作者: James C. Loebig , Bradford J. Riehle
DOI:
关键词: Turbofan 、 Bypass ratio 、 Microchannel 、 Simulation 、 Thrust 、 Inlet 、 Engineering 、 Mechanical engineering 、 Heat exchanger 、 Nozzle 、 Duct (flow)
摘要: An improved system, apparatus and method for intercooling a turbo fan engine, more specifically, system engine employing secondary bypass duct that minimizes pressure losses. The is radially inwardly disposed from receives air through an inlet. portion of flows one or microchannel minichannel heat exchangers. has outlet in communication with the stream downstream throat nozzle. accelerated at exit to create thrust.