This invention provides a bonding and
assembly mold for carbon
fiber skin honeycomb panels used in satellites, including a pressure equalizing plate, a positioning base plate, a pad, a retaining strip, retaining strip gaskets, fastening screws, positioning screws, and limiting pins. The pad and positioning base plate are placed sequentially on a roller platform, with their openings aligned. Fastening screws are then passed through the positioning base plate and retaining strip sequentially to install the retaining strip onto the positioning base plate. Limiting pins are then passed through the retaining strip and positioning base plate sequentially to limit the retaining strip's position. The retaining strip
gasket is attached to the inner side of the retaining strip. A lower
skin with
adhesive film applied is placed in the mold, with the
adhesive film facing upwards. The
honeycomb core is then placed. The positions of the front and side embedded parts are confirmed, and the
honeycomb cores at the corresponding positions are
cut. Positioning screws are then passed through the positioning base plate and lower
skin sequentially to position the front embedded part. Positioning screws are then passed through the retaining strip and retaining strip
gasket sequentially to position the side embedded part. An upper skin with
adhesive film applied is placed, with the adhesive film facing downwards. The pressure equalizing plate is placed, and positioning screws are then passed through the pressure equalizing plate and upper skin sequentially to position the front embedded part. This invention can be used for the bonding,
assembly, and high-temperature curing of carbon
fiber skin honeycomb panels for satellites.