CN112052522B - A simplified calculation method of ship hull structure optimization based on fatigue strength - Google Patents
A simplified calculation method of ship hull structure optimization based on fatigue strength Download PDFInfo
- Publication number
- CN112052522B CN112052522B CN202011007513.7A CN202011007513A CN112052522B CN 112052522 B CN112052522 B CN 112052522B CN 202011007513 A CN202011007513 A CN 202011007513A CN 112052522 B CN112052522 B CN 112052522B
- Authority
- CN
- China
- Prior art keywords
- fatigue
- hot spot
- wave
- calculation
- frequency
- 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.)
- Active
Links
- 238000004364 calculation method Methods 0.000 title claims abstract description 120
- 238000005457 optimization Methods 0.000 title claims abstract description 48
- 230000001186 cumulative effect Effects 0.000 claims abstract description 64
- 238000000034 method Methods 0.000 claims abstract description 45
- 238000001228 spectrum Methods 0.000 claims description 17
- 238000004458 analytical method Methods 0.000 claims description 7
- 238000011084 recovery Methods 0.000 claims description 3
- 238000011156 evaluation Methods 0.000 claims description 2
- 238000010183 spectrum analysis Methods 0.000 abstract description 30
- 238000013461 design Methods 0.000 abstract description 25
- 230000008569 process Effects 0.000 abstract description 10
- 238000011160 research Methods 0.000 description 6
- 230000003938 response to stress Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- NAWXUBYGYWOOIX-SFHVURJKSA-N (2s)-2-[[4-[2-(2,4-diaminoquinazolin-6-yl)ethyl]benzoyl]amino]-4-methylidenepentanedioic acid Chemical compound C1=CC2=NC(N)=NC(N)=C2C=C1CCC1=CC=C(C(=O)N[C@@H](CC(=C)C(O)=O)C(O)=O)C=C1 NAWXUBYGYWOOIX-SFHVURJKSA-N 0.000 description 2
- 238000009825 accumulation Methods 0.000 description 2
- 238000013213 extrapolation Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004044 response Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000007405 data analysis Methods 0.000 description 1
- 238000012938 design process Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F30/00—Computer-aided design [CAD]
- G06F30/10—Geometric CAD
- G06F30/15—Vehicle, aircraft or watercraft design
-
- 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]
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F2119/00—Details relating to the type or aim of the analysis or the optimisation
- G06F2119/02—Reliability analysis or reliability optimisation; Failure analysis, e.g. worst case scenario performance, failure mode and effects analysis [FMEA]
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F2119/00—Details relating to the type or aim of the analysis or the optimisation
- G06F2119/04—Ageing analysis or optimisation against ageing
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F2119/00—Details relating to the type or aim of the analysis or the optimisation
- G06F2119/14—Force analysis or force optimisation, e.g. static or dynamic forces
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Geometry (AREA)
- Theoretical Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Computer Hardware Design (AREA)
- Evolutionary Computation (AREA)
- General Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Computational Mathematics (AREA)
- Mathematical Analysis (AREA)
- Mathematical Optimization (AREA)
- Pure & Applied Mathematics (AREA)
- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
Abstract
本发明属于船体结构优化设计技术领域,具体涉及一种基于疲劳强度的船体结构优化简化计算方法。本发明通过船体典型节点结构在某一计算浪向的特定计算频率下,结构热点应力与该浪向的疲劳累积损伤度的关系,以及其每个计算浪向疲劳累积损伤度与疲劳累积总损伤度的关系,给出了一种基于疲劳强度的船体结构优化简化计算方法,该方法可以有效地解决由于船体结构疲劳损伤较大的位置往往是结构较为复杂的部位。相比于因谱分析方法计算过程较复杂,从而导致计算工作十分繁重的问题,本发明可以极大减少计算工作量,提高计算效率,为基于谱分析方法开展结构疲劳强度的优化设计带来极大便利。
The invention belongs to the technical field of ship hull structure optimization design, in particular to a simplified calculation method for ship hull structure optimization based on fatigue strength. In the present invention, the relationship between the hot spot stress of the structure and the fatigue cumulative damage degree of the wave direction, and the fatigue cumulative damage degree and the fatigue cumulative total damage of each calculated wave direction under the specific calculation frequency of a certain calculation wave direction of the typical node structure of the hull A simplified calculation method of hull structure optimization based on fatigue strength is given, which can effectively solve the problem that the position where the fatigue damage of the hull structure is large is often the part with more complex structure. Compared with the problem that the calculation process of the spectrum analysis method is complicated, which leads to the heavy calculation work, the present invention can greatly reduce the calculation workload, improve the calculation efficiency, and bring great advantages for the optimization design of structural fatigue strength based on the spectrum analysis method. Great convenience.
Description
技术领域technical field
本发明属于船体结构优化设计技术领域,具体涉及一种基于疲劳强度的船体结构优化简化计算方法。The invention belongs to the technical field of ship hull structure optimization design, in particular to a simplified calculation method for ship hull structure optimization based on fatigue strength.
背景技术Background technique
疲劳破坏是船体结构主要的失效模式之一,对于结构中出现的疲劳裂纹,需要及时进行修补,否则,裂纹扩展到一定程度将导致船体结构的灾难性破坏。世界上几大船级社都对疲劳强度校核进行了相关的规定,目前各国船级社提出的疲劳强度评估方法主要可分为简化计算和直接计算;直接计算又分为设计波法和谱分析法。其中,谱分析方法是首先计算目标船的不同装载工况、浪向和计算频率下的波浪载荷以及船体结构应力响应,进而得到应力传递函数;然后,结合特定海域的海浪谱和海况资料获得应力响应谱及应力的短期分布;最后,基于线性累积损伤理论并选取相应的曲线,计算得到疲劳评估部位总的累积损伤度;谱分析方法的流程见图1所示。Fatigue damage is one of the main failure modes of the hull structure. Fatigue cracks in the structure need to be repaired in time, otherwise, the crack expansion to a certain extent will lead to catastrophic damage to the hull structure. Several major classification societies in the world have made relevant regulations on fatigue strength checking. At present, the fatigue strength assessment methods proposed by various classification societies can be divided into simplified calculation and direct calculation; direct calculation is divided into design wave method and spectrum. Analysis. Among them, the spectral analysis method is to first calculate the wave load and hull structure stress response of the target ship under different loading conditions, wave directions and calculation frequencies, and then obtain the stress transfer function; then, combine the wave spectrum and sea state data of a specific sea area to obtain the stress The response spectrum and the short-term distribution of stress; finally, based on the linear cumulative damage theory and selecting the corresponding curve, the total cumulative damage degree of the fatigue assessment part is calculated; the flow of the spectrum analysis method is shown in Figure 1.
