Abstract: The present invention is a depth sensing visual prosthesis. By depth sensing objects within an image, items located at a certain depths from the user can be removed to declutter an image. The resulting image presents only objects within a range of depth from the visual prosthesis user. Depth sensing can be accomplished in various ways including structured light, time of flight, or preferably, a stereo camera pair.

Abstract: An apparatus and computerized method are provided for monitoring the positions of one or more aircraft. The apparatus comprises a first receiver configured to receive first aircraft position information, over a digital data link, from a first radio frequency source located onboard the aircraft at a first period, via one or more ground stations and a second receiver configured to receive second aircraft position information broadcasted from a second radio frequency source located onboard the aircraft at a second period, via one or more ground stations. The apparatus additionally comprises a third receiver configured to receive electronic geographical mapping data and a processor configured to receive the first and second aircraft position information, to filter the quantity of first and second aircraft position information to smooth the filtered information and then output the smoothed information such that it can be overlaid onto the electronic geographical mapping data.

Abstract: A computerised method is provided for monitoring the status of an aircraft. The method comprises sending, from an output module of an aircraft monitoring system, a reporting more report data signal response and monitoring, at an input module of the aircraft monitoring system, for received data signal to the aircraft monitoring system. This sets a contract with the aircraft that may be used to monitor for unexpected behaviour or non-compliance with the contract terms. The method further comprises determining, at a processor of the aircraft monitoring system, if one or more alert criteria have been satisfied by the received data signal responses and generating, at an alerting module of the aircraft monitoring system, an alert based on the determination.

Abstract: A container comprising a main body and a lid which define a chamber for a recipient product. A portion of the container is provided with a sensate substance which is released into the chamber to impart an organoleptic characteristic to a recipient product within said chamber.

Abstract: Pack (27) having a group of tobacco industry products wrapped in a laminate (2) to form a bundle (22). The pack has a base (28) containing the bundle, and a lid (30) mounted to the base for rotation between open and closed positions. The laminate has an outer layer (3) having a first cut (5) that defines an outer layer region bounded by said first cut and, an inner layer (4) having a second cut (6) that defines an inner layer region bounded by said second cut. A part of the outer layer region is attached to an inside surface of the lid such that, as the lid is rotated into its open position, the inner and outer layer regions are lifted causing the inner and outer layers to delaminate in a peripheral region (15) between the first and second cuts and an opening (19).

Abstract: Digital recording and replay system for an aircraft, comprising a Mission Computer with an Operational Flight Program for generating instrument data for onboard instruments of the aircraft; a Mission Data Recorder connected to said Mission Computer for recording said instrument data; and a Mission Debriefing System; wherein the Mission Debriefing System is configured to reproduce the onboard instruments of the aircraft based on instrument data retrieved from the Mission Data Recorder. Method for reproduction of onboard instrumentation of an aircraft, comprising the steps of connecting a Mission Data Recorder to a Mission Computer of an aircraft having an Operational Flight Program for generating instrument data for onboard instruments; recording instrument data; providing a Mission Debrief System and causing it to reproduce the onboard instruments of the aircraft based on instrument data retrieved from the Mission Data Recorder.

Abstract: An apparatus and computerised method are provided for monitoring the positions of one or more aircraft. The apparatus comprises a first receiver configured to receive first aircraft position information, over a digital data link, from a first radio frequency source located onboard the aircraft at a first period, via one or more ground stations and a second receiver configured to receive second aircraft position information broadcasted from a second radio frequency source located onboard the aircraft at a second period, via one or more ground stations. The apparatus additionally comprises a third receiver configured to receive electronic geographical mapping data and a processor configured to receive the first and second aircraft position information, to filter the quantity of first and second aircraft position information to smooth the filtered information and then output the smoothed information such that it can be overlaid onto the electronic geographical mapping data.

Abstract: A container for a consumable recipient product. The container also contains a non-consumable donor product carrier which contains a donor product which emits a substance to impart a characteristic to the recipient product in the container. The donor product carrier includes a barrier layer, disposed between the donor product and the recipient product, through which the substance can travel.

Abstract: A container for a recipient product. The container has a body and a lid which together define a first chamber when the lid is closed. The container has a substance carrier which emits a substance to impart a characteristic to a recipient product in the first chamber. The substance carrier has a seal to prevent emission of the substance from the substance carrier until the seal is opened.

Abstract: A container is disclosed which has a first chamber and a second chamber separated by a wall. The separating wall is configured so that at least one substance emitted by a donor product received in the second chamber is conveyed from the second chamber into the first chamber through said separating wall. In this way, a characteristic of the donor product is imparted to a recipient product in said first chamber.

Abstract: A container comprising a main body and a lid which define a chamber for a recipient product.

Abstract: The present invention provides pants, such as pants that are worn as work uniform pants, which are configured to provide significant improvements in a wearer's comfort, performance, and mobility over a predefined range of motions. Embodiments of the pants comprise one or more stretch panels that are configured to provide for stretching of the pant at an identified micro site in order to provide a wearer with enhanced mobility. Additionally, the manner in which the various portions of the pant are connected together may be adjusted in order to provide a wearer with enhanced mobility.

Abstract: Digital recording and replay system for an aircraft, comprising a Mission Computer with an Operational Flight Program for generating instrument data for onboard instruments of the aircraft; a Mission Data Recorder connected to said Mission Computer for recording said instrument data; and a Mission Debriefing System; wherein the Mission Debriefing System is configured to reproduce the onboard instruments of the aircraft based on instrument data retrieved from the Mission Data Recorder. Method for reproduction of onboard instrumentation of an aircraft, comprising the steps of connecting a Mission Data Recorder to a Mission Computer of an aircraft having an Operational Flight Program for generating instrument data for onboard instruments; recording instrument data; providing a Mission Debrief System and causing it to reproduce the onboard instruments of the aircraft based on instrument data retrieved from the Mission Data Recorder.

Abstract: A package (1) comprises a container enveloped in a wrapper (80) The wrapper (80) comprises a film (81) with overlapping portions which are sealed together. The wrapper (80) further comprises a tear strip (82) extending at least partially around the container and having an end tab. The wrapper is configured such that pulling the tab causes a tear to propagate through the film and the tear strip to come away from the container and the entire film to come away from the container attached to the tear strip. The tear strip (82) is defined by two reinforcing tear tapes (83a, 83b) on either side of the tear strip. Each tear tape (83a, 83b) has a respective first remote end (84a, 84b) at the tab, and the two tear tapes extend from the tab and diverge away from each other at least partially around the container such that the width of the tear strip enlarges around at least a part of the perimeter of the container.

Abstract: A wrapper (40) comprising a film (41) having a plurality of reinforcing tear strips (42a, 42b) extending at least partially across the film Each tear strip includes a tab portion (45a, 45b). The wrapper (40) is configured such that pulling the tab of a first tear strip causes a tear to propagate through the film (41) to separate a first portion of the film attached to the first tear strip, from the remainder of the film Pulling the tab of a second tear strip causes a second tear to propagate through the film to define a second portion of the film attached to the second tear strip. The second portion of film attached to the second tear strip comprises the remainder of the film once the first portion is removed with the first tear strip. Also, an apparatus and method for manufacturing such a wrapper.