• Title/Summary/Keyword: 동적 피로

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Noise Reduction Methods for the EMG Median Frequency Data in Fatiguing Isotonic Exercise (등장성 운동 시 근전도 중앙주파수 데이터의 잡음 제거 방법)

  • Cho, Sang-Hyun
    • Physical Therapy Korea
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    • v.8 no.4
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    • pp.31-43
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    • 2001
  • 19명의 건강한 성인 남자의 우세팔쪽 위팔두갈래근에서 피로가 생길 때까지 2.4초를 하나의 주기로 팔꿉을 반복적 등장성으로 굽히고 펴서 표면근전도 신호를 얻었다. 처리과정 A 중앙주파수(MDF )는 이 신호의 0.5초 구간을 power spectrum analy sis (PSA)로 계산하였는데 상당량의 잡음이 있었다. 중앙주파수의 잡음 양을 비교하기 위해, 동일한 표면근전도에서 3번까지 신호를 받았다 (2.4초 구간을 PSA로 계산한 처리과정 B, 13 point 로 moving averages한 처리과정 C, digital low pass filter한 처리과정 D). 그리고 나서 그 신호의 주요 주파수 성분을 뽑아내었다. 위의 중앙주파수 자료와 시간간의 회귀직선을 분석하면 초기 중앙주파수, 회귀기울기, 그리고 피로지수와 같은 모수를 얻을 수 있다. 비모수 검정의 하나인 Kendall 기법으로 네 개의 처리과정간의 모수를 비교하였다. 통계결과 잡음이 처리과정 A보다 B, C, D에서 적었고, D에서 가장 적게 나타났다. 중앙주파수를 digital low pass로 여과(filtering)함으로써 앞으로 있게 될 동적 운동 시 근피로 모니터기의 신뢰도를 높일 수 있다.

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Experimental Verification of Compressor Blade Aeromechanics (압축기 블레이드 Aeromechanics의 시험적 검증)

  • Choi, Yun Hyuk;Park, Hee Yong;Kim, Jee Soo;Shin, Dong Ick;Choi, Jae Ho;Kim, Yeong Ryeon
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2017.05a
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    • pp.240-244
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    • 2017
  • Experimental verification in the rig test stage for component development is a vital link between the aeromechanical design and structural integrity validation process. Based on this premise, Non-Intrusive Stress Measuring System was adopted on the axial compressor test rig to measure the static and dynamic tip deflection of all blades by using tip-timing sensors. Through analyzing vibration characteristics, we evaluated the vibratory stresses seen on the blades fatigue critical location; detected synchronous resonances which are the source of High Cycle Fatigue (HCF) in blades; presented non-synchronous vibration response by aerodynamic excitation and individual blade mis-tuning patterns.

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Mechanical Properties of a Lining System under Cyclic Loading Conditions in Underground Lined Rock Cavern for Compressed Air Energy Storage (복공식 지하 압축공기에너지 저장공동의 내압구조에 대한 반복하중의 역학적 영향평가)

  • Cheon, Dae-Sung;Park, Chan;Jung, Yong-Bok;Park, Chul-Whan;Song, Won-Kyong
    • Tunnel and Underground Space
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    • v.22 no.2
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    • pp.77-85
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    • 2012
  • In a material, micro-cracks can be progressively occurred, propagated and finally lead to failure when it is subjected to cyclic or periodic loading less than its ultimate strength. This phenomenon, fatigue, is usually considered in a metal, alloy and structures under repeated loading conditions. In underground structures, a static creep behavior rather than a dynamic fatigue behavior is mostly considered. However, when compressed air is stored in a rock cavern, an inner pressure is periodically changed due to repeated in- and-out process of compressed air. Therefore mechanical properties of surrounding rock mass and an inner lining system under cyclic loading/unloading conditions should be investigated. In this study, considering an underground lined rock cavern for compressed air energy storage (CAES), the mechanical properties of a lining system, that is, concrete lining and plug under periodic loading/unloading conditions were characterized through cyclic bending tests and shear tests. From these tests, the stability of the plug was evaluated and the S-N line of the concrete lining was obtained.

