Mathematical Problems in Engineering

Mathematical Problems in Engineering / 2020 / Article

Research Article | Open Access

Volume 2020 |Article ID 8763642 | https://doi.org/10.1155/2020/8763642

Dongfang Hu, Hang Su, Zuhui Shen, "Reliability Analysis of Key Components of the Pod Based on Grey System Theory", Mathematical Problems in Engineering, vol. 2020, Article ID 8763642, 13 pages, 2020. https://doi.org/10.1155/2020/8763642

Reliability Analysis of Key Components of the Pod Based on Grey System Theory

Academic Editor: Alessandro Gasparetto
Received22 Jun 2020
Accepted30 Jul 2020
Published17 Aug 2020

Abstract

For improving the reliability of key components in an airborne pod, gray system theory is introduced into the virtual design of airborne pod. Based on this theory, key components of airborne pod are analyzed and mathematical models of the gray relational model and absolute and relative gray relational model are established, respectively. The differences and relations of the three methods for evaluating the robustness of products are researched. Considering the influence of relevant factors, the change rate of each evaluation index is calculated, and the reliability analysis of the airborne pod body is realized ultimately. Finally, the No. 2 test pod body is the optimal solution, which provides an effective theoretical basis for determining the optimal structure of the airborne pod body.

1. Introduction

For any mechanical system, in order to make the design, development, and manufacturing reliable, that is, to study its reliability, it is necessary to study the reliability of a mechanical system. Mechanical systems are composed of many factors. For the grey system [1], the reliability of a mechanical engineering system describes the ability of the system to accurately, timely, and coordinately complete specified tasks under specified conditions and within a specified time. When this ability is measured with probability, it is reliability [2]. In the service process of a mechanical system, a reliable mechanical system will play a vital role in guaranteeing its working performance.

In recent years, scholars have conducted a series of research and exploration in the field of reliability analysis in view of the diversity and complexity of mechanical structure reliability. The most commonly used methods are probability statistics, fuzzy mathematics, evidence theory, and gray system theory. After consulting the relevant literature, the application research of uncertain systems in various engineering fields has made corresponding progress, for example, combining the analysis method and the checkpoint method with the MATLAB software platform to improve the reliability of key component analysis [3]. The gray system is extended to the theory of probability statistics, the gray probability density function and gray reliability calculation method are studied, and the gray reliability calculation model of stress intensity interference is established [4]. A generalized SPE flux sequence and an extreme value SPE flux sequence taking the occurrence time as a sequence are proposed, and a solar proton event prediction method based on gray GM (1,1) and interval is established [5]. An algorithm based on the self-help method and fuzzy mathematics is proposed, and a fuzzy self-help fuzzy mathematics model based on fusion of bad information objects is established. The measured data of bad information characteristic information objects are self-sampled, and the maximum entropy algorithm is used to obtain the measured data. Self-service distribution of data: self-service fusion sequence uses self-service distribution to estimate the true value and interval of the measured pressure value through the fuzzy membership function [6]. Combining the evidence theory analysis method, an effective model and an efficient and reliable mechanical structure are proposed [7].

However, according to the relevant literature review, the existing research content rarely sees the grayness in the structural design of aeronautical products, especially airborne equipment. This article is based on this purpose.

2. Establishment of the Mathematical Model

2.1. Deng’s Grey System Theory

If the behavior factor of a certain aspect of the mechanical system is and is affected by multiple factors , then this method of using the gray correlation degree of factor to factor to express the influence of on is called gray correlation analysis. The method in which affects the size is called the gray relational analysis method. Based on Deng’s gray relational analysis theory, the reliability of the outer frame of the airborne pod is regarded as a gray system, and its structural reliability assessment is determined by various performance indicators.

Selecting the structural reliability of the pod cabin as the research object and introducing the concept of behavior factors, the cabin structure evaluation index (one of the reliability evaluation indicators described in the technical parameter file of the airborne pod) system characteristic behavior sequence is

In the formula, it is the first evaluation data of a certain behavioral factor.

According to the relevant technical requirements of airborne pod, the reliability of the pod structure depends on the interaction of multiple behavior factors. Based on this, a gray relational mathematical model is constructed.

