The present invention relates to strength design of a composite material including FRP, and particularly to a technique effective to be applied to optimization and reliability evaluation of FRP as a structural member.
While environmental awareness has been increasing worldwide, weight reduction of mechanical structures such as railroad cars, construction machinery, and wind turbine generators is a very important issue because it greatly contributes to a reduction in energy consumption. From such a background, in various members constituting a mechanical structure, a composite material represented by Fiber-Reinforced Plastics (hereinafter, referred to as FRP), which is superior to metal materials in specific strength and specific rigidity has been widely applied.
In order to apply FRP to structural members, it is necessary to increase the thickness of FRP itself and increase the strength and rigidity by joining with different materials. In particular, the reliability of joining with different materials is an important issue in terms of material cost suppression. In general, FRP has a multi-layer structure in which layers with different fiber directions are stacked, and specs such as the number of layers and the direction of fibers determine mechanical properties of FRP. In addition, this specs greatly affects the reliability of the entire mechanical structure using FRP and the reliability of a joint.
As one of methods for evaluating the reliability of mechanical structures, a method of analyzing a response of a structure to an external force by a structure analysis using the finite element analysis has been widely used. As a method of analyzing a response of a mechanical structure using FRP by a structural analysis using the finite element analysis, there is a method using shell elements (for example, PTL 1). Since the shell element models a multi-layer structure with a single-layer element without thickness, it has advantages such as a reduction in calculation load and a reduction in time required to create a calculation model. On the other hand, it is a method that does not take into account the thickness, the accuracy of evaluation of stress that occurs in a thick FRP may decrease, or a spatial gap may occur in a joint, resulting in a reduction in accuracy of a reliability evaluation of the joint.
In a structural analysis using the finite element analysis, there is also a method of using solid elements that takes into account the thickness. When the solid element is used, a spatial gap does not occur in the joint, and the accuracy of a reliability evaluation of the joint can be maintained. However, when modeling a multi-layer structure with the solid elements, there are problems that it takes a lot of time to reflect corrections/changes of the stacking configuration in a calculation model, and modeling the stacking configuration in detail increases the calculation load. Therefore, it is difficult to efficiently evaluate the reliability of FRP with these methods.
PTL 1: JP 2004-110793 A
As described above, in the reliability evaluation of mechanical structures using FRP, the analysis using the shell elements has the advantages of reducing the calculation load and the time required to create the calculation model, but there is a problem that the accuracy of reliability evaluation of the joint is reduced.
Further, although the analysis using the solid elements can maintain the accuracy in the reliability evaluation of the joint, it has a problem that the calculation load increases and the time required to create the calculation model increases.
Therefore, an object of the present invention is to provide an FRP optimization system and an FRP optimization device capable of efficiently determining the most suitable FRP specs for improving the reliability of the entire mechanical structure using FRP as a structural member and its joints.
Further, another object of the present invention is to provide an FRP reliability evaluation method that is capable of accurately evaluating the reliability of FRP that is a structural member.
In order to solve the above problem, the present invention is an FRP (fiber reinforced plastic) optimization system that determines specs of FRP as a structural member, in which the optimization system includes one or more computing devices, and the computing device includes a first calculating means configured to calculate mechanical properties according to the specs of the FRP input to the optimization system, and a second calculating means configured to determine virtual specs that give properties equivalent to the properties with a smaller number of layers than the input specs of the FRP, and analyzes a response of a mechanical structure to an external force acting on the mechanical structure including the FRP using the virtual specs obtained from the second calculating means, calculates a stress generated in the FRP using the response and the input specs of the FRP, evaluates reliability of the FRP using the stress, and determines the specs of the FRP of the mechanical structure on a basis of a result of the evaluation.
Further, the present invention is an FRP (fiber reinforced plastic) optimization device that determines specs of the FRP as a structural member, the FRP optimization device including: an input unit configured to input the specs of the FRP; and a computation processing unit configured to determine the specs of the FRP of a target mechanical structure, in which the computation processing unit includes: a first calculating means configured to calculate mechanical properties of the FRP on a basis of the specs of the FRP input from the input unit; a second calculating means configured to calculate virtual stacking specs on a basis of the mechanical properties calculated by the first calculating means; a response analysis means configured to analyze a response of a mechanical structure to an external force acting on the mechanical structure including FRP on a basis of the virtual stacking specs calculated by the second calculating means; a stress calculating means configured to calculate a stress generated in the FRP on a basis of the response of the mechanical structure analyzed by the response analysis means and the specs of the FRP input from the input unit; a reliability parameter calculating means configured to calculate a reliability parameter correlated with reliability of the FRP on a basis of the stress calculated by the stress calculating means; and an optimum value calculating means configured to calculate an optimum value of the specs of the FRP of the mechanical structure on a basis of a value of the reliability parameter calculated by the reliability parameter calculating means.
Further, the present invention is an FRP (fiber reinforced plastic) reliability evaluation method for evaluating reliability of the FRP as a structural member, the FRP reliability evaluation method including: (a) a step of inputting specs of the FRP; (b) a step of calculating mechanical properties of the FRP on a basis of the specs of the FRP input in the step (a); (c) a step of calculating virtual stacking specs that give equivalent mechanical properties with a smaller number of layers than the specs of the FRP input in the step (a); (d) a step of analyzing a response of a mechanical structure to an external force acting on the mechanical structure including FRP on a basis of the virtual stacking specs calculated in the step (c); (e) a step of calculating a stress generated in the FRP on a basis of the response of the mechanical structure analyzed in the step (d) and the specs of the FRP input in the step (a); and (f) a step of calculating a reliability parameter correlated with reliability of the FRP on a basis of the stress calculated in the step (e).
