Pressure-loaded skin of aircraft's door incorporates reinforcing ribs guided in direction of loads to be supported and spaced apart so that skin is the supporting structure of door

摘要

The pressure-loaded skin of an aircraft's door incorporates reinforcing ribs (40-46) which are guided in the direction of the loads to be supported and spaced apart so that the skin is the supporting structure of the door. The reinforcing ribs are spaced apart in the fuselage's longitudinal direction and radially in relation to each other. The reinforcing ribs are guided in the radial direction of the fuselage but displaced in relation to each other in the fuselage's longitudinal direction.