• 제목/요약/키워드: Damage Tolerance Test

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

  • 박주원;정정래
    • 항공우주시스템공학회지
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    • 제14권spc호
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    • pp.1-6
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    • 2020
  • 미국 연방항공규정(FAR) §29.571 Amendment 55에서 다루고 있는 손상허용 평가 내용은 2012년에 개념 정립이 되었다. 최근 정립된 개념임에 따라 손상허용 평가 개념을 도입하여 입증 절차를 수행한 이력이 많지 않다. 본 논문은 회전익 항공기에서 주요 구조 요소(PSE; Principal Structure Element)로 분류된 주 로터 작동기 개발품을 FAR §29.571 요건의 손상허용 평가를 바탕으로 인증을 위해 수행한 일련의 과정 및 평가 방법들을 소개하고자 한다. 주 로터 작동기는 초기결함을 생성한 후 설계 목표수명의 2배수에 해당하는 손상허용 시험을 수행하였다. 이를 바탕으로 회전익 항공기 주 로터 작동기는 충분한 손상허용능력을 확보하고 있음을 입증하였다.

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

  • 박민영
    • 한국항공우주학회지
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    • 제46권6호
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    • pp.471-478
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    • 2018
  • 본 연구에서는 복합재 날개 구조물에 손상허용설계를 적용하고 이를 입증하기 위한 정하중 시험을 수행하였다. 복합재 날개 구조의 정적강도를 입증하기 위하여 5 조건의 설계 제한하중 시험과 3 조건의 설계 극한하중 시험을 수행하였다. 그 다음으로 손상허용 설계를 입증하기 위하여 관련 규정에 따라서 복합재 주익 주요 취약부위에 BVID 10개, Open hole 11개를 생성 후, 설계 극한하중 시험과 파단시험을 실시하였다. 날개 주요 부위의 변위 및 변형률 시험 결과는 구조해석 결과와 비교적 잘 일치하였으며, 파단시험의 최초 파단부위도 최소안전여유를 갖는 부위에서 발생하여 구조해석 모델 및 강도평가 결과가 실제 구조의 정적 거동과 유사함을 확인하였다.

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

  • 권정호;정성문
    • Composites Research
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    • 제26권2호
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    • pp.79-84
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    • 2013
  • 본 연구에서는 적층판 시편의 피로손상 균열진전 시험결과와 적층보강판 구조의 응력강도 해석결과를 기초로 충격손상을 모사한 원공과 노치손상을 내재한 보강재 본딩접합 적층보강판 구조의 피로손상 균열진전 수명예측에 대하여 고찰하였다. 그리고 적층보강판 구조시편에 대한 손상허용 시험결과와 손상진전 수명예측 해석결과를 비교분석한 결과 손상균열 길이 변화에 따라 최종파단에 대한 잔여강도를 예측하고 손상허용성 평가를 할 수 있었다.

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

  • 이원석;이현우
    • 한국정밀공학회지
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    • 제17권10호
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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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손상허용해석을 위한 균열성장모델 교정 (Calibration of crack growth model for damage tolerance analysis)

  • 주영식;김재훈
    • 한국군사과학기술학회지
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    • 제5권4호
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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.

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

  • 권정호;황경정
    • 한국항공우주학회지
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    • 제31권1호
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    • pp.8-17
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    • 2003
  • 항공기 주구조에서 맞대기중첩연결(Butt Lap Joint) 구조는 저속균열성장 개념의 손상허용설계를 한다. 이러한 연결부 구조는 볼트나 리벳 구멍 가장자리의 부재간 접촉면에서 프레팅에 의한 피로균열이 발생되어 다지점 균열성장 거동을 하는 경우가 많다. 본 연구에서는 초기 모서리균열을 내재한 볼트연결 맞대기중첩연결 구조시편에 프레팅 조건을 달리하여 비행하중스펙트럼 하에서 피로균열 성장거동을 실험적으로 분석하고 잔여강도를 비교하여 프레팅이 균열성장과 손상허용성에 미치는 영향을 고찰하였다. 또한 기존의 응력강도식으로 모서리균열의 성장패턴을 예측하고 실험결과와 비교 분석하였다.

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

  • 강석용;박용기
    • 대한본초학회지
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    • 제29권5호
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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
    • 한국작물학회:학술대회논문집
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    • 한국작물학회 2022년도 추계학술대회
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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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철갑탄 피격에 의한 군용 항공기 구조재료의 손상설계에 관한 연구 (A Study on the Damage Design of Military Aircraft Structure Material by Armor Piercing Bullet Hit)

  • 허장욱;현영진
    • 한국군사과학기술학회지
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    • 제13권6호
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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.

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

  • 김성준;김태욱
    • 한국항공운항학회지
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    • 제24권1호
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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.