Method can conveniently and efficiently obtain the Pareto optimal solution set of cyclone separating property, to select according to the actual situation for policymaker Select suitable guide vane parameter.
The purpose of the present invention is what is be achieved through the following technical solutions:
A kind of Multipurpose Optimal Method of single flow gas-liquid cyclone separator guide vane, which comprises
Step 1, the Model for Multi-Objective Optimization for establishing single flow gas-liquid cyclone separator guide vane, the multiple target established Optimized model is to maximize separative efficiency and minimize pressure drop as optimization aim, with blade number, outlet blade angle, width of blade It is design variable with this four blade construction parameters of subtended angle of blade;
Step 2 optimizes the Model for Multi-Objective Optimization established using second generation non-dominated sorted genetic algorithm and asks Solution obtains Pareto optimal solution set;
Step 3, according to the actual situation, selection maximizes separative efficiency and minimizes pressure from the Pareto optimal solution set The scheme of drop, and obtain corresponding guide vane structural parameters.
The mathematical model for the Model for Multi-Objective Optimization established in step 1 indicates are as follows:
Objective function:
Wherein, F1(X) separative efficiency is indicated;F2(X) pressure drop is indicated;X indicates that design variable, including blade number, blade go out This four blade construction parameters of bicker, width of blade and subtended angle of blade;
Constraint condition are as follows:
Wherein, gi(X) nonlinear restriction of design variable, h are indicatedi(X) linear restriction of design variable is indicated.
In step 2, the Model for Multi-Objective Optimization established is carried out using second generation non-dominated sorted genetic algorithm excellent Change the process solved specifically:
First using real coding method to this four optimizations of blade number, outlet blade angle, width of blade and subtended angle of blade Variable is encoded, and generates initial population of the individual as second generation non-dominated sorted genetic algorithm at random, and the optimization becomes The group matrix of amount composition is shown below:
Wherein, it is blade number, outlet blade angle, width of blade and leaf that four column of the group matrix are corresponding Piece cornerite;
Then it will increase the corresponding fitness value of each individual in the matrix of above formula expression, finally obtain a such as following formula institute The new matrix F shown:
Non-dominated ranking and crowding sequence are carried out to matrix F, realize the sequence of each individual in matrix F;
Genetic manipulation is carried out to matrix F again, the filial generation for generating parent with it using non-dominated ranking and crowding sequence Merge, generate the group containing 2N individual, after being ranked up, only takes top n individual as hereditary filial generation;
Then judge whether the number of iterations has reached defined maximum number of iterations, terminate to optimize if reaching;If no Reach defined maximum number of iterations, then check value is added to and continues to iterate to calculate in sample set, changes until reaching defined Generation number, and obtain Pareto optimal solution set;
It obtains after obtaining Pareto optimal solution set, using reducing, ratio factor method obtains multiple groups separative efficiency and pressure drop is same The solution of Shi Youhua.
The process that non-dominated ranking and crowding sequence are carried out to matrix F specifically:
Each individual i includes N in group matrix F "iAnd SiTwo parameters, wherein NiIt indicates that individual i can be dominated in population Individual amount, SiIndicate the individual collections dominated by individual i;
During quick non-dominated ranking, all N in population are first foundi=0 individual is simultaneously stored in set Fi', then examine Examine set Fi' each of individual j dominated individual collection Si, by set SiEach of individual k nkSubtract 1;
If nkIndividual k is then put into another set H by -1=0;
The F that will finally obtaini' the non-dominant individual collections of the first order are used as, the individual non-branch having the same in the set With sequence;
It then proceedes to make H above-mentioned progressive operation, the classification until realizing all individuals, after obtaining a non-dominated ranking Matrix F;
Finally, carrying out crowding sequence to matrix F, the sequence of each individual in matrix F is realized.
During carrying out genetic manipulation to matrix F:
Selecting operation uses the tournament method based on size relation between individual adaptation degree, and crossing operation is using uniformly friendship Fork, mutation operator is using uniformly variation.
The corresponding fitness value of the individual includes separative efficiency and pressure drop, and numerical value is obtained by SVM prediction It arrives.
As seen from the above technical solution provided by the invention, the above method can conveniently and efficiently obtain cyclone separation The Pareto optimal solution set of performance, to select suitable guide vane parameter according to the actual situation for policymaker.
