• Title/Summary/Keyword: 리벳 배열

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A Study on the Effect of Rivet Layout on the Stress Variation in Doubler Repair (보강재 수리시 리벳 배열이 응력 변화에 미치는 영향 연구)

  • Moon, Ju-Yeon;Shin, Ki-Su
    • Journal of the military operations research society of Korea
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    • v.36 no.1
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    • pp.91-102
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    • 2010
  • Doubler repair is one of the frequently applied methods to repair cracks which occur at the structure of aircraft weapon systems. The requirement of the doubler repair for some of aging aircraft has increased more recently. However very few researches have been conducted until now. In this paper, the effect of the various doubler repair methods was evaluated. Especially, the relationship between the array of revet and the effect of stress concentration was investigated. To calculate variation of the stress with different repair methods, commercial FEA program was utilized. As a result, it was shown that the main factor for the variation of stress is pitch and number of revet line. Furthermore the optimized array of revet for the specific geometries of doubler was suggested.

A Multiple Crack Propagation Analysis considering Initial Flaw and Stress Order in Riveted Specimens (리벳 시편의 초기결함과 응력배열을 고려한 다중균열진전해석)

  • Kim, Jung-Hoon;Zi, Goang-Seup;Kim, Min-Sung;Kong, Jung-Sik
    • Proceedings of the Computational Structural Engineering Institute Conference
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    • 2010.04a
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    • pp.326-329
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    • 2010
  • 항공기는 전체 수명동안 무수한 반복하중에 노출되기 때문에, 동체에 피로로 인한 다중균열이 불가피하게 발생하게 된다. 이 다중균열은 기체의 강성을 저하시킬 뿐 만 아니라, 종국적으로는 해당 기체구조의 파단을 야기할 수 있다. 초기 결함과 운용 중에 작용되는 응력 스펙트럼은 구조물의 피로수명에 영향을 끼치며 고려해야 한다. 본 논문에서는 초기결함 특성을 파악하기 위한 등가초기결함크기 분포를 산출하고 리벳 시편의 다중균열모델에 대해서 초기결함과 응력배열을 고려한 해석을 수행하였다.

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Non-Contact Ultrasonic Testing of Aircraft Joints using Laser Generated Lamb Wave (레이저 여기 램파를 이용한 항공기 판재 접합부의 비접촉식 초음파 검사)

  • Jhang, Kyoung-Young;Kim, Hong-Joon;Ceringlia, Donatella;Djordjevic, Boro
    • Journal of the Korean Society for Nondestructive Testing
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    • v.21 no.2
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    • pp.163-168
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    • 2001
  • Due to aging, adhesively bonded and riveted aircraft lap joints can contain distends, cracks around rivet holes, fatigue induced flaws, and corrosion. It is required for the safety of aircraft to inspect these defects through the whole region of mint in rapid speed. Bond quality or adhesively bonded and riveted aluminum lap splice joints is investigated using non-contact remote ultrasonic nondestructive evaluation (NDE). Non-contact ultrasonic tests are performed using laser generation and air-coupled transducer detection. A Q-switched Nd:YAG laser and a periodic transmission mask are used to generate a selected Lamb mode. The Lamb wave is generated on one side of the lap splice joint, propagates along the plate, interacts with the joint and is detected on the other side by a micromachined air-coupled capacitance transducer. Analysis of recorded signals allows to evaluate the condition of the bond.

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