Guided missile and unmanned aerial vehicle equipment compartment structural texture

• Main Authors: WANG ZAIYU, ZHU LIYUAN, DENG JIN, JIN JIACHAO, YI LONG, HUANG HAILONG, DONG HAOWEI, LIANG KEREN
• Format: Patent
• Language: English
• Published: 16.12.2015
• Subjects: AEROPLANES; AIRCRAFT; AMMUNITION; AVIATION; BLASTING; COSMONAUTICS; EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION; HEATING; HELICOPTERS; LIGHTING; MECHANICAL ENGINEERING; PERFORMING OPERATIONS; TRANSPORTING; WEAPONS

The utility model discloses a guided missile and unmanned aerial vehicle equipment compartment structural texture, including preceding frame, after -frame, long purlin, go up covering, covering, left flap, right flap and web down, on the circular frame of frame and after -frame is riveted in the front respectively at all long purlin both ends, the web is the rectangle wallboard, and the riveting is on top growth purlin and long purlin down and all long purlin, preceding frame and after -frame formation combination beam structural style, and left flap is through mounting screw frame, after -frame, upper left long purlin and a left side down on the long purlin in the front, and right flap is through mounting screw in the front under frame, after -frame, upper right long purlin and the right side on the long purlin. The one -tenth fitting up of equipment compartment is on the web, and the web also is a load -carrying construction spare. A dismountable when left side flap and right flap are maintained is not only as the dimension shape of cabin section but also as the inside installation maintenance channel that becomes the part. The utility model discloses make full use of the effective space of the cabin body, simple and direct convenience is safeguarded in the inside installation that becomes parts, the strong rigidity of whole that becomes the fitting up problem but also effectively improved the cabin body had not only been solved to well intersternite.