Abstract: A belly bar method and apparatus use to attach, carry and release external cargo from a hovering aircraft. The belly bar apparatus has articulated tubing tool connected to an airframe of the hovering aircraft at a first mounting end and at a second mounting end. The articulated tubing tool has a first external catch and a second external catch mounted on the articulated tubing tool. The first external catch is manually configured for optional attach, carry and release of the external cargo via the cyclic. The second external catch is electronically configured for optional attach, carry and release of the external cargo proximate the collective.

Abstract: A belly bar method and apparatus use to attach, carry and release external cargo from a hovering aircraft. The belly bar apparatus has articulated tubing tool connected to an airframe of the hovering aircraft at a first mounting end and at a second mounting end. The articulated tubing tool has a first external catch and a second external catch mounted on the articulated tubing tool. The first external catch is manually configured for optional attach, carry and release of the external cargo via the cyclic. The second external catch is electronically configured for optional attach, carry and release of the external cargo proximate the collective.

Abstract: An antenna includes a body support structure, an extruding mechanism to exert an extrusion force, an extrusion plate to inhibit motion of an extension plate, an extrusion support structure, a nadir panel including one or more communication patches; one or more petals including one or more additional communication patches, one or more extension arms, and an extension mechanism exert an extension force upon the extension plate. The relative position and orientation of the components are altered by the operation of the extension mechanism and the extension mechanism from a stowed state to an extruded state to an extended state. A control system may be included to initiate and control the state of the antenna as well as operate the communications of the antenna once deployed.

Abstract: A belly bar method and apparatus use to attach, carry and release external cargo from a hovering aircraft. The belly bar apparatus has articulated tubing tool connected to an airframe of the hovering aircraft at a first mounting end and at a second mounting end. The articulated tubing tool has a first external catch and a second external catch mounted on the articulated tubing tool. The first external catch is manually configured for optional attach, carry and release of the external cargo via the cyclic. The second external catch is electronically configured for optional attach, carry and release of the external cargo proximate the collective.

Abstract: An antenna includes a body support structure, an extruding mechanism to exert an extrusion force, an extrusion plate to inhibit motion of an extension plate, an extrusion support structure, a nadir panel including one or more communication patches; one or more petals including one or more additional communication patches, one or more extension arms, and an extension mechanism exert an extension force upon the extension plate. The relative position and orientation of the components are altered by the operation of the extension mechanism and the extension mechanism from a stowed state to an extruded state to an extended state. A control system may be included to initiate and control the state of the antenna as well as operate the communications of the antenna once deployed.

Abstract: A belly bar method and apparatus use to attach, carry and release external cargo from a hovering aircraft. The belly bar apparatus has articulated tubing tool connected to an airframe of the hovering aircraft at a first mounting end and at a second mounting end. The articulated tubing tool has a first external catch and a second external catch mounted on the articulated tubing tool. The first external catch is manually configured for optional attach, carry and release of the external cargo via the cyclic. The second external catch is electronically configured for optional attach, carry and release of the external cargo proximate the collective.

Abstract: A belly bar method and apparatus use to attach, carry and release external cargo from a hovering aircraft. The belly bar apparatus has articulated tubing tool connected to an airframe of the hovering aircraft at a first mounting end and at a second mounting end. The articulated tubing tool has a first external catch and a second external catch mounted on the articulated tubing tool. The first external catch is manually configured for optional attach, carry and release of the external cargo via the cyclic. The second external catch is electronically configured for optional attach, carry and release of the external cargo proximate the collective.

Abstract: A roller bearing assembly for a drawer slide providing a roller wheel having a threaded bore therethrough and a stud adjustably threaded into said bore, the stud attachable at an opposite end to either an interior wall channel of a cabinet or to a drawer, and said roller wheel rollable on a bracket provided on a respective other of said interior wall of the cabinet or the drawer. The lateral position of the roller wheel with respect to the cabinet or the drawer can be adjusted by selectively progressing the threaded stud into the threaded bore. The stud can be progressed into the bore by turning a hexagonal portion of the roller wheel surrounding the bore. The stud is typically anchored to the cabinet or drawer by insertion through an aperture and by deforming an end of the stud rivet style.