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Components for aircraft engine nacelle
Monolithic sandwich structures consisting of CFRP skin and aluminum honeycomb core
Part number:
Description
Intended use:
Components with airfoils for aircraft gas turbine engines and airframe attachment points.
Characteristics:
Diameter of engine nacelle doors – up to 2000 mm.
Components with airfoils for aircraft gas turbine engines and airframe attachment points.
Characteristics:
Diameter of engine nacelle doors – up to 2000 mm.