Abstract: An antenna system, in one example implementation, can include antenna portions including a first portion of the antenna to receive a radio frequency (RF) signal. The antenna can include a second portion capacitively coupled to the first portion, wherein the capacitive coupling of the second portion to the first portion increases the high-band resonances. The antenna can include a third portion of the antenna connected to a connector. The third portion can be capacitively coupled to the first portion to excite wide low-band resonances and high-band resonances. The connector can be a ground for the third portion.

Abstract: Example implementations relate to separate antennae.

Abstract: In some examples, an apparatus includes a housing to removably attach to an electronic device that includes first and second cameras spaced apart by a first distance. The apparatus includes a first light transmissive region of the housing to align with the first camera, the first light transmissive region to pass light from an environment to the first camera. The apparatus further includes a second light transmissive region of the housing spaced apart from the first light transmissive region by a second distance different from the first distance, and a light conduit to pass the light from the environment through the second light transmissive region to the second camera.

Abstract: An antenna and cap, in an example implementation, can include a system, comprising a computing device, a clearance region coupled to the computing device, and an antenna comprising a first antenna portion and a second antenna portion. The first antenna portion can be coupled to the computing device and to the clearance region, and the second antenna portion can be coupled to the clearance region. The system can include a first cap coupled to the second antenna portion via a first interconnection, and a second cap coupled to the second antenna portion via a second interconnection. The first cap and the second cap can be coupled to the computing device.

Abstract: Example implementations relate to a triband antenna. In one example, a triband antenna system as described herein can include a grounding system including a conductive housing of a wireless communication device and a ground slot structure. The triband antenna system may further include a triband antenna coupled to the grounding system, wherein the triband antenna includes a loop element coupled to the conductive housing, a feeding element, and a parasitic element located within a threshold distance of the feeding element.

Abstract: Examples described herein include examples of an antenna that includes a planar conductive body disposed in a first plane, a signal source, connection disposed on the planar conductive body, a direct feed antenna arm coupled to the signal source connection and disposed in a second plane parallel to the first plane, a coupled antenna arm disposed in the second plane and in proximity to a portion of the direct feed antenna arm, and a conductive interconnect element coupled to a region of the planar conductive body disposed in the first plane and the coupled antenna arm disposed in the second plane,

Abstract: A control device (34) for an aircraft wing (3) including upper and lower spoilers (35, 37) mountable to a wing (3) behind a leading edge slat (26), wherein each of the upper and lower spoilers (35, 37) are movable in a direction towards each other into a wing (3) from a neutral position, to an enabled position to form an airflow slot (52) between the slat (26) and said upper and lower spoilers (35, 37). Each of the upper and lower spoilers (35, 37) may also be movable in a direction away from each other out of a wing (3) from said neutral position.

Abstract: An aircraft (1) including a wing (5), the wing having an inner region (5a) and an outer region (5b), the inner and outer regions (5a, 5b) being connected by a hinge (11) defining a hinge line about which the outer region (5b) is foldable to reduce the span of the wing. The aircraft (1) includes an actuator (13) arranged to actuate the folding of the outer region (5b) of the wing with an actuation force. The wing (5) is braced by an external strut structure (9) for transferring some of the wing loadings in the outer region (5b) of the wing away from the inner region of the wing (5a). The actuator (13) is arranged to exert the actuation force via the strut structure (9).

Abstract: An aircraft wing includes a leading element; a trailing element positioned behind the leading element relative to a direction of movement of the aircraft and an actuation system for moving one of the elements between a retracted position and an extended position in which there is an air gap between a lower surface of the leading element and a surface of the trailing element. Two or more elongate stiffening ridges extend downwards from the lower surface of the leading element, and each adjacent pair of ridges is separated by a channel. The leading element is shaped to provide an improved air gap, preferably one which is parallel or convergent in all positions. Typically the volume of at least one of the ridges is less than the 50% of the volume of a channel defined by that ridge.

Abstract: A soil treatment apparatus (10) comprises an endless band (12) of resilient material with soil treatment teeth (14) projecting radially therefrom. The teeth are replacably attached to the band (12).

