FIELD: electricity.
SUBSTANCE: proposed by the invention shielded and leak-tight cable assembly is intended for using in aviation engine. The cable assembly includes conductive elements (20) enclosed into tubular protected and shielded structure (22) consisted of inner tubular textile braiding (24), intermediate metal braiding (26), electromagnetic shielding and external corrugated sheath (28) with its end being glued to thermocontracted pin (30) to have fixation on connector item or y-splice.
EFFECT: reduced weight of shielded and leak-tight cable assembly, that can form bending of small radius.
9 cl, 2 dwg
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Authors
Dates
2010-12-10—Published
2007-05-18—Filed