Helicopter cabin and method of making same

Aeronautics and astronautics – Aircraft structure – Fuselage and body construction

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Details

244117R, 264275, 264279, 264310, B64C 100, B29D 300, B29C 504

Patent

active

040531260

ABSTRACT:
The present invention relates to a process for making a thin-walled composite structure having resistance profiled elements, wherein a rotational-moulding mould is made, in the shape of said structure, then resistant profiled elements made of heat-conductive material are positioned in said mould, in order to form a main resistant frame-work for said structure, after which a suitable synthetic material is introduced into the mould and the known operations of rotational moulding are carried out. The structure thus produced may be used for the construction of aerodynes, and in particular in helicopter construction.

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patent: 3071217 (1963-01-01), Gould
patent: 3432979 (1969-03-01), Heiman
patent: 3555756 (1971-01-01), Curran et al.
patent: 3714312 (1973-01-01), Nitta et al.
patent: 3798300 (1974-03-01), Verbeke
patent: 3875275 (1975-04-01), Lemelson

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