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Aircraft panel system, aircraft, and method of operating the aircraft panel system
An aircraft panel system including a first panel, having a hinged coupling configured to couple the first panel to an aircraft structure, a second panel disposed adjacent to the first panel such that the first panel and the second panel together form cabin surface of an aircraft, and a latch mechanism configured to releasably couple the second panel to the aircraft structure, where the first panel is configured to pivot about the hinged coupling from a latched position to an actuation position to actuate the latch mechanism and cause a release of the second panel from the latch mechanism.
Aircraft panel system, aircraft, and method of operating the aircraft panel system
An aircraft panel system including a first panel, having a hinged coupling configured to couple the first panel to an aircraft structure, a second panel disposed adjacent to the first panel such that the first panel and the second panel together form cabin surface of an aircraft, and a latch mechanism configured to releasably couple the second panel to the aircraft structure, where the first panel is configured to pivot about the hinged coupling from a latched position to an actuation position to actuate the latch mechanism and cause a release of the second panel from the latch mechanism.
Aircraft panel system, aircraft, and method of operating the aircraft panel system
FILES JOE (author) / LOGUE ADAM A (author)
2023-05-09
Patent
Electronic Resource
English
AIRCRAFT PANEL SYSTEM, AIRCRAFT, AND METHOD OF OPERATING THE AIRCRAFT PANEL SYSTEM
| European Patent Office | 2020