| 摘要 |
The invention relates to an aircraft galley (10) comprising a main element (12) that is divided into a plurality of compartments (26) by a partition panel system (24). The partition panel system (24) comprises a first partition panel (28), in which at least one installation slot (40) is designed that extends from a first edge (42) of the first partition panel (28) in the direction of an inner region of the first partition panel (28), and a second partition panel (30). The installation slot (40) designed in the first partition panel (28) receives an installation section (44) of the second partition panel (30). The installation slot (40) designed in the first partition panel (28) and the installation section (44) of the second partition panel (30) are designed such that primary surfaces (32, 34) of the first partition panel (28) are aligned substantially vertically to the primary surfaces (36, 38) of the second partition panel (30). At least one lateral surface (52, 54) of the installation slot (40) designed in the first partition panel (28) carries a first guide device (56) that interacts with a complementary second guide device (58) arranged in the region of the installation section (44) of the second partition panel (30). An installation section (46) of the first partition panel (28), which extends from a face of the installation slot (40) designed in the first partition panel (28) in the direction of a second edge (48) of the first partition panel (28) opposite of the first edge (42) of the first partition panel (28), carries a third guide device (60) that interacts with a complementary fourth guide device (62) arranged in the region of a lateral surface (50; 82) of the second partition panel (30) facing the installation section (46) of the first partition panel (28). |
