A method and apparatus for conforming a display panel to a surface of an aircraft structure. The method positions the display panel within a resin barrier that is located on the surface such that a cavity is formed, places a film and the display panel together, and applies a force on the display panel that causes the display panel to conform to the surface of the aircraft structure. The display panel has a shape that changes to a first shape to match a second shape of the surface of the aircraft structure. The method also injects a resin into the cavity while the force is applied, and cures the resin in the cavity while the force is applied to form a cured resin. The cured resin holds the display panel in the first shape and attaches the display panel to the surface of the aircraft structure.

A method and apparatus for conforming a display panel to a surface of an aircraft structure. The method positions the display panel within a resin barrier that is located on the surface such that a cavity is formed, places a film and the display panel together, and applies a force on the display panel that causes the display panel to conform to the surface of the aircraft structure. The display panel has a shape that changes to a first shape to match a second shape of the surface of the aircraft structure. The method also injects a resin into the cavity while the force is applied, and cures the resin in the cavity while the force is applied to form a cured resin. The cured resin holds the display panel in the first shape and attaches the display panel to the surface of the aircraft structure.

An unmanned autonomous vehicle is configured to delivery packages in a product delivery network. The vehicle includes an outer housing, a conversion circuit, a battery, and a control circuit. The outer housing includes a first layer that is configured to collect solar radiation, and a second layer that is configured to render a visual display. The conversion circuit is disposed within the outer housing, and is coupled to the first layer. The conversion circuit is configured to convert the collected solar radiation to electrical charge and store the charge in a battery. The control circuit is coupled to the second layer and is configured to independently determine one or more images to render at the second layer, and to cause the one or more images to be rendered at the second layer. The solar radiation is collected at the first layer simultaneously with the images being rendered at the second layer.

An unmanned autonomous vehicle is configured to delivery packages in a product delivery network. The vehicle includes an outer housing, a conversion circuit, a battery, and a control circuit. The outer housing includes a first layer that is configured to collect solar radiation, and a second layer that is configured to render a visual display. The conversion circuit is disposed within the outer housing, and is coupled to the first layer. The conversion circuit is configured to convert the collected solar radiation to electrical charge and store the charge in a battery. The control circuit is coupled to the second layer and is configured to independently determine one or more images to render at the second layer, and to cause the one or more images to be rendered at the second layer. The solar radiation is collected at the first layer simultaneously with the images being rendered at the second layer.

A method and apparatus for conforming a display panel to a surface of an aircraft structure. The method positions the display panel within a resin barrier that is located on the surface such that a cavity is formed, places a film and the display panel together, and applies a force on the display panel that causes the display panel to conform to the surface of the aircraft structure. The display panel has a shape that changes to a first shape to match a second shape of the surface of the aircraft structure. The method also injects a resin into the cavity while the force is applied, and cures the resin in the cavity while the force is applied to form a cured resin. The cured resin holds the display panel in the first shape and attaches the display panel to the surface of the aircraft structure.

A method and apparatus for conforming a display panel to a surface of an aircraft structure. The method positions the display panel within a resin barrier that is located on the surface such that a cavity is formed, places a film and the display panel together, and applies a force on the display panel that causes the display panel to conform to the surface of the aircraft structure. The display panel has a shape that changes to a first shape to match a second shape of the surface of the aircraft structure. The method also injects a resin into the cavity while the force is applied, and cures the resin in the cavity while the force is applied to form a cured resin. The cured resin holds the display panel in the first shape and attaches the display panel to the surface of the aircraft structure.

An adhesive marking device generally includes an adhesive layer, a marking layer arranged on the adhesive layer, and a varnish layer that covers the marking layer. The marking layer includes a marking and a carrier film. The marking device generally has a moisture vapour transmission rate (MVTR) greater than or equal to 50 g/(m.sup.2.Math.day).

The present invention relates to an apparatus (100) and method (200) of affixing display material, more particularly, display material on aircraft interior surface such as overhead stowage bin, comprising the steps of: overlaying the display material on the bin surface (S201), then applying at least one holder on at least one bin edge securing the display material and the bin therein (S202).

The present invention relates to an apparatus (100) and method (200) of affixing display material, more particularly, display material on aircraft interior surface such as overhead stowage bin, comprising the steps of: overlaying the display material on the bin surface (S201), then applying at least one holder on at least one bin edge securing the display material and the bin therein (S202).

A projection system of the present disclosure includes: a flying object having an exterior body, a flying device that causes the exterior body to fly, and an image capturing device that captures an image; a projection device that projects a capture-dependent image on the exterior body, the captured-dependent image depending on the image; and a controller that causes the projection device to project the capture-dependent image.