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

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

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 comp...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: SCHLIPF, Bernhard, HUE, Xavier
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung: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.