• Title/Summary/Keyword: Thermal flow rate sensor

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Design and Implementation of a Hybrid-Type Mass Flow Controller (하이브리드형 질량 유량 제어기의 설계 및 실현)

  • 이명의;정원철
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.4 no.2
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    • pp.63-70
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    • 2003
  • In this paper, an MFC (Mass Flow Controller) which is widely used in many semiconductor manufacturing processes for controlling the mass flow rate of a gas is designed and implemented using the PIC 16F876 of Microchip, Inc. The MFC implemented in this thesis has the form of hybrid-type, i.e., the mixed-type of the analog-type MFC, which has many problems such as low accurary, and digital-type MFC, which use an expensive DSP (Digital Signal Processor) and an ADC (Analog to Digital Convertor) with high precision. The MFC is consists of the sensor unit, the control unit and the actuator unit, and it has used the automatic calibration algorithm and the reference table method for the improvement of the performance.

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Thermal Characteristics of the High Frequency Motor Spindle according to the Bearing Preloads and Cooling Conditions (예압과 냉각조건에 따른 고주파 모터 내장형 주축계의 열특성)

  • Choi D. B.;Kim S. T.;Jung S. H.;Kim J. H.;Kim Y. K.
    • Proceedings of the Korean Society of Machine Tool Engineers Conference
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    • 2005.05a
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    • pp.138-143
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    • 2005
  • The important problem in the high speed spindles is to reduce and minimize the thermal effect by the motor and ball bearings. Thermal characteristics according to the bearing preload and hollow shaft cooling are studied for the spindle with the oil mist lubrication and high frequency motor. Temperature distribution and thermal deformation according to the spindle speed, preload and flow rate are measured by thermocouple and gap sensor. Temperature distribution and thermal deformation are analyzed by using the finite element method. The results of analysis are compared with the measured data. This paper show that the suitable preload and hollow shaft cooling are very effective to minimize the thermal effect by the motor and ball bearings. This study indicates that temperature distribution and thermal deformation of the high speed spindle system can be estimated reasonably by using the three dimensional model through the finite element method and supports thermal optimization and more effective cooling method.

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Fabrication and Characteristics of Piezoresistive Flow Sensor with Microbeam Structures (미소 빔 구조를 가진 압저항형 유체센서의 제작 및 특성)

  • Park, Chang-Hyun;Kang, Sung-Gyu;Yu, In-Sik;Sim, Jun-Hwan;Lee, Jong-Hyun
    • Journal of Sensor Science and Technology
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    • v.8 no.5
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    • pp.400-406
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    • 1999
  • Piezoresistive flow sensors with four different types of microbeam structures were fabricated using (100), n/$n^+$/n three-layer silicon wafer and their characteristics were investigated. Piezoresistors were formed through boron diffusion and its values were about $1\;k{\Omega}$. Three-dimensional silicon microbeams were constructed by porous silicon micromachining and curled microbeams were fabricated by the difference in the thermal expansion coefficient between silicon and metal. The output response of the fabricated sensor was evaluated through half- bridge. The output voltage increased with increasing length of microbeam at the same flow velocity, while the detectable measurement range extended with decreasing length of microbeam. The output voltage of the fabricated sensors were increased with quotient of 3.2 of the flow rate since the stress of the beam versus the gas flow showed non-linear characteristics.

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Design and Performance Test of Cooling-Air Test Equipment for the Environmental Control System in Aircraft (항공기 ECS 냉각공기 시험장비 설계 및 성능 시험)

  • So, Jae-uk;Kim, Jin-sung;Kim, Jae-woo;Kim, Jin-bok
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.49 no.2
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    • pp.147-154
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    • 2021
  • In this paper, the configuration and design of the test equipment are presented to examine the impact of rapid temperature change in cooling-air that may occur during the operation of the fixed wing aircraft Environmental Control System (ECS) on avionic electronic equipment. At the start of the ECS, the temperature of the air supplied by the aircraft ECS may be increased to 5.0℃ per second. In order to ensure operating of the avionic electronic equipment that is mounted on the aircraft and receives cooling-air from the ECS, testing equipment that can implement the cooling-air characteristic test environment is required. During design of test equipment was verified cooling-air rapid rate of temperature change by performing a thermal/flow analysis, performance of the test equipment implemented was verified by applying an avionic electronic equipment.