• Title/Summary/Keyword: 피로 건전성

Search Result 108, Processing Time 0.033 seconds

Accelerated Life Prediction for STS301L Gas Welded Joint (I) - Fillet Type - (STS301L 가스용접 이음재의 가속수명예측 (I) - Fillet Type -)

  • Baek, Seung-Yeb
    • Transactions of the Korean Society of Mechanical Engineers A
    • /
    • v.34 no.4
    • /
    • pp.467-474
    • /
    • 2010
  • Stainless steel sheets are widely used as the structural material for railroad cars and commercial vehicles. Structures made of stainless steel sheets are commonly fabricated by gas welding, For the fatigue design of gas welded joints such as fillet joints, it is necessary to obtain design information of the stress distribution at the weldment as well as the fatigue strength of the gas-welded joints. Further, the influence of the geometrical parameters of gas-welded joints on stress distribution and fatigue strength must be evaluated. in this study, ${\Delta}P-N_f$ curves were obtained by fatigue tests. and, the ${\Delta}P-N_f$ curves were rearranged on the basis of the ${\Delta}{\sigma}-N_f$ relation for the hot-spot stresses at the gas-welded joints. These results, were used for conducting an accelerated life test(ALT) From the experiment results, an acceleration model was derived and factors were estimated. The objective is to obtain the information required for the analysis of the fatigue lifetime of fillet welded joints and for data analysis by the statistic reliability method to save time and cost and to develop optimum accelerated life prediction plans.

Active-Sensing Based Damage Monitoring of Airplane Wings Under Low-Temperature and Continuous Loading Condition (능동센서 배열을 이용한 저온 반복하중 환경 항공기 날개 구조물의 손상 탐지)

  • Jeon, Jun Young;Jung, Hwee kwon;Park, Gyuhae;Ha, Jaeseok;Park, Chan-Yik
    • Journal of the Korean Society for Nondestructive Testing
    • /
    • v.36 no.5
    • /
    • pp.345-352
    • /
    • 2016
  • As aircrafts are being operated at high altitude, wing structures experience various fatigue loadings under cryogenic environments. As a result, fatigue damage such as a crack could be develop that could eventually lead to a catastrophic failure. For this reason, fatigue damage monitoring is an important process to ensure efficient maintenance and safety of structures. To implement damage detection in real-world flight environments, a special cooling chamber was built. Inside the chamber, the temperature was maintained at the cryogenic temperature, and harmonic fatigue loading was given to a wing structure. In this study, piezoelectric active-sensing based guided waves were used to detect the fatigue damage. In particular, a beamforming technique was applied to efficiently measure the scattering wave caused by the fatigue damage. The system was used for detection, growth monitoring, and localization of a fatigue crack. In addition, a sensor diagnostic process was also applied to ensure the proper operation of piezoelectric sensors. Several experiments were implemented and the results of the experiments demonstrated that this process could efficiently detect damage in such an extreme environment.

Environmentally-Assisted Cracking of Austenitic Alloys in a PWR Environment (PWR 환경에서의 오스테나이트계 합금의 환경조장균열)

  • Hong, Jong-Dae;Jang, Hun;Jang, Changheui
    • CORROSION AND PROTECTION
    • /
    • v.12 no.1
    • /
    • pp.30-38
    • /
    • 2013
  • Austenitic stainless steels and Ni-base alloys are widely used as structural materials for major components and piping system in pressurized water reactors (PWRs). These austenitic alloys are known to be susceptible to environmental assisted cracking (EAC), such as environmentally-assisted fatigue (EAF) and primary water stress corrosion cracking (PWSCC) during long-term exposure to PWR primary water environment. In this paper, the current understanding on the phenomena and mechanisms of these EAC are briefly introduced using experimental results and literature review. The mechanisms for EAF and PWSCC for austenitic stainless steels and Ni-base alloys are discussed. Currently, austenitic stainless steels are known to be more susceptible to EAF, while less susceptible to PWSCC than Ni-base alloys. The possible explanations to such behaviors are proposed and discussed in view of the role of hydrogen and internal oxidation.

