Abstract: A jet pump for a system for supplying fluid to a turbomachine. The jet pump includes an active fluid inlet pipe including a tube delimiting the inlet pipe, and a passive fluid inlet pipe that is fluidically separated from the active fluid inlet pipe by the tube. The active fluid inlet pipe includes at least one twisted blade that is positioned within the tube and is configured to make the active fluid rotate with respect to the axis of the tube.

Abstract: Nozzles mix coolant from different sources together in an outlet to prevent differences in coolant output. Different flow path configurations are useable in the nozzle, including a multiple-path configuration with flows from different sources jacketed or concentrically arranged around flows from other sources. Swirl vanes may be installed in the nozzle to impart mixing or filtering the fluid flow. Diffusers may be used to passively suction or accelerate flow and mixing the same like a jet pump. Nozzles can be combined with filtration systems like trap filters that capture debris based on a momentum difference between the denser debris and fluid. Filters can use magnetic, adhesive, or porous materials to capture debris without blocking a flow path. Filters can be disengaged, such as when clogged, such that coolant flows around the system. Nozzles can be installed on feedwater sparger assemblies in varying manner to distribute coolant from multiple nozzles.

Abstract: A fuel pump module for a fuel tank having a plurality of fuel tank rooms includes a jet pump with a jet part, a suction part, and a swirling flow formation member that has relatively-small openings that are symmetrically disposed on a center axis of the jet part on one side of the member close to the suction part. The fuel passing through the openings are induced into a swirling flow that is injected into the suction part for transporting the fuel from one tank to an other tank. As a result, fuel may be efficiently transported from the one tank to the other tank without having a fuel pump in the one tank.

Abstract: A jet pump unit, including: a nozzle housing having a vacuum chamber formed therein and connected with a recirculation line; a jet nozzle in which a front end is placed in the vacuum chamber of the nozzle housing, a nozzle aperture injecting fluid to the outside is formed on the front end, a slanted surface is formed on an exterior with an outer diameter gradually decreasing toward the nozzle aperture, and a concave notch is concave toward a rear end of the nozzle aperture; and a mixture pipe in which the fluid injected from the nozzle aperture of the jet nozzle and recirculation fluid that is sucked into the vacuum chamber are mixed.

Abstract: A nozzle of an ejector depressurizes and injects fluid, which is supplied to the nozzle. The nozzle is received in a receiving space of a body. The nozzle and the body are formed by press working. The nozzle includes nozzle-side ribs, which extend in an axial direction and project radially outward. The body includes body-side ribs, which extend in the axial direction and project radially outward. In a predetermined cross section of each of the nozzle and the body, which is perpendicular to the axial direction and includes the corresponding ribs, the nozzle or the body is formed seamlessly as a continuous single piece member.

Abstract: A nozzle for use with a diffuser has a body with a fluid passageway extending through an interior thereof and having a fluid inlet and a fluid outlet. The body has an end surface formed at the fluid outlet. The body has an orifice formed through the end surface so as to communicate with the fluid passageway. The orifice has a first elliptical portion and a second elliptical portion. The elliptical portions are conjoined so as to communicate therebetween. The elliptical portions have major axes of equal length and minor axes of equal length. The nozzle is placed toward a mixing chamber of a jet pump.

Abstract: A vacuum pump ejector may include ejector body and a nozzle. The ejector body may have a passageway through which fluids may flow. The passageway may have an orifice. The nozzle may inject a purging gas to the orifice. The ejector may decrease a pressure between the vacuum pump and the scrubber, so that the vacuum pump may have improved efficiency. Thus, the vacuum pump may be effectively operated.

Abstract: In known devices for pumping fuel, suction jet pumps are used which are driven by the fuel flowing back from the internal combustion engine and pump fuel from a supply tank into an impoundment container of a fuel pumping unit. In known suction jet pumps, the suction power is limited by the fact that the fuel stream applies itself to the housing wall, so that the entire area of the fuel stream is no longer available for entraining fuel. The device of the invention lessens this effect by providing at least one rib between the first partial section of the fuel line and the mixing conduit.