事实上,船体结构的初始设计方案并非均能满足结构疲劳强度设计使用寿命的要求;因此,在实际的船体典型节点结构疲劳强度评估时,需要对无法满足设计要求的船体结构进行优化设计研究,常用的方法是根据形成的结构优化设计方案不断修改船体结构有限元模型,然后反复进行谱分析计算,其流程见图2;但船体结构疲劳损伤较大的位置往往是结构很复杂的部位,而且谱分析计算过程较复杂、计算工作量十分繁重,这为船体典型节点结构的优化设计带来了很大的难度。In fact, not all the initial design schemes of hull structures can meet the requirements of structural fatigue strength design service life; therefore, in the actual fatigue strength assessment of typical hull joint structures, it is necessary to conduct optimization design research on hull structures that cannot meet the design requirements. The commonly used method is to continuously modify the finite element model of the hull structure according to the formed structural optimization design scheme, and then repeatedly perform the spectral analysis and calculation, the process of which is shown in Figure 2; however, the position where the fatigue damage of the hull structure is large is often the part with very complex structure, and The calculation process of spectral analysis is complicated and the workload of calculation is very heavy, which brings great difficulty to the optimal design of the typical node structure of the hull.
发明内容SUMMARY OF THE INVENTION
本发明的目的在于提供一种基于疲劳强度的船体结构优化简化计算方法。The purpose of the present invention is to provide a simplified calculation method of ship hull structure optimization based on fatigue strength.
本发明的目的通过如下技术方案来实现:包括以下步骤:The object of the present invention is achieved through the following technical solutions: comprise the following steps:
步骤1:输入船体结构模型、待计算的浪向u和该浪向的频率ω,将船体结构模型转化为有限元分析模型;Step 1: Input the hull structure model, the wave direction u to be calculated and the frequency ω of the wave direction, and convert the hull structure model into a finite element analysis model;
步骤2:对船体结构的有限元分析模型进行疲劳强度评估,获取船体结构的疲劳热点;Step 2: Evaluate the fatigue strength of the finite element analysis model of the hull structure, and obtain the fatigue hot spots of the hull structure;
步骤3:对船体结构的疲劳热点施加n种不同角度的浪向,获取在每种浪向下疲劳热点处的疲劳累积损伤度Di,i=1,2,…,n;选择对应疲劳累积损伤度最大值的浪向,作为最危险浪向;最危险浪向对疲劳热点的疲劳累积损伤度为Dmax;Step 3: Apply n wave directions of different angles to the fatigue hot spot of the hull structure, and obtain the fatigue cumulative damage degree D i at the fatigue hot spot under each wave, i=1,2,...,n; select the corresponding fatigue accumulation The wave direction with the maximum damage degree is regarded as the most dangerous wave direction; the fatigue cumulative damage degree of the most dangerous wave direction to the fatigue hot spot is D max ;
步骤4:计算在最危险浪向下,疲劳热点的疲劳累积损伤度Dmax与总损伤度D的确定性关系系数p;Step 4: Calculate the deterministic relationship coefficient p of the fatigue cumulative damage degree Dmax of the fatigue hot spot and the total damage degree D under the most dangerous wave;
步骤5:对船体结构的疲劳热点施加不同的频率的最危险浪向,获取疲劳热点在最危险浪向下的RAO曲线图,选择对应结构热点应力最大值的频率,作为最危险频率,并获取该结构热点应力最大值σmax;Step 5: Apply the most dangerous wave directions of different frequencies to the fatigue hot spot of the hull structure, obtain the RAO curve of the fatigue hot spot in the downward direction of the most dangerous wave, select the frequency corresponding to the maximum stress value of the structural hot spot as the most dangerous frequency, and obtain The maximum hot spot stress of the structure is σ max ;
步骤6:计算疲劳热点的结构热点应力与浪向疲劳累积损伤度的关系系数R;Step 6: Calculate the relationship coefficient R between the structural hot spot stress of the fatigue hot spot and the cumulative damage degree of wave fatigue;
其中,m为设定的常数;Among them, m is the set constant;
步骤7:计算对疲劳热点施加频率为ω的浪向u时,疲劳热点处的结构热点应力σhot;Step 7: Calculate the structural hot spot stress σ hot at the fatigue hot spot when the wave direction u with frequency ω is applied to the fatigue hot spot;
步骤8:计算对疲劳热点施加频率为ω的浪向u时,疲劳热点处的疲劳累积总损伤度Du;Step 8: Calculate the fatigue cumulative total damage degree D u at the fatigue hot spot when the wave direction u with frequency ω is applied to the fatigue hot spot;
本发明还可以包括:The present invention can also include:
所述的步骤7中计算对疲劳热点施加频率为ω的浪向u时,疲劳热点处的结构热点应力σhot的方法具体为:In the step 7, when the wave direction u with frequency ω is applied to the fatigue hot spot, the method for calculating the structural hot spot stress σ hot at the fatigue hot spot is as follows:
选取疲劳热点附近的四个细化后有限元网格单元,获取各单元应力σkx、σky、τkxy,k=1,2,3,4;疲劳热点处的结构热点应力σhot为:Four refined finite element mesh elements near the fatigue hot spot are selected to obtain the element stress σ kx , σ ky , τ kxy , k=1, 2, 3, 4; the structural hot spot stress σ hot at the fatigue hot spot is:
所述的疲劳热点的结构热点应力与浪向疲劳累积损伤度的关系系数R还可以通过以下方法计算:The relationship coefficient R between the structural hot spot stress of the fatigue hot spot and the cumulative damage degree of wave fatigue can also be calculated by the following method:
其中,n为计算浪向的总数;δ为航率系数;TL为船舶疲劳计算的回复期;为设定的参数,根据船体结构疲劳规范进行选取;Γ()为伽玛函数;pnj为第j个浪向对应的船舶装载状态n出现的概率;pij为第j个浪向对应的海况i出现的概率;pj为第j个浪向出现的概率;ωek为船舶的遭遇频率;θ为浪向角;Qk为在浪向j的某个计算频率k下的结构热点应力与航向j下各计算频率对应的结构热点应力的加和结果的比值,可根据有限元模型直接计算结果获得,在船体典型节点结构的结构型式不变的情况下,其值为定值,且k=1,2,…l,l代表计算频率的总数,根据具体船型来设定;σhot-jk为在航向j的频率k下的结构热点应力;是与选定应用于该简化计算方法的计算频率相对应的结构热点应力的Qk值;Gηη(ωek,θ)为以遭遇频率ωek表达的与航向角θ有关的波能谱,且ωk为波浪频率;U为设定的船舶的航速;Gηη(ωk)为用有义波高Hs和平均跨零周期Tz来表达的波浪谱,且有义波高Hs和平均跨零周期Tz通过选定的海浪谱和海况资料来确定。Among them, n is the total number of calculated wave directions; δ is the voyage coefficient; T L is the recovery period of ship fatigue calculation; is the set parameter, selected according to the fatigue specification of the hull structure; Γ() is the gamma function; p nj is the probability of the occurrence of the ship loading state n corresponding to the jth wave direction; p ij is the corresponding to the jth wave direction. The probability of occurrence of sea state i; p j is the probability of occurrence of the jth wave direction; ω ek is the encounter frequency of the ship; θ is the wave direction angle; Q k is the structural hot spot stress at a certain calculation frequency k of the wave direction j The ratio of the summation results of the structural hot spot stress corresponding to each calculation frequency in the course j can be obtained directly from the finite element model. When the structural type of the typical node structure of the hull remains unchanged, its value is a fixed value, and k=1,2,...l, l represents the total number of calculation frequencies, which are set according to the specific ship type; σ hot-jk is the structural hot spot stress at the frequency k of the course j; is the Q k value of the structural hot spot stress corresponding to the calculation frequency selected to be applied to this simplified calculation method; G ηη (ω ek , θ) is the wave energy spectrum related to the heading angle θ expressed in the encounter frequency ω ek , and ω k is the wave frequency; U is the set speed of the ship; G ηη (ω k ) is the wave spectrum expressed by the significant wave height H s and the average zero-crossing period T z , and The significant wave height H s and the mean zero crossing period T z are determined from selected wave spectrum and sea state data.
