A blade seal for covering an interface between first and second components of an aircraft includes a mounting portion extending in a longitudinal first direction for connection to the first component. A contact portion maintains contact with the second component. A plurality of pockets positioned along the first direction are separated by projections extending in a second direction perpendicular to the length. Each pocket has a variable depth and facing the second component.
Aircraft blade seal
2020-05-05
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |