A noise abatement system for an aircraft landing gear is provided. The system may have a retention member and a covering member. In this regard, the system may be configured to block the airflow through a structural void to abate noise. Moreover, the system may be shaped to diminish aerodynamic drag.
Landing Gear Noise Abatement Devices
2016-12-29
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |