AERONACOSMIC DEVICE (OPTIONS) AND FLIGHT VEHICLE (OPTIONS), EXTENDED ELEMENT OF STRUCTURE OF AN AIR-SPACE DEVICE OR FLIGHT VEHICLE (OPTIONS), COMPLETE MONOGRAPHY CROP

摘要

1. An elongated structural element of the aerospace device made of a multilayer composite material, including a base and a rib extending from the base, the first surface of the base made with the possibility of its abutment to the structure of the aerospace device, the second surface of the base located on the opposite side from the first surface, the third the surface located on or in the rib, on the same layer of composite material with the first surface, the fourth surface located on the ribs e on the same side of the structural element as the second surface, the cross-section of the structural element, varying along at least part of its length with linear increase along the aforementioned at least part of the length of the structural element of the geodetic distance between the first reference line located on the first surface and the second reference line located on the third surface, which are geodesic lines running along the entire length of the aforementioned at least part of the length of the structural element, and the geodesic The distance is measured along the first and third surfaces of the structural element, and the structural element is made with the possibility of eliminating folds, stresses or tensile layers of the composite material in the zone of the said cross section of the elongated structural element. ! 2. The element according to claim 1, which contains an angle formed between the edge and the base of the structural element and changing along the length of the structural element. ! 3. The element according to claim 2, in which the third surface is made with the possibility of bending around the axis, essentially