An aircraft stowage unit 200 configured to provide a footwell 202 for an adjacent seating unit 201. The stowage unit may comprise an upper section (301,fig3) and a lower(302,fig3) section, the lower section may be configured to provide the footwell for the adjacent seating unit. The aircraft stowage unit may be a galley unit and may comprise a heated unit or a refrigerated unit (405,fig4). The length of the stowage unit in the direction parallel to the longitudinal axis of the aircraft may be less than 70cm. The seat may recline into a bed. The seat may be positioned less than 90 degrees to a front surface 203 of the stowage unit, and less than 90 degrees to the longitudinal axis of the aircraft. The stowage unit may be a first stowage unit, there may be a second stowage unit where the distance between the front surface of the first stowage unit and the back surface 602 of the second stowage unit is less than 260 degrees.
Aircraft stowage unit
2022-10-19
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |