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Evaluation and Design of Injector Hole Patterns Using CFD with a Fuel Tracer Diagnostic for Gasoline Direct Injection (GDI) Engines

机译:汽油直喷(GDI)发动机使用CFD和燃油示踪诊断技术对喷油嘴孔型进行评估和设计

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A CFD code is enhanced with a fuel tracer diagnostic to track the liquid and vapor fuel mass separately from individual spray plumes of a multi-hole injector and the wall film. The approach works by solving a set of additional scalar transport equations for fuel vapor generated from individual nozzle hole and the wall film. The diagnostic tool is first validated against experiments from a 4-valve, wall-guided spark-ignition direct-injection (S1DI) engine. A CFD analysis is carried out to understand the experimentally observed tradeoffs in combustion stability and smoke emissions between a 70degree hollow-cone swirl injector and a 40 degree, 5-hole, circular-type multi-hole injector at a lean, stratified idle operating condition. Engine tests show that the multi-hole injector results in lower COV of IMEP than the hollow-cone swirl injector at the expense of significantly higher smoke emissions. The CFD model predictions illustrate that the multi-hole injector resulted in richer fuel mass in the piston bowl and greater amount of liquid wall-film mass than the hollow-cone swirl injector. In particular, there exists more fuel vapor mass surrounding the spark gap for the multi-hole injector that correlates with the experimentally observed improvement in combustion stability. The majority of this fuel vapor mass originated from the spray plume targeted directly at the spark plug. On the other hand, the increased smoke emissions with the multi-hole injector agrees with the larger computed rich fuel vapor and liquid wall-film mass. The primary source of the liquid wall-film mass originated from the two spray plumes with the shortest penetration path length to the piston bowl surface. These findings are used to design a crescent-type multi-hole injector. Predictions using the redesigned injector show reduced liquid wall-film mass and a sufficient mixture distribution at the spark gap to suggest lower smoke emissions while maintaining good combustion stability.
机译:通过燃料示踪剂诊断功能增强了CFD代码,可独立于多孔喷油器和壁膜的各个喷雾羽流跟踪液体和蒸气燃料质量。该方法通过为从各个喷嘴孔和壁膜产生的燃料蒸气求解一组附加的标量传输方程而起作用。该诊断工具首先针对4阀,壁引导式火花点火直接喷射(S1DI)发动机的实验进行了验证。进行CFD分析以了解在稀薄分层空转运行条件下70度空心锥形旋流喷油器和40度5孔圆形多孔喷油器之间燃烧稳定性和烟雾排放的实验观察到的折衷。发动机测试表明,与中空锥形旋流喷油器相比,多孔喷油器产生的IMEP的COV较低,但烟气排放量却显着增加。 CFD模型的预测表明,与空心锥旋流式喷油器相比,多孔喷油器在活塞碗中产生了更丰富的燃料质量,并产生了更多的液体壁膜质量。特别地,在多孔喷射器的火花隙周围存在更多的燃料蒸气质量,这与实验观察到的燃烧稳定性的改善相关。这种燃料蒸气的大部分来自直接对准火花塞的喷雾羽流。另一方面,使用多孔喷油器增加的烟气排放量与较大的计算得出的浓燃料蒸气和液体壁膜质量相吻合。液体壁膜团的主要来源来自两个喷雾羽流,它们通向活塞碗表面的路径最短。这些发现用于设计月牙型多孔注射器。使用重新设计的喷油器进行的预测表明,液体壁膜质量降低,并且火花隙处的混合气分布充分,表明烟气排放量降低,同时保持良好的燃烧稳定性。

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