Abstract: An aircraft wing comprising a leading element and a trailing element moveably coupled together, said elements being positionable relative to each other so that air can flow from the underside of the leading element over the top of the trailing element through a gap between the leading element and the trailing element, wherein a trailing edge of the leading element proximate to the trailing element is configured to disrupt air flow as it flows over said trailing edge and through the gap.

Abstract: Various embodiments of an internal multi-band antenna architecture for a mobile computing device are described. An internal antenna architecture for a mobile computing device may include multiple antenna elements, including a first internal antenna element configured to operate in a downlink frequency sub-band of at least one frequency band for communication in a first mode, and a second internal antenna element configured to operate in an uplink frequency sub-band of the at least one frequency band for communication in the first mode. Other embodiments are described and claimed.

Abstract: A container for receiving a food product is formed from a shaped blank of paper, paperboard, cardboard or a similar material. A hinge arrangement comprising at least two and preferably three parts is provided between one of the side walls and one of the end walls to allow the partially formed container to be moved easily between a flat configuration suitable for transportation or storage and an erect configuration for receiving a food product. In the erect configuration one part of the hinge arrangement is sandwiched between another part of hinge arrangement and the end wail. In the flat configuration these two parts of the hinge arrangement lie in substantially the same plane. An integral lid may be provided.

Abstract: A container for receiving a food product is formed from a shaped blank of paper, paperboard, cardboard or a similar material. A hinge arrangement comprising at least two and preferably three parts is provided between one of the side walls and one of the end walls to allow the partially formed container to be moved easily between a flat configuration suitable for transportation or storage and an erect configuration for receiving a food product. In the erect configuration one part of the hinge arrangement is sandwiched between another part of hinge arrangement and the end wail. In the flat configuration these two parts of the hinge arrangement lie in substantially the same plane. An integral lid may be provided.

Abstract: Various embodiments of an internal multi-band antenna architecture for a mobile computing device are described. An internal antenna architecture for a mobile computing device may include multiple antenna elements, including a first internal antenna element configured to operate in a downlink frequency sub-band of at least one frequency band for communication in a first mode, and a second internal antenna element configured to operate in an uplink frequency sub-band of the at least one frequency band for communication in the first mode. Other embodiments are described and claimed.

Abstract: Methods and Systems of detecting and reporting fraud in real-time are described. The system receives an event, over a network, from a first on-line transaction processing platform. The event includes a first identity identifier that identifies a first identity and information that identifies a first activity performed by the first identity. The system generates reporting information based on the event. The reporting information includes a first score that is associated with the first identity. The first score is a measure of a likelihood that the first identity has performed a fraudulent activity. Finally, the system communicates the first score, over the network, to the first on-line transaction processing platform. The system communicates the first score in response to receiving the event.

Abstract: A soil treatment apparatus (10) comprises an endless band (12) of resilient material with soil treatment teeth (14) projecting radially therefrom. The teeth are replacably attached to the band (12).

Abstract: A container for receiving a food product is formed from a shaped blank of paper, paperboard, cardboard or a similar material. A hinge arrangement comprising at least two and preferably three parts is provided between one of the side walls and one of the end walls to allow the partially formed container to be moved easily between a flat configuration suitable for transportation or storage and an erect configuration for receiving a food product. In the erect configuration one part of the hinge arrangement is sandwiched between another part of hinge arrangement and the end wail. In the flat configuration these two parts of the hinge arrangement lie in substantially the same plane. An integral lid may be provided.

Abstract: An aircraft wing comprising a leading element and a trailing element moveably coupled together, said elements being positionable relative to each other so that air can flow from the underside of the leading element over the top of the trailing element through a gap between the leading element and the trailing element, wherein a trailing edge of the leading element proximate to the trailing element is configured to disrupt air flow as it flows over said trailing edge and through the gap.

Abstract: An aircraft wing comprising: a leading element; a trailing element positioned behind the leading element relative to a direction of movement of the aircraft; an actuation system for moving one of the elements between a retracted position and an extended position in which there is an air gap between a lower surface of the leading element and a surface of the trailing element. Two or more elongate stiffening ridges extend downwards from the lower surface of the leading element, and each adjacent pair of ridges is separated by a channel. The leading element is shaped to provide an improved air gap, preferably one which is parallel or convergent in all positions.