Detailed description of the invention
In order to illustrate the technical solution of the embodiments of the present invention more clearly, required use in being described below to embodiment Attached drawing be briefly described, it should be apparent that, drawings in the following description are only some embodiments of the invention, for this For the those of ordinary skill in field, without creative efforts, it can also be obtained according to these attached drawings other Attached drawing.
Fig. 1 is the Multipurpose Optimal Method stream of single flow gas-liquid cyclone separator guide vane provided in an embodiment of the present invention Journey schematic diagram;
Fig. 2 is the schematic diagram of optimization gained Pareto optimal solution set in the embodiment of the present invention.
Specific embodiment
With reference to the attached drawing in the embodiment of the present invention, technical solution in the embodiment of the present invention carries out clear, complete Ground description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.Based on this The embodiment of invention, every other implementation obtained by those of ordinary skill in the art without making creative efforts Example, belongs to protection scope of the present invention.
The embodiment of the present invention is described in further detail below in conjunction with attached drawing, is implemented as shown in Figure 1 for the present invention The Multipurpose Optimal Method flow diagram for the single flow gas-liquid cyclone separator guide vane that example provides, which comprises
Step 1, the Model for Multi-Objective Optimization for establishing single flow gas-liquid cyclone separator guide vane, the multiple target established Optimized model is to maximize separative efficiency and minimize pressure drop as optimization aim, with blade number, outlet blade angle, width of blade It is design variable with this four blade construction parameters of subtended angle of blade;
In this step, the process for establishing the Model for Multi-Objective Optimization of single flow gas-liquid cyclone separator guide vane is specific Are as follows:
According to the mathematical model of optimization design it is found that a problem is optimized need design variable, objective function with And constraint condition, below according to cyclone guide vane the characteristics of, analyze the three elements of optimization design.
(1) design variable
Design variable refers to the correlated variables that objective function is influenced in process of optimization.For an optimization problem, If the number of design variable is n, then design variable can be written as xi, i=1,2 ..., n.If by this n variable by certain rule into Row sequence, can be obtained an array X, it may be assumed that
X=[x1,x2,…,xn]T (1)
The entirety of the array (n-dimensional vector) may make up a design space (n-dimensional space), and each point therein indicates one Kind design scheme, commonly referred to as design point.It is exactly empty in design by certain method to the process that problem optimizes Between in find the process of optimal design point, this optimum point is exactly final Optimum Design Results.To single flow gas-liquid eddy flow point For optimization design from device guide vane, design variable mainly include blade number, outlet blade angle (blade exit tangentially with The angle of cyclone axial direction), width of blade and subtended angle of blade.
(2) objective function
Objective function is the index for being evaluated the result that optimization design obtains.As previously mentioned, optimization design is just It is that one or more design schemes are found out in design space under the constraint of design variable value range, so that objective function Obtain the process of optimal solution.According to the number of objective function in optimization problem, single goal and multiple-objection optimization two can be classified as Class.For separator, if only optimized to separative efficiency, other characteristics such as pressure drop are not considered, as single goal is excellent Change design problem.It for cyclone, needs to consider simultaneously separative efficiency and pressure drop, establishes the objective function of the two respectively. In addition, it is conflicting between separative efficiency and pressure drop, it can not simply evaluate the superiority and inferiority of a design scheme.Therefore, direct current The optimization problem of formula gas-liquid cyclone separator is a typical multi-objective optimization design of power problem.
(3) constraint condition
In general, the value of design variable needs in allowed limits, and is also possible to meet between each variable certain Relationship.Each specific optimization problem has certain limit to the relationship between the value range and variable of design variable System, these limitations are known as constraint condition.
By being analyzed above it is found that the mathematical model for the Model for Multi-Objective Optimization established indicates are as follows:
Objective function:
