Bombardier Inc.
Buffer zone for interior aircraft features
Last updated:
Abstract:
Several embodiments of buffer zones are provided that are contemplated to be disposed with respect to two or more adjacent elements on an aircraft. The buffer zones adjust for dynamic spacing between the elements to help control different gapping requirements between the elements installed in the aircraft. Embodiments include an aircraft interior panel configuration, an aircraft interior wall panel configuration, an adjustable width aircraft bulkhead, and an aircraft personal service unit.
Status:
Grant
Type:
Utility
Filling date:
20 Apr 2015
Issue date:
11 May 2021