• Title/Summary/Keyword: Spring-Ratchet

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A Study on Development of the Hybrid Shock Absorber for Lunar Lander (달 착륙선 하이브리드 충격 흡수장치의 개발에 관한 연구)

  • Lee, Jaehyeong;Hwang, Jai-hyuk;Bae, Jae-sung;Lim, Jaehyuk
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2012.10a
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    • pp.81-86
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    • 2012
  • The shock absorber is very important in various mechanical field. Without the shock absorber, the structure might be broken. For lunar lander, honeycomb shock absorber to absorber the shock by using plastic deformation of honeycomb has been used. It is cheap and simple to use but impossible using again without changing the honeycomb. The oleo-pneumatic type shock absorber is not able to use in the cosmos because it is vacuum and its temperature. This study suggests the hybrid shock absorber combined spring-ratchet mechanical shock absorber and eddy current electromagnetic damper. The ratchet restricts rebound of lunar lander and the spring converts the impact energy to the potential energy of the spring. The eddy current damper dissipates the impact energy by eddy current force without contact between the parts. This hybrid shock absorber is reusable while the honeycomb shock absorber isn't. The impact absorbing test of the hybrid shock absorber was carried out. This paper shows that the compared results the hybrid shock absorber with ratchet and without ratchet and evaluates the possibility of using for lunar lander.

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Failure Analysis of SCM435 Bolt for Fixing Automotive Air Brake Spring (자동차 에어 브레이크 스프링 고정용 SCM435 볼트의 파손 해석)

  • Yun, Seo-Hyun;Kim, Min-Heon;Nam, Ki-Woo
    • Journal of the Korean Society of Industry Convergence
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    • v.23 no.1
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    • pp.73-81
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    • 2020
  • This study analyzed the causes of failure of SCM435 bolts that fix the springs of automobile air brakes that have been fractured during use. The cause of failure was analyzed using SEM, EDS, metallogical microscope and Vickers hardness tester. In the fracture, the ratchet mark began at the outer boundary of crack origin, and the grains at crack origin were found to have clear intergranular corrosion. One SCM435 bolt was subjected to a stress of 398 MPa, it's a stress of about 80% of the fatigue limit. As a result of such a large applied stress, cracks occurred at the corrosion origin and were fractured. In order to prevent the SCM435 bolt from fracture, it is necessary to use the correct composition, the accuracy of heat treatment, preventing damage by external impact, preventing corrosion of the damage part by moisture, and introduction a compressive residual stress by peening.