Fortem Technologies, Inc.

Spectrum Aeronautical, LLC

Kendall James Fowkes

Jon Erik Knabenschuh

David Earl James

Devin Donald Lebaron

Justin Craig Huntington

Eric James Fowkes

Larry Jed Ashton

Matthew Robertson Morin

James David Mackie

Michael G Allman

Chester Parker Ferry

Brandon Robert Hicks

James Harrison Hofer, Jr

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

A cabin door assembly is provided for use with a pressurized aircraft. The assembly includes two door halves for engaging the fuselage of the aircraft. Structurally, each door half includes a waist section integral with an adjoining tapered section. Further, the assembly includes an activator that is mounted on the fuselage and attached to the door halves. Specifically, the activator is attached to each door half to concertedly move each door half between a closed configuration and an open configuration. In the closed configuration, the door halves are sealed to the fuselage and to each other for pressurization of the aircraft. In the open configuration, the door halves extend outwardly from the fuselage to allow for aircraft ingress and egress.

Aircraft door

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Provo, UT, United States of America

Kendall James Fowkes