本发明的有益效果在于:The beneficial effects of the present invention are:
本发明通过船体典型节点结构在某一计算浪向的特定计算频率下,结构热点应力与该浪向的疲劳累积损伤度的关系,以及其每个计算浪向疲劳累积损伤度与疲劳累积总损伤度的关系,给出了一种基于疲劳强度的船体结构优化简化计算方法,该方法可以有效地解决由于船体结构疲劳损伤较大的位置往往是结构较为复杂的部位。相比于因谱分析方法计算过程较复杂,从而导致计算工作十分繁重的问题,本发明可以极大减少计算工作量,提高计算效率,为基于谱分析方法开展结构疲劳强度的优化设计带来极大便利。In the present invention, the relationship between the hot spot stress of the structure and the fatigue cumulative damage degree of the wave direction, and the fatigue cumulative damage degree and the fatigue cumulative total damage of each calculated wave direction under the specific calculation frequency of a certain calculation wave direction of the typical node structure of the hull A simplified calculation method of hull structure optimization based on fatigue strength is given, which can effectively solve the problem that the position where the fatigue damage of the hull structure is large is often the part with more complex structure. Compared with the problem that the calculation process of the spectrum analysis method is complicated, which leads to the heavy calculation work, the present invention can greatly reduce the calculation workload, improve the calculation efficiency, and bring great advantages for the optimization design of structural fatigue strength based on the spectrum analysis method. Great convenience.
附图说明Description of drawings
图1为谱分析流程图。Figure 1 is a flow chart of spectral analysis.
图2为疲劳谱分析优化流程图。Figure 2 shows the optimization flow chart of fatigue spectrum analysis.
图3为疲劳优化简化方法流程图。Figure 3 is a flowchart of the simplified method for fatigue optimization.
图4为疲劳热点附近的应力梯度图。Figure 4 is a graph of the stress gradient near the fatigue hot spot.
图5为热点应力插值方式示意图。Figure 5 is a schematic diagram of a hot spot stress interpolation method.
图6为疲劳热点的位置示意图。Figure 6 is a schematic diagram of the location of fatigue hot spots.
图7为疲劳热点的有限元细化图。Figure 7 is a finite element refinement of the fatigue hot spot.
图8为疲劳热点180度浪向的RAO曲线图。Figure 8 shows the RAO curve of the fatigue hot spot in 180-degree wave direction.
图9为本发明实施例中浪向疲劳累积损伤度Di与疲劳累积总损伤度D关系表。FIG. 9 is a table showing the relationship between the cumulative damage degree D i of wave direction fatigue and the total cumulative damage degree D of fatigue in the embodiment of the present invention.
图10为本发明实施例中疲劳热点采用简化计算方法的优化结果表。FIG. 10 is a table of optimization results obtained by adopting a simplified calculation method for fatigue hot spots in an embodiment of the present invention.
图11为本发明实施例中疲劳热点采用谱分析计算方法的优化结果表。FIG. 11 is a table of optimization results obtained by adopting the spectral analysis calculation method for fatigue hot spots in the embodiment of the present invention.
图12为本发明实施例中简化计算方法优化结果误差分析表。FIG. 12 is an error analysis table of an optimization result of a simplified calculation method in an embodiment of the present invention.
具体实施方式Detailed ways
下面结合附图对本发明做进一步描述。The present invention will be further described below with reference to the accompanying drawings.
本发明涉及船体结构优化设计领域,特别是涉及基于疲劳强度评估结果的船体结构优化设计的简化计算方法。本发明主要通过船体典型节点结构在某一计算浪向的特定计算频率下,结构热点应力与该浪向的疲劳累积损伤度的关系,以及其每个计算浪向疲劳累积损伤度与疲劳累积总损伤度的关系,给出了一种基于疲劳强度的船体结构优化简化计算方法。该方法可以有效地解决由于船体结构疲劳损伤较大的位置往往是结构较为复杂的部位,且谱分析方法计算过程较复杂,从而导致计算工作十分繁重,为采用谱分析方法对基于疲劳强度的典型节点结构优化设计带来了很大难度的问题。该简化计算方法可以极大减少计算工作量,提高计算效率,为基于谱分析方法开展结构疲劳强度的优化设计带来极大便利。The invention relates to the field of ship hull structure optimization design, in particular to a simplified calculation method for ship hull structure optimization design based on fatigue strength evaluation results. The present invention mainly analyzes the relationship between the structural hot spot stress and the cumulative fatigue damage degree of the wave direction under the specific calculation frequency of a certain calculation wave direction of the typical node structure of the hull, and the relationship between the fatigue cumulative damage degree and the fatigue cumulative damage degree of each calculated wave direction. The relationship of damage degree, a simplified calculation method of ship structure optimization based on fatigue strength is given. This method can effectively solve the problem that the position where the fatigue damage of the hull structure is large is often the part with more complex structure, and the calculation process of the spectrum analysis method is complicated, which leads to heavy calculation work. The optimal design of the node structure brings a very difficult problem. The simplified calculation method can greatly reduce the calculation workload, improve the calculation efficiency, and bring great convenience to the optimization design of structural fatigue strength based on the spectral analysis method.
本发明意在提供一种基于疲劳强度的船体结构优化简化计算方法,以解决采用谱分析方法进行船体典型结构优化设计中存在的优化过程耗时长、工作量巨大的问题。The present invention aims to provide a simplified calculation method for optimization of ship hull structure based on fatigue strength, so as to solve the problems of long time-consuming and huge workload in the optimization process in the optimization design of typical ship hull structure using the spectral analysis method.
