FIELD: construction.
SUBSTANCE: present invention relates to a method and an apparatus for manufacturing structural inserts configured to receive loads in honeycomb structures in an aircraft. Sandwich structure comprises a core with a cavity in which a structural insert is placed. Structural insert comprises a first number of parts configured to receive a load, and a second number of parts assembled with the first number of parts to form the structural insert. Density of the first number of parts is different at different portions of said first number of parts based on the expected load.
EFFECT: higher strength of the structure.
12 cl, 26 dwg
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