Theorem 1. Assume that there are all kinds of factors affecting the reliability of products. By testing and extracting relevant data, the sequence of behavioral indicators of the first factor is obtained as follows:

In the formula, I represents the number of the first influencing factors, ;K is the serial number of data, ; and is the K measured value of influencing factor .

From formulas (1) and (2), the corresponding forms of the sequence of system characteristic behavior and comparison data are deduced, which are, in turn, as follows:

2.2. Determination of Mechanical Reliability Parameters

Mechanical reliability can generally be divided into structural reliability and mechanical reliability. Structural reliability mainly considers the strength of the mechanical structure and the failure caused by fatigue, wear, and fracture under load; the mechanism reliability does not consider the failure caused by the strength, but the failure caused by the kinematics during the action, so the reliability is not bias.

As showed in Figure 1, the appearance of the pod body frame is generally spherical. According to the design technical parameters of the pod body, such as the azimuth attitude during flight, the symmetrical shape of aerodynamic characteristics, the extreme environmental requirements at high and low temperatures, the air tightness requirements of the internal environment, the antivibration, and anti-impact requirements, 30 closely related evaluation indicators are determined.

Due to the difference of units between data, there are obvious differences in the order of magnitude of each other. It is obviously necessary to integrate data in dimension. Referring to the evaluation criteria of aeronautical product quality parameters, it is artificially divided into 10 grades: when the evaluation coefficient is 8–10, the index is good, when the evaluation coefficient is 6-7, the index is general, and when the index is 4-5, the index is secondary. Based on 30 performance indicators, the performance of the virtual prototype was tested sequentially. According to the test data, 15 indicators for an evaluation coefficient of 6 were selected as the key factors. According to the given technical requirements document for pod design, the 15 evaluation indexes are sorted from important to general according to the key parts embodied in the design document, as shown in Table 1.


Serial numberSymbol tEchnical parameterEvaluation coefficient (≤10)

1Strength and stiffness of outer spherical shells7 (good)
2Strength and stiffness of the inner frame9 (perfect)
3Antivibration characteristics of outer spherical shells6 (good)
4Vibration resistance of the inner frame8 (perfect)
5Symmetry characteristics of outer spherical shells7 (good)
6Symmetry characteristic of the inner frame7 (good)
7Gas tightness characteristics of the outer spherical shell8 (perfect)
8Corrosion resistance of outer spherical shells6 (good)
9Corrosion resistance of the inner frame8 (perfect)
10Temperature characteristics of outer spherical shell materials8 (perfect)
11Temperature characteristics of inner frame materials9 (perfect)
12Vibration resistance of the azimuth motor7 (good)
13Strength and stiffness of connectors6 (good)
14Fatigue resistance of the bearing drive7 (good)
15Impact resistance of the bearing drive8 (perfect)

According to the research emphasis, the structural reliability of the pod body is selected as the research object, and the system characteristic behavior sequence composed of 15 evaluation indexes of the airborne pod body is obtained:

In the simulation environment, 10 sets of representative virtual test prototypes are selected from a large number of random test prototypes (i.e., random samples) according to different design ideas. According to the abovementioned performance tests, the evaluation tests of the abovementioned 15 indicators were carried out, respectively. According to the corresponding experimental conditions, 10 sets of comparative data sequences of different results are obtained:

Thus, a preliminary data sample for evaluating the reliability of the pod structure is obtained.

3. Establishment of Dun’s Grey Correlation Model

3.1. Interval Value Processing

Based on the correlation degree problem in the gray system theory, it is known that the reliability analysis is mainly to characterize the similarity degree of the system characteristic behavior line graphs of each comparison data line, and the representation index is exactly 15 points, selected according to the point coordinates. The similarity on the graph is used to estimate the result. Then, the evaluation range 1∼10 will be the key to the interval value, and the interval value method will be selected for processing. The interval-valued operator will be introduced to obtain the following relationship:

Then, according to the interval operator quoted by equations (6) and (7), 11 sets of different data ( is the feature sequence) are interval-valued, and the gray system algorithm program is written by Microsoft Visual C++ software. The interval-valued data sequence is

3.2. Difference Sequence and Range

The 11 sets of new sequences derived after interval-valued are, respectively, recorded as , and the following relations are derived from the four axioms of gray correlation [8]:

