FIELD: transport.
SUBSTANCE: invention relates to structural element and airframe of aircraft or spacecraft with said structural element. Structural element is composed of load-bearing component to strengthen aircraft or spacecraft inner skin. Structural element comprises hollow section to receive system medium. Structural element has mounting post to attach said structural element to skin. Said mounting post has base arranged on skin and may be secured to skin and receiving part configured to receive hollow section.
EFFECT: reduced weight.
11 cl, 3 dwg
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