Abstract: A condenser/evaporator heat exchanger comprising a plurality of vertically oriented panel units spaced moderately from one another. Each panel unit comprises a pair of thin film plastic sheets bonded to one another along a plurality of vertically extending bond lines transversely spaced from one another at regular intervals. The two sheets form between adjacent pairs of bond lines a plurality of vertical tubular condensing chambers adapted to receive pressurized steam. Brine is directed onto the outer surfaces of the panel units at the upper ends thereof, the brine descending down the outer surfaces of the panel units to be in heat exchange relationship with the steam inside the tubular condensing chambers.

Abstract: A ruddevator assembly for controlling movement of an aircraft refueling boom, comprising two ruddevators mounted to the boom, each at a dihedral angle of about 42.degree.. Each ruddevator has an outboard section, which is an advanced technology cambered airfoil for high lift at transonic speeds, with a raked wing tip. The inboard portion of the airfoil has a forwardly extending strake-like member having a sharp leading edge which in planform comprises three sections. There is a curved forward edge section and two rearwardly extending edge sections, which in operation are positioned at high sweep angles. The side edge portions of the strake-like member create vortices which travel over the inboard portion of the ruddevator to augment lift over a wide range of surface deflection of the ruddevator (i.e., angle of attack).

Abstract: An engine particularly adapted to travel at high supersonic and hypersonic velocities. The engine has a forward turbine positioned at the engine inlet and a rearwardly positioned compressor driven by the turbine through an interconnecting longitudinal shaft. In a first embodiment, a cryogenic fuel, such as hydrogen, is introduced into the engine at a location between the turbine and the compressor, with vaporization and heating of the fuel causing a reduction in the compressor inlet temperature and a consequent increase in compressor discharge for a given turbine power shaft input. The resulting fuel/air mixture passes through the compressor and then into a rearwardly positioned combustion chamber where it is ignited, with the combustion products then being expanded from the compressor discharge pressure to atmospheric pressure through an outlet nozzle as jet exhaust.

Abstract: A process for preparing an improved asphalt mixture by adding coal materials thereto. Low carbon content coal materials are separated into first and second portions, the first portion being soft-burned at approximately 600.degree. F., and the second portion being exposed to a number of wetting and drying cycles, followed by a thorough leaching. The first and second portions are crushed and screened to produce a fine particulate coal material having a maximum diameter passing through a 200 mesh screen, and a larger size coal material having a maximum diameter of 3/4 of an inch. In a first embodiment, an asphalt paving material is produced by adding the fine particulate coal materials to an asphalt/aggregate mixture in a proportion of approximately 75% of the first portion and approximately 25% of the second portion of the fine particulate coal materials, such that the coal materials equal approximately 6 to 8% by weight of the total mixture. The resulting asphalt mixture is heated at approximately 300.degree.

Abstract: A sound reproducing system having right and left speakers which transmit right and left stereo sounds, respectively. The right signal, in addition to driving the right speaker, is inverted and delayed to produce a compensating signal which is transmitted to the left speaker to produce a delayed compensating sound pattern from the left speaker. The amount of delay and amplitude of the compensating sound pattern is selected so that the major sound pattern emanating from the right speaker is at least partially cancelled at the location of the hearer's left ear. The signal for the left speaker is inverted and delayed in a similar manner to produce a compensating sound pattern from the right speaker to at least partially cancel the major sound pattern emanating from the left speaker at the location of the hearer's right ear. The result is to give the hearer a greater dimensionalized impression of the overall sound patterns.

Abstract: Water at a very high pressure (e.g. fifty thousand psi) is directed through a nozzle orifice to produce a coherent high velocity water jet particularly adapted for cutting. Prior to pressurizing the water and directing it through the nozzle, the water is treated to remove dissolved solids, desirably to an extremely low level to provide very pure water (e.g. where the total dissolved solids are as little as ten parts per million or lower). This is done by directing the water through several ion exchange reactions to precipitate the solids which are then removed by filtering. The operating life of the nozzle is greatly extended by this process.

Abstract: A heat exchange apparatus comprising a plurality of vertically aligned modular panel units, positioned adjacent to one another in a closed housing. Each panel unit comprises a perimeter frame and a plurality of vertical spacing elements. Two sheets of thin film plastic are placed on opposite sides of each panel unit and define with the spacing units vertical passageways within the panel unit. An evaporating liquid heat exchange medium, such as brine, is directed into the upper ends of the passageways against the inside surfaces of the sheets to form a falling liquid film. A gaseous condensing heat exchange medium, such as steam, is directed into the areas between adjacent panels to cause condensation in the form of water on the outside surface of the thin film sheets.

Abstract: A main engine support structure having a rear portion hinge-mounted at two laterally spaced locations to a leading edge of a wing in a manner to permit limited up and down swing movement of the engine relative to the wing. A generally vertically aligned forward support link connects a forward inboard side portion of the engine support structure to the airplane fuselage, thus providing vertical support for the engine at its forward end. At the rear of the support structure there is a laterally extending link, connecting the support structure to the wing and resisting lateral loads exerted on the engine. This mounting system reliably mounts the engine to the wing, does not interfere with the wing's ability to flex upwardly and downwardly, and properly transmits the loads from the engine into the aircraft structure.