FIELD: aviation.
SUBSTANCE: invention relates to machining and assembling parts of aircraft and, in particular, to assembly of structural unit of airborne aircraft without using any adjusting pads, locating devices or boring conductors to produce finished holes of required size. Method of assembly of structural unit of aircraft includes support of body sections on appropriate adjustable supports and arrangement in required position between them of connecting body section. Assembly consists of multiple sections. Pre-drilled holes of connection in connecting body section are aligned with pre-drilled holes of mating in body sections with subsequent installation of fasteners.
EFFECT: higher quality of assembly.
12 cl, 17 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD FOR DYNAMIC ASSEMBLY OF AIRCRAFT GLIDERS AGGREGATE UNITS AND DEVICE FOR ITS IMPLEMENTATION | 2018 |
|
RU2695017C1 |
| SYSTEM FOR DRILLING PANELS DURING FINAL ASSEMBLY OF AIRCRAFT | 2017 |
|
RU2748241C2 |
| METHODS AND SYSTEMS FOR FRONT EDGES OF AEROSPACE VEHICLES | 2017 |
|
RU2674725C2 |
| METHOD FOR PRODUCING THREE-DIMENSIONAL OBJECT OF COMPOSITE MATERIAL | 2013 |
|
RU2623772C2 |
| LARGE-SIZED AERODYNAMIC MODEL | 2015 |
|
RU2607675C1 |
| IMPROVED WORKING DEVICES FOR INTERFERENCE FIT OF FASTENERS | 2017 |
|
RU2750927C2 |
| METHOD OF MAKING A GASKET AND AN ASSEMBLY UNIT OF AN AIRCRAFT, COMPRISING SUCH A GASKET | 2016 |
|
RU2733001C2 |
| MECHANICALLY DISTRIBUTED POWER PLANT AND METHOD OF AIRCRAFT OPERATION CONTROL | 2019 |
|
RU2743903C2 |
| PERFORATED STRUCTURE OF COVERING FOR SYSTEMS WITH A LAMINAR FLOW | 2003 |
|
RU2324625C2 |
| METHOD OF ASSEMBLING AIRCRAFT PARTS TO MAKE ASSEMBLY UNIT (VERSIONS), AIRCRAFT ASSEMBLY UNIT AND SET OF STRIPS | 2006 |
|
RU2485024C2 |
