AIRCRAFT SAFETY SYSTEM Russian patent published in 2011 - IPC B64D25/12 B64C1/32 

Abstract RU 2425781 C2

FIELD: transport.

SUBSTANCE: aircraft 10 comprises fuselage 12 with top piloted section 10a and bottom detachable section 10B jointed to top section 10A in normal flight. Top wing 14A is jointed with fuselage top piloted section 10A while bottom wing 14B is jointed with bottom detachable fuselage section 10B. Split fasteners serves to joint bottom detachable section 10B with top section 10A. Split fasteners may be actuated in flight to allow detachment of top piloted section 10A from bottom detachable section 10B. Top piloted section 10A may perform controlled flight without bottom detachable section 10B.

EFFECT: lower weight and reduced production costs.

39 cl, 138 dwg

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RU 2 425 781 C2

Authors

Bertani Romolo Lorentso

Dates

2011-08-10Published

2006-08-28Filed