Bonding process and measurement technique based on ceramic-based radomes

Abstract The radome is a key component of a high-speed vehicle, generally located in the front end of a missile or an airplane, and its assembly precision will directly determine the flight performance of the vehicle. The connection between the radome body part and the connecting ring currently has bolts, threaded connection, adhesive connection, welding connection, snap connection, flange connection, etc. In this paper, for the actual production of the traditional assembly of the head cone and connecting ring by manual adjustment, there are problems such as poor bonding accuracy, low degree of automation and inefficiency, so the semi-automated bonding method is chosen. Based on the above problems for the radome overall assembly program design, determine the main positioning structure and measurement technology, according to the main structure to determine the cone mask bonding process and the whole cone mask bonding process; for the design of the positioning technology and measurement technology to clarify the key points of the bonding technology and the difficulties and problems to be solved; for the equipment to meet the requirements of the technical specifications, after the bonding of the measurements, the collection of measurement data to verify that Whether to meet the technical requirements of bonding, test equipment functionality.