Laminar flow control system and suction panel for use therewith

Details Laminar flow control system and suction panel for use therewith Laminar flow control system and suction panel for use therewith

B - Operations, Transporting

64

C

B64C 21/06 (2006.01) B64C 1/12 (2006.01) B64C 3/26 (2006.01) F15D 1/12 (2006.01)

Patent

CA 2370647

A laminar flow control system for incorporation in, for example, an aircraft flying surface includes a suction panel comprising a perforated skin (20, 40) mounted on a base member (60), a plenum chamber (30) being in communication with a plurality of micro channels (90) formed in the top surface of the base member (60), the micro channels (90) being in communication with the holes (40) in the skin (20).

Un système de régulation d'écoulement laminaire destiné à l'incorporation, par exemple, d'une surface volante d'aéronef, comprend un panneau d'aspiration comportant une enveloppe perforée (20, 40) fixée sur un élément de base (60), une chambre de tranquillisation (30) en communication avec plusieurs micro-canaux (90) formés à la surface supérieure de l'élément de base (60), lesdits micro-canaux (90) étant en communication avec les trous (40) situés sur l'enveloppe (20).

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