Abstract: An apparatus for generating electric power from water currents comprises a housing having at least one pair of channel, at least one pair of turbine assemblies and at least one pair of generator assemblies. Each channel of the pair has an axial intake, an axial discharge opening and a side intake. Each side intake extends along a length of the channel and faces in an upstream direction to receive a side inflow of water and directs the side inflow up against an interior surface of the channel to create a vortical flow structure having a low pressure core. The vortical flow structures are produced downstream of the turbine assemblies to effect an increase in a pressure drop across each of the turbine assemblies. The apparatus also has partition extending between the channels near said axial intakes.

Abstract: A delivery device for delivering fuel out of a fuel tank (1) has a suction connection (13) of a fuel pump (3) connected to a mixing tube (11) of a sucking jet pump (6). The sucking jet pump (6) sucks fuel out of the fuel tank (1) via a foot valve (12). The mixing tube (11) has an overflow valve (17) that controls a connection to a swirl pot (2). This enables the fuel pump (3) to suck fuel out of the fuel tank (1) when the swirl pot (2) is empty.

Abstract: A method and apparatus for treating fluids includes a vortex nozzle assembly having improved vortex nozzles. The overall system and system layout, which includes an elbow design, are improved as well as vortex system methods. The vortex nozzle assembly includes an access port and methods for measuring physical properties at the fluid flows. A frame assembly provides support for the vortex system.

Abstract: A method and apparatus for treating fluids includes a vortex nozzle assembly having improved vortex nozzles. The overall system and system layout, which includes an elbow design, are improved as well as vortex system methods. The vortex nozzle assembly includes an access port and methods for measuring physical properties at the fluid flows. A frame assembly provides support for the vortex system.

Abstract: A method and apparatus for treating fluids includes a vortex nozzle assembly having improved vortex nozzles. The overall system and system layout, which includes an elbow design, are improved as well as vortex system methods. The vortex nozzle assembly includes an access port and methods for measuring physical properties at the fluid flows. A frame assembly provides support for the vortex system.

Abstract: A method and apparatus for treating fluids includes a vortex nozzle assembly having improved vortex nozzles. The overall system and system layout, which includes an elbow design, are improved as well as vortex system methods. The vortex nozzle assembly includes an access port and methods for measuring physical properties at the fluid flows. A frame assembly provides support for the vortex system.

Abstract: In a method and apparatus for treating fluids, a pump delivers a fluid flow from a fluid source to a manifold. The manifold divides the fluid flow into first and second fluid flows, which are delivered from the manifold to a housing. The housing includes therein a first vortex nozzle positioned in opposed relationship to a second vortex nozzle. The first fluid flow enters the first vortex nozzle to create a first rotating fluid flow, and the second fluid flow enters the second vortex nozzle to create a second rotating fluid flow. The first and second vortex nozzles impinge the first and second rotating fluid flows in a collision chamber, thereby treating the fluid.

Abstract: A fluid flow promoter for increasing and accelerating the flow of fluids through channels, and useful in marine propulsion and aeration of liquids includes 1) an outer shell including an inlet end wall, an outlet end wall, and a solid truncated wall, 2) a fluid inlet generally centrally located in the inlet end wall, 3) an inner truncated cone with an inlet corresponding to the outer shell inlet and an outlet corresponding to the outer shell outlet, disposed within the outer shell and comprising end and side walls defining a space between the outer shell and the inner cone, the end and side walls of the inner truncated cone being perforated to permit fluid flow therethrough, and 4) a plurality of secondary fluid inlets disposed in the end or side wall of the outer shell. The apparatus is also useful in increasing the thrust of rockets and other jet exhaust devices, and for moving light gases such as helium in modular helium reactors.

Abstract: A jet pumping device includes an injection nozzle (1) intended for injection of a working fluid, placed in a line (3) including from upstream to downstream, a substantially cylindrical barrel (4), a convergent neck (5), a mixing channel (6) and a diffuser (7). The nozzle is placed at the end of a nozzle holder (9) on the longitudinal axis of the line, the pumped fluid circulates in an annular space (3) contained between the barrel (4) and the outside of the nozzle and of the nozzle holder, and the orifice of the nozzle has the longitudinal axis as the axis of symmetry.

