• 제목/요약/키워드: aircraft measurement

검색결과 251건 처리시간 0.029초

원통 플런지 연삭에서의 연삭력에 관한 연구

  • 박종찬;박철우;이상조
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 1996년도 춘계학술대회 논문집
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    • pp.34-38
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    • 1996
  • Cylindrical plunge grinding is widely used for final machining process of precision parts such as automobile, aircraft, measurement units. In order to make parts which have high precison accuracy and high surface integrity, it is neccessary to consider grinding characteristics. these grinding characteristics are closely related grinding force. Soin this study, to examine closely characteristics of grinding force, effects of dressing condition, depth of cut and speed ratio on grinding force are considered. As the result, It is shown that grinding forces are affected bydressing condition, depth of cut and speed ratio and that there exist threshod grinding force and it also affected by dressing conditon.

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항공기를 이용한 대기오염 측정 (Measurement of Air Pollution Monitoring Using Aircraft)

  • 이덕길;한진석;홍유덕;공부주;박준대;안준영;김정호;김소영
    • 한국대기환경학회:학술대회논문집
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    • 한국대기환경학회 2002년도 춘계학술대회 논문집
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    • pp.161-162
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    • 2002
  • 현재의 환경문제는 국가적인 경계를 떠나서 지역적 및 범 지구적인 수준으로 인류의 생존을 위협하고 있다. 특히 한반도를 포함한 동북아지역은 전 세계적으로 인구가 밀집되어 있으며 경제발전속도가 빠른 지역으로서 심각한 대기오염문제를 야기 시킬 수 있는 상당한 양의 대기오염물질이 배출되고 있으며 이 지역의 풍향은 주로 서풍이기 때문에 중국의 풍하측에 위치한 한반도와 일본 등지에서는 중국에서 발생한 대기오염물질로 인한 피해가 급증하고 있으며 이에 대한 대책마련에 노력과 관심을 쏟고 있다. (중략)

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초음파에 의한 볼트의 축력측정 (Study on the measurement of bolt axial force by ultrasonic wave)

  • 한응교;김재열
    • 오토저널
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    • 제10권3호
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    • pp.38-44
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    • 1988
  • It is important to control the axial forces of high tension bolts such as the automobile, construction machine, aircraft, marine engine bolts. However, the direct method to measure the axial forces of bolts practically have not been found out. The ultrasonic techniques is based on the principles that the bolt tensile elongation and ultrasonic velocity changes are proportional to the axial force below the yield point of the materials. From the result of the experiment, the coefficient of acoustoelasticity k could be measured as - 11.18*10$_{-5}$m $m^{2}$k $g_{f}$./.

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공항에서의 항공교통 지체현상 분석 (Analysis of Air Traffic Delays at an Airpor)

  • 김병종
    • 한국항공운항학회지
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    • 제8권1호
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    • pp.57-66
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    • 2000
  • Benefit-cost analysis is one of key elements of feasibility study on a large scale investment for transportation infrastructure improvements. Benefit-cost analysis requires measuring expected benefits after the investment is completed. Reduction of delays is the major source for the benefit among other measurable benefits. Measurement methods for delays reduction have been reviewed and two methods were recommended for passenger delay and aircraft operation delay. Using these method, the effects of Cheju International Airport Improvement Projects were evaluated.

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스테레오 영상을 이용한 비행 중인 항공기 날개의 변위 및 진동 측정 (Measurement of Aircraft Wing Deformation and Vibration Using Stereo Pattern Recognition Method)

  • 김호영;윤종민;한재흥;권혁준
    • 한국소음진동공학회논문집
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    • 제25권8호
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    • pp.568-574
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    • 2015
  • The present study was conducted by using stereo pattern recognition method(SPR method) to measure the displacement and vibration of an airplane wing in flight condition. A SPR based measurement system was developed using two visible light stereo cameras. The visible light stereo images were processed to obtain marker points by adaptive threshold method and marker filtering technique. The marker points were used to reconstruct 3D point, displacement, and vibration data. The SPR system was installed on F-16 fighter. The wing displacement and vibration were measured in flight condition. Therefore, this paper presents a possibility that SPR based measurement system using visible light stereo camera can be very useful for measuring displacement and vibration of an airplane in flight condition.

무인기 관성측정 센서의 비모델 복합 고장진단기법 (Model-Free Hybrid Fault Detection and Isolation For UAV Inertial Measurement Sensors)

  • 김승균;김유단
    • 제어로봇시스템학회논문지
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    • 제11권3호
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    • pp.200-206
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    • 2005
  • In this paper, a redundancy management system for aircraft is studied, and FDI (Fault Detection and Isolation) algorithm of inertial sensor system is proposed. UAV system cannot allow triple or quadruple hardware redundancy due to the limitations on space and weight. In the UAV system with dual sensors, it is very difficult to identify the faulty sensor. Also, conventional FDI method cannot isolate multiple faults in a triple redundancy system. In this paper, hardware based FDI technique is proposed, which combines a parity equation approach with the wavelet based technique, which is a model-free FDI method. To verify the effectiveness of the proposed FDI method, numerical simulations are performed.

Determination of the elastic properties in CFRP composites: comparison of different approaches based on tensile tests and ultrasonic characterization

  • Munoz, Victor;Perrin, Marianne;Pastor, Marie-Laetitia;Welemane, Helene;Cantarel, Arthur;Karama, Moussa
    • Advances in aircraft and spacecraft science
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    • 제2권3호
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    • pp.249-261
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    • 2015
  • The mechanical characterization of composite materials is nowadays a major interest due to their increasing use in the aeronautic industry. The design of most of these materials is based on their stiffness, which is mainly obtained by means of tensile tests with strain gauge measurement. For thin laminated composites, this classical method requires adequate samples with specific orientation and does not provide all the independent elastic constants. Regarding ultrasonic characterization, especially immersion technique, only one specimen is needed and the entire determination of the stiffness tensor is possible. This paper presents a study of different methods to determine the mechanical properties of transversely isotropic carbon fibre composite materials (gauge and correlation strain measurement during tensile tests, ultrasonic immersion technique). Results are compared to ISO standards and manufacturer data to evaluate the accuracy of these techniques.

상황인식에 대한 측정 및 차세대 원자로 운전원 성능 평가에서의 활용방법에 관한 이론 연구 (A Review on Measurement and Applications of Situation Awareness for an Evaluation of Korea Next Generation Reactor Operator Performance)

  • 이동하;이현철
    • 산업공학
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    • 제13권4호
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    • pp.751-758
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    • 2000
  • Situation awareness is defined as a person's perception of the elements of the environment within a volume of time and space, the comprehension of their meaning and the projection of their status in the near future. Situation awareness is important in attempting to evaluate human behavior in operating complex systems such as aircraft, air traffic control, and nuclear power plant systems. From the literatures this study reviews the relationship between situation awareness and numerous individual, system and environmental factors, and also reviews the methodologies for the empirical measurement of situation awareness applicable to Korea Next Generation Reactor (KNGR) design project. Attention, working memory, workload, stress, system complexity, and automation are presented as critical factors limiting operator's situation awareness. Mental models and goal-directed behavior are hypothesized as important mechanisms overcoming these limits. This study summarized hypothesized guidelines for interface design to improve situation awareness of reactor operators. Some of the guidelines should be tested in the KNGR evaluation experiments in the future.

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