FIELD: machine building.
SUBSTANCE: invention relates to structural system for aircraft and to method of increasing ability to withstand retraction of composite elongated element during aircraft operation. Claimed system comprises long composite element, channel and multiple composite structures. Composite elongated element is made on the side for attachment to the structure. Channel is located on side of elongated element and extends along length of composite elongated element. Plurality of composite structures can be arranged in channel and secured to section of composite elongated element side to structure.
EFFECT: plurality of composite structures is configured to increase the ability of the composite elongated element to withstand forces that pull the composite elongated element from the structure.
14 cl, 20 dwg
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