• Title/Summary/Keyword: 저온 연소

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Extension of Low Temperature Combustion Regime by Turbocharging Using Diesel and Biodiesel Fuels (과급에 의한 디젤 및 바이오디젤의 저온연소 운전영역 확장에 관한 연구)

  • Jang, Jae-Hoon;Oh, Seung-Mook;Lee, Yong-Gyu;Lee, Sun-Youp
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.36 no.11
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    • pp.1065-1072
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    • 2012
  • Due to its oxygen (O) content, biodiesel (BD) is advantageous in that it lowers PM emissions in CI engines. Therefore, BD is considered one of the best candidates for low temperature combustion (LTC) operation because its use can extend the regime for simultaneous reduction of PM and $NO_x$. Thus, in this study, LTC operation was realized using BD and diesel with a 5~7% $O_2$ fraction. Engine test results show that the use of BD increased the efficiency and reduced emissions such as PM, THC, and CO; furthermore, IMEP reduced by 10~12% owing to the lower LHV of the fuel. In particular, smoke was suppressed by up to 90% because O atoms in the BD enhanced the soot oxidation reaction. To compensate the IMEP loss, turbocharging (TC) was then tested, and the results showed that the power output increased and PM was reduced further. Moreover, TC in BD engine operation allowed a similar level of reduction in both $NO_x$ and PM at 11~12% $O_2$ fraction, suggesting that there is a potential to widen the operating range by the combination of TC and BD.

Construction of a High-Altitude Ignition Test Facility for a Small Gas-turbine Combustor (소형 가스터빈 연소기 고공환경 점화 시험 설비 구축 및 검증 실험)

  • Kim, Tae-Woan;Lee, Yang-Suk;Kim, Ki-Woo;Kim, Bo-Yean;Ko, Young-Sung;Kim, Sun-Jin;Kim, Hyung-Mo;Jung, Yong-Wun
    • Journal of the Korean Society of Propulsion Engineers
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    • v.14 no.3
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    • pp.61-68
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    • 2010
  • A small high altitude test facility has been developed to investigate ignition performance of a small gas-turbine combustor under high altitude conditions. Supersonic diffusers and a heat exchanger were used to perform a low pressure and a low temperature condition, respectively. Experimental results showed that the low pressure environment could be controlled by upstream pressure of primary nozzle flow and low temperature environment by mixture ratio of cooled air and ambient air. Ignition performance tests were performed to verify the performance of the facility under simulated high altitude conditions. Conclusively, it was proven that the test facility could be used for ignition performance test of a small gas-turbine combustor under high altitude condition of approximately 6,100m.

Effects of Aromatics and T90 Temperature of Low Cetane Number Fuels on Exhaust Emissions in Low-Temperature Diesel Combustion (저온디젤연소에서 저세탄가 연료의 방향족 및 T90 온도가 배기가스에 미치는 영향)

  • Han, Man-Bae
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.34 no.12
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    • pp.1121-1126
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    • 2010
  • This study is to investigate the effects of aromatics and T90 for low cetane number (CN) fuels on combustion and exhaust emissions in low-temperature diesel combustion. We use a 1.9-L common rail direct injection diesel engine at 1500 rpm and 2.6 bar BMEP. Low temperature diesel combustion was achieved via a high external EGR rate and strategic injection control. The tested fuels four sets: the aromatic content was 20% (A20) or 45% (A45) and the T90 temperature was $270^{\circ}C$ (T270) or $340^{\circ}C$ (T340) with CN 30. Given the engine operating conditions, the T90 was the stronger factor on the ignition delay time, resulting in a longer ignition delay time for higher T90 fuels. All the fuels produced nearly zero PM because of the extension of the ignition delay time induced by the low cetane number. The aromatic content was the main factor that affected the NOx and the NOx increased with the aromatic content.

