United Technologies Corporation

Sikorsky Aircraft Corporation

Larry J Osiecki

Thomas Arthur Carstensen

William V Forster

Kenneth M Nowak

William J Hall

Joseph M Carlos

Darryl Mark Toni

Peter L Grant

Steven R Hayse

Craig F Johnson

Method for making honeycomb core composite articles

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. In order to improve the low observability characteristics of the structure, the cells of the flow directing honeycomb are preferably coated with a radar absorbent material, such as carbon, which acts to minimize the amount of electromagnetic energy that is reflected therefrom.

Duct cover for directing a fluid therethrough

A simulator dome for a motion base simulator comprises one or more fiber reinforced outer layers, inner layers of a similar material and an intermediate core. The intermediate core is preferably a structural foam of variable density to allow selectively lowering the dome center of gravity to enhance the simulation capabilities of the motion system to simulate various flight maneuvers. By producing the dome from fiber reinforced polymer and using a core of variable density, a dome of unitary construction with no through fasteners is produced, having high strength for withstanding high G maneuvers without cracking or distortion, enhancing simulator effectiveness and increasing the accuracy of the simulated flight conditions.

Method of making a composite sphere for a motion base simulator with a

Composite sphere for a motion base simulator

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Oxford, CT, United States of America

Larry J Osiecki