为实现对采用谱分析方法,基于疲劳强度的船体典型结构优化设计过程的简化,本方法通过船体典型结构在某一计算浪向的特定计算频率下,结构热点应力与该浪向的疲劳累积损伤度的关系,以及其每个计算浪向的疲劳累积损伤度与疲劳累积总损伤度的关系,确定了船体结构优化设计的简化计算方法。该方法可以极大减少计算工作量,提高计算效率,为基于谱分析方法开展结构疲劳强度的优化设计带来极大便利。In order to realize the simplification of the optimization design process of the typical hull structure based on the fatigue strength using the spectral analysis method, this method uses the typical hull structure in a certain calculation frequency of a certain wave direction, the hot spot stress of the structure and the fatigue cumulative damage of the wave direction. and the relationship between the fatigue cumulative damage degree of each calculated wave direction and the fatigue cumulative damage degree, the simplified calculation method of the optimal design of the hull structure is determined. This method can greatly reduce the computational workload, improve the computational efficiency, and bring great convenience to the optimization design of structural fatigue strength based on the spectral analysis method.
在谱分析方法中,考虑Nload个装载状态,船体结构的疲劳累积损伤度表示为:In the spectral analysis method, considering N load loading states, the fatigue cumulative damage degree of the hull structure is expressed as:
式中:δ-在航率系数;TL—船舶疲劳计算的回复期,规定TL=20年=6.3x108秒;m-所用S-N曲线的两个参数,根据船体结构疲劳规范进行选取;-伽玛函数;m0ijn-第n个装载及海况i和航向j下,应力响应谱的零阶矩;pn-第n个装载的时间分配系数;pi-第i个海况出现的概率;pj-第j个航向出现的概率;υijn-第n个装载,海况i和航向j的应力响应过零率,m2ijn-第n个装载及海况i和航向j下,应力响应谱的二阶矩。In the formula: δ - coefficient of voyage; T L - recovery period of ship fatigue calculation, it is stipulated that T L = 20 years = 6.3x10 8 seconds; m - The two parameters of the SN curve used are selected according to the fatigue specification of the hull structure; - Gamma function; m 0ijn - the zeroth moment of the stress response spectrum for the nth loading and sea state i and heading j; p n - the time distribution coefficient of the nth loading; p i - the probability of occurrence of the ith sea state ; p j - the probability of occurrence of the jth heading; υ ijn - the nth load, the zero-crossing rate of the stress response in sea state i and heading j, m 2ijn - the second moment of the stress response spectrum for the nth load and at sea state i and heading j.
对于本发明,其原理具体如下:For the present invention, its principle is as follows:
1)热点应力计算方法1) Calculation method of hot spot stress
因为无法直接提取热点处的应力,所以根据热点附近的应力梯度运用线性外插的方法计算获得。见图4所示,对细化后的网格模型提取距离热点3t/2和t/2处的表面应力,根据线性关系外插便得到热点处的应力。Because the stress at the hot spot cannot be directly extracted, it is calculated by linear extrapolation according to the stress gradient near the hot spot. As shown in Figure 4, the surface stress at 3t/2 and t/2 distances from the hot spot is extracted from the refined mesh model, and the stress at the hot spot is obtained by extrapolation according to the linear relationship.
同时,由于谱分析方法是把不同频率的单位波幅规则波产生的各项载荷按实部和虚部分别处理,进而得到相应的响应σc、σs;因此,需要对上述应力进行合成处理,得到船体结构在对应计算频率下的应力计算结果,合成应力可表示为σ=σc+iσs,从而有:At the same time, since the spectral analysis method is to treat the loads generated by the regular waves of different frequencies with unit amplitude as the real part and the imaginary part, and then obtain the corresponding responses σ c , σ s ; therefore, it is necessary to synthesize the above stresses, The stress calculation result of the hull structure at the corresponding calculation frequency is obtained, and the resultant stress can be expressed as σ=σ c +iσ s , thus:
选取疲劳热点附近的四个细化后有限元网格单元,可采用如图5所示的应力插值方式,对采用公式(2)处理计算得到的各单元应力σkx、σky、τkxy(k=1,2,3,4)按照公式(3)插值计算获得热点处的应力σhot,x、σhot,y、τhot,xy。Select four refined finite element mesh elements near the fatigue hot spot, and the stress interpolation method as shown in Fig. 5 can be used, and the stress σ kx , σ ky , τ kxy ( k=1, 2, 3, 4) According to formula (3), the stress σ hot,x , σ hot,y , and τ hot,xy at the hot spot are obtained by interpolation calculation.
然后,热点应力σhot可由公式(4)计算确定:Then, the hot spot stress σ hot can be calculated and determined by formula (4):
且σhot取为公式(4)中在插值单元平面45°范围内的计算值。And σ hot is taken as the calculated value in formula (4) within 45° of the plane of the interpolation unit.
2)船体结构浪向疲劳累积损伤度的简化计算方法2) Simplified calculation method of cumulative damage degree of hull structure in wave direction
根据公式(1),船体典型节点结构在某一装载状态、某一海况的某个浪向下的浪向疲劳累积损伤度可由公式(5)计算得到:According to formula (1), the cumulative damage degree of wave direction fatigue of a typical node structure of a hull in a certain loading state and a certain wave down in a certain sea state can be calculated by formula (5):
式中:n-表示计算浪向的总数;pnj-第j个浪向对应的船舶装载状态n出现的概率;pij-为第j个浪向对应的海况i出现的概率;In the formula: n- represents the total number of calculated wave directions; p nj - the probability of the occurrence of the ship loading state n corresponding to the j-th wave direction; p ij - is the probability of the occurrence of the sea state i corresponding to the j-th wave direction;
进一步地,对公式(5)进行简化,此时仅需获得船体典型节点结构在其某一浪向的某个计算频率下的结构热点应力σhot-jk,即可根据公式(6)计算得到船体典型节点结构的航向疲劳累积损伤度:Further, formula (5) is simplified. At this time, it is only necessary to obtain the structural hot spot stress σ hot-jk of the typical node structure of the hull at a certain calculation frequency in a certain wave direction, which can be calculated according to formula (6). The cumulative damage degree of directional fatigue of typical node structure of hull:
其中,定义Rjk为结构热点应力σhot-jk与浪向疲劳累积损伤度Dj的关系系数,有:Among them, R jk is defined as the relationship coefficient between the structural hot spot stress σ hot-jk and the cumulative damage degree D j of wave fatigue, as follows:
式中:ωek-船舶的遭遇频率;θ-航向角,rad;定义Qk为在航向j的某个计算频率k下的结构热点应力与航向j下各计算频率对应的结构热点应力的加和结果的比值,可根据有限元模型直接计算结果获得,在船体典型节点结构的结构型式不变的情况下,其值为定值,且是与选定应用于该简化计算方法的计算频率相对应的结构热点应力的Qk值;Gηη(ωek,θ)-以遭遇频率ωek表达的与航向角θ有关的波能谱,且ωk-波浪频率;U-航速,knots;Gηη(ωk)-用有义波高Hs和平均跨零周期Tz来表达的波浪谱,且其中,Hs-有义波高,Tz-平均跨零周期,二者可通过选定的海浪谱和海况资料来确定。In the formula: ω ek - the encounter frequency of the ship; θ - the heading angle, rad; Q k is defined as the addition of the structural hot spot stress at a certain calculation frequency k of the heading j and the structural hot spot stress corresponding to each calculation frequency on the heading j. The ratio of the result to the result can be obtained directly from the calculation result of the finite element model. Under the condition that the structural type of the typical node structure of the hull remains unchanged, its value is a fixed value, and is the Q k value of the structural hot spot stress corresponding to the calculation frequency chosen to apply this simplified calculation method; G ηη (ω ek , θ) - the wave energy spectrum expressed in the encounter frequency ω ek related to the heading angle θ, and ω k - wave frequency; U - speed, knots; G ηη (ω k ) - wave spectrum expressed in terms of significant wave height H s and mean zero crossing period T z , and Among them, H s - significant wave height, T z - mean zero crossing period, both of which can be determined by selected wave spectrum and sea state data.
