Application of Nondestructive Detecting Technology for Geological Radar in a Large-Scale Highway Lanslide Treatment

Zhang, Qiang Yong; Wen, Xin; Li, Xiao Jing

doi:10.4028/0-87849-456-1.2309

Cited by 2 publications

(1 citation statement)

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“…Based on the damage tolerance design theory, 35 the existing crack length (see Fig. 8) of every critical point of ZLJ5551JQZ110V remanufacturing truck crane jib structure is obtained by the nondestructive detecting technology 36 and is taken as the initial crack length. The stress ratios for critical points are confirmed by the stress amplitude and mean spectrums.…”

Section: Fatigue Residual Life Calculationmentioning

confidence: 99%

Fatigue remaining life estimation for remanufacturing truck crane Jib structure based on random load spectrum

Dong

Ren

et al. 2016

Fatigue Fract Eng Mat Struct

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For remanufacturing truck cranes with the characteristic of single piece production, the coupling effect of multi‐physical fields and the correlation of multi‐defect modes are also faced in service. This causes that the safety of crane jib structures has great volatility and uncertainty and is difficult to be judged by fatigue test and damage test. To solve the above problems, an approach of fatigue remaining life evaluation based on random load spectrum is presented. By collecting operating cycle times corresponding to characteristic parameter values during the given time period, the small‐sample measured load spectrum is acquired. Six probability distribution models are used to fit the lifting weight sample in characteristic parameters and the optimal distribution model based on Akaike's information criterion (AIC) is obtained. With the Latin hypercube sampling (LHS) method, a random sample of lifting weight is determined within the fixed inspection cycle. In addition, combining with the rated lifting weight table of truck crane, the corresponding jib length and working range are confirmed. Through defining random values of character parameters and matched operating cycle times, a random load spectrum is gained, thus enabling the extension of measured load spectrum. Depending on the remanufacturing information database, the remanufacturing information of truck crane are retrieved to determine fatigue dangerous cross sections and critical points of jib structures. In order to reflect the variation of structure stress level, the equivalent cross sections of dangerous cross sections are constructed. The first principal stress–time history simulation model for critical points is established, and the rain‐flow counting technology is adopted to extract the two‐dimensional stress spectrum from simulation results. Using the Paris formula combined with the greatest risk principle, the fatigue residual life of jib structure is estimated. Furthermore, the fatigue remaining life evaluation system for jib structure of remanufacturing truck crane is developed for easier application of the proposed method. Finally, as an illustrative example, jib structures of ZLJ5551JQZ110V remanufacturing truck crane are provided to demonstrate the validity and feasibility of this method and system.

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Section: Fatigue Residual Life Calculationmentioning

confidence: 99%