In order to meet the requirements of full-scale static test verification of the leading edge slat structure on large passenger aircraft, attitude adjustment devices are designed. The devices are composed of track simulation part, gear simulation part, bearing, bolts, etc. The structures are designed reasonable, which can meet the needs of slat installation and attitude adjustment. Load transfer analysis shows that the load state of the devices is highly consistent with the real structure, which indicating that the devices can meet the requirements of slat static test.
Machine Design and Manufacturing Engineering