Tubular carrier framework for use in aeronautic field, has zone driven in displacement along direction parallel to axis of components under action of axial deformation, where axial deformation neutralizes displacement effects of zone

摘要

The framework has a connection component (5) presenting dilatation and dimensional characteristics so as to axially retract or dilate the component along a direction corresponding to a displacement direction of a linking zone (10) of connection components (5, 6). The zone is driven in displacement along a direction parallel to a longitudinal axis of the components under the action of axial deformation of a connection node (3) and the component (6) connected to the node. The axial deformation neutralizes the displacement effects of the zone between the components on a tubular element (2). The tubular element has low dilatation coefficient. An independent claim is also included for a mold formed by a tubular carrier framework and a molding skin supported by the framework.