Experimental Study on Dynamic Behavior of a Titanium Specimen Using the Thermal-Acoustic Fatigue Apparatus (열음향 피로 시험 장치를 이용한 티타늄 시편의 동적 거동에 관한 실험적 연구)

  • Go, Eun-Su;Kim, Mun-Guk;Moon, Young-Sun;Kim, In-Gul;Park, Jae-Sang;Kim, Min-Sung
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.48 no.2
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    • pp.127-134
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    • 2020
  • High supersonic aircraft are exposed to high temperature environments by aerodynamic heating during supersonic flight. Thermal protection system structures such as double-panel structures are used on the skin of the fuselage and wings to prevent the transfer of high heat into the interior of an aircraft. The thin-walled double-panel skin can be exposed to acoustic loads by supersonic aircraft's high power engine noise and jet flow noise, which can cause sonic fatigue damage. Therefore, it is necessary to examine the behavior of supersonic aircraft skin structure under thermal-acoustic load and to predict fatigue life. In this paper, we designed and fabricated thermal-acoustic test equipment to simulate thermal-acoustic load. Thermal-acoustic testing of the titanium specimen under thermal-acoustic load was performed. The analytical model was verified by comparing the thermal-acoustic test results with the finite element analysis results.

A Particle Swarm Optimization based Control Scheme for Super peer Ratio in Unstructured Peer-to-Peer System (비구조적 피어-투-피어 시스템에서 입자 군집 최적화를 이용한 우수 피어 비율 조절 기법)

  • Jang Hyung-Keun;Han Sung-Min;Park Sung-Yong
    • Proceedings of the Korean Information Science Society Conference
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    • 2006.06d
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    • pp.163-165
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    • 2006
  • 비구조적인 피어-투-피어 시스템은 구조적 피어-투-피어 시스템에 비해 동적인 상황에 적합하지만 메시지가 여러 다른 피어를 이동하면서 검색하기 때문에 검색 시간이 길고 검색의 성공률이 낮다. 이러한 문제를 해결하기 위해 우수 피어를 사용한 계층적 피어-투-피어 시스템이 연구 되었다. 효율적인 계층적 피어-투-피어 시스템을 구성하기 위해서는 어떤 피어가 얼마나 많이 우수 피어로 선택되어야 하는지가 중요하다. 본 논문에서는 기존에 연구된 자기 조직적 링 구조 기법을 기반으로 우수 피어의 비율을 환경에 적응하게 하는 시스템을 제안한다. 환경에 적합한 비율 조절을 위해 효율적으로 최적 또는 최적에 가까운 해를 찾는 것으로 알려진 입자 군집 최적화(PSO : Particle Swarm Optimization)기법을 사용하였고 성능 평가 결과 PSO를 적용한 시스템에서 성능 향상을 볼 수 있었다.

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Characterization and Fatigue Life Evaluation of Rubber/Clay Nanocomposites (고무-점토 나노복합체 물성 및 피로내구성 평가)

  • Woo, Chang-Su;Park, Hyun-Sung;Joe, Deug-Hwan;Jun, Young-Sig
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.35 no.10
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    • pp.1199-1203
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    • 2011
  • Nanocomposites were prepared through the compounding of rubber and clay. Measurements of the static and dynamic mechanical properties of different compositions over a temperature range $70-100^{\circ}C$ showed that the mechanical properties of these rubber/clay nanocomposites are superior to those of existing rubber materials. In this study, by using the parameter of the maximum Green.Lagrange strain appearing at certain locations, the relationship between fatigue life and maximum Green.Lagrange strain, and the correlations between test-piece tests and bench tests of actual rubber components are proved. In order to predict the fatigue life of rubber components at the design stage, a simple procedure of life prediction is suggested. The predicted fatigue lives of the rubber engine mounts agree fairly well with the fatigue lives determined experimentally.

