65results about How to "Flow loss minimization" patented technology

An improved outlet guide vane system is disclosed for axial flow fans. Construction details are described which reduce losses in the end wall regions of the vanes, particularly for axial flow fans operating at low flow coefficient with strong localized swirl associated with upstream rotor tip clearance flows. In the preferred embodiment, the vane spanwise airfoil stacking line is approximately straight, while leaning circumferentially toward the incoming swirl flow over the majority of the radial span. The stacking line then curves abruptly in the opposite direction over the radially outboard spanwise portion, so as to lean away from the incoming swirl at the vane tip station. The radially outboard portion of the vanes simultaneously include a gradual increase in vane stagger angle, vane camber angle and vane chord. The vane may also include an axial sweep component.

Disclosed herein is an air-blowing apparatus of a cleaner. The air-blowing apparatus comprises a fan having a plurality of blades spaced apart from each other in the circumferential direction of the fan for generating a blowing force in the centrifugal direction thereof, and a diffuser disposed outside the fan in the radial direction of the fan for diffusing air blown from the fan. Each blade is formed such that at least a part of the blade is shorter than the other part of the blade extending to the outer diameter of the fan, whereby noise is reduced while blowing efficiency is not affected.

An air conditioning apparatus is provided. The air conditioning apparatus includes a cover assembly having an indoor air suction hole, a filter assembly cleaning indoor air sucked through the indoor air suction hole, and a grill. The grill includes a discharge grill formed on a side for discharging the indoor air cleaned by the filter assembly to an indoor area, and an exhaust grill for discharging indoor air to an outdoor area. A fan assembly draws indoor or outdoor air toward the grill. A rear panel is coupled to the grill. The rear panel includes a suction hole formed in one side for introducing outdoor air and an exhaust hole formed beside the suction hole for discharging indoor air to the outdoor area.

A blade cascade of a turbomachine whose at least one side wall is configured to be circumferentially undulated and which has at least two elevations and at least one depression or at least two depressions having at least one elevation, as well as a turbomachine having a blade cascade of this kind.

The present invention relates to a product for fluidic applications, with at least one surface segment having a plurality of ribs in contact with a fluid flowing in a flow direction and adjacent ribs delimit between them in each case a valley and a method for production and a use of such a product. The product according to the invention can be produced economically with further improved flow properties; in that at least two ribs with the valley they respectively delimit are combined in a group, that at least two groups are present, and separated from each group arranged adjacent to it, viewed transverse to the flow direction S of the fluid, by a valley, and that the height profile of the valley differs in each case from the height profile of the valleys delimited by those ribs of the groups which are adjacent to the valley separating the groups.

The invention discloses an integrated tapered cold-end heat exchanger for a linear pulse tube refrigerator and a manufacturing method. The heat exchanger mainly comprises a shell, a tapered slit body and a T-shaped guide core column, wherein the shell is a main heat-dispersing surface and a coupled interface, protects the tapered slit body and the T-shaped guide core column and is connected with a regenerator and a pulse tube; the tapered slit body is cut inside the shell by a low-speed wire cutting technology; the T-shaped guide core column is arranged in the center; and a core column slit is cut on the guide core column. According to the heat exchanger, the heat exchanging area is maximized within a limited volume by uniformly cutting the tapered slit in unequal diameters; the cutting way makes a natural transition from a large diameter end to a small diameter end; the thermal resistance and flow loss are minimized; and the gas in the pulse tube is laminarized without an additional gas director. The heat exchanger greatly improves the performance of the whole linear pulse tube refrigerator and is very significant to the practicality of the linear pulse tube refrigerator, aerospace application and other aspects.

Systems for taking exhaust gas samples are known. Use is normally made of CVS systems in which an exhaust gas channel (4) is fluidically connected to an exhaust gas source (6) via an exhaust gas inlet (2) and an air channel (10), into which ambient air is sucked via an air filter (16), opens in a first mixing zone (22) which merges into a dilution tunnel (24) from which the samples are taken. The invention now proposes that the system have a second exhaust gas channel (38) which is fluidically connected to a second exhaust gas source (36) via a second exhaust gas inlet (34) and has a second mixing zone (46), wherein the diluted exhaust gas/air mass flows flow either from the first exhaust gas source (6) or from the second exhaust gas source (36) into the one dilution tunnel (23) and to the sampling probe (26). A particularly advantageous embodiment is described in this respect. The system is suitable for the connection of diesel and spark ignition engines, the exhaust gas of which can thereby be removed and analysed for the first time via only one sampling point and using only one dilution tunnel and one pump in a common system.

