• Title/Summary/Keyword: Damage Tolerance Test

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A Study on Flaw Tolerance Evaluation of a Main Rotor Actuator for Rotorcraft (회전익 항공기용 주 로터 작동기에 대한 손상허용 평가 연구)

  • Park, Juwon;Jeong, Jeongrae
    • Journal of Aerospace System Engineering
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    • v.14 no.spc
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    • pp.1-6
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    • 2020
  • The flaw tolerance evaluation requirement prescribed in Federal Aviation Regulation (FAR) §29.571 Amendment 55 was established in 2012. As a result, there are not many datas of flaw tolerance evaluation. This paper introduces the series of processes and evaluation methods carried out for certification based on the flaw tolerance evaluation. An initial flaws were artificially formed on the main rotor actuator and then the damage tolerance test was performed, which was twice life time of design requirements, to demonstrate that the main rotor actuator of the rotorcraft is sufficiently capable of flaw tolerance.

Static Test of a Composite Wing with Damage Tolerance Design (손상 허용 설계를 적용한 복합재 날개의 정하중 시험)

  • Park, Min-Young
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.46 no.6
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    • pp.471-478
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    • 2018
  • Static tests of the composite wing structure were performed to verify damage tolerance design. Both 5 cases of DLLT and 3 cases of DULT were completed to meet requirements for static strength. After inducing BVID and open hole damages on the critical areas of the composite wing based on associated regulations, the DULT and fracture test were performed. In major wing parts, the measured strains and displacements agreed well with those of structural analysis. The initial structural fracture occurred at the area having minimum margin of safety as expected by analysis. As a result, it was confirmed that results from analytic model and strength evaluation were similar to behaviors of the composite wing structure.

A Study on Prediction of Fatigue Damage Crack Growth for Stiffener Bonded Composite Laminate Panel (보강재 본딩접합 복합재 적층판구조 피로손상 균열진전 수명예측에 대한 연구)

  • Kwon, Jung-Ho;Jeong, Seong-Moon
    • Composites Research
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    • v.26 no.2
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    • pp.79-84
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    • 2013
  • The prediction and analysis procedure of fatigue damage crack growth life for a stiffener bonded composite laminate panel including center hole and edge notch damage, was studied. It was performed on the basis of fatigue damage growth test results on a laminated skin panel specimens and the analysis results of stress intensity factor for the stiffener bonded composite panel. According to the comparison between experimental test and prediction results of fatigue damage growth life, it was concluded that the residual strength and damage tolerance assessment can be carried out along to the edge notch crack growth.

A Study of Crack Growth Behavior of Al2024 (Al2024의 균열성장거동에 관한 연구)

  • Lee, Won-Seok;Lee, Hyun-Woo
    • Journal of the Korean Society for Precision Engineering
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    • v.17 no.10
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    • pp.49-55
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    • 2000
  • This study describes the fatigue characteristics for Al2024 alloy, which is aircraft structure material. For this work, the plane-strain fracture toughness test, the plane-stress fracture toughness test and the crack growth rates test were conducted under the standard testing method. Test equipment is a computer-controlled closed-loop fatigue testing machine. The data of each test result is very important to aircraft structure reliability estimation, life prediction, design analysis, endurance analysis and damage tolerance analysis. In addition, the fatigue crack growth threshold($\DeltaKth$) value decreased as the stress ratio increased. Also, $\DeltaKth$ decreased as the thickness increased in LT, TL directions.

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Calibration of crack growth model for damage tolerance analysis (손상허용해석을 위한 균열성장모델 교정)

  • 주영식;김재훈
    • Journal of the Korea Institute of Military Science and Technology
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    • v.5 no.4
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    • pp.67-77
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    • 2002
  • This paper introduces the calibration results of the fatigue crack growth models for damage tolerance analysis of the aircraft structures. Generalized Willenborg model and Wheeler model are calibrated with experimental data tested under the load spectrum of a trainer. The retardation factors such as, shut-off ratio in Generalized Willenborg model and shaping exponent in Wheeler model, are evaluated for aluminum alloys AL2024-T3511, AL7050-T7451 and AL7075-T73511. It is shown that the retardation effect of the crack growth rate depends on the yield strength of material and the maximum stress in the load spectrum. Generalized Willenborg model and Wheeler model give satisfactory prediction of crack growth life but the calibration of the experimental parameters with test is required.

