FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Central torsion box 5 comprises two lateral surfaces 6 comprising, in their turn, in fact, inner and outer layers 2 and 1, a bit spaced apart. Inner and outer layers 2 and 1 of lateral surface 6 are interjointed by sections 3. Aircraft is distinguished for central torsion box 5.
EFFECT: aircraft stability.
9 cl, 4 dwg
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Authors
Dates
2011-02-27—Published
2006-05-11—Filed