HIGH LIFT COMPONENT FOR AN AIRCRAFT, HIGH LIFT SYSTEM, METHOD FOR ADJUSTING THE HIGH LIFT CHARACTERISTICS OF AN AIRCRAFT AND AIRCRAFT

摘要

A high lift component includes at least one intermediate seal on at least one lateral surface, wherein the intermediate seal includes at least one hollow body made of an elastic material, which hollow body includes a fluid inlet that is connectable to a fluid source. A gap between two high lift components, which gap is subjected to dynamic changes in geometry, can be flexibly sealed in this manner.