Wherein, F1(X) separative efficiency is indicated;F2(X) pressure drop is indicated;X indicates that design variable, including blade number, blade go out This four blade construction parameters of bicker, width of blade and subtended angle of blade;
Constraint condition are as follows:
Wherein, gi(X) nonlinear restriction of design variable, h are indicatedi(X) linear restriction of design variable is indicated.
Step 2 optimizes the Model for Multi-Objective Optimization established using second generation non-dominated sorted genetic algorithm and asks Solution obtains Pareto optimal solution set;
In step 2, the Model for Multi-Objective Optimization established is carried out using second generation non-dominated sorted genetic algorithm excellent Change the process solved specifically:
First using real coding method to this four optimizations of blade number, outlet blade angle, width of blade and subtended angle of blade Variable is encoded, and generates initial population of the individual as second generation non-dominated sorted genetic algorithm at random, and the optimization becomes Shown in the group matrix such as following formula (4) for measuring composition:
Wherein, it is blade number, outlet blade angle, width of blade and leaf that four column of the group matrix are corresponding Piece cornerite;
Then it will increase the corresponding fitness value of each individual in the matrix of formula (4) expression, individual corresponding adaptation here Angle value includes separative efficiency and pressure drop, and numerical value is obtained by SVM prediction, finally obtains one as shown in formula (5) New matrix F:
Non-dominated ranking and crowding sequence are carried out to matrix F, realize the sequence of each individual in matrix F;
Genetic manipulation is carried out to matrix F again;
Then expand sample space by introducing elitism strategy, progeny population and parent population are combined, jointly Next-generation population is generated after competition, is specifically merged parent with the filial generation that it is generated using non-dominated ranking and crowding sequence, The group containing 2N individual is generated, after being ranked up, only takes top n individual as hereditary filial generation;
Judge whether the number of iterations has reached defined maximum number of iterations, terminates to optimize if reaching;If not reaching Check value is then added to and continues to iterate to calculate in sample set by defined maximum number of iterations, until reaching defined iteration time Number obtains Pareto optimal solution set;
It obtains after obtaining Pareto optimal solution set, using ratio factor method is reduced, obtains multiple groups separative efficiency and pressure drop Simultaneously all than preferably solving.
In the specific implementation, the above-mentioned process for carrying out non-dominated ranking and crowding sequence to matrix F specifically:
Each individual i includes N in group matrix F "iAnd SiTwo parameters, wherein NiIt indicates that individual i can be dominated in population Individual amount, SiIndicate the individual collections dominated by individual i;
During quick non-dominated ranking, all N in population are first foundi=0 individual is simultaneously stored in set Fi', then examine Examine set Fi' each of individual j dominated individual collection Si, by set SiEach of individual k nkSubtract 1;
If nkIndividual k is then put into another set H by -1=0;
The F that will finally obtaini' the non-dominant individual collections of the first order are used as, the individual non-branch having the same in the set With sequence;
It then proceedes to make H above-mentioned progressive operation, the classification until realizing all individuals, after obtaining a non-dominated ranking Matrix F;
Finally, carrying out crowding sequence to matrix F, the sequence of each individual in matrix F is realized.
In addition, during carrying out genetic manipulation to matrix F:
Selecting operation uses the tournament method based on size relation between individual adaptation degree, and crossing operation is using uniformly friendship Fork, mutation operator is using uniformly variation.
Step 3, according to the actual situation, selection maximizes separative efficiency and minimizes pressure from the Pareto optimal solution set The scheme of drop, and obtain corresponding guide vane structural parameters.
Above-mentioned optimization method is described in detail with specific example below:
Step 1 establishes the Model for Multi-Objective Optimization of single flow gas-liquid cyclone separator guide vane, to maximize separation Efficiency and minimum pressure drop are optimization aim, with this four blades of blade number, outlet blade angle, width of blade and subtended angle of blade Structural parameters are optimized variable, and the value range of optimized variable is as shown in table 1.
The value range of optimized variable selected by table 1
Note: N indicates blade number
Step 2, using the multiple-objection optimization for the guide vane that second generation non-dominated sorted genetic algorithm obtains step 1 Model is solved, and one group of Pareto optimal solution set is obtained, the specific steps are as follows:
