FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Proposed lever comprises main body extending in lengthwise direction and including a connector extending radially from said main body. In compliance with this method, insert including base with connector made thereat is produced. Mandrel including insert base is made so that mandrel outer side section is confined by insert base outer side section. One or several plies of reinforcement fibres are laid around said mandrel. Resin is injected into ply or plies. Resin is polymerised for rigid bonding of reinforcement fibres and insert base.
EFFECT: higher mechanical strength at decreased weight.
5 cl, 10 dwg
Authors
Dates
2014-07-10—Published
2011-01-19—Filed