Lockheed Martin Corporation

Stephen J Schober

David Luverne Vos

Ryan M Alderfer

Nicholas L Barnes

Michael John Malia

Brian M Fuller

Timothy J Marley

A deployment or hinge mechanism and, more particularly, a compact unmanned aerial vehicle (UAV) wing deployment mechanism is provided. The deployment mechanism includes a hinged mechanism that stows in a stacked configuration and deploys in a level configuration.

Deployment mechanism

Some embodiments relate to constructing a heat exchanger using nanoink as a thermal bond interface between portions of the heat exchanger. The heat exchanger may comprise fins and at least one base. A nanoink may be applied to at least a portion of the fins. The pieces of the heat exchanger may be sintered such that the nanoink melts and forms a bond between the pieces of the heat exchanger. Some embodiments include a second base. Some embodiments incorporate dissimilar materials within the heat exchanger construction.

Heat exchanger construction using low temperature sinter techniques

An air data system including a housing, a bore, a dynamic port, a static port, a gas permeable membrane, and a device configured to determine a pressure differential. The bore may be located within the housing and may extend from an inlet for receiving air flow to an outlet. The dynamic port may be located in the bore and be configured and positioned to receive air passing through the bore. The static port may be configured and positioned to receive unmoving or ambient air. The device may determine the pressure differential between dynamic air received at the dynamic port and static air received at the static port. And the membrane may span the dynamic port, the static port, or both and is configured to direct moisture away from the port which it spans.

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Ithica, NY, United States of America

Stephen J Schober