(1) using real number coding method to this four optimizations of blade number, outlet blade angle, width of blade and subtended angle of blade Variable is encoded, and generates initial population of the individual as NSGA-II algorithm at random.The group matrix of optimized variable composition As shown in formula (6), it is blade number, outlet blade angle, width of blade and blade packet that wherein four column of matrix are corresponding Angle.
(2) the corresponding fitness value of each individual (separative efficiency and pressure drop) will be increased in the matrix of formula (6) expression, counted Value is predicted to obtain by support vector machine method, finally obtains a new matrix F as shown in formula (7).
(3) non-dominated ranking.Each individual i includes N in F "iAnd SiTwo parameters, wherein NiIt indicates to dominate in population The individual amount of individual i, SiIndicate the individual collections dominated by individual i.During quick non-dominated ranking, population is first found In all Ni=0 individual is simultaneously stored in set Fi', then investigate set Fi' each of individual j dominated individual collection Si, will Set SiEach of individual k nkSubtract 1.If nkIndividual k is then put into another set H by -1=0.It will finally obtain Fi' the non-dominant individual collections of the first order are used as, the individual non-dominated ranking having the same in the set.It then proceedes to make H Above-mentioned progressive operation, the classification until realizing all individuals, the F matrix after obtaining a non-dominated ranking.Finally, being carried out to F Crowding sequence, realizes the sequence of each individual in matrix F.
(4) genetic manipulation is carried out to matrix F.Wherein, Selecting operation is used based on size relation between individual adaptation degree Tournament method, crossing operation use uniform crossover, and mutation operator is using uniformly variation.The control parameter setting such as table of genetic manipulation Shown in 2.
Parameter setting when 2 genetic algorithm optimization cyclone guide vane of table
(5) expand sample space by introducing elitism strategy, progeny population and parent population are combined, it is common competing Next-generation population is generated after striving.Parent is merged with the filial generation that it is generated using non-dominated ranking and crowding sequence, generation contains There is the group of 2N individual, after being ranked up, only takes top n individual as hereditary filial generation.
(6) judge whether the number of iterations has reached defined maximum number of iterations, if reaching, terminate to optimize;If no Reach defined maximum number of iterations, then check value is added to and continues to iterate to calculate in sample set, changes until reaching defined Generation number.
After obtaining optimal solution set, uses and reduce ratio factor method (in the present embodiment scale factor value for 0.3), obtain Several groups of separative efficiencies and pressure drop are simultaneously all than preferably solving.
Step 3 has been carried out more using guide vane of the optimization method being established above to single flow gas-liquid cyclone separator Objective optimization has obtained including 60 individual Pareto optimal solution sets, has been illustrated in figure 2 in the embodiment of the present invention and optimizes institute The schematic diagram of Pareto optimal solution set is obtained, as can be seen from Figure 2: not dominating mutually between these design points, that is, from one Design point is moved to another design point, and one of objective function improves, then another objective function is necessarily deteriorated.It is deposited in figure In five special optimal design points;Separative efficiency is minimum at point A, pressure drop is also minimum, separative efficiency highest, pressure drop at point E Maximum, when point A is mobile to point B, separative efficiency can be increased substantially by increasing pressure drop;And when point D is mobile to point E, it improves and divides Pressure drop can be dramatically increased from efficiency;Point C is separative efficiency and pressure drop preferably design points.
It is worth noting that, the content being not described in detail in the embodiment of the present invention belongs to professional and technical personnel in the field's public affairs The prior art known.
In conclusion the method for the embodiment of the present invention using maximize separative efficiency and minimize pressure drop as optimization aim into The optimization of row single flow gas-liquid cyclone separator guide vane can find one group of Pareto optimal solution to cut both ways simultaneously Collection, meets the needs of oil and gas gas-liquid separation field difference operating condition, facilitates policymaker according to the actual situation, to select Suitable guide vane structural parameters.
The foregoing is only a preferred embodiment of the present invention, but scope of protection of the present invention is not limited thereto, Within the technical scope of the present disclosure, any changes or substitutions that can be easily thought of by anyone skilled in the art, It should be covered by the protection scope of the present invention.Therefore, protection scope of the present invention should be with the protection model of claims Subject to enclosing.

