• Title/Summary/Keyword: Trip Fuel

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EXPERIMENTAL ANALYSIS OF DRIVING PATTERNS AND FUEL ECONOMY FOR PASSENGER CARS IN SEOUL

  • Sa, J.-S.;Chung, N.-H.;Sunwoo, M.-H.
    • International Journal of Automotive Technology
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    • v.4 no.2
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    • pp.101-108
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    • 2003
  • There are a lot of factors that influence automotive fuel economy such as average trip time per kilometer, average trip speed, the number of times of vehicle stationary, and so forth. These factors depend on road conditions and traffic environment. In this study, various driving data were measured and recorded during road tests in Seoul. The accumulated road test mileage is around 1,300 kilometers. The objective of the study is to identify the driving patterns of the Seoul metropolitan area and to analyze the fuel economy based on these driving patterns. The driving data which was acquired through road tests was analysed statistically in order to obtain the driving characteristics via modal analysis, speed analysis, and speed-acceleration analysis. Moreover, the driving data was analyzed by multivariate statistical techniques including correlation analysis, principal component analysis, and multiple linear regression analysis in order to obtain the relationships between influencing factors on fuel economy. The analyzed results show that the average speed is around 29.2 km/h, and the average fuel economy is 10.23 km/L. The vehicle speed of the Seoul metropolitan area is slower, and the stop-and-go operation is more frequent than FTP-75 test mode which is used for emission and fuel economy tests. The average trip time per kilometer is one of the most important factors in fuel consumption, and the increase of the average speed is desirable for reducing emissions and fuel consumption.

An Analysis of a Post-Trip Return-to-Power Steam Line break Events

  • Baek, Seung-Su;Lee, Cheol-Sin;Song, Jin-Ho;Lee, Sang-Yong
    • Proceedings of the Korean Nuclear Society Conference
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    • 1995.05a
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    • pp.544-549
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    • 1995
  • An analysis for Steam Line Break (SLB) events which result in a return-to-power conditions after reactor trip was performed for a postulated Yonggwang Nuclear Power Plant Unit 3 cycle 8. Analysis methodology for post-trip return-to-power SLB is quite different from that of a no return-to-power SLB and is more complicated. Therefore, it is necessary to develop an methodology to analyze the response of the NSSS parameter and the fuel performance for the post-trip return-to-power SLB events. In this analysis, the cases with and without offsite power were simulated by crediting 3-D reactivity feedback effect due to local heatup around stuck CEA and compared with the cases without 3-D reactivity feedback with respect to fuel performance, departure from nucleate boiling ratio (DNBR) and linear heat generation rate (LHGR).

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FLB Event Analysis with regard to the Fuel Failure

  • Baek, Seung-Su;Lee, Byung-Il;Lee, Gyu-Cheon;Kim, Hee-Cheol;Lee, Sang-Keun
    • Proceedings of the Korean Nuclear Society Conference
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    • 1996.05b
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    • pp.622-627
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    • 1996
  • Detailed analysis of Feedwater Line Break (FLB) event for the fuel failure point of view are lack because the event was characterized as the increase in reactor coolant system (RCS) pressure. Up to now, the potential of the rapid system heatup case has been emphasized and comprehensively studied. The cooldown effects of FLB event is considered to be bounded by the Steam Line Break (SLB) event since the cooldown effect of SLB event is larger than that of the FLB event. This analysis provides a new possible path which can cause the fuel failure. The new path means that the fuel failure can occur under the heatup scenario because the Pressurizer Safety Valves (PSVs) open before the reactor trips. The 1000 MWe typical C-E plant FLB event assuming Loss of Offsite Power (LOOP) at the turbine trip has been analyzed as an example and the results show less than 1% of the fuel failure. The result is well within the acceptance criteria. In addition to that, a study was accomplished to prevent the fuel failure for the heatup scenario case as an example. It is found that giving the proper pressure gap between High Pressurizer Pressure Trip (HPPT) analysis setpoint and the minimum PSV opening pressure could prevent the fuel failure.

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Techno-Economic Analysis of Reversible Solid Oxide Fuel Cell System Couple with Waste Steam (폐스팀을 이용한 가역 고체산화물 연료전지의 기술적 경제적 해석)

  • GIAP, VAN-TIEN;LEE, YOUNG DUK;KIM, YOUNG SANG;AHN, KOOK YOUNG
    • Journal of Hydrogen and New Energy
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    • v.30 no.1
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    • pp.21-28
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    • 2019
  • Reversible solid oxide fuel cell (ReSOC) system was integrated with waste steam for electrical energy storage in distributed energy storage application. Waste steam was utilized as external heat in SOEC mode for higher hydrogen production efficiency. Three system configurations were analyzed to evaluate techno-economic performance. The first system is a simple configuration to minimize the cost of balance of plant. The second system is the more complicated configuration with heat recovery steam generator (HRSG). The third system is featured with HRSG and fuel recirculation by blower. Lumped models were used for system performance analyses. The ReSOC stack was characterized by applying area specific resistance value at fixed operating pressure and temperature. In economical assessment, the levelized costs of energy storage (LCOS) were calculated for three system configurations based on capital investment. The system lifetime was assumed 20 years with ReSOC stack replaced every 5 years, inflation rate of 2%, and capacity factor of 80%. The results showed that the exergy round-trip efficiency of system 1, 2, 3 were 47.9%, 48.8%, and 52.8% respectively. The high round-trip efficiency of third system compared to others is attributed to the remarkable reduction in steam requirement and hydrogen compression power owning to fuel recirculation. The result from economic calculation showed that the LCOS values of system 1, 2, 3 were 3.46 ¢/kWh, 3.43 ¢/kWh, and 3.14 ¢/kWh, respectively. Even though the systems 2 and 3 have expensive HRSG, they showed higher round-trip efficiencies and significant reduction in boiler and hydrogen compressor cost.