Abstract: A gas flow director for exhausting gases from chambers, and useful in the operation of operation of gas turbines, jet engines and rockets, as well as vacuum pumps and gas compressors. The gas flow director includes 1) an outer truncated cone including a closed larger end wall, a generally open smaller end comprising a gas outlet, and a solid truncated wall, 2) a gas inlet generally centrally located in the larger end, and 3) an inner truncated cone disposed within the outer truncated cone and corresponding generally in shape to the outer truncated cone, and including end and side walls generally parallel to the end and side walls, respectively, of the outer truncated cone to define a space therebetween. The end and side walls of the inner truncated cone are perforated to permit gas flow therethrough. The gas flow director also includes 4) a plurality of secondary gas inlets disposed in the side wall of the outer truncated cone, adjacent the end wall, or in the larger end wall adjacent the side wall.

Abstract: A pumping device providing direct energy exchange between a working fluid and a pumped fluid, comprising at least a first ejector propelling the working fluid in one direction and at least a second ejector propelling working fluid in a second direction. The axial thrust induced by the jet emitted in the first direction compensates at least partly that of a jet emitted in the second direction.

Abstract: A fluid injector assembly for drawing a first fluid into the flow of a second fluid. The injector assembly includes an eductor including an inlet having a plurality of openings, a first outlet port, and a first fluid passage extending between the inlet and the first outlet port. The openings are generally disposed tangentially to the first fluid passage. The inlet is adapted to be placed in fluid communication with the second fluid such that the second fluid flows through the first fluid passage from the inlet to the first outlet port. The fluid injector assembly also includes a throat having an inlet port, a second outlet port and a second fluid passage extending between the inlet port and the second outlet port. The inlet port of the throat is spaced apart from the first outlet port of the eductor forming a gap therebetween. The gap is adapted to be placed in fluid communication with the first fluid.

Abstract: A jet pump includes a power fluid inlet, a pumped fluid inlet having a conduit therein, a fluid outlet and a downstream structure of generally frustoconical shape having a small end adjacent the pumped fluid inlet conduit, a large end downstream of the small end and a central passage. In several embodiments, the downstream structure is a series of washer like rings of increasing size. In other embodiments, the downstream structure is a solid body. Several embodiments include an upstream structure having a central power fluid inlet conduit sealed relative to the pump housing having a disc thereon downstream of the pumped fluid inlet. The disc provides a series of passages in the form of notches in the disc periphery or openings through the disc body.

Abstract: A spiral flow connector imparts a spiral flow of air to urge parts being transmitted toward a central axis to avoid contact with the walls of the transmission passages of a pneumatic transmission apparatus. The invention is especially useful for preventing damage to fragile parts such as small resin molds, metal parts or powdered material. The spiral air flow prevents air stalling in the transmission passages.

Abstract: A spiral jet mixer for mixing fluids comprises an elongated body having a first inlet nozzle for introduction of a primary fluid, a mixing chamber having a diverging wall and a converging wall, a plurality of angled, helical passageways in the diverging wall for introduction of a secondary fluid into the mixing chamber in a spiralling turbulent, initially convergent flow pattern. Removable inlet nozzles allow a plurality of inlet nozzle orifice diameters.

Abstract: A radial mixing header for use with apparatus that removes solids from a liquid by dissolved air flotation (DAF). The header comprises a par of concentric pipes circumscribed by a concentric mixing chamber having a tangential port for introduction of the recycled gas-liquid stream thereinto. The recycled stream achieves rotary and turbulent motion and mixes in a larger diameter pipe with the raw solids-containing stream which flows through a smaller diameter pipe.

