An aircraft galley cart bay door (10) includes a door main structure (16) having an inwardly facing peripheral inner edge (24) with an inner surface (26), and a surface seal (28) on the inner surface of the inwardly facing peripheral inner edge of the inner wall (18). A substantial majority of the main structure of the door is formed from a high strength molded carbon fiber composite material. The door main structure may optionally define a recess (38), and insulation material (36) can be disposed in the recess defined by the main structure of the door.
Aircraft galley cart bay door
2016-02-10
Patent
Elektronische Ressource
Englisch