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US 2006/0065782 A1Published application
Reinforced door
AssigneeAirbus SAS
InventorsClive French, Smail Maksen
Life of this patent
Estimating the term…
Abstract
This door includes components (20, 21, 22, 24) that form an internal structure (16). This internal structure (16) is reinforced by a network (82) of harnesses that link the majority of the components forming the internal structure. These harnesses are for instance carbon fiber strips glued onto the internal structure.
Claims7
Reinforced door (12) for an aircraft and comprising components (20, 21, 22, 24) that form an internal structure (16) characterized by the fact that the internal structure (16) is reinforced by a network (82) of harnesses linking the majority of the components that form the internal structure.
Dependencies are inferred from the claim text.