FIELD: process engineering.
SUBSTANCE: invention relates to aerospace engineering. Reinforcing element comprises intake area and pressure area adapted to intake area geometry. Pressure element fits in reinforcing element intake area. Reinforcing element and pressure element fitted in place are bonded together by plug-in joint. Said plug-in joint comprises one male part fitted at pressure element and one female element fitted at reinforcing element. Reinforcing element with pressure element secured thereto is applied to reinforcing element from fibrous composite to make a forming part. For bonding of reinforcing element with component from fibrous comprises the forming part is solidified. Plug-in connector and pressure element are removed from reinforcing component of fibrous composite.
EFFECT: higher accuracy of produced components.
13 cl, 8 dwg
Authors
Dates
2014-06-27—Published
2010-09-07—Filed