Abstract: A jet pump structure for a fuel tank having first and second chambers therein includes first, second and third fuel pipes all of which are connected to a vacuum chamber provided within the fuel tank. The first pipe returns oversupplied fuel into the vacuum chamber, the second pipe transfers fuel stored in the first chamber into the vacuum chamber, and the third pipe receives the fuel from the first and second pipes and discharge same into the second chamber. A flow guide member is provided within the first pipe, which receives the oversupplied fuel to form same into a swirl flow. The swirl flow is ejected from the first pipe as a jet flow into the vacuum chamber to provide a vacuum therearound within the vacuum chamber. The ejected swirl flow further works to seal the vacuum chamber against the third pipe so that the vacuum generated within the vacuum chamber is prevented from being released through the third pipe to effectively suck the fuel from the first chamber.

Abstract: A jet pump structure for a fuel tank having first and second chambers therein includes first, second and third fuel pipes all of which are connected to a vacuum chamber provided within the fuel tank. The first pipe returns oversupplied fuel into the vacuum chamber, the second pipe transfers fuel stored in the first chamber into the vacuum chamber, and the third pipe receives the fuel from the first and second pipes. A silencer unit is connected to the third pipe for receiving the fuel from the third pipe and discharging the fuel into the second chamber. A flow guide member is provided within the first pipe receives the oversupplied fuel and forms same a swirl flow. The swirl flow is ejected from the first pipe to provide a vacuum the vacuum chamber.

Abstract: The invention relates to a multiple liquid injector composed of several identical elementary injection tubes 2, disposed in a rim around a central tube. Each tube 2 has an inlet conduit 3, itself comprising a converging truncated cone 6 and a cylinder 7, followed by an aeration zone 4 comprising an aeration chamber 8 fed tangentially by a conduit 9 perpendicular to the tubes 2, a jet centering funnel 10, followed by mixing cylinder 11, and lastly a diverging outlet conduit 12.

Abstract: A fuel supply system including a fuel tank, a feed conduit through which fuel is pumped from the fuel tank, and a return conduit through which excess fuel is returned to the fuel tank. The fuel tank has first and second sumps. The system comprises an ejector pump having a pressure chamber opening through a throat into the first sump. The pressure chamber is connected through a communication conduit to the second sump. The ejector pump includes a fuel nozzle having an inlet port connected to the return conduit and a discharge end opening into the pressure chamber for discharging a jet of fuel into the pressure chamber to create a negative pressure in the pressure chamber so as to suck fuel through the communication conduit from the second sump. In one aspect of the invention, a relief valve is provided which is responsive to a back pressure produced in the fuel nozzle for relieving the back pressure to the first sump when the back pressure exceeds a predetermined value.

Abstract: A jet pump has a chamber with a jet nozzle at the inlet port and a diffuser fitted into the outlet port with a suction port fitted in the chamber. A ball valve having a passage therethrough is fitted ahead of the jet nozzle and angular rotation of the ball valve creates a swirling action in the jet nozzle and adjustment thereof will provide maximum pumping action for various operating conditions.

Abstract: A burner assembly provides for 100% premixing of fuel and air by drawing the air into at least one high velocity stream of fuel without power assist. Specifically, the nozzle assembly for injecting the fuel into a throat comprises a plurality of nozzles in a generally circular array. Preferably, swirl is imparted to the air/fuel mixture by angling the nozzles. The diffuser comprises a conical primary diffuser followed by a cusp diffuser.

Abstract: An air pump useful in pumping gases containing abrasive particles is disclosed. A housing is constructed with a primary flow channel centered around the pump axis and a secondary flow channel annularly surrounding the primary channel just inside the outer housing wall. Within the midsection of the pump a powered impeller rotating within an axially symmetric shroud accelerates air drawn from the primary flow channel causing it to be discharged through an annular shaped ejector nozzle into a suction chamber. Presence of the high velocity airstream in the suction chamber draws the contents of the secondary flow channel into the suction chamber. The entrained contents of the primary and secondary flow channels are carried into the diffuser where the velocity energy of the mixture is converted into pressure. The pressurized mixture is then discharged through the exhaust section.

Abstract: A jet pump for use in inline piping embodying a venturi tube and a deflection nozzle for creating a vacuum by reversing the flow of an inducing liquid through the venturi tube, the resulting suction of which causes a liquid flow through the venturi tube and piping system.