Claims (6)

1. a kind of Multipurpose Optimal Method of single flow gas-liquid cyclone separator guide vane, which is characterized in that the method packet It includes:
Step 1, the Model for Multi-Objective Optimization for establishing single flow gas-liquid cyclone separator guide vane, the multiple-objection optimization established Model is to maximize separative efficiency and minimize pressure drop as optimization aim, with blade number, outlet blade angle, width of blade and leaf This four blade construction parameters of piece cornerite are optimized variable;
Step 2 optimizes the Model for Multi-Objective Optimization established using second generation non-dominated sorted genetic algorithm, obtains Obtain Pareto optimal solution set;
Step 3, according to the actual situation, selection maximizes separative efficiency and minimizes pressure drop from the Pareto optimal solution set Scheme, and obtain corresponding guide vane structural parameters.
2. the Multipurpose Optimal Method of single flow gas-liquid cyclone separator guide vane, feature exist according to claim 1 In the mathematical model for the Model for Multi-Objective Optimization established in step 1 indicates are as follows:
Objective function:
Wherein, F1(X) separative efficiency is indicated;F2(X) pressure drop is indicated;X indicates design variable, including blade number, blade exit This four blade construction parameters of angle, width of blade and subtended angle of blade;
Constraint condition are as follows:
Wherein, gi(X) nonlinear restriction of design variable, h are indicatedi(X) linear restriction of design variable is indicated.
3. the Multipurpose Optimal Method of single flow gas-liquid cyclone separator guide vane, feature exist according to claim 1 In in step 2, being optimized using second generation non-dominated sorted genetic algorithm to the Model for Multi-Objective Optimization established Process specifically:
First using real coding method to this four optimized variables of blade number, outlet blade angle, width of blade and subtended angle of blade It is encoded, generates initial population of the individual as second generation non-dominated sorted genetic algorithm, the optimized variable group at random At group matrix be shown below:
Wherein, it is blade number, outlet blade angle, width of blade and blade packet that four column of the group matrix are corresponding Angle;
Then will above formula indicate matrix in increase the corresponding fitness value of each individual, finally obtain one it is shown in following formula newly Matrix F:
Non-dominated ranking and crowding sequence are carried out to matrix F, realize the sequence of each individual in matrix F;
Genetic manipulation is carried out to matrix F again, is merged parent with the filial generation that it is generated using non-dominated ranking and crowding sequence, The group containing 2N individual is generated, after being ranked up, only takes top n individual as hereditary filial generation;
Then judge whether the number of iterations has reached defined maximum number of iterations, terminate to optimize if reaching;If not reaching Check value is then added to and continues to iterate to calculate in sample set by defined maximum number of iterations, until reaching defined iteration time Number, and obtain Pareto optimal solution set;
It obtains after obtaining Pareto optimal solution set, using reducing, ratio factor method obtains multiple groups separative efficiency and pressure drop is excellent simultaneously The solution of change.
4. the Multipurpose Optimal Method of single flow gas-liquid cyclone separator guide vane, feature exist according to claim 3 In the process for carrying out non-dominated ranking and crowding sequence to matrix F specifically:
Each individual i includes N in group matrix F "iAnd SiTwo parameters, wherein NiIndicate that individual i can be dominated in population Body quantity, SiIndicate the individual collections dominated by individual i;
During quick non-dominated ranking, all N in population are first foundi=0 individual is simultaneously stored in set Fi', then investigate collection Close Fi' each of individual j dominated individual collection Si, by set SiEach of individual k nkSubtract 1;
If nkIndividual k is then put into another set H by -1=0;
The F that will finally obtaini' the non-dominant individual collections of the first order are used as, the individual non-dominant row having the same in the set Sequence;
It then proceedes to make H above-mentioned progressive operation, the classification until realizing all individuals, the square after obtaining a non-dominated ranking Battle array F;
Finally, carrying out crowding sequence to matrix F, the sequence of each individual in matrix F is realized.
5. the Multipurpose Optimal Method of single flow gas-liquid cyclone separator guide vane, feature exist according to claim 3 During carrying out genetic manipulation to matrix F:
Selecting operation uses the tournament method based on size relation between individual adaptation degree, and crossing operation uses uniform crossover, becomes Xor is using uniformly variation.
6. the Multipurpose Optimal Method of single flow gas-liquid cyclone separator guide vane, feature exist according to claim 3 In the corresponding fitness value of the individual includes separative efficiency and pressure drop, and numerical value is obtained by SVM prediction.
CN201811426191.2A 2018-11-27 2018-11-27 A kind of Multipurpose Optimal Method of single flow gas-liquid cyclone separator guide vane Pending CN109522665A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201811426191.2A CN109522665A (en) 2018-11-27 2018-11-27 A kind of Multipurpose Optimal Method of single flow gas-liquid cyclone separator guide vane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201811426191.2A CN109522665A (en) 2018-11-27 2018-11-27 A kind of Multipurpose Optimal Method of single flow gas-liquid cyclone separator guide vane

