The invention proposes an aircraft-seat assembly (10a-e) having a first aircraft-seat arrangement (20a-e) and having a second aircraft-seat arrangement (22a-e), which is arranged directly behind the first aircraft-seat arrangement (20a-e) and is designed to be at least substantially identical to the first aircraft-seat arrangement (20a-e), wherein the second aircraft-seat arrangement (22a-e) has a housing (32a-e), which forms a backrest wall (34a-e) at least in a sub-region of the housing (32a-e) of the second aircraft-seat arrangement (22a-e), wherein, in an aircraft-seat region (36a-e), the second aircraft-seat arrangement (22a-e) comprises a seat base (52a-e), which has a front edge (54a-e), wherein a main-extent axis of the front edge (54a-e) of the seat base is oriented at an angle of at least 5 degrees in relation to a transverse axis (26a) of the second aircraft-seat arrangement (22a-e), wherein a reclining direction (46a) of the aircraft-seat region (36 a-e) is oriented at an angle of at least 30 degrees in relation to a longitudinal axis (24a) of the second aircraft-seat arrangement (22a-e), wherein the reclining direction (46a) is directed away from an access region (48a-e) of the aircraft-seat region (36a-e).
FLUGZEUGSITZANORDNUNG
AIRCRAFT-SEAT ASSEMBLY
ENSEMBLE SIÈGE D'AÉRONEF
2024-05-22
Patent
Elektronische Ressource
Deutsch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |