HYBRID AIRCRAFT FUSELAGE CELL STRUCTURE Russian patent published in 2013 - IPC B64C1/06 B64G1/22 

Abstract RU 2482995 C1

FIELD: transport.

SUBSTANCE: invention relates to aircraft engineering. Proposed aircraft structure comprises skin panel with dual shell, skin single-piece panel, stiffness element arranged between skin panels and lengthwise strip to load transition section. said lengthwise trap is located in the area of lengthwise seam and comprises first and second lengthwise flanges shifted relative to each other and jointed together by strap. Load transition section is located in the area of transverses seam for connection of lengthwise stiffness element at skin single-piece panel with dual-shell panel.

EFFECT: decreased weight of aircraft skin.

20 cl, 6 dwg

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RU 2 482 995 C1

Authors

Dol'Tsinski Vol'F-Ditrikh

Khel'Tsh Norbert

Khartvig Arne

Mjuller Markus

Veber Markus Jorg

Prove Jens-Ul'Rikh

Jern Paul'

Dates

2013-05-27Published

2010-03-16Filed