FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, and can be used for assembly of helicopter rotor blades, for performing assembly operation of frame rail assembly, lining of anti-icing system and counterbalance of composite blade of helicopter rotor. Proposed device comprises frame (1) accommodating columns (3) furnished with bearing assemblies (4). In bearing assemblies (4) on columns (3) there are wheels (5) with fasteners (6) and fastening flanges (7) with installed brackets (8, 9), fixed on them mandrel (12) and beams (20, 21), equipped with clamps (22), at that, on frame (1) on both sides of mandrel (12) there are hinged lodgments (25) with clamps (26). Frame (1) is equipped with rollers (2). Mandrel (12) and lodgments (25) repeat the theoretical outline of blade elements.
EFFECT: provides mobility of design, reduced time of assembly, reduced load on personnel.
4 cl, 4 dwg
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