ATTACHMENT POINT BETWEEN CERAMIC FAIRING AND FLYING-VEHICLE BODY Russian patent published in 2005 - IPC

Abstract RU 2258283 C1

FIELD: aircraft and rocket technology; antenna fairings for high-speed rockets of various classes.

SUBSTANCE: through longitudinal slots, 1 - 2 mm wide, half or two thirds of adhesive bond between ceramic fairing and metal frame in length, are provided in metal frame of attachment point between ceramic fairing and flying-vehicle body; these slots are disposed through center of adhesive bond and spaced apart through distance equal to length of adhesive bond; specified bonding joint thickness equals maximal difference between radial temperature displacements of ceramic fairing and frame at maximal operating temperature level of up to 500 °C.

EFFECT: enhanced operating time and reliability of fairing at attachment point heating to maximal operating temperature.

1 cl, 1 dwg

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RU 2 258 283 C1

Authors

Suzdal'Tsev E.I.

Kurakin V.I.

Kharitonov D.V.

Khora A.N.

Dates

2005-08-10Published

2004-03-19Filed