Cooling system for an aircraft, aircrft comprising the cooling system and cooling method

作者: Hans Mårtensson , Anders Hellgren

DOI:

关键词:

摘要: The invention relates to a cooling system (20) for an aircraft (1) comprising circuit (21) transporting coolant, with the running component (22) in that is heated up during flying order take heat from heated-up via coolant. runs jet engine (2) propulsion of release flow gas (IV)

参考文章(22)
Frank E. Altoz, John D. McClure, Apparatus for cooling electronic components in aircraft ,(1989)
Robert Edward Goeller, Michael Edward Colman, Gas turbine engine component cooling system ,(1984)
Pierce L. Lawing, LaVerne L. Pagel, Robert A. Frosch, Cooling system for high speed aircraft ,(1979)
John P. Beck, James G. Griffin, Robert J. McHale, Raymond A. Dreisbach, Balancing the heat flow between components associated with a gas turbine engine ,(1981)
Jean-Loïc Hervé Lecordix, Pascal Noël Brossier, Marc Georges Loubet, Michel François Raymond Franchet, Bruno Albert Beutin, Cooling system for a turbomachine speed reducer ,(2000)