FIELD: transport.
SUBSTANCE: invention relates to aircraft building and concerns assembly technique of aeroplane units panels, in particular to aeroplane centre-section assembly technique. Method for assembling panels of aeroplane units includes assembling and riveting of specifically curved covering and straight stringers. Before assembling and riveting, stringers are preliminary shaped on loft with introducing deflection with advance of 3.0 mm to 5.0 mm and then strengthened on knock-drum device. Produced panels are used to perform assembling of aeroplane units.
EFFECT: improved quality of assembling and providing specified geometrical parameters of riveted panels.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF ASSEMBLY OF AIRCRAFT FUSELAGE | 1997 |
|
RU2121452C1 |
| METHOD OF RIVETING OF CURVILINEAR PANELS AT DRILLING-RIVETING MACHINE | 2014 |
|
RU2555263C1 |
| METHOD OF ASSEMBLY OF FLYING VEHICLE UNITS | 1999 |
|
RU2179136C2 |
| METHOD OF CONNECTING ITEMS BY PERMANENT RIVETED SEAM | 2006 |
|
RU2288380C1 |
| METHOD OF ASSEMBLY OF THIN-WALLED PANELS FOR AIRCRAFT | 1996 |
|
RU2093297C1 |
| METHOD FOR MODULAR ASSEMBLY OF THE BOX OF AN AIRCRAFT WING CONSOLE WITH PARTS MADE OF CARBON POLYMER COMPOSITE MATERIALS AND METALS AND AN ASSEMBLY LINE WITH DEVICES FOR IMPLEMENTING THE METHOD | 2021 |
|
RU2774870C1 |
| METHOD TO ASSEMBLE ITEM AT SEVERAL WORKING STAGES, COMPLEX OF ASSEMBLING ACCESSORIES AND PORTABLE ASSEMBLY ACCESSORY USED IN THEM | 2012 |
|
RU2517920C1 |
| 0 |
|
SU201051A1 | |
| DOOR OF ENGINE COMPARTMENT OF HELICOPTER ENGINE NACELLE AND MANUFACTURING METHOD THEREOF | 2020 |
|
RU2739827C1 |
| DEVICE FOR MAKING A BLADE | 2019 |
|
RU2714961C1 |
