| 摘要 |
A pressurized aircraft fuselage, comprising a pressure bulkhead (1) installed on a fuselage structure (2), which forms a barrier between an internal pressurized cabin area (3) and an outside area (4), wherein the edge of the pressure bulkhead (1) is circumferentially attached to the fuselage structure (2) by movable fastening means, wherein the movable fastening means comprise at least one clamping element (5a, 5b) which is arranged inside a trapezoidal shaped mounting bracket (6) which corresponds to an inserted edge of the pressure bulkhead (1), in order to form a clamping connection for the pressure bulkhead (1) towards the fuselage structure (2). |