Effects of Soybean Biodiesel Fuel on Exhaust Emissions in Compression Ignition Combustion (대두유 바이오 디젤연료가 압축 착화 연소에서 배기가스에 미치는 영향)

  • Han, Man-Bae
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.34 no.10
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    • pp.941-946
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    • 2010
  • This study aims to investigate the effects of soybean biodiesel fuel on exhaust emissions with regards to two combustion modes: conventional combustion(existence of PM-NOx trade-off behavior) and low temperature combustion(LTC) in a 1.7 L common rail direct injection diesel engine. As compared to conventional combustion, LTC was achieved by adopting a heavier exhaust gas recirculation and strategic injection parameter optimization. Two sets of fuels, i.e. ultra low sulfur diesel(ULSD) and 20% volumetric blends of soybean biodiesel with ULSD(B20) were used. Regardless of the fuel type, in LTC the simultaneous reduction of PM and NOx was observed and both levels were significantly lower than in case of conventional combustion. Under the given engine operating condition in the case of conventional combustion, B20 produced less PM and more NOx than ULSD. In the case of LTC combustion, B20 produced more PM and NOx than ULSD.

Development of an Igniter for Pyrostarters (파이로스타터용 점화기 개발)

  • Park, Ho-Jun;Hong, Moon-Geun;Kwon, Mi-Ra;Lee, Soo-Yong
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.11a
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    • pp.149-152
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    • 2009
  • A pyrostarter is a sort of gas generator, which supplies the energy to drive turbines by the combustion gas of a solid propellant charged internally. The igniter of the pyrostarter should guarantee the ignition reliability expecially for the solid propellant with a low fame temperature. For the development of the igniter, several closed bomb testes have been performed to decide several design parameters to get a sufficient chamber pressure build-up for the ignition. Moreover, as a result of the firing testes with pyrostarters, the ignition reliability have been verified and the amount of igniter propellants has been reviewed.

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Development of the Drive-away Motor for Cold Launch System (저온 사출장치용 이탈모타 개발)

  • Baek, Gook-Hyun;Oh, Jong-Yun;Lee, Young-Won;Lee, Ji-Hyung;Jung, Jin-Suk
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.11a
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    • pp.369-374
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    • 2011
  • To solve the combustion instability, especially chuffing phenomena, happened during development process of the drive-away motor that was required for cold launch system of missile, we tried various technical approaches and performed ground firing tests. The supplying content or method of ignition energy, generally that is deeply related with the chuffing phenomena, does not affect suppression of the chuffing, but the addition of 2% ZrC as a damping material is effective to suppress the chuffing. Therefore we could newly experience a special solution of the combustion instability in double base propellant.

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Effect of Injection Pressure on Low Temperature Combustion in CI Engines (압축착화 엔진에서 분사압이 저온연소에 미치는 영향)

  • Jang, Jaehoon;Lee, Sunyoup;Lee, Yonggyu;Oh, Seungmook;Lee, Kihyung
    • Journal of ILASS-Korea
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    • v.18 no.1
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    • pp.21-26
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    • 2013
  • Diesel low temperature combustion (LTC) is the concept where fuel is burned at a low temperature oxidation regime so that $NO_x$ and particulate matters (PM) can simultaneously be reduced. There are two ways to realize low temperature combustion in compression ignition engines. One is to supply a large amount of EGR gas combined with advanced fuel injection timing. The other is to use a moderate level of EGR with fuel injection at near TDC which is generally called Modulated kinetics (MK) method. In this study, the effects of fuel injection pressure on performance and emissions of a single cylinder engine were evaluated using the latter approach. The engine test results show that MK operations were successfully achieved over a range of with 950 to 1050 bar in injection pressure with 16% $O_2$ concentration, and $NO_x$ and PM were significantly suppressed at the same time. In addition, with an increase in fuel injection pressure, the levels of smoke, THC and CO were decreased while $NO_x$ emissions were increased. Moreover, as fuel injection timing retarded to TDC, more THC and CO emissions were generated, but smoke and $NO_x$ were decreased.

Development of the Drive-away Motor for Cold Launch System (저온 사출장치용 이탈모타 개발)

  • Baek, Gook-Hyun;Oh, Jong-Yun;Lee, Young-Won;Lee, Ji-Hyung;Jung, Jin-Suk
    • Journal of the Korean Society of Propulsion Engineers
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    • v.16 no.4
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    • pp.93-98
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    • 2012
  • To solve the combustion instability, especially chuffing phenomena, happened during development process of a drive-away motor that was required for cold launch system of missile, various technical approaches have been performed through ground firing tests. The ignition energy or its supply system, generally closely related with the chuffing phenomena, does not affect suppression of the chuffing, but the increase of characteristic length($L^*$) as well as the addition of 2% ZrC as a damping material is effective to suppress the chuffing. Therefore we could have a typical experience on the combustion instability in double base propellant.