Rjk也可通过有限元模型直接计算结果获得,且在船体典型节点结构的结构型式不变的情况下,其值为定值;k代表频率,k=1,2,…l;l代表计算频率的总数,根据具体船型来设定;σhot-jk为在航向j的频率k下的结构热点应力,可根据公式(4)计算得到;m一般取为3。R jk can also be obtained directly by the finite element model, and its value is a fixed value when the structural type of the typical node structure of the hull remains unchanged; k represents the frequency, k=1, 2,...l; l represents the calculation The total number of frequencies is set according to the specific ship type; σ hot-jk is the structural hot spot stress at the frequency k of the course j, which can be calculated according to formula (4); m is generally taken as 3.
3)船体结构的疲劳累积总损伤度的简化计算方法3) Simplified calculation method of fatigue cumulative total damage degree of hull structure
在谱分析方法中,船体典型节点结构的疲劳累积总损伤度与浪向疲劳累积损伤度有如下关系:In the spectral analysis method, the fatigue cumulative damage degree of the typical node structure of the hull is related to the wave direction fatigue cumulative damage degree as follows:
其中:j代表浪向,j=1,2,…,n;n代表总的浪向数,由浪向角的大小决定,当浪向角设为30°间隔时,取n=12;Dj代表j浪向的疲劳累积损伤度。Among them: j represents the wave direction, j=1,2,...,n; n represents the total wave direction number, which is determined by the size of the wave direction angle. When the wave direction angle is set to 30° interval, take n=12; D j represents the fatigue cumulative damage in the j wave direction.
因此,船体典型节点结构的疲劳累积损伤度也可由下式计算得到:Therefore, the fatigue cumulative damage degree of the typical node structure of the hull can also be calculated by the following formula:
式中:σhot-jk为与浪向j下的计算频率k对应的结构热点应力。where: σ hot-jk is the structural hot spot stress corresponding to the calculated frequency k in the wave direction j.
进一步地,本专利中,对于满足浪向疲劳累积损伤度占比疲劳累积总损伤度为定值的船体典型节点结构,确定其在某一浪向的疲劳累积损伤度与疲劳总累积损伤度有如下关系:Further, in this patent, for a typical node structure of a hull that satisfies the proportion of the cumulative fatigue damage degree in the wave direction to a fixed value, it is determined that the cumulative fatigue damage degree in a certain wave direction and the total fatigue cumulative damage degree are related. The following relationship:
其中,定义pn-j为船体结构的浪向疲劳累积损伤度与其疲劳累积总损伤度的关系系数,可通过有限元模型直接计算结果获得,且在船体典型节点结构的结构型式不变的情况下,其值为定值;j代表浪向,定义同上。Among them, p nj is defined as the relationship coefficient between the wave-direction fatigue cumulative damage degree of the hull structure and its total fatigue cumulative damage degree, which can be obtained directly by the finite element model. Its value is a fixed value; j represents the wave direction, and the definition is the same as above.
此时,船体典型节点结构的疲劳累积损伤度可由下式计算得到:At this time, the fatigue cumulative damage degree of the typical node structure of the hull can be calculated by the following formula:
进一步地,可定义Kjk为结构热点应力与疲劳累积总损伤度的关系系数,令此时有:Further, K jk can be defined as the relationship coefficient between the hot spot stress of the structure and the cumulative total damage degree of fatigue, let At this point there are:
本发明的具体方法为:The concrete method of the present invention is:
对于船体某一典型节点结构,在开展结构优化设计过程中,只需计算其在某个浪向的任意计算频率下的结构热点应力,即可计算得到该优化方案下的典型节点结构的疲劳累积总损伤度,而不需要进行全浪向全频率的结构疲劳谱分析计算。For a typical node structure of the hull, in the process of structural optimization design, it is only necessary to calculate the structural hot spot stress at any calculation frequency in a certain wave direction, and then the fatigue accumulation of the typical node structure under the optimization scheme can be calculated. The total damage degree does not need to be calculated by the structural fatigue spectrum analysis of all wave directions and all frequencies.
在获得了船体典型节点结构在某个浪向某计算频率下的结构热点应力后,可结合公式(6)计算出其在该浪向下的浪向疲劳累积损伤度,可根据公式(8)或公式(10)计算出该结构的疲劳累积总损伤度。在获得了船体典型节点结构在某一浪向的疲劳累积损伤度,且能确定其浪向疲劳累积损伤度与疲劳累积总损伤度存在确定关系,则可根据公式(9)计算出该结构的疲劳累积总损伤度;After obtaining the structural hot spot stress of the typical node structure of the hull under a certain wave direction and a certain calculation frequency, the cumulative damage degree of wave fatigue in the wave direction can be calculated according to the formula (6), which can be calculated according to the formula (8) Or formula (10) to calculate the fatigue cumulative total damage of the structure. After obtaining the fatigue cumulative damage degree of a typical node structure of the hull in a certain wave direction, and it can be determined that there is a definite relationship between the fatigue cumulative damage degree in the wave direction and the fatigue cumulative damage degree, the structure can be calculated according to formula (9). Fatigue cumulative total damage;
一种基于疲劳强度的船体结构优化简化计算方法,可概括为:A simplified calculation method of hull structure optimization based on fatigue strength can be summarized as:
1)通过船体典型节点结构在某浪向的某一计算频率下结构热点应力与疲劳累积总损伤度D的关系进行船体结构优化的简化计算;1) The simplified calculation of the hull structure optimization is carried out through the relationship between the structural hot spot stress and the fatigue cumulative total damage D under a certain calculation frequency of a certain wave direction of the typical node structure of the hull;
2)通过船体典型节点结构的浪向疲劳累积损伤度Dj与疲劳累积总损伤度D的关系来进行船体结构优化的简化计算;2) The simplified calculation of the optimization of the hull structure is carried out by the relationship between the cumulative damage degree D j of fatigue in the wave direction and the total cumulative damage degree D of fatigue of the typical node structure of the hull;
3)根据Qk、Rjk的计算公式、或通过船体典型节点结构全浪向全频率的谱分析计算结果获得系数Qk、Rjk;然后,根据公式(6)可计算得到待优化船体典型节点结构在研究浪向下的航向疲劳累积损伤度Dj。3) The coefficients Q k , R jk are obtained according to the calculation formulas of Q k and R jk , or the calculation results of the spectrum analysis of the typical node structure of the hull in the full wave direction and full frequency; then, the typical hull to be optimized can be calculated according to formula (6). The cumulative damage degree D j of the nodal structure under the direction of the studied wave.