Evaluation of Pyrolysis Carbon Black Modified Asphalt Binder for Fatigue and Low Temperature Crack (열분해 카본블랙을 이용한 아스팔트 바인더의 피로 및 저온 성능 평가)

  • Lee, Dong-Hang;Lee, Kwan-Ho
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.14 no.5
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    • pp.2511-2515
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    • 2013
  • Carbon black from pyrolysis of waste tires was used to modify and improve the fatigue properties and low temperature cracking of asphalt binder. 0%, 5%, 10%, 15% and 20% of pyrolyzed carbon black was mixed. Couple of laboratory tests, such as dynamic shear rheometer test and bending beam rheometer test, were carried out. The use of pyrolyzed carbon black decreased the fatigue at room temperature and improved the resistance of low temperature cracking up to $-12^{\circ}C$, but, was off the criteria at $-18^{\circ}C$.

Facial Behavior Recognition for Driver's Fatigue Detection (운전자 피로 감지를 위한 얼굴 동작 인식)

  • Park, Ho-Sik;Bae, Cheol-Soo
    • The Journal of Korean Institute of Communications and Information Sciences
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    • v.35 no.9C
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    • pp.756-760
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    • 2010
  • This paper is proposed to an novel facial behavior recognition system for driver's fatigue detection. Facial behavior is shown in various facial feature such as head expression, head pose, gaze, wrinkles. But it is very difficult to clearly discriminate a certain behavior by the obtained facial feature. Because, the behavior of a person is complicated and the face representing behavior is vague in providing enough information. The proposed system for facial behavior recognition first performs detection facial feature such as eye tracking, facial feature tracking, furrow detection, head orientation estimation, head motion detection and indicates the obtained feature by AU of FACS. On the basis of the obtained AU, it infers probability each state occur through Bayesian network.

High Cycle Fatigue Life Evaluation of Damaged Composite Rotor Blades (손상된 복합재 로터 블레이드의 고주기 피로수명 평가)

  • Kee, Young-Jung;Kim, Seung-Ho;Han, Jeong-Ho;Jung, Jae-Kwon;Heo, Jang-Wook
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.36 no.10
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    • pp.1275-1282
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    • 2012
  • Helicopter rotor systems are dynamically loaded structures with many composite components such as the main and the tail rotor blades. The fatigue properties of composite materials are extremely important to design durable and reliable helicopter rotor blades. The safe-life methodology has generally been used in the helicopter industry to substantiate dynamically loaded composite components. However, it cannot be used to evaluate the strength reducing effects of flaws and defects that may occur during manufacturing and operational usage. The damage tolerance methodology provides a proper means to overcome this shortcoming; however, it is difficult to economically apply it to every composite component. The flaw tolerant methodology is an equivalent option to the damage tolerance methodology for civil and military rotorcraft. In this study, the flaw tolerant safe-life evaluation is described and illustrated by means of successful application to substantiate the retirement time of composite rotor blades.

Prediction of Fatigue Life Using Dynamic Simulation and Finite Element Anlaysis for Construction Equipment (중장비의 동적시뮬레이션과 유한요소법을 이용한 피로수명에측)

  • Kwon, Soon-Ki;Park, Hyung-Jin
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.20 no.5
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    • pp.1392-1400
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    • 1996
  • The need of companies shorten the design-to-manufacturing process for new products with improved quality in cost effective manner places increasing demends on engineers to simulate the performance characteristics of a design before it is built of a prototype is developed. For theses demands CAE(Computer-Aided Engineering) offers engineers not only giving confidence of their design but also eliminating potential errors due totesting prototypes in small numbers. This paper present the method to predict the fatigue life using dynamics simulation and FEA(Finite Element Analysis) for construciton equipment in the computer before building prototype. The dynamicsimulatio is to get the load-time history corresponding to the maneuvering and driving of the construction equipment. The FEA is to build a model of the structure and then analyse to define the local stress response to applied loadings using linear static analysis.