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Implementation of Fuel Quantity Measurement System for Aircraft Using Capacitive Fuel Sensor
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정전용량형 연료센서를 이용한 항공기 연료량측정시스템 구현

논문 기본 정보

Type
Academic journal
Author
Junmo Yang (한국항공대학교) Sungwook Yang (한국항공대학교) Sangchul Lee (한국항공대학교) Yongsik Yi (한국항공우주산업)
Journal
항공우주시스템공학회 Journal of Aerospace System Engineering Vol. 12 No. 6 KCI Accredited Journals
Published
2018.12
Pages
17 - 22 (6page)

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Implementation of Fuel Quantity Measurement System for Aircraft Using Capacitive Fuel Sensor
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Research history (3)

2018

Implementation of Fuel Quantity Measurement System for Aircraft Using Capacitive Fuel Sensor
Junmo Yang ,  Sungwook Yang ,  Sangchul Lee and others 1 Journal of Aerospace System Engineering 2018.12 Academic journal
Implementation of Fuel Quantity Measurement System Using Supersonic Aircraft Fuel Sensor
Junmo Yang ,  Sungwook Yang ,  Sangchul Lee 항공우주시스템공학회 학술행사 논문집 2018.04 Proceeding

2017

양준모 항공우주및기계공학과 2017.01 Thesis
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Abstract· Keywords

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The amount of fuel, which affects aircraft endurance, needs to be measured accurately. This paper deals with the implementation of a fuel quantity measurement system that consists of capacitive fuel sensor, DAQ board, and Labview software. The main circuit of the implemented system for measuring fuel quantity is simulated with Pspice to identify parameters, which are related to the change of fuel quantity. After simulation, we established that Vrms changes with the variation of fuel amount. The Vrms, which is the output of fuel sensor, is transmitted to the Labview software via the DAQ board of the implemented fuel quantity measurement system. The fuel quantity is also calculated using this software. The present simulation results indicated that the accuracy of the implemented fuel quantity measurement system improved with the filter application.
#Fuel Quantity Measurement System(연료량측정시스템) #Capacitive Fuel Sensor(정전용량형 연료센서) #Moving Average Filter(이동평균필터)

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Abstract
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2. 본론
3. 결론
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References (9)

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W. H. Park / 2015 / Study on the Instrumentation System for the Dorsal Air Refueling Tank Installation / Proc. of KSAS Spring Conference :933~936 google schola J. H. Jung / 2011 / Integrated Fuel system Test Equipment for UAV / Proc. of KSAS Fall Conference :1604~1607 google schola US Department of Transportation / 2003 / TSO-C55 Fuel and Oil Quantity Instrument google schola 1971 / USAF MIL-C-26988C, Gage, Liquid Quantity, Capacitor Type Transistorized, General Specification google schola Electronics International Inc / 2008 / P-300C Fuel Probe and IMC Product Information and Specifications google schola

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