Abstract: Motor housings and shrouds are detailed. Inlets of the shrouds may be included on any or all portions of their peripheries (as well as on rears of shrouds if desired). Air hence need not necessarily be drawn wholly linearly into the shrouds, permitting the shrouds to abut, or at least be closely proximate, other objects without materially diminishing air flow into the shrouds. Moreover, plates within the shrouds may be positioned so as to create torturous paths through which the air must travel. Channeling air through these torturous paths helps reduce noise as the air moves to the fans.

Abstract: An engine, a rotary device, a power generation system, and methods of manufacturing and using the same are disclosed. The engine includes a detonation and/or combustion chamber configured to detonate a fuel and rotate around a central rotary shaft extending from the detonation and/or combustion chamber, a fuel supply inlet configured to provide the fuel to the detonation and/or combustion chamber, at least two rotating arms extending radially from the detonation and/or combustion chamber and configured to exhaust detonation gases from detonating the fuel in the detonation and/or combustion chamber and provide a rotational thrust and/or force, the rotating arms having inner and outer walls and a nozzle at a distal end thereof, the nozzle being at or having an angle configured to provide the rotational thrust and/or force, and a plurality of cooling coils between the inner and outer walls. Alternatively, the rotary device may include a rotary disc.

Abstract: A centrifugal compressor assembly for compressing refrigerant in a 250-ton capacity or larger chiller system comprising a motor, preferably a compact, high energy density motor or permanent magnet motor, for driving a shaft at a range of sustained operating speeds under the control of a variable speed drive. Another embodiment of the centrifugal compressor assembly comprises a mixed flow impeller and a vaneless diffuser sized such that a final stage compressor operates with an optimal specific speed range for targeted combinations of head and capacity, while a non-final stage compressor operates above the optimum specific speed of the final stage compressor.

Abstract: A device for supplying electrical energy to a load. A supporting element made of electrically insulating material is provided, which has at least one electrical strip conductor formed from an electrically conductive layer. At least one electrically conductive contact face per strip conductor is provided on the source side, via which the strip conductor is contactable with the voltage source. A flat plug that includes the load-side ends of the strip conductors is provided on the supporting element and effects the electrical connection to the load. A system for electrification of an electrical load on a furniture item is provided. At least one device, a support and at least one vertical profile are provided. The device is mounted on the support and the strip conductors of the support are electrified by inserting the support into the profile. For that purpose, the profile has at least one vertically arranged conductor rail.

Abstract: A microgenerator for use in petroleum distribution systems includes a casing defining an interior portion and an exterior portion. The casing has an opposed first support wall and second support wall coupled within an inner diameter of a cylinder containment wall. At least one fluid inlet penetrates the cylinder containment wall. The fluid inlet is fluidly coupled to an energized fluid source. At least one nozzle is fluidly coupled to the fluid inlet. The nozzle is configured to accelerate the fluid into the interior portion. At least one fluid outlet penetrates the cylinder containment wall. The fluid outlet is configured to discharge the fluid from said interior portion of the casing. An impulse turbine is located within the interior portion. The turbine has a first stator coupled to the first support wall and a second stator coupled to the second support wall opposite the first stator. A rotor is rotatably mounted between the first stator and the second stator on a shaft at a central axis of the rotor.

Abstract: A fluidic torque transfer device is configured such that the attachment angle of a turbine blade at a fluid outlet of a turbine runner is smaller than the attachment angle of the turbine blade at a fluid inlet of the turbine runner. Furthermore, the turbine runner is structured so that a cross-sectional area St of a turbine flow path defined by the turbine shell, adjacent turbine blades, and the turbine core, which is perpendicular to a centerline of the turbine flow path, satisfies |St?Sref|/Sref?0.2, where a reference area Sref is an average of maximum and minimum values of a cross-sectional area of a pump flow path defined by the pump shell, adjacent pump blades, and the pump core of the pump impeller, which is perpendicular to a centerline of the pump flow path.

