Fortem Technologies, Inc.

Legrand North America, LLC

Jon Erik Knabenschuh

Justin Craig Huntington

David Earl James

Matthew Robertson Morin

James David Mackie

Chester Parker Ferry

Kendall James Fowkes

Nathan J Packard

Matthew Elliott Argyle

Adam Eugene Robertson

Bryan Alan Davis

Devin Donald Lebaron

Daniel Glen Bezzant

Lyman Davies Horne

Tyler Drue Park

Eric James Fowkes

James Beagley

Douglas E Allen

Brandon Robert Hicks

Jared Lemke

Scott Chandler

Michael Whatcott

James Harrison Hofer, Jr

Systems, methods, and computer-readable media are described for compact radar systems. In some examples, a compact radar system can include a first set of transmit antennas, a second set of receive antennas, one or more processors, and at least one computer-readable storage medium storing computer-executable instructions which, when executed by the one or more processors, cause the radar system to coordinate digital beam steering of the first set of transmit antennas and the second set of receive antennas, and coordinate digital beam forming with one or more of the second set of receive antennas to detect one or more objects within a distance of the radar system.

Compact radar system

A radar system is generated by a process including generating a first substrate layer adjacent to a ground plane of a patch antenna array in the radar system, etching an opening in the substrate layer, inserting a mechanically-locking foot of a threaded insert into the opening, adding a second substrate layer adjacent to the first substrate layer to embed the threaded insert, applying a thermal coupling between a heat sink layer and the second substrate layer of the radar system and screwing a screw through the heat sink layer and into the threaded insert to adhere the heat sink layer to the radar system. Such a radar system can enable the attachment of the heat sink layer to the radar system in a removable fashion such that the heat sink layer can be removed by removing the screw and repairs can be done without damaging respective layers.

System and method for managing heat dissipation in an antenna array

A projectile module is attached to a gun component which operates as a system to launch a projectile at a flying device. The gun component is configured to be removably and electro-mechanically attached to a flying vehicle. A cylindrical gas valve is part of the gun component and has a safety component configured on an exterior surface of the cylindrical gas valve to enable the gun component only to attach to the flying vehicle when the projectile module is locked into position. A splitter component configured on the gun component adjacent to the cylindrical gas valve and has an output opening for gas flow. The projectile module is removable and includes weights attached to a projectile, wherein the weights are positioned in channels on the projectile module. The projectile is fired when gas flow is initiated from a reservoir the cylindrical gas valve and splitter component to the channels containing the weights.

Detachable projectile module system for operation with a flying vehicle

The present disclosure provides improved dimming or dimmer assemblies/modules for controlling lights or loads (e.g., as part of a control or automation system). More particularly, the present disclosure provides for systems and methods for utilizing dimmer control assemblies/modules advantageously having: (i) an adjustable output response, (ii) enhanced thermal management, (iii) a voltage detector to determine amplitude and zero-crossing, and/or (iv) an estimation of power consumption for multiple loads (e.g., using a single sensor).

Dimming control including an adjustable output response

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Orem, UT, United States of America

Jon Erik Knabenschuh