According to equations (9) and (10), the difference data sequence (retaining 2 significant digits) is obtained, which essentially calculates the geometric distance between the corresponding two points:

For each set of different sequences, the data are retrieved according to the written C++ program, and the maximum and minimum values are, respectively, recorded as

According to equations (12) and (13), it is necessary to find the extreme difference value, wherein corresponding to the first group is the maximum value and the minimum value of the corresponding sequence of the group, and the rest is denoted as ; then, there are

From each limit value, find the extreme difference between the maximum value and the minimum value:

3.3. Correlation Coefficient Sequence and Relevance

Definition 1. The system behavior sequence and the comparison data sequence are as shown in equation (3), defining the resolution coefficient ; letThe given real number constitutes a sequence of gray correlation coefficients. If the coefficient satisfies the gray correlation four axioms, it is called the gray correlation degree of to . According to formulas (12), (13), (16), and (17), the following operation is performed, and the formula of the correlation coefficient is rewritten asAccording to formula (18), the gray correlation coefficient sequence and Deng’s gray correlation degree are derived:Since the weights of each sequence data are similar, the resolution coefficient is 0.5, and the abovementioned algorithm is implemented by C++ program to obtain the corresponding data sequence:The gray correlation degrees corresponding to areIn summary, has the greatest correlation with the behavioral data sequence in the data sequence of 10 sets of virtual prototype performance tests, that is, the test index of the test cabin No. 2 is the most consistent with the assessment criteria.
In order to visually explain the accuracy of the gray correlation analysis, 10 sets of data are, respectively, made into data line diagrams composed of 10 sets of data sequences, as shown in Figure 2.
Figure 2 shows that the 15 performance indicators extracted from the cabin reliability analysis correspond to 15 coordinate points, respectively. According to the Deng’s gray correlation analysis model, the closeness of the data lines and is compared by 15 points. The value is judged by the proximity of the standard value (the corresponding value of the behavioral feature sequence). Therefore, Deng’s gray correlation method is also called the “point correlation method” [9]. Through theoretical calculations, the gray relational order is obtained:In Figure 2, the correlation between the corresponding 10 sets of comparison data sequence lines and the standard characteristic data sequence lines is consistent with the “point correlation method” analysis trend. According to the gray correlation sequence, the case of the virtual prototype cabins and standard characteristic data sequences of No. 2 and No. 7 is investigated.
As shown in Figure 3(a), it can be seen from the comparison between the data display and the test sample cabin No. 1 in Figure 3(b) that although has the greatest correlation with , is not the best in shape similar to . set of data line graphs, such as , has a better degree of similarity. The so-called similarity is the degree to which the graph is consistent with the shape of the standard line graph E. Since the cabin has an economic cost as one of its design requirements, the similarity and proximity of the standard line should be considered separately. Obviously, C is more consistent with B in the similar aspect, but the point correlation does not clearly distinguish this. From the perspective of relevance, as shown in Figure 4, the higher the value, the better the relevance of the indicator.
In the figure, the 15-point correlation index between and is distributed between 0.4 and 1.0. If 8 is taken as the baseline, the virtual prototype of the 7th has 6 indicators that meet the requirements, while the virtual prototype 2 has eight, and if 0.9 is used as the baseline, there are 2 on the 7th and 3 indicators on the 2nd, so the performance of the No. 7 virtual prototype is slightly worse.
The abovementioned results are consistent with Deng’s related analysis results. The main reason is that Deng’s gray correlation analysis model focuses on the similarity of the two curves on the relative displacement of several points on the curve, and the specific analysis does not reflect the characteristics of the system. The relative change rate of the curve and the comparison curve, that is, formula (16), contains only local parameters that reflect the closeness of the two curves and lacks the overall parameters that reflect the closeness of the two curves. The method is judged by the closeness of the limited point, and it cannot fully reflect the specific gray-related requirements such as economic factors, product demand factors, and social factors of the entire mechanical product research object. Therefore, a correlation analysis model based on a macroperspective is needed to ensure that the similarity of similar prototypes is not excluded. The introduction of generalized gray correlation analysis is to consider the relative rate of change factors. The meaning is here.
The biggest innovation in the generalized gray relational analysis system is that the similarity and proximity of the curves can be discussed separately for different engineering actual requirements.

