Heat exchanger unit for an aircraft
作者： Herve Marche
DOI:
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摘要: A propulsion system for an aircraft includes a heat exchange unit through which hot air stream and cooling flow. The inlet pipe situated on rear face of the unit, to carry into discharge expel from being concentric with each other. flows forward front then so as be expelled via unit.
lens.org 参考文章(16)
Youichi Nakajima, Yoshinori Nishimura, Jun Zamma, Takayuki Kaneko, Heat exchanger with U-tubes ,(1980)
Herve Marche, Jean-Marc Martinou, Propulsion unit for aircraft and aircraft comprising at least one such propulsion unit ,(2006)
Alain Porte, Turbofan provided with a pre-cooler ,(2006)
William Charles Groll, Rolf Robert Hetico, James Edward Stoker, William Andrew Bailey, Robert Eugene Kraft, Nelson Dirk Gibbens, Shrouded turbofan bleed duct ,(2006)
Tsukasa Yoshinaka, Turbine engine with intercooler in bypass air passage ,(1997)
Konrad Nassauer, Heat exchanger for cooling hot gases, especially those deriving from the synthesis of ammonia ,(1984)
Morris G. Anderson, William E. Alford, David K. Winstanley, Michael L. Trego, Ron Haugland, Cooling systems for use on aircraft ,(2008)
Zirin Louis Isadore, Recuperative arrangement for gas turbine engines ,(1963)
Herve Marche, Heat exchanger, propulsion unit, and aircraft comprising such a propulsion unit ,(2006)