Creanova Universal Closures Limited

Ge Aviation Systems Limited

Mark Andrew Smith

Rodney M Druitt

James Dimond

Rodney Malcolm Druit

Rodney Druitt

Closure (), for sealing of a neck finish () of a liquid container, comprising a top deck () and an outer skirt () extending from the top deck () in an axial direction (z) away from the top deck (). The outer skirt () comprises a top section () arranged adjacent to the top deck () and a bottom section () separated from the top section () by a gap (). The top section () and the bottom section () are interconnected to each other by a hinge (). The outer skirt () comprises an inwardly protruding locking bead () extending along an inner surface () of the outer skirt (), wherein the locking bead () at at least one location continues across the gap ().

Hinged closure

A touch screen display assembly can include a touch sensitive screen having a screen surface, and at least one hand anchor located adjacent the screen surface. The at least one hand anchor can also be configured to form a stabilizing feature when a user interacts with the touch sensitive screen.

Touch screen display assembly and method of operating vehicle having same

A method and apparatus for operating a display module includes a backlight illuminator, an ambient light sensor configured to generate an output signal, and a backlight controller module operably coupled with the backlight illuminator, the ambient light sensor, and configured to determine the operational status signal of the ambient light sensor based on the output signal and operate backlight illuminator in accordance with the operational status signal.

Method and apparatus for a display module control system

A landing system for controlling operation of an aerial vehicle flying a final approach to a runway includes a computing device and a LIDAR scanner. The device obtains a first data set indicative of a reference flight path for the final approach. The first data set includes a time-of-flight measurement for each light beam of a first plurality of light beams emitted prior to the aerial vehicle flying the final approach. The device determines an actual flight path for the final approach based, at least in part, on a second data set comprising a time-of-flight measurement for each light beam of a second plurality of light beams emitted from the light source of the LIDAR scanner. Based on the first and second data sets, the device determines the actual flight path deviates from the reference flight path and generates a control action to adjust operation of the aerial vehicle.

Landing system for an aerial vehicle

The present disclosure relates to a closure, especially a closure for packages for liquids such as beverages. In particular the invention relates to a closure for containers for carbonated liquids such as soft drinks. The closure comprises an outer shell with a reduced weight and a sealing means which actively compensates the deformation of the outer shell to avoid loss of performance.

Closure

Closure () comprising a ring shaped base () laterally surrounding a cap () which is functionally interconnected to the ring shaped base () via a hinge arrangement (), whereby the ring shaped base () is having an in general horizontal section () on which a first end of the hinge arrangement () is fixed protruding vertically (z) above the horizontal section () of the ring shaped base () and whereby a second end of the hinge arrangement () is laterally fixed to an outer sidewall () of the cap ().

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Cheltenham, United Kingdom

Mark Andrew Smith