根据待优化结构的优化设计方案修改结构模型,并对之施加计算载荷,采用公式(2)处理得到的单元应力σkx、σky、τkxy(k=1,2,3,4);然后,按照公式(3)插值计算获得热点处的应力σhot,x、σhot,y、τhot,xy;再根据公式(4)计算得到其热点应力σhot。Modify the structural model according to the optimal design scheme of the structure to be optimized, and apply the calculated load to it, and use the element stress σ kx , σ ky , τ kxy (k=1, 2, 3, 4) obtained by formula (2); then , and the stress σ hot,x , σ hot,y , τ hot,xy at the hot spot is obtained by interpolation calculation according to formula (3); and the hot spot stress σ hot is obtained by calculation according to formula (4).
结合公式(5)和公式(6)、或通过船体典型节点结构全浪向全频率的谱分析计算结果获得系数Rjk;然后,根据公式(6)可计算得到待优化船体典型节点结构在研究浪向下的浪向疲劳累积损伤度Dj。Combine formula (5) and formula (6), or obtain the coefficient R jk through the spectral analysis and calculation results of the typical hull node structure in all wave directions and all frequencies; The wave-direction fatigue cumulative damage degree D j for the downward wave.
Rjk还可由以下公式计算:R jk can also be calculated by the following formula:
式中:ωek-船舶的遭遇频率;θ-航向角,rad;定义Qk为在航向j的某个计算频率k下的结构热点应力与航向j下各计算频率对应的结构热点应力的加和结果的比值,可根据有限元模型直接计算结果获得,在船体典型节点结构的结构型式不变的情况下,其值为定值,且是与选定应用于该简化计算方法的计算频率相对应的结构热点应力的Qk值;Gηη(ωek,θ)-以遭遇频率ωek表达的与航向角θ有关的波能谱,且ωk-波浪频率;U-航速,knots;Gηη(ωk)-用有义波高Hs和平均跨零周期Tz来表达的波浪谱,且其中,Hs-有义波高,Tz-平均跨零周期,二者可通过选定的海浪谱和海况资料来确定。In the formula: ω ek - the encounter frequency of the ship; θ - the heading angle, rad; Q k is defined as the addition of the structural hot spot stress at a certain calculation frequency k of the heading j and the structural hot spot stress corresponding to each calculation frequency on the heading j. The ratio of the result to the result can be obtained directly from the calculation result of the finite element model. Under the condition that the structural type of the typical node structure of the hull remains unchanged, its value is a fixed value, and is the Q k value of the structural hot spot stress corresponding to the calculation frequency chosen to apply this simplified calculation method; G ηη (ω ek , θ) - the wave energy spectrum expressed in the encounter frequency ω ek related to the heading angle θ, and ω k - wave frequency; U - speed, knots; G ηη (ω k ) - wave spectrum expressed in terms of significant wave height H s and mean zero crossing period T z , and Among them, H s - significant wave height, T z - mean zero crossing period, both of which can be determined by selected wave spectrum and sea state data.
船体典型节点结构的疲劳累积总损伤度可根据公式(8)计算得到,此时需要研究该结构的所有计算浪向;在确定了pn-j的情况下,船体典型节点结构的疲劳累积总损伤度也可根据公式(10)计算得到。The fatigue cumulative damage degree of the typical node structure of the hull can be calculated according to formula (8). At this time, all the calculated wave directions of the structure need to be studied; when p nj is determined, the fatigue cumulative total damage degree of the typical node structure of the hull It can also be calculated according to formula (10).
本发明的特点如下:The characteristics of the present invention are as follows:
在开展疲劳热点的结构优化设计过程中,只需计算疲劳热点在某一计算浪向的某个计算频率下的结构热点应力σhot,再结合公式或即可计算得到该优化方案下的典型节点结构的疲劳累积损伤度,而不需要进行全浪向全频率的结构疲劳谱分析计算。In the process of carrying out the structural optimization design of fatigue hot spots, it is only necessary to calculate the structural hot spot stress σ hot of the fatigue hot spot at a certain calculation frequency in a certain calculation wave direction, and then combine the formula or The fatigue cumulative damage degree of the typical joint structure under the optimization scheme can be calculated without the need to perform the structural fatigue spectrum analysis and calculation in the full wave direction and the full frequency.
1)该简化计算方法可以极大减少计算工作量,提高计算效率。设有n个计算浪向、l个计算频率,那么该方法最少可用原全浪向全频率的谱分析计算时间的时间完成疲劳热点的优化设计工作。1) The simplified calculation method can greatly reduce the calculation workload and improve the calculation efficiency. If there are n calculation wave directions and l calculation frequencies, then this method can at least use the spectral analysis calculation time of the original full wave direction and full frequency. Time to complete the optimal design of fatigue hot spots.
2)该简化计算方法的计算过程简单,可靠性高。经过大量数据的分析研究发现,该简化计算方法计算得到的疲劳热点的疲劳累积损伤度与采用全浪向全频率的谱分析计算方法的误差基本在1%范围内,最高误差可控制在5%左右。2) The simplified calculation method has a simple calculation process and high reliability. After a large amount of data analysis and research, it is found that the error between the fatigue cumulative damage degree of fatigue hot spots calculated by this simplified calculation method and the spectrum analysis calculation method using the full wave direction and full frequency is basically within the range of 1%, and the maximum error can be controlled within 5%. about.
