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ENGINE AIR MANAGEMENT SYSTEM

机译:发动机空气管理系统

摘要

An air management assembly (10) for use in an engine (12) with an exhaust manifold (14) that outputs an exhaust gas and an intake manifold (16), with a filter (18) in fluid communication between the exhaust manifold (14) and turbocharger (20). The air management assembly (10) provides a compressor (22), a turbine (24), at least one gaseous fluid cooler (32, 36, 44), at least one bypass (28, 28)' and a housing (30) where the compressor (22), turbine (24), at least one gaseous fluid cooler (32), (36, 44), bypass (28, 28'), or combination thereof are integrated into the housing (30). The compressor (22) is in fluid communication with the intake manifold (16). The turbine (24) is in fluid communication with the exhaust manifold (14). The turbine (24) and the compressor (22) are moveably coupled and move in conjunction with one another. The gaseous fluid coolers (32, 36, 44) are in fluid communication with the compressor (32), turbine (24), or combination thereof. The bypass (28') is in fluid communication with an output of the turbine (24) and an input of the compressor (22) for selective bypassing of the gaseous fluid cooler (44).
机译:一种用于发动机(12)的空气管理组件(10),其具有输出排气的排气歧管(14)和进气歧管(16),并且过滤器(18)在排气歧管(14)之间流体连通)和涡轮增压器(20)。空气管理组件(10)提供压缩机(22),涡轮(24),至少一个气态流体冷却器(32、36、44),至少一个旁路(28、28)'和壳体(30)。其中压缩机(22),涡轮(24),至少一个气态流体冷却器(32),(36、44),旁路(28、28')或其组合被集成到壳体(30)中。压缩机(22)与进气歧管(16)流体连通。涡轮24与排气歧管14流体连通。涡轮(24)和压缩机(22)可移动地联接并彼此联合运动。气态流体冷却器(32、36、44)与压缩机(32),涡轮(24)或其组合流体连通。旁路(28')与涡轮(24)的输出和压缩机(22)的输入流体连通,以选择性地旁路气态流体冷却器(44)。

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