MA Gang, HE Bin, LIU Jianhu, PEI Du, YAN Bo, XIE Teng. Research on the correlation between the medium-weight shock test load and the design shock load for ship equipment[J]. Explosion And Shock Waves. doi: 10.11883/bzycj-2025-0227
Citation:
MA Gang, HE Bin, LIU Jianhu, PEI Du, YAN Bo, XIE Teng. Research on the correlation between the medium-weight shock test load and the design shock load for ship equipment[J]. Explosion And Shock Waves. doi: 10.11883/bzycj-2025-0227
MA Gang, HE Bin, LIU Jianhu, PEI Du, YAN Bo, XIE Teng. Research on the correlation between the medium-weight shock test load and the design shock load for ship equipment[J]. Explosion And Shock Waves. doi: 10.11883/bzycj-2025-0227
Citation:
MA Gang, HE Bin, LIU Jianhu, PEI Du, YAN Bo, XIE Teng. Research on the correlation between the medium-weight shock test load and the design shock load for ship equipment[J]. Explosion And Shock Waves. doi: 10.11883/bzycj-2025-0227
At present, there is a lack of research on the correlation between the shock design load specified in GJB1060.1-1991 and the shock test load corresponding to the test conditions specified in GJB150.18-1986 in China. Without a clear understanding of the severities of shock design loads and shock test loads, it is impossible to accurately guide the anti-shock design for the evaluation and testing of ship equipment. Taking the medium-weight shock test specified in GJB150.18-1986 standard as a case, a multi-degree-of-freedom mass stiffness damping dynamic model is established. Considering the single-degree-of-freedom rigid installation equipment installed on the hull (the equipment itself is assumed to be rigid), the shock test load calculation under the standard conditions can be carried out. It can be found that there are upper and lower limits for the shock spectrum velocity of the test load anvil where the lower limit is about 1.75 m/s and the upper limit is about 2.40 m/s. A calculation formula of the shock test spectrum velocity is fitted. Based on the DDAM (dynamic design analysis method) method and the shock design spectrum value specified in GJB1060.1-1991, the shock design spectrum velocity calculated is compared with the shock test load, and the influences of equipment installation frequency, equipment mass and pendulum height on the shock design load and shock test load are analyzed. Based on the comparison results, it is found that the shock design load is more severe than the shock test load. However, when the channel steel span is relatively large (greater than 90 cm) and the equipment installation frequency is relatively high (greater than 80 Hz), the shock test load may be more severe. In addition, the quantitative ratio between the velocity of the shock design spectrum and that of the shock test spectrum is provided. The research results prove the correlation between the shock design load and the shock test load, which can provide reference for the shock resistance design and shock test of the equipment and the revision of relevant standards.
WANG J F, ZHANG Z Y. Impact analysis of impact test machine based on LS-DYNA [J]. Noise and Vibration Control, 2007, 27(6): 10–12. DOI: 10.3969/j.issn.1006-1355.2007.06.004.
WANG X. Optimization of pendulum and numerical simulation of impact for a high-impact shock testing machine with medium [D]. Wuhan: Huazhong University of Science & Technology, 2014.
FENG S, HE Y, WEN Y, et al. Dynamic characteristics of shipborne equipment medium weight shock testing machine [J]. Science Technology and Engineering, 2017, 17(26): 221–226. DOI: 10.3969/j.issn.1671-1815.2017.26.036.
[5]
王涛. 中量级强冲击试验机运动过程力学特性研究 [D]. 武汉: 华中农业大学, 2014.
WANG T. Study on mechanical movement characteristics of middle weight high impact tester [D]. Wuhan: Huazhong Agricultural University, 2014.
[6]
ALEXANDER J E. Damped 2DOF model of MIL-S-901D medium-weight shock machine test [J]. Sound & Vibration, 2016, 50(11): 7–13.
[7]
CLEMENTS E W. Shipboard shock and navy devices for its simulation: SF35-422-110-15046 [R]. Stennis Space Center: Naval Research Laboratory, 1972.
[8]
CLAUDE P, BRUNO A. MIL-S-901 shock testing machines simulation for the selection and prequalification of elastic mountings [C]//Proceedings of the 87th Shock and Vibration Symposium. 2017.
MA G, HE B, LIU J H, et al. Research on the dynamics model of medium-weight impact testing for ship equipment [J]. Shipbuilding of China, 2024, 65(5): 222–232. DOI: 10.3969/j.issn.1000-4882.2024.05.019.
Figure 1. Structure diagram (left) and appearance photo (right) of medium-weight impact machine
Figure 2. Dynamic model of medium-weight impact test[9]
Figure 3. The comparison between the model calculation results and the test results
Figure 4. Impact design acceleration at different hull installation frequencies
Figure 5. Typical rigid installation equipment impact design acceleration and impact test acceleration with span change curve
Figure 6. Curves of impact design spectrum velocity $ {V}_{1} $ and impact test spectrum velocity $ {V}_{2} $ of different equipment mass with installation frequency
Figure 7. The change curves of impact design spectrum velocity $ {V}_{1} $ and impact test spectrum velocity $ {V}_{2} $ with mass at different equipment installation frequencies
Figure 8. Impact test anvil impact spectrum velocity $ {V}_{2} $ with the height of the pendulum change curve
Figure 9. The relationship between the impact spectrum velocity and the mass and frequency of the anvil with a height of 165 cm (the red dotted line is the fitting result, and the black solid line is the calculation result)
Figure 10. The comparison between the calculation results of the impact spectrum velocity formula of the anvil and the simulation results
Figure 11. The ratio of impact design spectrum velocity to impact test spectrum velocity varies with equipment quality and channel steel span