4. Generalized Grey Relational Analysis Model

4.1. Generalized Grey Relational Method

The generalized gray relational analysis model has three objectives for the analysis of pod reliability: first, the curve approach of Deng’s gray correlation analysis further demonstrates the basis of reliability optimal solution selection from a new perspective; second, the data sequence curve. The relative change rate problem between the two is added to the gray correlation analysis, and the original “point correlation analysis” is changed to the “face correlation analysis” between the curves. Starting from the overall situation of the curve distribution, the two curves are obtained by the starting point of zeroing. They are all placed on the coordinate axis, and the size of the area sandwiched between them is used as the criterion for judging the optimal solution of reliability analysis from the macroscopic perspective of the data. Third, the difference between the proximity and similarity of the curve is analyzed accordingly. Also, in the engineering practice, the corresponding factors of economic and design requirements are added. The generalized gray relational analysis is divided into three categories: absolute association method, relative association method, and comprehensive association method, which do not strictly satisfy the gray association four axioms.

4.2. Grey Absolute Correlation Method

Theorem 2. Set the behavior sequence and record the corresponding polyline as ; then,

Definition 2. Let the behavior sequence and D be defined as sequence operators and have the following relationship:According to equations (24) and (25), D is called the starting point zeroing operator, and the starting point of is zeroed, which is recorded as

Theorem 3. We arbitrarily take two sequences of behavior:

The starting point zero image is

It is referred to as

If is always above , then ; if is always below , then ; and if intersects with , the sign is indefinite.

Definition 3. The sequence of : the sum of the time intervals between the observation data is the length of . It should be pointed out that the number of observations in two sequences of equal length is not necessarily equal.

Theorem 4. Let sequence and be of the same length, and are as described in equation (15) of Theorem 2, and is as described in equation (19) of Theorem 2; then,

Equation (30) is the absolute degree of gray correlation between and .

According to the satisfaction condition, for 11 sets of data sequences, since the time intervals between adjacent observation data are the same, and are said to constitute an isochronous sequence.

Theorem 5. Let sequence and be the same length, and both are 1-time-distance sequences, with the corresponding relationship:

The abovementioned sequence is the starting point zeroing image of and , respectively, and the following correspondence is given:

From equations (32)–(34), the following absolute correlation algorithm is derived:

According to the gray absolute relevance theory, the related algorithm is written based on the C++ programming language, and the starting point zeroing process is performed according to the data sequence obtained by and :

The corresponding absolute relevance is

According to the theory of gray absolute correlation analysis, the corresponding C++ program is written to calculate the gray absolute correlation order, which is discharged from left to right according to the degree of relevance:

It can be seen from the results of the absolute correlation degree that the results based on the “face correlation method” are numerically different from those based on the “point correlation method,” mainly because the considerations are different because the corresponding curve of and to the absolute degree of correlation reflects the similarity between the curves.

Specifically, to evaluate the reliability of the test prototype, as shown in Figures 5(a) and 5(b), the area between the data line and the data line in (a) is smaller to the data line in Figure 5(b). The area between the data lines is essentially reflecting the similarity between the curves. After the starting point is zeroed, the starting points are classified into the same point, which is more convincing for the comparison of similarities. With reference to the design requirements of the pod cabin, the optimal solution of the pod structure is studied. The proximity of the standard index will be used as an important reference. In order to meet the requirements of high-quality structural design, No. 2 cabin should be selected in the sixth cabin.

4.3. Grey Relative Correlation Method

The gray relative association method is to characterize the approximate relationship between the behavior sequence and the rate of change of the comparison sequence relative to the starting point. The closer the rate of change of and is, the larger the relative correlation degree will be.

Definition 4. Let and have the same length, and the initial values are not equal to 0. and are their initial values, respectively, and then, the absolute correlation between and is the relative degree of and .
According to the parameters of the existing data sequences and , the initial value processing is performed, that is, the data is divided by the first item number of the sequence, and the new series is obtained, which is consistent with the absolute gray correlation degree algorithm, and is written according to C++. Program operation get its corresponding gray relative relevance: