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The main case of loading the airtight fuselage of the non-circular shape, determining static strength, durability and hardiness of the design is the case of overpressure.
Hie bearing scheme of a cross-section fuselage, typically including a skin, strong frames, stringers and transverse frame beams, is sufficiently effective.
Operation of the upper and the lower portions of such a fuselage significantly differs form operation of bearing elements in circular cylindrical fuselages.
A wide fuselage upon a such maneuver causes an additional complexity in a creation of well controllability.
The stressed condition and construction elements in cylindrical portions of such a fuselage, beyond the edge effect zone at the transition sites, do not differ from those in circular fuselages.
In the retracted position of the takeoff and landing wings, these blocks are reinforced by the retracted position locks of the fuselage.
The fuselage of such a type creates a lift in addition to the wing 4 lift and it may be named as a lifting fuselage.
They close a significant portion of tensile loads occurring between the top and lower parts of the fuselage.
With a second roar and tornado force, air inside the aircraft, until this moment maintained at normal pressure, swept through the ruptured fuselage to dissipate in the high altitude near-vacuum outside.С оглушительным воем воздух устремился через образовавшееся отверстие в разреженные высокие слои атмосферы.АэропортХейли, Артур© Издательство "Художественная литература", 1978AirportHailey, Arthur© 1968, 2000 by Arthur Hailey, Ltd.Hailey, Arthur / AirportХейли, Артур / Аэропорт
Such materials are recommended to be used in aircraft fuselage.
The longitudinal axis of symmetry of the fuselage is the longitudinal axis of symmetry of the fuselage viewed in plan.
Operation of bearing elements of the side portion of such a fuselage with a typical curvature radius, under effect of overpressure, is similar to operation of these elements in circular fuselages.
The guarantee of buoyancy and additional durability of survival aircraft design is provided with that in the bottom fuselage part and wings there are the cavities filled rigid floating material (polyfoam).
However, the circular shape of the fuselage cross- section imposes certain restrictions on disposal solutions for accommodating passengers and loads.
The pitot pressure probes in the system are usually attached to the fuselage nose.
fineness ratio of fuselage
относительное удлинение фюзеляжа
носовая часть фюзеляжа
fuselage aft portion
хвостовая часть фюзеляжа
fuselage aft section
хвостовой отсек фюзеляжа
fuselage finishing angle
контурный уголок фюзеляжа
fuselage forward section
передний отсек фюзеляжа
fuselage mid section
хвостовая часть фюзеляжа
pressurized fuselage part
герметичная часть фюзеляжа
задняя часть фюзеляжа
двухфюзеляжное воздушное судно