Aeronautics and astronautics – Aircraft structure – Fuselage and body construction
Patent
1975-11-19
1977-10-11
Hoag, Willard E.
Aeronautics and astronautics
Aircraft structure
Fuselage and body construction
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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Barnoin Pierre
Duret Maurice Louis
Hoag Willard E.
Societe Nationale Industrielle Aerospatiale
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