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Chinese Journal of Engineering Design  2026, Vol. 33 Issue (2): 265-274    DOI: 10.3785/j.issn.1006-754X.2026.05.192
Reliability and Quality Design     
Reliability assessment method for RV reducers considering probability-interval hybrid uncertainties
Hongjuan XIE1(),Huajin LEI2,Jia WANG1
1.School of Electrical Engineering, Hebei University of Technology, Tianjin 300401, China
2.Aerospace Life-Support Industries Ltd. , Aviation Industry Corporation of China, Xiangyang 441003, China
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Abstract  

RV (rotate vector) reducers are widely used in complex mechanical systems such as robots. Their reliability directly affects the performance and service life of the entire system, and reliability assessment serves as a crucial foundation for reliability design and optimization. Currently, the reliability assessment for RV reducers is usually based on probability theory. However, due to the complexity of mechanical systems and the multiple sources of factors influencing reliability, it is difficult to obtain the probability distributions of all uncertain factors in practical engineering. Relying solely on probability theory makes it hard to ensure the accuracy of reliability assessment results. To address this issue, the probability-interval hybrid uncertainty theory was innovatively introduced into the reliability assessment of RV reducers. Based on the stress-strength interference theory, the multi-component failure criteria for RV reducers were established, and a new reliability assessment method for RV reducers was proposed. Specifically, a double-layer nested loop solution framework was established to solve the problem of probability-interval hybrid reliability calculation. To tackle the low efficiency of multi-dimensional hybrid reliability calculation, the modified chaos control method and the multiplicative dimensionality reduction method were respectively adopted to improve the solution efficiency of probabilistic reliability and interval uncertainty. The results of numerical examples showed that the characterization method of uncertain factors had a significant impact on the reliability assessment results. Using probability-interval hybrid uncertain parameters to describe the uncertain factors was more in line with the actual service reliability of RV reducers. The proposed method provides a new approach for the reliability evaluation of RV reducers, which can offer valuable support for the reliability design and optimization of complex equipment.



Key wordsRV (rotate vector) reducer      hybrid uncertainty      reliability assessment      failure criterion     
Received: 10 September 2025      Published: 28 April 2026
CLC:  TH 132.46  
Cite this article:

Hongjuan XIE,Huajin LEI,Jia WANG. Reliability assessment method for RV reducers considering probability-interval hybrid uncertainties. Chinese Journal of Engineering Design, 2026, 33(2): 265-274.

URL:

https://www.zjujournals.com/gcsjxb/10.3785/j.issn.1006-754X.2026.05.192     OR     https://www.zjujournals.com/gcsjxb/Y2026/V33/I2/265


考虑概率-区间混合不确定性的RV减速器可靠性评估方法

RV(rotate vector,旋转矢量)减速器广泛应用于机器人等复杂机械系统,其可靠性直接影响整机性能和使用寿命,而可靠性评估是可靠性设计与优化的重要基础。目前,RV减速器的可靠性评估通常基于概率理论。但由于机械系统的复杂性以及可靠性影响因素的多源性,在实际工程中很难获取所有不确定因素的概率分布,单纯基于概率理论难以保证可靠性评估结果的准确性。为此,创新性地将概率-区间混合不确定性理论引入RV减速器的可靠性评估中,并基于应力-强度干涉理论构建RV减速器的多部件失效准则,从而提出了一种新的RV减速器可靠性评估方法。其中,针对概率-区间混合可靠性计算问题,建立了一种双层嵌套循环求解框架;针对多维混合可靠性计算效率低的问题,分别基于修正混沌控制方法和乘法降维法,提高了概率可靠性和区间不确定性的求解效率。算例结果表明,不确定因素表征方式对可靠性评估结果存在显著影响,采用概率-区间混合不确定参量描述可靠性影响因素,更符合RV减速器服役可靠性的实际情况。所提出的方法为RV减速器的可靠性评估提供了新思路,这可为复杂装备的可靠性设计与优化提供有力支撑。


