소형(小型) 디젤엔진의 예연소실(豫燃焼室) 형상(形狀)이 냉시동성(冷始動性)에 미치는 영향(影響)에 관(關)한 실험적(實驗的) 연구(硏究)

Effects of Precombustion Chamber Shape on the Start ability of Small Diesel Engine under the Cold Weather

  • 문계송 (경상대학교 농공기계공학과) ;
  • 김용환 (경상대학교 농공기계공학과) ;
  • 이승규 (경상대학교 농공기계공학과)
  • 발행 : 1982.01.20

초록

소형(小型) 디젤엔진의 예연소실(豫燃燒室) 형상(形狀)이 저온시(低溫時)의 시동성(始動性)에 미치는 영향(影響)을 구명(究明)하기 위해 8종(種)의 예연소실(豫燃燒室)과 2종(種)의 실린더헤드를 제작(製作)하여 $2^7$ 요인실험법(要因實驗法)에 의해 1회(回) 조작시(操作時) 최저(最低) 시동가능(始動可能) 온도(溫度), 최대출력(最大出力), 전부하(全負荷)(4/4) 및 과부하(過負荷)(11/10)시(時)의 연료소비율(燃料消費率)을 측정(測定)하여 분석(分析)한 결과(結果)를 요약(要約)하연 다음과 같다. 가. 피스톤 상면(上面)에 대한 주분사구(主噴射口)의 상대각도(相對角度)가 $20^{\circ}$에서 $18^{\circ}$로 감소(減少)하면 최저(最低) 시동가능(始動可能) 온도(溫度)가 약(約) $2.4^{\circ}C$ 낮아졌으며 최대출력(最大出力)은 약(約) 0.3ps 증가(增加)되었다. 나. 실린더헤드 홈 각도(角度)가 $20^{\circ}$에서 $18^{\circ}$로 작아짐에 따라 최저(最低) 시동가능(始動可能) 온도(溫度)가 약(約) $3.3^{\circ}C$ 낮아졌으며, 최대출력(最大出力)은 약(約) 0.3ps 감소(減少)되었다. 다. 예연소실(豫燃燒室) 길이가 17.5mm에서 15.5mm로 짧아지면 최저(最低) 시동가능(始動可能) 온도(溫度)가 $2^{\circ}C$ 낮아졌으며 최대출력(最大出力)은 0.2ps정도(程度) 감소(減少)되었다. 라. 주분사구(主噴射口) 직경(直俓)이 4.8mm에서 4.5mm로 작아지면 최대출력(最大出力)은 0.2ps정도(程度) 증가(增加)했으나, 주분사구(主噴射口) 직경(直俓)만이 변화(變化)에 따른 시동성(始動性)의 차이(差異)는 인정(認定)되지 않았다. 마. 주분사구(主噴射口) 각도(角度)가 $47^{\circ}$이고 실린더헤드 홈 각도(角度)가 $18^{\circ}$일 경우(境遇) 시동가능(始動可能) 온도(溫度)가 가장 낮았으며, 주분사구(主噴射口) 직경(直俓)이 4.5mm이고 예연소실(豫燃燒室) 길이가 17.5mm일 경우(境遇) 최대출력(最大出力)도 가장 높았고, 전부하(全負荷) 및 과부하시(過負荷時)의 연료소비율(燃料消費率)도 가장 낮았다. 바. 실린더 헤드홈 각도(角度)와 주분사구(主噴射口)의 각도(角度)가 각각(各各) 시동성(始動性) 향상(向上)에 가장 큰 영향(影響)을 미쳤으며, 또한 주분사구(主噴射口) 직경(直俓)과 예연소실(豫燃燒室) 길이와의 교호작용(交互作用)이 최대출력(最大出力)에 가장 큰 영향(影響)을 미쳤으므로 이들 요인(要因)에 대한 처리수(處理數)를 늘려 시험(試驗)해 볼 필요성(必要性)이 있는 것으로 사료(思料)된다. 사. 본(本) 실험(實驗)에서 최적조건(最適條件)으로 나타난 시작(試作) 예연소실(豫燃燒室)은 기존(旣存) 예연소실(豫燃燒室)보다 약(約) $-6^{\circ}C$의 시동성(始動性) 향상(向上)을 나타냈다.

The aim of this study was to improve the startability of the diesel engine at low temperature. The specific objective was to determine the optimum type of precombustion chamber. The eight different types of precombustion chamber and two different types of the cylinder head were designed and tested by $2^7$ factorial experiments with four replications. The lowest starting temperature for first operation, the maximum output, and the specific fuel consumption at full load and overload were checked and analyzed. The results of the study are summarized as follows; 1. The lowest starting temperature was lowered as much as $2.4^{\circ}C$ and the maximum output was increased as much as 0.3 ps with respect to the difference in the relative angle of the main passageway against the piston head from 20 degree to 18 degree. 2. The lowest starting temperature and the maximum out-put were lowered as much as $3.3^{\circ}C$ and 0.3 ps respectively with respect to the difference in the angle of the cylinder head groove from 20 degree to 18 degree. 3. The lowest starting temperature and the maximum out put were lowered as much as $2^{\circ}C$ and 0.2 ps respectively with respect to the difference in the length of the precombustion chamber from 17.5 mm to 15.5mm. 4. There was no significant difference in the startability but the maximum output was increased as much as 0.2 ps with respect to the difference in the diameter of the main passageway from 4.8mm to 4.5mm. 5. The lowest starting temperature was obtained under the condition at 47 degree in the angle of the main passageway and at 18 degree in the angle of the cylinder head groove. The maximum output and the minimum specific fuel consumption was obtained under the condition at 4.5mm in the diameter of the main passageway and at 17.5mm in the length of the precombustion chamber. 6. The angle of the cylinder head groove and the main passageway appeared to the major factors affecting the startability significantly. The interaction between the diameter of the main pass ageway and the length of the precombustion chamber had an significant influence on the maximum output. So it would be recommended to study further on the interaction between two factors mentioned above by expanding their levels. 7. The optimum condition suggested by this study could lower the starting temperature by $6^{\circ}C$ compared to the conventional precombustion chambers.

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