SHINTO F3B/F3F

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.