Grid-like reinforcement structure for reinforcing skin field of fuselage of aircraft, has rigid parts merged in intersection regions, and load transfer element arranged in intersection region and in active connection with parts

摘要

The structure (6) has rigid parts (8, 10) merged in intersection regions (16), and a load transfer element (2) arranged in the intersection region and in active connection with the rigid parts. The load transfer element has two arms, and a projection for load transfer is designed in a connecting section of the arms. The projection is provided above the intersection region. The load transfer element is formed by two oppositely lying V-shaped bodies that exhibit a common connecting section. The load transfer element exhibits an opening for guiding the rigid parts.