Invention Application
US20130062461A1 NACELLE FOR AN AIRCRAFT ENGINE 审中-公开
飞机发动机的NACELLE

NACELLE FOR AN AIRCRAFT ENGINE
Abstract:
A supporting half-structure for an aircraft engine nacelle is provided that includes at least one longitudinal beam and a front half-frame connected to each other and formed at least partly in composite materials. The half-structure includes a connecting hinge positioned in a junction area of the longitudinal beam and of the half-frame, the hinge being formed by composite materials laid out so that fibres of the composite materials are positioned in alignment with fibres of composite materials forming said front half-frame.
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