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Deformable panel element for engine of aircraft, has chamber containing fluid pressurized to deform element toward constraint configuration by opposing force, and frame returning element to rest configuration by releasing pressure
Deformable panel element for engine of aircraft, has chamber containing fluid pressurized to deform element toward constraint configuration by opposing force, and frame returning element to rest configuration by releasing pressure
The element (1) has a deformable elastomer body (2) equipped with a frame (3) made of elastic material and forming an inflatable sealing chamber (4) containing fluid. The chamber presents a rest configuration corresponds to conformation of the panel element. The fluid in the chamber is pressurized for deforming the element toward a constraint configuration, corresponding to another conformation of the panel element, by opposing restoring force that returns the frame toward the rest configuration. The frame returns the element to the rest configuration by releasing pressure. An independent claim is also included for a deformable panel comprising a deformable panel element.
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