Helicopter rotor blade in multi-spar composite material...

Details Helicopter rotor blade in multi-spar composite material... Helicopter rotor blade in multi-spar composite material...

B - Operations, Transporting

64

C

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B64C 27/46 (2006.01) B29D 99/00 (2010.01) B64C 27/473 (2006.01)

Patent

CA 1311735

ABREGE DESCRIPTIF L'invention concerne une pale pour rotor d'hélicoptère en matériau composite dont l'ossature résistante multilongeron voisine du bord d'attaque (4) est disposée de façon à former deux caissons superpo- sés (2 et 3). Application à la construction des aéronefs. Figure 8.-

496846

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