Publications (1)

Publication Number Publication Date
CN109522665A true CN109522665A (en) 2019-03-26

Family

ID=65793241

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201811426191.2A Pending CN109522665A (en) 2018-11-27 2018-11-27 A kind of Multipurpose Optimal Method of single flow gas-liquid cyclone separator guide vane

Country Status (1)

Country Link
CN (1) CN109522665A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111125904A (en) * 2019-12-20 2020-05-08 哈尔滨工业大学 Large-scale high-speed rotation equipment blade sorting method based on multi-target regulation
CN111339610A (en) * 2020-02-04 2020-06-26 中国人民解放军空军工程大学 Impeller mechanical rotor blade assembly optimizing and sequencing method
CN112901698A (en) * 2021-03-10 2021-06-04 北京航空航天大学 Isothermal air spring
CN114218688A (en) * 2021-10-28 2022-03-22 北京建筑大学 Method for optimizing characteristic parameters of blades of sectional inclined grooves of ventilated brake disc

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2003106298A (en) * 2001-09-28 2003-04-09 Hitachi Ltd Method and system for designing turbo type fluid machinery
CN107368920A (en) * 2017-07-01 2017-11-21 南京理工大学 A kind of off-peak period multi-train movement energy conservation optimizing method
CN107844835A (en) * 2017-11-03 2018-03-27 南京理工大学 Multiple-objection optimization improved adaptive GA-IAGA based on changeable weight M TOPSIS multiple attribute decision making (MADM)s

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2003106298A (en) * 2001-09-28 2003-04-09 Hitachi Ltd Method and system for designing turbo type fluid machinery
CN107368920A (en) * 2017-07-01 2017-11-21 南京理工大学 A kind of off-peak period multi-train movement energy conservation optimizing method
CN107844835A (en) * 2017-11-03 2018-03-27 南京理工大学 Multiple-objection optimization improved adaptive GA-IAGA based on changeable weight M TOPSIS multiple attribute decision making (MADM)s