Abstract: A fluidic torque transfer device configured with a pump impeller that includes a pump shell, a pump blade attached to the pump shell, and a pump core attached to the pump blade; a turbine runner that includes a turbine shell, a turbine blade attached to the turbine shell, and a turbine core attached to the turbine blade; and a stator that includes a stator blade, and rectifies a flow of a hydraulic fluid from the turbine runner to the pump impeller. The outer contour line of the turbine blade extends outward in an extending direction of a rotation center axis of the pump impeller and the turbine runner on the fluid outlet side of the turbine runner more than an outer contour line of the pump blade on the pump shell side.

Abstract: A fastening arrangement of a pipe is provided. The fastening arrangement is coaxial to a longitudinal axis, on a shaft step, which is rotatably mounted around the longitudinal axis, for connecting of the two component parts, with a coaxial circumferential surface located on the shaft step, upon which circumferential surface at least partially lies the inner side of the pipe end which faces the shaft step. In order to disclose the creation of a fastening arrangement which is especially simple and inexpensive to manufacture and also free of wear during operation, it is proposed that the pipe end has notches distributed over the circumference, and an encompassing annular slot on the inner side of the pipe in the region of the notches, with a sleeve which is installed in the annular slot, covers the notches, and at least partially lies on the circumferential surface of the shaft step.

Abstract: A fan with supercharging device has a hub and fan blades. A hub has a shape similar to a cone with a tip end and a circumferential side. The fan blades extend radially from the circumferential side of the hub. Each of the fan blades has a joining end being attached to the circumferential side, a free end extending outward the hub and a front edge and a rear edge being between the joining end and the free end respectively. The rear edge of the respective fan blade is shielded by the front edge of another fan blade next to it. The unshielded portion of the respective fan blade has an area gradually increases from the joining end to the free end. A projection is disposed at the free end along a direction of fluid flow. Hence, fluid pressure is capable of increasing significantly while the fan is in operation.

Abstract: A hydrocarbon well pump has impellers and diffusers configured with inner and outer sections. The central section contains impeller passages configured for pumping liquid. The outer section contains turbine blades for compressing gas. A cylindrical sidewall separates the two sections. A driven shaft rotates the central and outer sections in unison.

Abstract: A stator blade for a hydrokinetic torque converter, the blade profile having geometric characteristics that improve torque flow efficiency in the converter torque flow circuit, whereby the torque converter efficiency at high speed ratios is improved without significant adverse effects on the converter torque ratio at stall and at low speed ratios.

Abstract: A multi-blade centrifugal fan, the fan arranged with a plurality of blades in round shape and equipped with an end plate mounted with a tip end of the plurality of blades, wherein the end plate is centrally mounted with protruded hub toward an air intake, and here a protruded height (Hb) of the hub is less than 0.3 times the outer diameter (Df), such that although a hub is mounted with a driving motor, an overall structural size is miniaturized to minimize a flow rate loss and to prevent a remarkable fan performance decrease.

Abstract: A stator for a hydrodynamic torque converter which is produced by injection molding with axially drawn dies. The stator hub has stator blades produced by use of a thermoplastic material to fill the dies in the injection molding process. The stator blades are positioned relative to one another on the stator hub in such a way that the flow outlet of every stator blade is arranged at an offset of only the width of a gap relative to the flow inlet of the subsequent stator blade in the circumferential direction.

Abstract: A centrifugal fan including a fan hub lying generally in a plane normal to the axis of fan rotation and having a central opening for receiving a motor housing, and a plurality of fan blades of substantially identical construction spaced circumferentially evenly around the fan hub and extending away from the fan hub in a direction parallel to the axis of fan rotation. Each fan blade includes a leading edge at its innermost radial periphery, and the leading edge, at least at the axially upper one-half section thereof, is convexly curved in the shape of a quarter ellipse having a major axis, Mg, substantially parallel to the axis of fan rotation and a minor axis, mh, normal to the major axis Mg. The fan also includes a continuous shroud joined to each fan blade at an axially upper section of the radially outer portion thereof and the shroud is concave in cross-section.

Abstract: A vacuum pump assembly which comprises at least two cylinders of different diameters and arranged coaxially relative to each other to define an annular space therebetween and a helical member positioned within the space to define a helical path between the cylinders. Rotation of the cylinders is effected relative to the helical member, or vice versa, about their longitudinal axis.

