AIRCRAFT BLEEDING DUCT IN COMPOSITE MATERIAL

摘要

The invention provides non-straight ducts for conducting fluids at temperatures higher than 280ºC and pressures higher than 4 bar made of a composite material and, particularly, hot air bleed ducts of an aircraft made of a carbon-fiber reinforced polymer aimed to reduce weight of the bleeding system by replacing most of the metallic material from which the bleeding ducts are currently made.