FIELD: physics.
SUBSTANCE: proposed method consists in making model components including fuselage integrated with wings, front horizontal and tail units, as well as parts with boundary layer drain channels. Parts with engine duct inner passages are moulded from carbon fiber-reinforced plastic, injection mould being divided into top and bottom parts. Note here that mould bottom part accommodates parts with boundary layer drain channels and parts with engine duct inner passages for fuselage with wings or metal plate for attachment of tail unit to airframe. Produced top and bottom halves hardened, they are jointed together on building block till complete hardening with the help of epoxy resin. Airframe is assembled on said building block. Said airframe comprises not profiled core with brackets, aforesaid top and bottom halves. Replaceable nose cone is fitted on core. Front and tail units and intake and outlet nozzles are screwed to fuselage.
EFFECT: reduced time of producing aerodynamic model.
3 dwg
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Authors
Dates
2011-04-27—Published
2009-11-09—Filed