Method of assessment for allowable size of weld defects (熔接缺陷의 許容限界 評價方法)

  • 강성원
    • Journal of Welding and Joining
    • /
    • v.9 no.3
    • /
    • pp.10-17
    • /
    • 1991
  • 용접구조물에서 용접이음부가 차지하는 비율은 매우 작은 경우가 많지만 용접이음부에는 각종 초기결함(이들 결함으로부터 진전하는 피로 균열, 환경에 의한 균열등을 포함) 및 용접 초기의 부정형을 비롯해서 형상적 불연속 등에서 유기되는 국부적인 응력, 변형률의 집중, 잔류응력, 구속응력, 용접금속이 갖는 숙명적인 야금적 특성의 불균일, bond부 및 HAZ부에서의 용접열 싸이클에 의한 재질의 국부적 강도저하등 용접부의 강도를 저하시키는 인자들이 복합되기 쉽고, 용접구조물 전체의 내파괴 건전성평가에서 용접부가 파괴 강도는 매우 중요하다. 용접구조물의 설계, 시공의 목적은 소요성능의 확보에 있고 구조물이 사용중에 성능손실이나 불안정 파괴가 발생하지 않도록 하는 것이 주요요건이 될 것이다. 현재의 제강기술수준에서 볼 때 모재의 강 도보다 오히려 용접부의 강도 특히 피로강도 및 파괴 인성을 적절하고 합리적으로 평가하는 것이 매우 중요하다고 해도 과언이 아닐 것이다. 용접부의 강도를 평가하는데 있어서 용접부에 발 생하는 용접결함에 대한 평가는 매우 중요하며 이들 결함에 대한 허용결함한계를 평가하여 보수 여부 및 용접구조물의 신뢰성을 평가 할 필요가 있다.

  • PDF

A Study on the Structural Integrity of the First Stage Turbine Blade Caused by Thermal Barrier Coatings and the Cooling Design of the Nozzle (터빈 노즐 및 열차폐 코팅에 따른 고압 1 단 터빈 블레이드의 구조 건전성 영향에 대한 연구)

  • Huh, Jae Sung;Kang, Young Seok;Rhee, Dong Ho
    • Transactions of the KSME C: Technology and Education
    • /
    • v.4 no.2
    • /
    • pp.93-99
    • /
    • 2016
  • High pressure nozzles and turbines of a gas turbine engine should be required to be operated under extreme operating conditions in order to maximize the performance. Engine manufactures have utilized nickel-base superalloys, enhanced cooling design, and thermal barrier coating techniques to overcome them and furthermore, material modeling, finite element analysis, optimization techniques, and etc. have been utilized widely for elaborate predictions. We aim to evaluate the effects on the low cycle fatigue life of the high pressure turbine blade caused by thermal barrier coatings and the cooling design of the endwall of the first stage turbine nozzle. To achieve it, the structural analysis, which utilized the results of conjugate heat transfer analysis as loading boundary conditions, was performed and then the results were the input for the assessment of low cycle fatigue life at several critical zones.

Compatibility Analysis of Communication Networks for the Reactor Protection Systems (원자로 보호계통 데이터 통신망의 설계 적합성 분석)

  • Kang, Young-Doo;Koh, Jung-Soo;Goo, Cheol-Soo;Kim, Bok-Ryul
    • Proceedings of the KIEE Conference
    • /
    • 2003.07d
    • /
    • pp.2037-2039
    • /
    • 2003
  • 원자력 발전소의 원자로보호계통(Plant Protection Systems)은 그 특성상 안전성과 신뢰성을 중시하며, 매우 엄격한 설계 요건을 요구한다. 또한 원자로 보호계통에 사용되는 데이터 통신망은 최악의 예상된 조건에서도 신뢰할 수 있는 성능을 보여야 하며, 실증 시험을 통해 확인되어야 한다. 이러한 특성을 고려하여 국산화과제로 개발 중인 원자로보호계통의 데이터 통신망은, 개방형 통신 프로토콜인 프로피버스(Profibus)를 적용하고 있다. 본 논문에서는 적용된 통신 프로토콜인 Profibus에 대한 성능 모델을 제시하고, 제시된 성능 모델을 통해 데이터통신망이 결정론적(Deterministic) 요건을 만족한 수 있는 성능 특성을 분석하고자 한다. 이를 통해 Profibus를 적용한 데이터 통신망이 요구되는 성능, 신뢰성, 독립성 및 건전성 요건을 만족하도록 하기 위한 설계 요건을 제시하고자 한다.