A Study on Damage Tolerance Assessment for the Butt Lap Joint Structure with the Effects of Fretting Fatigue Cracks (프레팅 피로균열 영향을 고려한 항공기 맞대기중첩연결 구조 손상허용성 연구)

  • Kwon, Jung-Ho;Hwang, Kyung-Jung
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.31 no.1
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    • pp.8-17
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    • 2003
  • The butt lap joint structures which are usually designed by the concept of slow crack growth damage tolerance, show frequently the behaviors of multiple site fatigue crack growth around the fastener hole edges due to the fretting between the two jointed parts. In this paper, experimental tests of fatigue crack growth have been performed of a bolted butt lap joint structure having an initial corner crack at the fastener hole edge, with different fretting conditions under a flight load spectrum. The obtained test results were reviewed to investigate the effects of fretting fatigue cracks on the damage tolerance crack growth life. Computations of corner crack growth were also carried out using an existed model to compare with test results.

Comparison of the efficacy of the herbs for upper medication on glucose tolerance induced by high fat/high sucrose feeding-induced mice (본초 귀경에 따른 상소한약의 당내성 유발 마우스에서의 개선 효능 비교 연구)

  • Kang, Seok Yong;Park, Yong-Ki
    • The Korea Journal of Herbology
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    • v.29 no.5
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    • pp.1-8
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    • 2014
  • Objectives : To prove the channel-tropism theory of herbal medicines on diabetes mellitus as emaciation-thirst disease in Korean Medicine Theory, we investigated the selective therapeutic effects of Mori Cortex Radidus (MCR), Schisandrae Fructus (SF), Anemarrhenae Rhizoma (AR) for the upper emaciation on different organs in high fat and high sucrose (HF/HS) feeding-induced prediabetic mice. Methods : Diabetes in C57BL/6 mice was induced by the administration of high fat (45 kal%) and high sucrose (32 kal%) for 8 weeks, and them treated with each extract at 250 or 500 mg/kg body weight for 4 weeks (once a day). Oral glucose tolerance test and body weight was measured once a week. Insulin, total cholesterol, triglyceride, ${\gamma}GTP$, GOT and GPT were measured in the sera of all mice. Histopathological changes of different organs, lung, heart, pancreas, stomach, liver, and kidney were observed by H&E staining. Results : The results revealed that MCR extract inhibited the impaired glucose tolerance and lung damage, and increased serum insulin levels in HF/HS-induced prediabetic mice. SF extract inhibited the impaired glucose tolerance and lung damage, increased serum insulin levels, and decreased serum triglycerige levels. Meanwhile, AR extract inhibited the impaired glucose tolerance and lung damage, and decreased serum levels of insulin, total cholesterol and triglycerige levels. Conclusions : These results demonstrated that MCR, SF, and AR extract as the upper emaciation herbal medicines were followed their channel-tropism theory like a lung, and may have a selective therapeutic potential for control of diabetic stage.

Cold Tolerance Characteristic Test of High Yield Tongil-type Rice Breeding Lines for Processing

