METHOD FOR ASSEMBLING PARTS OF THE AIRCRAFT WITH THE FORMATION OF THE AIRCRAFT UNIT (OPTIONS), THE AIRCRAFT ASSEMBLY AND THE GASKET SET

摘要

1. The method of assembly of the parts of the aircraft with the formation of the node of the aircraft, in which the first surface of the first part is adjacent to the second surface of the second part, characterized in that the first and second parts are measured first in a state separate from each other, and then calculated from the obtained measurement results the size and shape of the space that will be formed between the first and second surfaces after assembly, then, according to the calculation results, a gasket of variable thickness is taken and the first and second are assembled th part with the gasket to its position between said parts, with changes in the above space compensated by variable thickness of the gasket. ! 2. The method according to claim 1, characterized in that the measurement of the first part is carried out when fixing the first part on the slipway. ! 3. The method according to claim 2, characterized in that the measurements of the first part are carried out with the measurement of the positions of the first part relative to the base point on the slipway. ! 4. The method according to claim 1, characterized in that the variability of the thickness of the strip is created depending on the variability of the profile of each opposite front side of the strip. ! 5. The method according to claim 1, characterized in that the gasket is obtained in an additional manufacturing process. ! 6. The method according to claim 1, characterized in that in the presence of a group of surfaces adjacent to one another, a corresponding gasket is made for each adjacent surface of the first and second parts, and when assembling the named parts, a corresponding gasket is placed between each of the adjacent surfaces. ! 7. The method according to claim 6, characterized in that it is used in exchange