FIELD: transport.
SUBSTANCE: invention relates to aircraft fuselage with sealed cabin provided with multiple airport holes and/or through holes. Aircraft fuselage comprises skin 1 reinforced by several vertical frames 7 and several horizontal stringers 8. Skin 1 has several airports 5. Every said airport has frame 6. Stringer 7 extends through airport frame 6 to that frame 7 terminates at airport frame top section 9 and bottom section 10. Transition between airport stringer 7 and frame 6 has frame fork 11 to produce triangle 12 in said fork composed by airport stringer 7 and frame 6.
EFFECT: optimum design and distribution of stresses in fuselage structure.
3 cl, 1 dwg
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