  • Kang-Su Kwak;Sea-Kwan Oh;Kuk-Hyun Jung;Dae-Ha Seo
    • Proceedings of the Korean Society of Crop Science Conference
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    • 2022.10a
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    • pp.278-278
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    • 2022
  • Recently, the yield potential of high yield Tongil-type rice varieties has greatly increased, reaching 817kg/10a(Geumgang No.1). Moreover, in order to promote rice consumption and strengthen the competitiveness of the rice processing industry, the R&D of high yield Tongil-type rice varieties for each processing purpose, such as rice noodles, grain feed and industrial materials, has been continuously carried out. However, because Tongil-type rice varieties or lines are generally very vulnerable to cold damage, cold tolerance test can be said to be absolutely necessary to improve the cultivation safety. This study is the result of the seedling and field cold tolerance characteristic tests carried out in 2021 of high yield Tongil-type rice breeding lines. For the cold tolerance characteristic test of seedlings, total 303 high yield rice breeding lines for processing were treated in cold water of 13℃ and irrigation depth of 4cm for 10 days from the third-leaf age, then it was evaluated by comparing the degree of discoloration and withering with the checked varieties(Boramchan, Hanahreum No.2). Also, for the test of field, total 186 high yield rice breeding lines for processing were treated in cold water of 17℃ by keeping pouring day and night from 30 days after transplanting to ripening stage, then it was evaluated by comparing the degree of discoloration, delay of heading, shortening rate of stem length and percent of fertile grain etc. with the checked varieties. And the cold tolerance evaluative criteria were classified as strong(1~3), medium(4~6) and weak(7~9) in overall cold tolerance. (Seedling test) As for the degree of cold tolerance of the check variety, 'Boramchan' and 'Hanahreum No.2' showed a response of 'medium' and 'weak', respectively. However, there was no 'strong' line in the high yield rice breeding lines, 2 lines showed a 'medium' response, and 301 lines showed a 'weak' response. Therefore, except for a few lines(0.7%), most lines(99.3%) showed a 'weak' response. (Field test) In terms of the overall cold tolerance of the check variety, both 'Boramchan' and 'Hanahreum No.2' showed a 'medium' response. Similarly, there was no 'strong' line in the case of high yield rice breeding lines, 20 lines showed a 'medium' response, and 166 lines showed a 'weak' response. Therefore, except for some(10.8%) lines, most(89.2%) lines showed a 'weak' response. From the above results, we selected about 100 individuals with less seed shattering and degeneration of the ear tip, and with a relatively high percent of fertile grain, and are continuing to select lines with improved cold tolerance in the F4~F5 group in this year. As such, most of the Tongil-type rice varieties have poor cold tolerance and thus have low cultivation safety at low temperatures. However, it is important to select improved lines through generational progress because there are some lines that still have a certain level of cold tolerance among them.

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A Study on the Damage Design of Military Aircraft Structure Material by Armor Piercing Bullet Hit (철갑탄 피격에 의한 군용 항공기 구조재료의 손상설계에 관한 연구)

  • Hur, Jang-Wook;Hyun, Young-Jin
    • Journal of the Korea Institute of Military Science and Technology
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    • v.13 no.6
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    • pp.1051-1057
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    • 2010
  • Database for the damage reference by armor piercing bullet test was established for both tube and plate specimens having a range of thickness. As the inclined angles of hit are increasing, it has been found that penetration damage diameter tends to increases accordingly in both specimen of the tube and plate, and such penetration damage diameter on the rear side becomes bigger than those on the front side. The tube specimen showed that the damage becomes bigger when central areas rather than the peripheral were hit. Through the plate test, it also has been found that the penetration ballistic limit for Al alloy is about 25.4mm and that of stainless steel about 12.7mm. From the fatigue analysis results using the database for damage reference, it has been identified whether the safety requirements of military aircraft could be met.

Study on aircraft fatigue life substantiation method (항공기 피로수명 입증방법 연구)

  • Kim, Sung Joon;Kim, Tae-Uk
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.24 no.1
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    • pp.41-46
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    • 2016
  • This paper reviews and summarizes overall fatigue substantiation method of aircraft. The fatigue substantiation method has been studied using the related regulation and examples of industry application. And the comparisons of fatigue substantiation procedure between safe-life and damage tolerance design have been performed. Fatigue substantiation methods have wide variability depend on design methodology and type of aircraft such as fixed wing and rotorcraft. In this study, fatigue substantiation methodologies have been reviewed using analysis and test methods.