Fan by-pass duct for intercooled turbo fan engines

作者: James C. Loebig , Bradford J. Riehle

DOI:

关键词: TurbofanBypass ratioMicrochannelSimulationThrustInletEngineeringMechanical engineeringHeat exchangerNozzleDuct (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.

参考文章(14)
Paul C. Daiber, Scott C. Morton, Michelle L. Taylor, Alexander E. Vermejan, Gas turbine engine fan cooled heat exchanger ,(1993)
Georges Mazeaud, Didier Yvon, Vincent Fonquerne, Laurent Palmisano, Bruno Beutin, Cooling system for hot parts of an aircraft engine, and aircraft engine equipped with such a cooling system ,(2004)
William Charles Groll, Rolf Robert Hetico, James Edward Stoker, William Andrew Bailey, Robert Eugene Kraft, Nelson Dirk Gibbens, Shrouded turbofan bleed duct ,(2006)
Jack W. Wilson, John E. Ryznic, Ceramic regenerator for a gas turbine engine ,(2008)