• Title/Summary/Keyword: Aircraft measurement

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원통 플런지 연삭에서의 연삭력에 관한 연구

  • 박종찬;박철우;이상조
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 1996.04a
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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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Measurement of Air Pollution Monitoring Using Aircraft (항공기를 이용한 대기오염 측정)

  • 이덕길;한진석;홍유덕;공부주;박준대;안준영;김정호;김소영
    • Proceedings of the Korea Air Pollution Research Association Conference
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    • 2002.04a
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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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Study on the measurement of bolt axial force by ultrasonic wave (초음파에 의한 볼트의 축력측정)

  • 한응교;김재열
    • Journal of the korean Society of Automotive Engineers
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    • v.10 no.3
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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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Analysis of Air Traffic Delays at an Airpor (공항에서의 항공교통 지체현상 분석)

  • Kim, B.J.
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.8 no.1
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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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Measurement of Aircraft Wing Deformation and Vibration Using Stereo Pattern Recognition Method (스테레오 영상을 이용한 비행 중인 항공기 날개의 변위 및 진동 측정)

  • Kim, Ho-Young;Yoon, Jong-Min;Han, Jae-Hung;Kwon, Hyuk-Jun
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.25 no.8
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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.

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

  • Kim, Seung-Keun;Kim, You-Dan
    • Journal of Institute of Control, Robotics and Systems
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    • v.11 no.3
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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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    • v.2 no.3
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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.

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

  • Lee, Dhong-Ha;Lee, Hyun-Chul
    • IE interfaces
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    • v.13 no.4
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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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