According to the present invention, it is possible to achieve an FRP optimization system and an FRP optimization device capable of efficiently determining the most suitable FRP specs for improving the reliability of the entire mechanical structure using FRP as a structural member and its joints.
Further, it is possible to achieve an FRP reliability evaluation method capable of accurately evaluating the reliability of FRP that is a structural member.
This makes it possible to efficiently determine the FRP specs most suitable for improving the reliability of the mechanical structure including the FRP, and improve the reliability of a mechanical structure portion.
The problems, configurations, and effects other than those described above will be more clarified in a description of embodiments described below.
An example of the present invention is described below in conjunction with the drawings. Note that, in each drawing, the same configurations are designated by the same reference numerals, and detailed description of the same portions will be omitted.
With reference to
As shown in
Next, mechanical properties of the FRP are calculated according to the specs of the FRP set in step S1. (Step S2)
Subsequently, virtual stacking specs that give equivalent mechanical properties with a smaller number of layers than the FRP specs set in step S1 is determined (calculated). (Step S3)
Subsequently, a response of a mechanical structure 3 to an external force 4 acting on the mechanical structure 3 including the FRP is analyzed using the virtual stacking specs determined (calculated) in step S3. (Step S4)
Subsequently, a stress generated in the FRP is calculated using the response of the mechanical structure 3 analyzed in step S4 and the FRP specs set in step S1. (Step S5)
Subsequently, the stress calculated in step S5 is used to evaluate (calculate) parameters having a correlation with the reliability of FRP (hereinafter referred to as reliability parameters). (Step S6)
Subsequently, an optimum value of the FRP specs most suitable for improving the reliability of the mechanical structure 3 is searched (calculated) using the value of the reliability parameters evaluated (calculated) in step S6. (Step S7)
Finally, the optimum value of the FRP specs searched (calculated) in step S7 is displayed on an external display device (not shown). (Step S8)
As shown in
Q: Rigidity of each layer of virtual stack
t: Thickness of each layer of virtual stack
A: In-plane rigidity of actual stack
D: Bending rigidity of actual stack
t: Thickness of actual stack
Further, as shown in Equation 4, a stress σ generated in the FRP calculated in step S5 of
[Formula 4]
{σij}=└Qij┘{εij} (i, j=1, 2, 6) (Equation 4)
A device 20 including the optimization system 1 of the present example, as shown in
The first calculating means 200 calculates the mechanical properties of the FRP in step S2 of
As described above, with the FRP optimization system of the present example and the device including the same, it is possible to efficiently search (calculate) an optimum value of the FRP specs most suitable for improving the reliability of the mechanical structure 3 such as a railroad car without sequentially modeling FRP stacking configurations having different specs.
Further, unlike the case of modeling the FRP without taking into account the thickness, the joint can be modeled without a spatial gap, and a reduction in accuracy of reliability evaluation of the joint can be avoided.
Note that the evaluation of the reliability of the entire mechanical structure using FRP as a structural member and its joints can be performed by executing the processing from step S1 to step S6 shown in
An FRP optimization system according to Example 2 will be described with reference to
The optimization system 1 of the present example is different from the optimization system of Example 1 in that the computing device 2 further includes a database 100 in which past operation information of the mechanical structure 3 is accumulated (stored).
As shown in
The stress generated in the FRP is calculated using the response of the mechanical structure 3 analyzed in step S4 and the FRP specs set in step S1. (Step S5)
Then, similarly to the processing flow of
This makes it possible to determine the optimum FRP specs for improving the reliability of the mechanical structure 3 while dealing with a more complicated response during operation than in the optimization system of Example 1.
An FRP optimization system according to Example 3 will be described with reference to
The optimization system 1 of the present example differs from the optimization system of Example 1 in that the computing device 2 further includes a database 120 in which existing specs of FRP are accumulated (stored).
In the optimization system 1 of the present example, as shown in
This makes it possible to select manufacturable FRP specs and to design a structure using existing specs.
An FRP optimization system according to Example 4 will be described with reference to
The optimization system 1 according to the present example is different from the optimization system according to Example 1 in that steps S11 and S12 are further executed in the computing device 2 between step S5 and step S6 of Example 1 (
With the optimization system 1 of the present example, as shown in
This makes it possible to predict the reliability of the mechanical structure 3 with higher accuracy and determine the optimum FRP specs according to the prediction result. Furthermore, it becomes possible to more efficiently determine the optimum value of the FRP specs.
The optimization system in each of the examples described above can also analyze the response of the mechanical structure 3 according to the operation data of the mechanical structure 3 and, based on the analysis result, determine the FRP specs most suitable for improving the reliability of the mechanical structure 3 in operation. This makes it possible to determine, for example, the repair method for the FRP included in the mechanical structure 3 in operation.
Note that, in each of the examples, a railroad car is assumed as a specific example of the mechanical structure 3, but similar effects can be obtained in the field of products requiring a mechanical strength and using thick composite materials such as a construction machine or a wind turbine generator other than the railroad car.
Further, the present invention is not limited to the above-mentioned examples, but includes various modifications. For example, the above-described examples have been described in detail in order to describe the present invention in an easy-to-understand manner, and are not necessarily limited to those having all the configurations described. Further, a part of the configuration of a certain example can be replaced with the configuration of another example, and the configuration of another example can be added to the configuration of a certain example. Further, it is possible to add/delete/replace another configuration with respect to a part of the configurations of the examples.
Number | Date | Country | Kind |
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2018-090051 | May 2018 | JP | national |
Filing Document | Filing Date | Country | Kind |
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PCT/JP2019/003356 | 1/31/2019 | WO | 00 |