Propulsion unit for aircraft and aircraft comprising at least one such propulsion unit
作者： Herve Marche , Jean-Marc Martinou
DOI:
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摘要: The invention concerns an aircraft propulsion unit comprising a turbojet (1) and heat exchanger (13) located above the drawing cooling air stream (7) hot in turbojet. is characterized that intake surfaces housing are directed forward of have normal lines (n1, n2) inclined relative to axis (A) also equipped with at least one such unit.
lens.org 参考文章(9)
Franklin D. Farrington, High efficiency environmental control systems and methods ,(1998)
David A. Thompson, Air-to-air heat exchanger with frost preventing means ,(1989)
William Charles Groll, Rolf Robert Hetico, James Edward Stoker, William Andrew Bailey, Robert Eugene Kraft, Nelson Dirk Gibbens, Shrouded turbofan bleed duct ,(2006)
Morris G. Anderson, William E. Alford, David K. Winstanley, Michael L. Trego, Ron Haugland, Cooling systems for use on aircraft ,(2008)
Boris Abramzon, Jacob Danan, Shlomo Ostersetzer, Condenser heat exchanger ,(1997)
Alain Porte, Device for bleeding off and cooling hot air at an aircraft engine ,(1995)
Franklin Elliott Miller, Precooling heat exchange arrangement integral with mounting structure fairing of gas turbine engine ,(1990)
Richard G Stretton, Martyn Richards, Heat exchanger arrangement ,(2007)