A gas turbine engine nacelle includes an inner skin surrounded by a radially outer skin. The inner skin terminates at an exhaust outlet. The outer skin terminates at a recess in the inner skin extending into a closed cavity under the outer skin.
RECESSED ENGINE NACELLE
AUSGESPARTE TRIEBWERKSGONDEL
CARTER-MOTEUR EN RETRAIT
28.09.2016
Patent
Elektronische Ressource
Englisch