Abstract: A method for analyzing solid material in a liquid sample comprises the steps of: distributing the sample equally by passage through a number of discrete wells adapted to retain the solid material, the concentration of solid material being such that it is absent in at least one well; and analyzing the wells for the presence of retained solid material. A device adapted for use in a method for analyzing solid material in a liquid sample comprises the combination of: a container for the sample; a unit comprising a number of discrete wells adapted to retain the solid material and allow the passage of liquid under the application of reduced pressure; structure for drawing liquid from the container and through the wells under reduced pressure; and a manifold or other element that provides uniform distribution of the sample passing from the container into the wells.

Abstract: A duct cover for use with a duct within a vehicle, the duct cover operative for directing a fluid flow. The duct cover being further operative for minimizing the entrance of foreign object debris into the duct. The duct cover has a flow directing honeycomb portion for conducting the passing fluid flow in a preferred direction. The flow directing honeycomb comprises an array of continuous, polygon shaped open cells which are biased with respect to the initial fluid flow direction. The periphery of the flow directing honeycomb is rigidized to stiffen the same for minimizing the displacements thereof. The rigidity is provided by a framing member comprising upper and lower skin structures affixed to a core material. The framing member is preferably adhesively bonded to the flow directing honeycomb by means of a foaming adhesive and a barrier member. The barrier member is operative for minimizing the expansion of the foaming adhesive into the open cells of the honeycomb.

Abstract: A fairing 122 is provided for covering a wire strike cutter 120. The fairing 122 comprises a microwave energy absorbing core 150 covered by dielectric skin 160,161,165,166. The fairing 122 reduces the radar signature of the wire cutter and fractures in response to a wire strike so as to permit the cutter to capture and cut a wire/cable. At least one projection 135 is formed on the fairing 122 for catching a slack wire/cable as it slides up the fairing, the projection holds the wire/cable until tension develops to fracture the fairing, thereby permitting the wire/cable to pass through to the wire cutter where it is subsequently cut. The fairing 122 minimizes drag and improves the aircraft's aerodynamic characteristics by directing the airflow around the wire cutter and equipment adjacent to the wire cutter.

Abstract: A support truss for the main rotor assembly of a helicopter is configured to structurally support the main rotor assembly in integrated combination with the helicopter airframe and to transmit dynamic and static longitudinal, lateral, vertical, and torsional loads of the main rotor assembly into the helicopter airframe at two distinct, spaced-apart load transfer levels.