연료전지 무인기를 위한 화학수소화물 기반 수소 발생기
- Author(s)
- 박대일
- Issued Date
- 2011
- Abstract
- Unmanned Aircraft utilizing electric motors have various advantages and disadvantages. Electric motors are superior to internal combustion engines in that they are quiet and are free of unwanted vibrations. However, electric motors offer a shorter flight time due to the battery’s low energy density. To solve this problem, various studies on fuel cells are currently in progress. This study considers the application of an efficient hydrogen supply system and the PEMFC system to UAV’s power system with low mass and stable operation. sodium borohydride (NaBH4) has been intensively studied as a hydrogen storage material because of its advantages of nonflammability and stability in air, easily controlled hydrogen generation rate, side product recyclability, and high H2 storage efficiency. In this study, Co-Ni-P-B catalysts supported on Ni foam were prepared using electroless plating. The surface morphology of the catalysts/Ni foam was observed using SEM and EDS analysis. Also, the characteristics of hydrogen generation with Co-Ni-P-B/Ni foam catalyst was investigated at the variety of NaBH4 and NaOH concentrations. Durability test was performed, resulting in the stable hydrogen generation for long hours.
Secondly, Performance of a hydrogen generator for a fuel cell unmanned aircraft was evaluated as the change of temperature environment. The hydrogen gas was generated by the hydrolysis reaction using a catalytic reactor. Reaction chambers were set up with the range of temperatures from -20 to 40 oC. The hydrogen generation rate and temperatures changes of reactor and separator were measured at the NaBH4 concentrations of 20 and 25wt.%.
Finally, performance of two kinds hydrogen generator for under the same conditions was evaluated. Based on this, performance of one chamber for the fuel concentration, pump voltage and so on such as hydrogen generator was evaluated. And high efficient and a lightweight fuel cell system for application as the propulsion system for a UAV was to utilize its safety and stability in a long-term bench test.
- Alternative Title
- Chemical Hydride-based Hydrogen Generator for Fuel Cell Unmanned Aircraft
- Alternative Author(s)
- Park, Dae il
- Affiliation
- 조선대학교 대학원
- Department
- 일반대학원 항공우주공학과
- Advisor
- 김태규
- Awarded Date
- 2012-02
- Table Of Contents
- 목 차
LIST OF FIGURES ............................................................................................................. ⅲ
LIST OF TABLES .............................................................................................................. ⅵ
ABSTRACT ........................................................................................................................... ⅶ
제 1 장 서 론 .............................................................................................................. 1
제1절 개 요 .......................................................................................................... 1
제2절 문헌 조사 .......................................................................................... 7
1. PEMFC ................................................................................................................... 7
2. 그 외 연료전지 ................................................................................ 11
3. 수소저장방식 ............................................................................... 14
제3절 수소화붕소나트륨(NaBH4) ......................................................................... 17
제4절 연구 내용 및 범위 ............................................................................................ 19
제 2 장 연료전지 무인기용 촉매 개발 ......................................................................... 20
제1절 촉매/지지체 제조 및 특성 ............................................................................. 20
제2절 촉매 반응 특성 .................................................................................................. 23
1. NaBH4 농도에 따른 촉매 반응 특성 ............................................................ 24
2. NaOH 농도에 따른 촉매 반응 특성 ............................................................. 25
2. 촉매의 내구성 ....................................................................................................... 26
제 3 장 수소발생기의 온도환경 성능평가 .................................................................. 28
제1절 수소 발생기 및 온도환경 실험장치 구축 ................................................... 28
제2절 온도환경 실험 조건 .......................................................................................... 31
제3절 온도환경 실험 결과 .......................................................................................... 32
1. 20wt.% NaBH4에서의 온도 환경 실험 .......................................................... 32
2. 25wt.% NaBH4에서의 온도 환경 실험 .......................................................... 34
3. 온도 환경에 따른 수소 발생기 성능 저하 원인분석 .................................. 36
제 4 장 수소 발생기의 컴팩트화 연구 .......................................................................... 40
제1절 챔버 구성에 따른 수소 발생 성능평가 ....................................................... 42
제2절 컴팩트 수소 발생기의 펌프 전압별 성능 ................................................. 46
제3절 컴팩트 수소 발생기의 NaBH4 농도에 따른 성능 ................................... 48
제4절 컴팩트 수소 발생기 보완 ................................................................................ 50
1. 실험 결과 ......................................................................... 51
제 5 장 연료전지 시스템 실험 ....................................................................... 54
제1절 실험 조건 및 장치 구축 .................................................................................. 54
제2절 전류에 따른 연료전지 시스템 성능평가 ..................................................... 55
제3절 장시간 테스트 .................................................................................................... 56
제 6 장 결 론 .............................................................................................................. 57
참 고 문 헌 ........................................................................................................................... 59
- Degree
- Master
- Publisher
- 조선대학교
- Citation
- 박대일. (2011). 연료전지 무인기를 위한 화학수소화물 기반 수소 발생기.
- Type
- Dissertation
- URI
- https://oak.chosun.ac.kr/handle/2020.oak/9397
http://chosun.dcollection.net/common/orgView/200000256826
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