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US 2018/0022445 A1Published application
Landing gear noise abatement devices
AssigneeGoodrich Corporation
InventorRONY GIOVANNI GANIS
Life of this patent
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Abstract
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.
Claims6
An aircraft landing gear comprising:
- a forward main post comprising a forked clevis;
- a trailing arm connected to the forward main post by an articulating joint at the forked clevis, the forked clevis having a void;
- and
- a noise abatement system limiting airflow through the void.
1 more element
Dependencies are inferred from the claim text.