3)该简化计算方法的计算结果偏于安全。通过合理地取定系数Rjk、系数pn-j的值,可保证该简化计算方法的计算结果与采用全浪向全频率的谱分析方法计算结果的误差在可接受的范围,进而能充分保障船体结构的疲劳强度安全。3) The calculation result of this simplified calculation method is on the safe side. By taking the values of the fixed coefficient R jk and the coefficient p nj reasonably, it can be ensured that the error between the calculation result of the simplified calculation method and the calculation result of the spectrum analysis method using the full wave direction and full frequency is within an acceptable range, and then the hull can be fully guaranteed. The fatigue strength of the structure is safe.
对于任何浪向及在某一浪向的任意频率下,该简化计算方法均成立;但在典型结构的最危险浪向及在该浪向下的最危险频率时,可确保该方法的准确性更高、效果更好。This simplified calculation method is valid for any wave direction and at any frequency of a wave direction; however, the accuracy of the method can be guaranteed in the most dangerous wave direction of a typical structure and the most dangerous frequency in the downward direction of the wave Higher and better.
Rjk、pn-j值的选定有一定的要求,在满足要求的情况下,该简化计算方法的效果最佳。There are certain requirements for the selection of R jk and p nj values. When the requirements are met, the simplified calculation method has the best effect.
Rjk、pn-j与船体结构的结构型式有关;在需要采用改变结构型式来进行结构优化的情况下,需要重新确定Rjk、pn-j的值;而在船体结构的结构型式不变,只改变结构的各结构板板厚时,Rjk、pn-j的值保持不变。R jk , p nj are related to the structural type of the hull structure; in the case that the structural type needs to be changed for structural optimization, the values of R jk and p nj need to be re-determined; while the structural type of the hull structure remains unchanged, only changing When the thickness of each structural plate of the structure, the values of R jk and p nj remain unchanged.
实施例1:Example 1:
研究对象:目标船具有高而长的上层建筑,且其在船舯附近终止,造成上建端部与主甲板(1甲板)连接处存在明显的应力集中。在对目标船典型节点结构进行疲劳强度评估时,发现图6标注位置的疲劳热点的疲劳累积损伤度过大,远大于1。因此,选取该疲劳热点作为研究对象;同时,研究发现:该结构的浪向疲劳累积损伤度与疲劳累积总损伤度存在确定关系。疲劳热点研究位置示意图见图6,研究位置的有限元细化模型见图7。Research object: The target ship has a tall and long superstructure, and it terminates near the midship, resulting in obvious stress concentration at the connection between the end of the superstructure and the main deck (1 deck). When evaluating the fatigue strength of the typical node structure of the target ship, it is found that the fatigue cumulative damage of the fatigue hot spots marked in Fig. 6 is too large, far greater than 1. Therefore, this fatigue hotspot is selected as the research object; at the same time, it is found that there is a definite relationship between the cumulative damage degree of wave-direction fatigue and the total cumulative damage degree of fatigue of the structure. The schematic diagram of the fatigue hotspot research location is shown in Figure 6, and the finite element refinement model of the research location is shown in Figure 7.
疲劳热点初始设计方案的各浪向累积损伤度与疲劳累积总损伤度的关系见图9。其中,疲劳热点的谱分析计算的计算浪向个数n=12,各浪向的计算频率个数k=18。由图9可知,疲劳热点的最危险浪向为180°。因此,考虑计算结果的安全性,根据pn-j的取值原则,首先确定pn-j=pn-7=0.15。The relationship between the cumulative damage degree of each wave direction and the total cumulative damage degree of fatigue in the initial design scheme of the fatigue hot spot is shown in Figure 9. Among them, the number of wave directions calculated by the spectral analysis of fatigue hot spots is n=12, and the number of calculation frequencies of each wave direction is k=18. It can be seen from Figure 9 that the most dangerous wave direction of the fatigue hot spot is 180°. Therefore, considering the security of the calculation result, according to the value principle of p nj , first determine p nj =p n-7 =0.15.
疲劳热点在180°浪向的RAO曲线见图8。由图8可知,疲劳热点在该浪向的最危险频率为0.8;对应地,结构的热点应力σhot=57.95Mpa。The RAO curve of the fatigue hot spot in the 180° wave direction is shown in Figure 8. It can be seen from Fig. 8 that the most dangerous frequency of the fatigue hot spot in this wave direction is 0.8; correspondingly, the hot spot stress of the structure is σ hot =57.95Mpa.
此时,考虑简化计算结果的安全性,根据Rjk的计算方法和取值原则,确定Rjk=R78=0.000006。At this time, considering the safety of the simplified calculation result, R jk =R 78 =0.000006 is determined according to the calculation method and value principle of R jk .
首先,考虑采用增加疲劳热点位置结构板板厚的方法来进行结构优化设计工作。采用该简化计算方法最终获得该优化方案的最终优化结果,具体见图10。First, the method of increasing the thickness of the structural plate at the fatigue hot spot position is considered to carry out the structural optimization design work. Using the simplified calculation method, the final optimization result of the optimization scheme is finally obtained, as shown in Figure 10.
对于该优化方案进行一次全浪向全频率的谱分析计算,得到疲劳热点的疲劳累积总损伤度D和180°浪向的浪向疲劳累积损伤度D7,具体见图11。For this optimization scheme, a spectrum analysis and calculation in all wave directions and all frequencies is performed to obtain the fatigue cumulative total damage degree D of the fatigue hot spot and the wave direction fatigue cumulative damage degree D 7 of the 180° wave direction, as shown in Figure 11.
对于该优化方案,已经获得了疲劳热点采用简化计算方法的优化结果和采用谱分析方法的优化结果,现对简化计算方法获得的优化结果进行误差分析,具体见图12。For this optimization scheme, the optimization results of fatigue hot spots using the simplified calculation method and the optimization results of the spectral analysis method have been obtained. Now, the error analysis of the optimization results obtained by the simplified calculation method is carried out, as shown in Figure 12.
由图12可以看出,疲劳热点采用该简化计算方法得到的疲劳累积总损伤度与全浪向全频率的谱分析方法计算结果相比,其误差为1.08%,误差较小,可以认为该简化计算方法是可行的。同时,由图11可知,该优化方案未能使疲劳热点达到疲劳使用寿命的设计要求,因此,需要考虑改变结构型式的优化方案;针对该方案,由于疲劳热点的结构型式发生了改变,在使用该简化计算方法时,就需要重新确定Rjk和pn-j的值,具体计算过程及最终的优化结果不再赘述。It can be seen from Fig. 12 that, compared with the calculation result of the spectrum analysis method in the full wave direction and the full frequency, the error of the fatigue cumulative total damage obtained by the simplified calculation method for the fatigue hot spot is 1.08%, and the error is small. It can be considered that this simplified calculation method is used. The calculation method is feasible. At the same time, it can be seen from Fig. 11 that the optimization scheme fails to make the fatigue hot spot meet the design requirements of fatigue life. Therefore, it is necessary to consider the optimization scheme of changing the structural type; for this scheme, due to the change of the structural type of the fatigue hot spot, the In this simplified calculation method, the values of R jk and p nj need to be re-determined, and the specific calculation process and the final optimization result will not be repeated.