The simulation of turbine trip on range mode of Shoaiba desalination plant (Shoaiba 산업용 보일러의 range mode 운전시 turbine trip 모사)

  • Lee, Chi-Hwan;Kim, Sung-Ho;Cho, Chang-Ho
    • Proceedings of the KSME Conference
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    • 2001.11b
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    • pp.885-890
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    • 2001
  • This simulation shows turbine trip on range mode, combined operation of 4 boilers and 5 turbines, for shoaiba desalination plant which is being operated in Saudi Arabia. In this model, unit master controller controls load demand, fuel and air flowrate to be consumed during operating of the plant. Feedwater controller controls drum level to compensate feedwater with superheater steam flow. This analysis was performed by constructing a dynamic model of the plant using ProTRAX and running it through the appropriate.

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eXtended Statistical Combination of Uncertainties (XSCU) Method for Digital Nuclear Power Plants

  • In, Wang-Kee;Hwang, Dae-Hyun;Kim, Joon-Sung;Auh, Geun-Sun
    • Nuclear Engineering and Technology
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    • v.30 no.6
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    • pp.617-627
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    • 1998
  • A technically more direct Statistical Combination of Uncertainties (SCU) method, extended SCU (XSCU), was developed to statistically combine the uncertainties associated with the DNBR alarm setpoint and the DNBR trip setpoint of digital nuclear power plants. The Modified SCU (MSCU) method is currently used as the USNRC approved design method to perform the same function. In this study, the MSCU and XSCU methods were compared in terms of the total uncertainties, and the thermal margins to the DNBR alarm and trip setpoints. The MSCU method resulted in small total uncertainties due to large negative biases which are unphysical. The XSCU method gives virtually unbiased total uncertainties which are physically meaningful in order to represent the actual magnitude of the total uncertainties associated with the DNBR alarm and trip setpoints. But the thermal margins to the DNBR alarm and trip setpoints by the MSCU method agree with those by the XSCU method within allowable statistical Variations.

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OPΔT and OTΔT Trip Setpoint Generation Methodology (OPΔT 및 OTΔT트립설정치의 생산방법)

  • Ki In Han
    • Nuclear Engineering and Technology
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    • v.16 no.2
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    • pp.106-115
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    • 1984
  • Core safety limits define reactor operating conditions and parameters that will assure fuel rod and reactor system's integrity. Limiting safety system settings (LSSS) programmed into reactor protection system (RPS) then ensure a rapid reactor trip to prevent or suppress conditions which might violate the core safety limits. Generation of the LSSS must properly take into account uncertainties in both calculated and measured parameters in order to assure, with an appropriate degree of confidence, that the RPS will protect the core safety limits. Reviewed in this report are Westinghouse RPS setpoint generation philosophy, methodology of safety limit development and LSSS generation procedure. The Westinghouse RPS trip setpoint generation methodology has been established based on the calculation of core safety limits and the selection of LSSS allowing appropriate uncertainties in a conservative manner. Such conservative values of setpoint assure a high degree of core protection against fuel melting and occurrence of DNB.

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A Study on Aircraft Fuel Requirements (항공기 연료탑재 기준에 관한 연구)

  • Noh, K.S.;Choi, Y.C.;Yoo, K.E.
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.13 no.1
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    • pp.9-19
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    • 2005
  • Airplane fuel takes large portion of airline operation cost and recently it has been grown up to about 25% of operating cost. So airlines are making efforts to reduce fuel consumption continuously and also aircraft manufacturers are making efforts to develop less fuel-consuming engines but it takes great expenses and times to develop such engines. In this study, fuel requirements of FAR and JAR, especially contingency fuel requirements, are compared and the effectiveness of each method is analyzed.

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A Study on Fuel Saving Measure by Fuel Efficiency Analysis Associated with Weight. (중량에 따른 연료효율 분석을 통한 연료 절감 방안 연구)

  • Lee, Jun-Oh;Jeon, Je-hyung;Park, Jeongmin
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.26 no.4
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    • pp.142-148
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    • 2018
  • In recent years, Korea's aviation industry has been developing rapidly due to the emergence of low-cost airlines. In order to survive in such competition, airlines are making various efforts to save the operation cost as much as possible. Fuel costs account for more than 25% of operating costs. For airlines, reducing aircraft fuel costs is an important part of improving profitability. In this study, analyzing the difference weight between flightplan and W&B Manifest for calculated the fuel that was unnecessarily loaded. As a method to calculate the unnecessary fuel was used by Airbus company flight planning program.