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
DEB K,ET AL: "A fast and elitist multi-objective genetic algorithm:NSGA-II", 《IEEE TRANSACTIONS ON EVOLUTIONARY COMPUTATION》 *
卫德强等: "内联式脱液器导叶几何参数优化的数值研究", 《水动力学研究与进展》 *

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111125904A (en) * 2019-12-20 2020-05-08 哈尔滨工业大学 Large-scale high-speed rotation equipment blade sorting method based on multi-target regulation
CN111125904B (en) * 2019-12-20 2024-01-16 哈尔滨工业大学 Large-scale high-speed rotation equipment blade sequencing method based on multi-target regulation and control
CN111339610A (en) * 2020-02-04 2020-06-26 中国人民解放军空军工程大学 Impeller mechanical rotor blade assembly optimizing and sequencing method
CN111339610B (en) * 2020-02-04 2023-04-07 中国人民解放军空军工程大学 Impeller mechanical rotor blade assembly optimizing and sequencing method
CN112901698A (en) * 2021-03-10 2021-06-04 北京航空航天大学 Isothermal air spring
CN114218688A (en) * 2021-10-28 2022-03-22 北京建筑大学 Method for optimizing characteristic parameters of blades of sectional inclined grooves of ventilated brake disc
CN114218688B (en) * 2021-10-28 2024-04-12 北京建筑大学 Sectional type inclined groove blade characteristic parameter optimization method for ventilated brake disc

Similar Documents

Publication Publication Date Title
CN109522665A (en) A kind of Multipurpose Optimal Method of single flow gas-liquid cyclone separator guide vane
CN106096727B (en) A kind of network model building method and device based on machine learning
CN103745258B (en) Complex network community mining method based on the genetic algorithm of minimum spanning tree cluster
CN109190278B (en) Method for sequencing turbine rotor moving blades based on Monte Carlo tree search
CN108509335A (en) Software Test Data Generation Method based on genetic algorithm optimization
CN106971049A (en) A kind of new multi objective optimization method of catalytic cracking piece-rate system
CN107909208A (en) Damage method drops in a kind of taiwan area distribution
CN110068741A (en) A method of the transformer fault diagnosis based on categorised decision tree
CN102629305A (en) Feature selection method facing to SNP (Single Nucleotide Polymorphism) data
CN102708047B (en) Data flow test case generating method
CN104200272A (en) Complex network community mining method based on improved genetic algorithm
CN105512783A (en) Comprehensive evaluation method used for loop-opening scheme of electromagnetic looped network
CN110288048A (en) A kind of submarine pipeline methods of risk assessment of SVM directed acyclic graph
Arshi et al. A multi-objective shuffled frog leaping algorithm for in-core fuel management optimization
Liu et al. Water bloom warning model based on random forest
CN108062363A (en) A kind of data filtering method and system towards active power distribution network
CN108280289A (en) Bump danger classes prediction technique based on local weighted C4.5 algorithms
CN114266110A (en) Efficient optimization design method of cyclone desander based on Ansys Workbench
CN107276093B (en) The Probabilistic Load calculation method cut down based on scene
CN102708157A (en) Apparatus and method for determining stage using technology lifecycle
CN105137238A (en) Fault diagnosis system for gas insulation combination electric appliance
Li et al. A multi-objective particle swarm optimizer with distance ranking and its applications to air compressor design optimization
CN103020864A (en) Corn fine breed breeding method
CN109543759A (en) A kind of prediction technique of single flow gas-liquid cyclone separator separating property
Kandiller A combinatorial optimization tour in cell formation via hypergraphs

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication

Application publication date: 20190326

RJ01 Rejection of invention patent application after publication