Lockheed Martin Corporation

Greg W Klein

Corey Adam Fleischer

Tushar K Shah

Mahendra Maheshwari

David Conrad Briggs

Buddy R Paul

Matthew M Kapelanczyk

Michael W Poppek

Adam M Knabe

George Gregory Miller

A UAV capture system including a cable array comprising at least two laterally-spaced cables carried by a first cable support structure. Catches disposed on respective port and starboard wings of a UAV are positioned to engage the cables when the UAV flies into them. A payout device pays out the engaged cables after they have been engaged by the UAV and a brake decelerates the UAV by resisting the pay out of the cables.

UAV capture system

A crew transfer system for transferring personnel from a vessel to a stationary platform, such as an oil rig, is disclosed. In the illustrative embodiment, the system includes a ramp that is coupled to the vessel and an interface that is attached to the stationary platform. The ramp is coupled to the vessel in such a way as to permit one translational and three rotational degrees of freedom at the vessel-end of the ramp. The ramp is coupled to the interface in such a way as to permit no translational and at least one rotational degree-of-freedom at the rig-end of the ramp with respect to the interface. The interface is rotatably coupled to the stationary platform in such a way as to permit a rotation of the interface about the yaw axis. Permitted rotation of the interface enables a range of acceptable angles of orientation between the vessel and the platform.

Rotating gangway support platform

An armor that is used, for example, in multi-cell missile launchers is disclosed. In some embodiments, the armor includes three layers. The inner-most layer undergoes explosive welding when exposed to a pressure wave from an explosion. An intermediate layer in-elastically deforms when exposed to the explosion. The third and outer-most layer includes a plurality of elongated, pressurized tubes that contain fire retardant, among other chemicals. Silicone gel is interposed between the tubes.

Apparatus comprising armor

An electrical connector that avoids some of the disadvantages associated with electrical connectors in the prior art. In particular, the illustrative embodiment of the present invention uses spring-loaded contacts to maintain connection in the presence of the vibration associated with a rocket launch, and also includes an environmental seal and electro-magnetic shield so as to provide an environment for the electrical contacts that is isolated from the ambient environment and external electromagnetic radiation. Furthermore, the illustrative embodiment avoids the possibility of bent connector pins, which would make mating between the electrical connectors.

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Bel Air, MD, United States of America

Greg W Klein