以上所述仅为本发明的优选实施例而已,并不用于限制本发明,对于本领域的技术人员来说,本发明可以有各种更改和变化。凡在本发明的精神和原则之内,所作的任何修改、等同替换、改进等,均应包含在本发明的保护范围之内。The above descriptions are only preferred embodiments of the present invention, and are not intended to limit the present invention. For those skilled in the art, the present invention may have various modifications and changes. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention shall be included within the protection scope of the present invention.
Claims (3)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202011007513.7A CN112052522B (en) | 2020-09-23 | 2020-09-23 | A simplified calculation method of ship hull structure optimization based on fatigue strength |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202011007513.7A CN112052522B (en) | 2020-09-23 | 2020-09-23 | A simplified calculation method of ship hull structure optimization based on fatigue strength |
Publications (2)
Publication Number | Publication Date |
---|---|
CN112052522A CN112052522A (en) | 2020-12-08 |
CN112052522B true CN112052522B (en) | 2022-09-27 |
Family
ID=73604388
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202011007513.7A Active CN112052522B (en) | 2020-09-23 | 2020-09-23 | A simplified calculation method of ship hull structure optimization based on fatigue strength |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN112052522B (en) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112906269B (en) * | 2021-02-08 | 2023-09-26 | 南通中远海运船务工程有限公司 | Method for prolonging fatigue life of complex structure of crude oil-to-barge |
CN113221421B (en) * | 2021-05-17 | 2022-06-21 | 哈尔滨工程大学 | Rapid calculation method for fatigue accumulation total damage degree of optimized structure of ship body |
CN113221245B (en) * | 2021-05-17 | 2022-09-02 | 哈尔滨工程大学 | Rapid calculation method for stress response function curve of hull optimization structure |
CN113268876B (en) * | 2021-05-27 | 2024-05-10 | 大连理工大学 | Marine fan integral coupling fatigue analysis method with additional culture net cage |
CN115230910A (en) * | 2022-08-10 | 2022-10-25 | 南通中远海运川崎船舶工程有限公司 | Intelligent health monitoring system and method for ship structure based on wave radar |
CN118708913B (en) * | 2024-08-28 | 2024-10-25 | 中海油田服务股份有限公司 | Fatigue damage assessment method for floating platform based on wave characteristic parameters |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20080096855A (en) * | 2001-06-13 | 2008-11-03 | 컴퓨메딕스 리미티드 | Methods and apparatus for monitoring consciousness |
US20130116980A1 (en) * | 2011-07-01 | 2013-05-09 | Nirod K. Das | Modular modeling and design of antennas and radio frequency circuits that are arranged in a class of composite structural configurations |
US11471982B2 (en) * | 2017-08-18 | 2022-10-18 | The Regents Of The University Of Michigan | Unified fatigue life evaluation method for welded structures |
CN108733951B (en) * | 2018-05-29 | 2022-06-14 | 上海船舶研究设计院(中国船舶工业集团公司第六0四研究院) | Ship motion response calculation method and device |
CN109376427B (en) * | 2018-10-23 | 2022-07-12 | 哈尔滨工程大学 | 3D Numerical Method for Ship Wave Resistance Increase Considering Pool Wall Effect |
CN109614689B (en) * | 2018-12-07 | 2022-12-13 | 大连船舶重工集团有限公司 | Method for determining long-term fatigue life of ship structure under combined load action |
CN110816772B (en) * | 2019-10-18 | 2020-09-18 | 中船澄西船舶修造有限公司 | Anti-crack design method for ship body structure of wood chip ship |
CN111625980A (en) * | 2020-05-28 | 2020-09-04 | 中国船舶工业集团公司第七0八研究所 | FPSO structure fatigue life calculation method |
-
2020
- 2020-09-23 CN CN202011007513.7A patent/CN112052522B/en active Active
Also Published As
Publication number | Publication date |
---|---|
CN112052522A (en) | 2020-12-08 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN112052522B (en) | A simplified calculation method of ship hull structure optimization based on fatigue strength | |
CN107291995B (en) | Floating marine structure stress calculation method based on spectral analysis method | |
De Masi et al. | Ship motion prediction by radial basis neural networks | |
CN109359336A (en) | A method for building a similar distortion model for lashing bridges based on multi-objective optimization | |
Sutrisno et al. | Analysis static load to strength a Ship-RUV structure using finite element method | |
Li et al. | Advanced empirical formulae for the ultimate strength assessment of continuous hull plate under combined biaxial compression and lateral pressure | |
Li et al. | Assessment of operational limits: Effects of uncertainties in sea state description | |
CN112231842B (en) | Unmanned aerial vehicle structure design method based on fatigue strength | |
Romanoff et al. | Limit State Analyses in Design of Thin-Walled Marine Structures—Some Aspects on Length-Scales | |
Iijima et al. | Effects of weather routing on maximum vertical bending moment in a ship taking account of wave-induced vibrations | |
CN116738889A (en) | A rapid prediction method for near-field sonic explosions in all circumferential angles of supersonic civil aircraft | |
Silva-Campillo et al. | Effect of bow hull form on the buckling strength assessment of the corner bracket connection | |
CN109598084A (en) | A kind of analogy method of the full flank of tooth grinding residual stress of splined driveshaft | |
Bouhlal et al. | Proposal to evaluate the integration of IoT technologies in the maritime domain | |
CN109406027A (en) | An auxiliary decision-making method for ship docking maintenance | |
CN114117950B (en) | Flutter judgment method for shuttle aircraft based on acting principle | |
Xu et al. | Cracking pattern of indented ice sheet bending failures | |
CN110285939A (en) | Random crack growth suppression system for railway steel bridge joint welds based on vibration control | |
Wang et al. | Breaking Pattern of Semi-Infinite Ice Sheets During Bending Failures Against Sloping Structures | |
Zhang et al. | Nonlinear wave loads’ prediction based on three-dimensional hydroelasticity theory in irregular waves | |
Cui et al. | Numerical Modeling and Dynamic Response Analysis of an End-Anchored Floating Bridge With a Damaged Pontoon Under Repair Operation | |
Ringsberg et al. | Committee II-1: Quasi-Static Response | |
Choung et al. | Fully stochastic fatigue analysis for FPSO based on shipyard practices | |
Chen et al. | A numerical method of the ship structures analysis based on meshless local Petrov-Galerkin method | |
Brandão et al. | Generation of Multiple Equivalent Regular Waves for Preliminary Analyses of Floating Production Systems |
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 | ||
GR01 | Patent grant | ||
GR01 | Patent grant |