An airflow profile structure having a leading and/or trailing edge profiled with a serrated profile having a succession of teeth and depressions. Along the leading and/or trailing edge, from a first location to a second location, the teeth of the serrated profile are individually inclined towards the second location.
TURBOMACHINE POUR AÉRONEF ET AÉRONEF ASSOCIÉ
TURBOMACHINE FOR AIRCRAFT AND CORRESPONDING AIRCRAFT
STRÖMUNGSMASCHINE FÜR FLUGZEUG UND ZUGEHÖRIGES FLUGZEUG
2022-07-20
Patent
Electronic Resource
French
IPC: | F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64C AEROPLANES , Flugzeuge / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F15D FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS , Strömungsdynamik, d.h. Verfahren oder Vorrichtungen zum Beeinflussen der Strömung von Gasen oder Flüssigkeiten |
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