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SHINTO technology
Shinto F3B/F3F wing joiner construction
1 - Joiner caps of high modulus carbon fiber (for F3B) and high-strength carbon (for F3F);
2 -Joiner shear web with ballast box of carbon braids;
3 - Joiner vertical caps of high-strength carbon perceive shock during landing.
Shinto fuselage tail part construction
1,2 - Outer and inner layers of Carboline 65 2/45 perceive the torsional loads of the V-tail;
3 - The longitudinal layers of high modulus carbon fiber provide high stiffness of the fuselage.
Shinto F3B/F3F wing construction
1 - Outer layer of Carboline 65 2/45 with D-box reinforced on the front part;
2 - The wing back shear web;
3 - The inner layer of Carboline 39 2/45;
4 - The flap hinge;
5 - The flap shear web;
6 - The sandwich material;
7 - The spar bottom cap of high modulus carbon fiber;
8 - The spar top cap of high modulus carbon fiber;
9 - High-strength epoxy glue for the sparr;
10 - Main spar shear web of balsa plywood with direction ±45 degree;
11 - The wing ballast box.