FIELD: transport.
SUBSTANCE: aircraft higher-pressure fuselage in lengthwise direction comprises several sections 1a-1f. Rear dome-shape tight frame 2 is designed to form aircraft high-pressure inner space 3. Fuselage section 1a-1f is equipped with carcass element ring profile 5 for radial external attachment of dome-like tight frame 2. Carcass element profile 5 on the side of dome-like tight frame 2 comprises profile U-like section. First lateral end section 6 of the latter is secured to rear part of dome-like tight frame 2 by connector 7. Note here that elongated second branch 8 of frame 2 extending radially outward to make the connection with fuselage section 1e, 1f for connector 7 to be fitted in place from fuselage high-pressure inner space.
EFFECT: decreased quantity of connection elements.
12 cl, 4 dwg