A refrigerator comprises: a fan for blowing cool air generated by an evaporator to a freezing chamber or a refrigerating chamber; a scroll guide for discharging cool air discharged from the fan in two directions; a guide pipeline formed at the scroll guide in two directions for guiding cool air discharged from the scroll guide; and a cool air duct connected to the guide pipeline for supplying cool air to the freezing chamber or the refrigerating chamber. An optimum scroll guide that can be applicable even when a plurality of cool air ducts are implemented is provided, thereby reducing a flow loss of cool air discharged from the fan and decreasing consumption power.

The vacuum suctioning unit of the present invention includes: a cover provided with an air entrance; an impeller for circulating air that enters the air entrance; a motor provided with a shaft connected to the impeller; a guide device for guiding the flow of air that exits an exit of the impeller; and a motor housing that houses the motor and is provided with an air exit. The guide device includes: a guide body disposed below the impeller; a first guide vane formed on a side surface of the guide body and guiding air discharged from the impeller; and a second guide vane formed on the bottom surface of the guide body and connected to the first guide vane to guide air that is moved by the first guide vane. The entrance angle of the first guide vane is within the range of 10 to 27 degrees.

A ring structure with a metal design for a moving blade of axially flowed through compressor and turbine stages, particularly in gas turbine engines is provided. The ring structure includes a circular ring-shaped outer wall, a circular ring-shaped inner wall, which is located at a short radial distance from the moving blade tips, and includes a joining structure provided in the form of hollow chamber structure between the outer wall and the inner wall. The outer wall is provided in the form of a closed, mechanically stable housing wall of the compressor or turbine stage, and the joining structure provided in the form of hollow chamber structure is joined in a fixed manner to the outer wall and to the inner wall, for example, by soldering, diffusion welding or other joining techniques. The inner wall is provided in the form of a closed, mechanically stable structure, which serves as a run-in lining for the moving blade tips and which is made of a metal woven fabric and/or of a metal felt.

A collecting chamber of a flow machine which expands in the direction of circumference, including at least one outer shell part and a contour insert is provided. The contour insert is provided with a groove which extends in the circumferential direction and is preferably configured as a helical spiral. The contour insert, is cut from a whole unit and is delimited at one end in the circumferential direction by a bent edge so that the flow losses are minimized during the passage from the collecting chamber into a subsequent diffuser.

The invention relates to a rotor (10) for a turbo machine, in particular for an aircraft turbine, with rotating blades (12) that are joined to a basic rotor body (16), whereby at least one channel (22) extending between the high-pressure side (HD) and the low-pressure side (ND) of rotor (10) radially underneath a blade platform (18) of at least one rotating blade (12) is provided, whereby a slope of a principal axis of extension (H) of channel (22) relative to an axis of rotation (D) of rotor (10) has the same sign as a slope of a principal axis of extension (R) of a radially inner boundary of the flow channel of rotor 10. In addition, the invention relates to a turbo machine having a rotor (10) as well as to a method for manufacturing a rotor (10) for a turbo machine.

A structure for reducing a refrigerant flow loss in a compressor includes a refrigerant flow resistance reducing unit to reduce a refrigerant channel resistance at a lower surface of a rotor facing a compression mechanism unit. When the high temperature and high pressure refrigerant gas discharged from the compression mechanism unit flows to the discharge pipe through the refrigerant passage including the gap between the rotor and the stator of the electric mechanism unit, the flow resistance of the refrigerant gas is reduced. Therefore, since the refrigerant can flow smoothly, a flow loss of the refrigerant can be reduced and, as a noise generation is reduced, a reliability can be heightened.

The invention discloses a clutch device used for a transmission system of a vehicle. The clutch device comprises an input side connected with a driving motor; a first output side and a second output side, which are respectively used for connection with an input shaft of a transmission. The clutch device comprises a torque converter connected between the input side and the first output side. The coupling of the torque converter is adjusted, and then the improving of the positive or negative rotating speed of the input side with respect to the first output side can be adjusted.

A method for creating an impeller and an impeller of a radial turbo fluid energy machine includes a wheel disc, cover disc, blades, and hub. The hub is mounted on a shaft which extends along an axis, the wheel disc extends substantially radially from the hub, and the cover disc is connected to the wheel disc by the blades such that flow channels separated from one another in the circumferential direction are defined by the blades. The impeller has a first flow passage in a substantially axial direction in the radial proximity of the hub, and the impeller has a second flow passage in a substantially radial direction radially farther away from the hub than the first flow path passage. The cover disc surface facing the wheel disc has a lower degree of roughness at least in some regions than the wheel disc surface facing the cover disc.