Fuselage structure for helicopter

Aeronautics and astronautics – Aircraft structure – Fuselage and body construction

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Details

244117R, 244119, B64C 106, B64C 112, B64C 122

Patent

active

055622640

ABSTRACT:
The invention relates to a helicopter fuselage of the type including a central structure to which are linked a front structure, a rear structure and a landing gear, and which supports a transmission gearbox, a main rotor and at least one engine (50), and of the type in which the central structure includes a skeleton (16) fitted with covering elements which define the external shape of the fuselage.
According to the invention, the skeleton (16) of the central structure exhibits substantially the shape of a regular hexahedron consisting of skeleton panels (28, 30, 32, 34, 36, 38) assembled together.
The invention finds an application especially for producing light helicopters.

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patent: 4676545 (1987-06-01), Bonfilio
patent: 4925132 (1990-05-01), Zider
patent: 5037041 (1991-08-01), Unterhitzenberger

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