FIELD: in-flight refueling systems.
SUBSTANCE: invention relates to an in-flight refueling system. The parachute skirt (1) of the sensor cone (2) of the in-flight refueling pendant contains a fabric dome (3). The dome (3) is made in the form of wedges in an amount equal to the number of ribs-levers (6). Wedges are assembled from pieces of heat-resistant rectangular fabric with oriented warp and weft directions. Each power cable (4,5) at the points of attachment to the ribs-levers (6) is equipped with an elastic sleeve made of a material whose melting temperature is close to the limiting operating temperature of the dome (3) fabric.
EFFECT: invention increases its temperature resistance and fixes signs of exposure to elevated temperatures.
1 cl, 5 dwg
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