Abstract: An electronic device may have a display mounted in a housing. The display may have a pixel array that produces images. A display cover layer may overlap the pixel array. The display cover layer may have a planar central area surrounded by a peripheral edge area with a curved cross-sectional profile. From an on-axis viewing angle, an image on the pixel array is fully viewable through the planar central area and the peripheral edge area. From an off-axis viewing angle, the image is partly viewable through the peripheral edge area and not through the central area. To avoid an undesired color cast in the partly viewable image seen through the peripheral edge area of the display cover layer, the display may be provided with color cast compensation structures such as a guest-host liquid crystal layer that exhibits an anisotropic colored light absorption characteristic, a diffuser layer, and/or other optical structures.

Abstract: A retainer device for a cable used in an aircraft includes a base. A moveable member is movably connected to the base and forms a channel with the base that is adapted to receive a cable. A pad-deforming portion is defined in the moveable member, which is displaceable between an open position in which a portion, of the moveable member is separated from the base to provide access to the channel, and closed positions, in which the moveable member is releasably connected to the base. A resilient pad is located in the pad-deforming portion to contact the cable received in the channel. The resilient pad is sized to deform from a rest state to a deformed state by the pad-deforming portion during insertion thereinto. The resilient pad is held captive after insertion into the pad-deforming portion by reforming toward the rest state.

Abstract: A device connects a wire harness to a structure. A fixation portion of the device is secured to the structure. A spacing portion is connected to the fixation portion and to a connector portion. A retaining clip on the connector portion deforms when a wire harness connector component moves axially toward the fixation portion. The clip opposes an abutment edge against the component into engagement position when the component is past the clip to prevent it from moving back onto the clip. An abutment surface contacts another portion of the component in engagement position to prevent further axial movement of the component toward the fixation portion. The component is held captive between the edge and the abutment surface. Also provided are a cable support for connecting the wire harness to the device, a method for connecting and disconnecting the wire harness to a structure with the device, and an aircraft.

Abstract: A retainer device for a cable used in an aircraft includes a base. A moveable member is movably connected to the base and forms a channel with the base that is adapted to receive a cable. A pad-deforming portion is defined in the moveable member, which is displaceable between an open position in which a portion, of the moveable member is separated from the base to provide access to the channel, and closed positions, in which the moveable member is releasably connected to the base. A resilient pad is located in the pad-deforming portion to contact the cable received in the channel. The resilient pad is sized to deform from a rest state to a deformed state by the pad-deforming portion during insertion thereinto. The resilient pad is held captive after insertion into the pad-deforming portion by reforming toward the rest state.

Abstract: A device connects a wire harness to a structure. A fixation portion of the device is secured to the structure. A spacing portion is connected to the fixation portion and to a connector portion. A retaining clip on the connector portion deforms when a wire harness connector component moves axially toward the fixation portion. The clip opposes an abutment edge against the component into engagement position when the component is past the clip to prevent it from moving back onto the clip. An abutment surface contacts another portion of the component in engagement position to prevent further axial movement of the component toward the fixation portion. The component is held captive between the edge and the abutment surface. Also provided are a cable support for connecting the wire harness to the device, a method for connecting and disconnecting the wire harness to a structure with the device, and an aircraft.