The invention relates to an aerodynamic body for flying objects having a hybrid laminar flow control, wherein the aerodynamic body comprises:- a load bearing supporting structure (11) having at least one hollow chamber forming a low-pressure suction plenum (18);- a perforated panel skin (20) arranged on the supporting structure of the aerodynamic body having an outer surface (23), the perforated panel skin has a plurality of openings being in fluid communication with the low-pressure suction plenum; and- at least one compressor (40) having at least one inlet (41) and at least one outlet (42);characterized in that- the compressor is located inside the hollow chamber; and- the inlet of the compressor protrudes into the low-pressure suction plenum and the outlet sticks out of the low-pressure suction plenum into an ambient pressure compartment so that a low-pressure within the low-pressure suction plenum established by the compressor results in air suction through the openings of the perforated panel skin.
AERODYNAMIC BODY FOR FLYING OBJECTS
AERODYNAMISCHER KÖRPER FÜR FLUGOBJEKTE
CORPS AÉRODYNAMIQUE POUR DES OBJETS VOLANTS
2022-11-23
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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