Role of structural noise in aircraft pressure cockpit from vibration action of new-generation engines

Abstract

The evolution of new-generation aircraft engines is transitioning from a bypass ratio of 4–6 to an increased ratio of 8–12. This is leading to substantial broadening of the vibration spectrum of engines with a shift to the low-frequency range due to decreased rotation speed of the fan rotor, in turn requiring new solutions to decrease structural noise from engine vibrations to ensure comfort in the cockpits and cabins of aircraft.