关键词: RV(rotate vector)减速器,  混合不确定性,  可靠性评估,  失效准则 
Fig.1 Schematic diagram of RV reducer structure
Fig.2 Schematic diagram of limit state function in the two-dimensional plane
Fig.3 Iterative process of different probability-based reliability solving methods
Fig.4 Solution process of probability-interval hybrid reliability
参数数值1数值2分布类型参数数值1数值2分布类型
ZN1.50.06正态分布σH lim/MPa1 18035正态分布
ZR0.970.019 4正态分布d/mm240.24正态分布
ZV0.980.019 6正态分布b/mm70.14正态分布
ZW10.02正态分布n/(r/min)45045正态分布
ZL0.960.019 2正态分布u20常数
ZE/(MPa)1/2189.83.0正态分布KA1.50.15区间分布
ZX10常数KV1.040.031 2区间分布
ZH2.50常数KHβ1.20.06区间分布
Zε0.850常数KHα1.0170.03区间分布
Zβ0.990常数
Table 1 Values and distributions of relevant parameters used for contact fatigue failure analysis of planetary gear tooth surface
参数数值1数值2分布类型参数数值1数值2分布类型
YST0.70.02对数正态分布Yε0.980常数
YNT0.20.02对数正态分布Yβ0.690常数
YδrelT10.03Gumbel分布mn/mm1.50常数
YRrelT10.03Gumbel分布σF lim/MPa83025正态分布
YX0.750.015正态分布KFβ1.60.16区间分布
YFa3.80.125 4正态分布KFα1.40.14区间分布
YSa1.630.065 2正态分布
Table 2 Values and distributions of relevant parameters used for bending fatigue failure analysis of planetary gear tooth root
参数数值1数值2分布类型参数数值1数值2分布类型
Z1N1.40.07正态分布K10.13区间分布
Z1L0.970.024 3正态分布K1A1.50.45区间分布
Z1V0.960.019 2正态分布K1V1.040.041 6区间分布
Z1R0.950.019正态分布K1H1.20.06区间分布
Z1W10.02正态分布σ1H lim/MPa1 65050正态分布
Z1X10常数σ1H0/MPa938.775正态分布
Table 3 Values and distributions of relevant parameters used for contact fatigue failure analysis of cycloidal gear tooth surface
样本量100 000200 0001 000 0002 000 000
最大失效概率0.278 50.277 40.276 70.276 9
Table 4 Calculation results of maximum failure probability for planetary gear tooth surface contact fatigue based on MCS method
Fig.5 Variation curves of maximum failure probability of planetary gear tooth surface contact fatigue with safety factor
计算方法λ=0.2λ=0.4λ=0.6λ=0.8
相对误差/%2.532.532.532.53
MCS0.276 70.276 70.276 70.276 7
MCCM-MDRM0.269 70.269 70.269 70.269 7
Table 5 Calculation results of maximum failure probability of planetary gear tooth surface contact fatigue under different control parameters
计算方法λ=0.2λ=0.4λ=0.6λ=0.8
AK-MCS53535353
MCCM-MDRM48241510
Table 6 Iterative solution numbers of maximum failure probability of planetary gear tooth surface contact fatigue under different control parameters
Fig.6 Variation curves of maximum failure probability of planetary gear tooth root bending fatigue with safety factor
计算方法sf2=1.1sf2=1.2sf2=1.3
相对误差/%3.032.171.07
MCS0.006 270.023 510.065 34
MCCM-MDRM0.006 080.023 000.064 64
Table 7 Calculation results of maximum failure probability of planetary gear tooth root bending fatigue under different safety factors
计算方法sf2=1.1sf2=1.2sf2=1.3
AK-MCS887645
MCCM-MDRM201918
Table 8 Iterative solution numbers of maximum failure probability of planetary gear tooth root bending fatigue under different safety factors
Fig.7 Variation curves of maximum failure probability of cycloidal gear tooth surface contact fatigue with safety factor
计算方法sf3=1.0sf3=1.1sf3=1.2
相对误差/%1.651.361.01
MCS0.015 150.106 830.333 95
MCCM-MDRM0.015 400.105 380.337 32
Table 9 Calculation results of maximum failure probability of cycloidal gear tooth surface contact fatigue under different safety factors
计算方法初值条件
U0=0.2IY0=Yc+0.2YrU0=-?0.2IY0=Yc-0.2YrU0=0.4IY0=Yc+0.4YrU0=-?0.4IY0=Yc-?0.4Yr
相对误差/%1.011.011.011.01
MCS0.333 950.333 950.333 950.333 95
MCCM-MDRM0.337 320.337 320.337 320.337 32
Table 10 Calculation results of maximum failure probability of cycloidal gear tooth surface contact fatigue under different initial value conditions
 
 
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