The Boeing Company
Aircraft radome apparatuses and methods

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Abstract:

Aircraft radome apparatuses and methods are described. In some examples, a radome is to be mounted on an aircraft. In some examples, the radome includes an outer mold line having a closure angle. In some examples, the closure angle is configured to reduce a footprint of the radome. In some examples, the closure angle is also configured to reduce a likelihood of separated airflow from occurring proximate a trailing portion of the radome during a flight of the aircraft. In some examples, the radome is to be mounted on the aircraft at a location that reduces a rate of change of a transverse cross-sectional area of the aircraft.

Status:
Grant
Type:

Utility

Filling date:

9 May 2017

Issue date:

28 Apr 2020