Abstract: Disclosed is a centrifugal liquid pump, preferably of the rotary disc type, which incorporates a gas injection assembly of very simple yet efficient structure, whereby up to 15% per volume of a gas such as air, may be mixed with the pumped liquid. The gas injection is achieved with a gas feed pipe that enters the pump through its axial inlet and with a plurality of gas injector pipes that projects from the gas feed pipe radially within the impeller.

Abstract: A multiple stage centrifugal compressor has baffle rings attached at the inlet to each of the impellers, between a shroud side curvature and a hub side curvature. The dimensions and spacings of the baffle rings are selected as a function of the shroud side radius of curvature R.sub.S and the hub side radius of curvature R.sub.H. For two baffle rings, the radii areR.sub.C1 =(R.sub.c.sup.2 .times.R.sub.H).sup.1/3 and R.sub.C2 =(R.sub.S .times.R.sub.H.sup.2).sup.1/3.

Abstract: An internal combustion engine according to the present invention is comprised of a conduit means that directs the flow of exhaust from an internal combustion engine to a relatively low speed turbine connected to a generator. The conduit means also acts as a mixing means for mixing appreciable quantities of outside air with the exhaust for recombustion prior to entry into the turbine. The turbine is designed to utilize the energy of the recombusted gases through impact and redirection of the gases upon the turbine blades. This invention comprises a dual function conduit means connecting internal combustion engine exhaust to a relatively low speed turbine wherein the conduit means also induces an appreciable flow of outside air to mix with the exhaust gases to effectively lower the temperature of the gases imposed on the turbine but without lowering the total energy of the gases.

Abstract: A centrifugal turbine rotor is rotated by fluid from a distributor provided with fluid channels which are continuously convergent in the direction of flow. These fluid channels are also deviated with respect to the radial direction of the distributor. The centrifugally directed fluid is transmitted from the distributor through an obturator which adjusts the size of the distributor channel outlets, and across an open space where the fluid is aerated before it strikes the rotor buckets to rotate the rotor.

Abstract: A containment system for a radial flow turbine assembly includes a housing assembly, and a turbine rotor journalled for rotation about an axis and having a hub portion and a generally tapering disc portion extending radially outward from the hub portion. An annular nozzle assembly normally secured in the housing assembly against rotation forms a tapered rotor chamber within which the rotor rotates with minimum axial and radial clearance between the rotor and the chamber. A plurality of support struts extend axially inward from the nozzle assembly to a minimal axial and radial clearance with the hub portion of the rotor and forms a first stage of containment. The rotor must first break through the nozzle struts and separate the nozzle assembly. A rotatable nozzle assembly then absorbs some of the force by rotating in the housing assembly and containment ring. An armored containment ring stops the fragments that escape the nozzle assembly and finally, an outer housing provides still further containment.

Abstract: An improved cutter pump subassembly for use in a centrifugal pump adapted for chopping and pumping an influent liquid containing solids is disclosed. In such a cutter pump, a suction inlet, discharge outlet, means for driving an impeller and a cutter pump subassembly are provided. The improved cutter pump subassembly comprises a housing, an impeller and a stationary cutter. The housing defines a pump chamber and contains the impeller. The housing also contains a centrally located suction aperture that receives the influent liquid and a spiral channel that conducts the liquid out of the housing. The impeller has a shroud and impeller vanes and is rotatably driven by the means for driving an impeller. The impeller vanes each have an outer circumferential end and an inner shearing edge. The stationary cutter is secured adjacent the suction aperture. The cutter has teeth each having at least one blade.

Abstract: A rotary gas/liquid separator includes a housing having a free running rotor mounted to rotate about a vertical axis in the housing. The rotor has an inverted conical inside surface, and a plurality of turbine blades adjacent an upper end of the conical inside surface. A gas/liquid inlet mixture is forced under pressure through stator vanes for directing flow of the inlet mixture tangentially into the turbine blades for rotating the rotor. The turbine blades divert the inlet mixture radially outwardly and then axially downwardly toward the conical inside surface of the rotor, and centrifugal force exerted on the inlet mixture by the rotating turbine blades separates liquid from the gas in the inlet mixture. The separated liquid flows downwardly in a thin film along the inside surface of the rotor and drips from a free lip at the bottom of the rotor for collection. A plurality of fan blades on the rotor discharge separated gas from a first chamber below the rotor to a second chamber above the rotor.