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    (A) Study on the Simulation of the Fuel Injection System in a Large Low-speed Marine Diesel Engine

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    It has been a major research to improve the performance and reliability of diesel engine, since internal combustion engine has been invented originally. However, recently much of these researches are focused on the reduction of exhaust emission for environmental pollution protection with the concerns of the low fuel consumption rate. The charactristics of fuel injection system have a strong influence on the air-fuel mixing process and engine output, thermal efficiency, durability, noise, and exhaust emissions. The performance and exhaust emission of diesel engine is related to the fuel injection rate and injection pressure, injection duration. Combustion in diesel engine is mainly governed by characteristics of fuel injection. In this study, a simulation program was developed, which could simulate a fuel injection system for low-speed marine diesel engine. The fuel injection system was composed of fuel injection pump, high pressure pipe and fuel injection valve. The unsteady flow in the high pressure injection pipe was analyzed by the method of characteristics, considering cavitation and variation of fuel density and bulk modulus. It was assured that the simulation results agree well with experimental results of injection pressure and quantity at the high pressure distributor in fuel injection system for the training ship "M/V Hannara". And the effects of the high pressure pipe length and diameter, plunger diameter, nozzle opening pressure, nozzle hole diameter and maximum needle lift were also investigated utilizing the simulation program developed in this study.Abstract = 4 ๊ธฐํ˜ธ์„ค๋ช… = 6 ์ œ 1 ์žฅ ์„œ๋ก  = 9 ์ œ 2 ์žฅ ์—ฐ๋ฃŒ๋ถ„์‚ฌ๊ณ„ํ†ต์˜ ๋ชจ๋ธ = 11 2-1 ์—ฐ๋ฃŒ๋ถ„์‚ฌ๊ณ„ํ†ต์˜ ์ž‘๋™์›๋ฆฌ = 13 2-2 ์—ฐ๋ฃŒ์ˆœํ™˜๊ณ„ํ†ต์˜ ๊ตฌ์กฐ = 14 2-2-1 ์—ฐ๋ฃŒํŽŒํ”„ = 14 2-2-2 ์—ฐ๋ฃŒ๋…ธ์ฆ = 21 2-3 ์‡ฝ์—…์†Œ๋ฒ„(Shock absorber) = 22 2-4 ์—ฐ๋ฃŒ์บ  Control ์„ ๋„ = 24 2-5 ์ฃผ๊ธฐ๊ด€ ์—ฐ๋ฃŒ ์ˆœํ™˜ ๋ฐ ๊ณต๊ธ‰ ์„ ๋„ = 26 2-6 ๊ฐ€๋ณ€ ๋ถ„์‚ฌ์‹œ๊ธฐ ์žฅ์น˜(VIT) = 28 2-7 ํ”Œ๋Ÿฐ์ € ์œ ํšจํ–‰์ • = 32 2-8 ํŽŒํ”„ ๋ฐฐ๋Ÿด์˜ ์—ฐ๋ฃŒ์ฐจ๋‹จ๊ตฌ๋ฉ์˜ ์œ ๋กœ ๋‹จ๋ฉด์  = 34 2-8-1 ์—”์ง„๋ถ€ํ•˜ ์ค‘์ง€์  ์ดํ•˜์—์„œ์˜ ์œ ๋กœ ๋‹จ๋ฉด์  = 34 2-8-2 ์—”์ง„๋ถ€ํ•˜ ์ค‘์ง€์  ์ด์ƒ์—์„œ์˜ ์œ ๋กœ ๋‹จ๋ฉด์  = 37 2-9 ์—ฐ๋ฃŒ๋…ธ์ฆ์˜ ์œ ๋กœ ๋‹จ๋ฉด์  = 38 ์ œ 3 ์žฅ ์—ฐ๋ฃŒ๋ถ„์‚ฌ๊ณ„ํ†ต์˜ ์ด๋ก  ํ•ด์„ = 40 3-1 ์—ฐ๋ฃŒ๋ถ„์‚ฌ๊ณ„ํ†ต์˜ ๊ธฐ๋ณธ ๊ฐ€์ • = 40 3-2 ์—ฐ๋ฃŒ๋ถ„์‚ฌ๊ณ„ํ†ต์˜ ์ง€๋ฐฐ ๋ฐฉ์ •์‹ = 41 3-2-1 ์—ฐ๋ฃŒํŽŒํ”„ = 41 3-2-2 ์—ฐ๋ฃŒ๋…ธ์ฆ = 42 3-2-3 ๊ณ ์••๋ถ„์‚ฌํŒŒ์ดํ”„ = 44 3-3 ๊ฐ ๋‹จ์—์„œ์˜ ๊ฒฝ๊ณ„์กฐ๊ฑด= 49 3-4 ๋ฌผ์„ฑ์น˜์™€ ๊ณ„์ˆ˜ = 52 3-5 ๊ณ„์‚ฐ ์•Œ๊ณ ๋ฆฌ์ฆ˜ = 55 ์ œ 4 ์žฅ ์‹คํ—˜์žฅ์น˜ ๋ฐ ์‹คํ—˜๋ฐฉ๋ฒ• = 57 4-1 ์‹คํ—˜์žฅ์น˜ = 57 4-2 ์‹คํ—˜๋ฐฉ๋ฒ• = 57 ์ œ 5 ์žฅ ๊ฒฐ๊ณผ ๋ฐ ๊ณ ์ฐฐ = 60 5-1 ์‹คํ—˜๊ฒฐ๊ณผ์™€ ๊ณ„์‚ฐ๊ฒฐ๊ณผ์˜ ๋น„๊ต = 60 5-1-1 ์—ฐ๋ฃŒํŽŒํ”„์˜ ์†๋„๋ณ€ํ™”์— ์˜ํ•œ ์˜ํ–ฅ = 60 5-2 ๋ถ„์‚ฌ๊ณ„์˜ ํŒŒ๋ผ๋ฉ”ํ„ฐ์— ๋”ฐ๋ฅธ ์‹œ๋ฎฌ๋ ˆ์ด์…˜๊ณผ ๋ถ„์„ = 64 5-2-1 ๋ถ„์‚ฌํŒŒ์ดํ”„์˜ ๊ธธ์ด ๋ฐ ์ง๊ฒฝ ๋ณ€ํ™”์— ์˜ํ•œ ์˜ํ–ฅ = 64 5-2-2 ํ”Œ๋Ÿฐ์ € ์ง๊ฒฝ ๋ณ€ํ™”์— ์˜ํ•œ ์˜ํ–ฅ = 67 5-2-3 ์—ฐ๋ฃŒ๋…ธ์ฆ ๊ฐœ๋ฐฉ์••๋ ฅ ๋ณ€ํ™”์— ์˜ํ•œ ์˜ํ–ฅ = 71 5-2-4 ๋…ธ์ฆ ํ™€ ์ง๊ฒฝ ๋ณ€ํ™”์— ์˜ํ•œ ์˜ํ–ฅ = 73 5-2-5 ๋…ธ์ฆ ๋‹ˆ๋“ค๋ฐธ๋ธŒ ๋ฆฌํ”„ํŠธ ๋ณ€ํ™”์— ์˜ํ•œ ์˜ํ–ฅ = 76 ์ œ 6 ์žฅ ๊ฒฐ๋ก  = 78 ์ฐธ๊ณ ๋ฌธํ—Œ = 8
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