FAIRING Russian patent published in 2018 - IPC H01Q1/42 

FIELD: rocket engineering.

SUBSTANCE: invention relates to the field of aviation and missile technology and can be used primarily in the manufacture of aerial fairings for high-speed air-to-air or air-to-surface missiles. Essence of the invention lies in the fact that a fairing, including a ceramic shell, bonded by an elastic adhesive with a metal frame consisting of an adapter made of an Invar alloy and a butt element, joined together by means of collars and pins. On the outer surface of the adapter, in the region of its connection with the end zone of the ceramic shell, an annular groove is formed, perpendicular to which in the part of the connection of the adapter with the shell, the slots are uniformly arranged along the circumference. In the adapter collar, a discrete support element is placed adjacent to the shoulder of the butt joint, and a fastening element in the region of the pins. In the supporting element, axial grooves are placed in a staggered manner with respect to the slots of the adapter, and an additional annular groove is provided in the element.

EFFECT: technical result is an increase in the temperature and power performance parameters of the fairings of missiles of different classes.

1 cl, 1 dwg