Aircraft with a fluid-duct-system

Details Aircraft with a fluid-duct-system Aircraft with a fluid-duct-system

B - Operations, Transporting

64

C

B64C 21/02 (2006.01) F15D 1/12 (2006.01)

Patent

CA 2563571

An aircraft with a fluid-duct system for extraction of the laminar layer and/or blowing out of fluid at vulnerable places of the outer skin, wherein the fluid-duct system (26, 19, 18) by means of switchable valves (6, 4) is connectable to a pump facility (3), which is driven by the exhaust air from the cabin for generating a reduced pressure for the extraction of the laminar layer.

L'invention concerne un avion ayant un système de conduit de fluide permettant d'extraire la couche laminaire et/ou de souffler le fluide aux endroits vulnérables de l'enveloppe externe. Le système de conduit de fluide (26, 19, 18) peut être raccordé, par des valves commutables (6, 4), à un système de pompe (3) qui est entraîné par l'air d'évacuation émanant de la cabine pour générer une pression réduite aux fins d'extraction de la couche laminée.

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