  • PDF

Structural design and integrity evaluations for reactor vessel of PGSFR sodium-cooled fast reactor (PGSFR 소듐냉각고속로 원자로용기 설계 및 구조건전성 평가)

  • Koo, Gyeong Hoi;Kim, Sung Kyun
    • Transactions of the Korean Society of Pressure Vessels and Piping
    • /
    • v.12 no.1
    • /
    • pp.70-77
    • /
    • 2016
  • In this paper, the structural design and integrity evaluations for a reactor vessel of PGSFR sodium-cooled fast reactor(150MWe) are carried out in compliance with ASME BPV III, Division 5 Subsection HB. The reactor vessel is designed with a direct contact of primary sodium coolant to its inner surface and has a double vessel concept enclosing by containment vessel. To assure the structural integrity for 60 years design lifetime and elevated operating temperature of $545^{\circ}C$, which can invoke creep and creep-fatigue damage, the structural integrity evaluations are carried out in compliance with the ASME code rules. The design loads considered in this evaluations are primary loads and operation thermal cycling loads of normal heat-up and cool-down. From the evaluations, the PGSFR reactor vessel satisfies the ASME code limits but it was found that there is a little design margin of creep damage for inner surface at the region of cold pool free surface.

A Study on Reliability Design of Fracture Mechanics Method Using FEM (유한요소법을 이용한 파괴 역학적 방법의 신뢰성설계기술에 관한 연구)

  • Baik, Seung-Yeb;Lee, Bong-Gu
    • Journal of the Korea Academia-Industrial cooperation Society
    • /
    • v.16 no.7
    • /
    • pp.4398-4404
    • /
    • 2015
  • Stainless steel sheets are widely used as the structural material for dynamic machine structures, These kinds structures used stainless steel sheets are commonly fabricated by using the gas welding, For fatigue design of gas welded joints such as various type joint. It is necessary to obtain design information on stress distribution at the weldment as well as fatigue strength of gas welded joints. Thus in this paper, ${\Delta}P-N_f$ curves were obtained by fatigue tests. and, ${\Delta}P-N_f$ curves were rearranged in the ${\Delta}{\sigma}-N_f$ relation with the hot spot stresses at the gas welded joints. Using these results, the accelerated life test(ALT) is conducted. From the experiment results, an life prediction model is derived and factors are estimated. So it is intended to obtain the useful information for the fatigue lifetime of welded joints and data analysis by statistic reliability method, to save time and cost, and to develop optimum accelerated life prediction plans.

Case Study of F-15 Airframe Battle Damage Repair Design and Assessment Procedure (F-15 기체 전투손상 수리설계 및 평가기법 사례연구)

  • Kim, Jong-Heon;Joo, Young-Sik
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.37 no.1
    • /
    • pp.105-112
    • /
    • 2009
  • For the purpose of facing battle damage that a fighter is subject to in combat, following recovery procedures such as damage assessment, repair design and structural integrity evaluation are investigated. A sample study is presented on the battle damage of F-15 ECS bay, which is comprised of damage assessment and repair design based on ABDR(Aircraft Battle Damage Repair) skills and work procedure complying with AFTO(Air Force Technical Order) forms. Further, the flight safety of repaired structure is validated and the time the permanent repair should be done is estimated through the evaluation of structural integrity such as the calculation of static strength and fatigue life.

A Study on Variations of the Low Cycle Fatigue Life of a High Pressure Turbine Nozzle Caused by Inlet Temperature Profiles and Installation Conditions (고압터빈 노즐에서 입구온도분포와 장착조건에 따른 저주기 피로 수명 영향에 대한 연구)

  • Huh, Jae Sung;Kang, Young Seok;Rhee, Dong Ho;Seo, Do Young
    • Transactions of the Korean Society of Mechanical Engineers A
    • /
    • v.39 no.11
    • /
    • pp.1145-1151
    • /
    • 2015
  • High pressure components of a gas turbine engine must operate for a long life under severe conditions in order to maximize the performance and minimize the maintenance cost. Enhanced cooling design, thermal barrier coating techniques, and nickel-base superalloys have been applied for overcoming them and furthermore, material modeling, finite element analysis, statistical techniques, and etc. in design stage have been utilized widely. This article aims to evaluate the effects on the low cycle fatigue life of the high pressure turbine nozzle caused by different turbine inlet temperature profiles and installation conditions and to investigate the most favorable operating condition to the turbine nozzle. To achieve it, the structural analysis, which utilized the results of conjugate heat transfer analysis as loading boundary conditions, was performed and its results were the input for the assessment of low cycle fatigue life at several critical zones.