| 摘要 |
The frame-clamping device has connecting means (1,2) for connecting frame-clamping device at the first frame of the fuselage. A fixing means for force fitting and friction engaging fixing of first shell (10) and second shell of the fuselage is provided by which it is possible to produce first group of first bores of first shell in stress-free manner. An independent claim is also included for the method for longitudinal assembly of fuselage. |
