发明名称 BUFFER ZONE FOR INTERIOR AIRCRAFT FEATURES
摘要 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.
申请公布号 WO2015162542(A9) 申请公布日期 2016.11.24
申请号 WO2015IB52876 申请日期 2015.04.20
申请人 BOMBARDIER INC.;SHORT BROTHERS PLC 发明人 MALEK, Bruce;HOLOWKA, Stefan;BEAUDIN, Nikolas
分类号 B64C1/06 主分类号 B64C1/06
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