A seat system (10) for a passenger aircraft includes a passenger seat frame (22) (i) a plurality of spreader bars (29) and (ii) a plurality of laterally extending spar tubes (50) connecting the plurality of spreader bars (29) to one another and at least one canted leg assembly (40,42) connected to the seat frame (22) for attachment to fixed, spaced apart attachment points on a supporting surface of the passenger aircraft. The canted leg assembly (40,42) includes: (i) a front leg portion (62) including a front joint clamp (66) for receiving one of the plurality of laterally extending spar tubes (50) in a non-perpendicular attachment point; and (ii) an aft leg portion including an aft joint clamp (68) for receiving another one of the plurality of laterally extending spar tubes (50) in a non-perpendicular attachment point, whereby the seat system (10) is adapted to be laterally positioned and attached to provide different spaced apart passenger seating configurations. A seat back tray table (20) may be attached to the back of the passenger seat frame (22).
SEAT SYSTEM HAVING A CANTED LEG ASSEMBLY
SITZSYSTEM MIT EINER GEKANTETEN BEINANORDNUNG
SYSTÈME DE SIÈGE DOTÉ D'UN ENSEMBLE DE PIEDS INCLINÉ
2021-12-22
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |