Abstract: Provided is a turbo compressor that includes: a compressor unit compressing a gas; a motor driving the compressor unit; and a motor casing accommodating the motor. In the turbo compressor, the motor casing includes: a body portion which is molded in a cylindrical shape; an annular diameter reduced portion which is connected to at least one end portion of the body portion in the rotation axis direction of the motor and of which the diameter is reduced as it moves away from the body portion; and a flat portion which is connected to the central end portion of the diameter reduced portion and is molded in a planar shape.

Abstract: A reinforced fan frame structure includes a frame body and at least one metal ring. The frame body has a seat portion with a centered bearing cup axially forward extended from the seat portion. The metal ring is integrally associated with the seat portion and has an inner circumferential edge facing toward the bearing cup. With the metal ring integrally associated with the seat portion of the frame body, it is able to effectively control the deformation and the flatness of the seat portion and accordingly, effectively upgrade the overall structural strength of the seat portion.

Abstract: A nacelle for a turbofan propulsion system that extends along a centerline includes a forward cowling and an aft cowling. To improve the fit of a turbofan propulsion system in the space between the wing and ground of a fixed-wing aircraft, the aft cowling of the nacelle is modified. The aft cowling has a non-circular cross-sectional geometry disposed in a plane substantially perpendicular to the centerline. The non-circular cross-sectional geometry includes a radially recessed section disposed between first and second curved sections. The first and the second curved sections each have a radius that is greater than a radial distance between the centerline and a center point of the radially recessed section.

Abstract: It is an object of the present invention to provide a compressor that has a simple structure, produces a damping effect and improves aerodynamic performance. In a compressor including stator blades 4 circumferentially mounted to an inner circumferential surface side of a casing 6 forming a annular path; and an inner barrel 7 supported by the casing and arranged on the radially inside of the stator blade as a partition wall on the radial side of the annular path; the stator blade includes an outer shroud 10 mounted to an inner circumferential surface of the casing at a position facing the inner barrel, and an inner shroud 11 supporting a blade portion at an inner diameter side, the inner shroud being disposed in an annular groove formed in an outer circumferential surface of the inner barrel facing the inner shroud. The stator blade including the outer shroud 10, the inner shroud 11 and the blade portions 9 are formed in a monolithic structure by milling.

Abstract: An air duct includes a cover and two adjusting pieces. The cover includes a top board and two end boards extending downwards from two opposite ends of the top board. The cover defines an air outlet in a front of the cover and an air intake in a rear of the cover. Two adjusting pieces are slantingly extended from rear ends of the two side boards toward the air outlet.

Abstract: A fan unit which in use forms part of a gases supply unit, the gases supply unit suitable for use as part of a system for providing heated humidified gases to a user, the fan unit having a casing that has an inlet aperture and an outlet passage, the outlet passage including an exit aperture, the fan unit also including a fan which is located inside the casing and which is adapted for connection to a motor to drive rotation of the fan in use, the fan drawing gases into the casing via the inlet aperture, and forcing these gases out of the casing via the outlet passage as a gases stream, the outlet passage further including at least one bypass vent hole independent of the exit aperture and arranged at an angle to the path of the gases stream through the outlet passage.

Abstract: A turbine moving blade cascade 30 of a turbine rotor assembly 35 has root portions of plural moving blades 13 fitted and held in a root groove circumferentially formed on the outer circumferential portion of a rotor disk 15 of a turbine rotor 14 and has a notch blade 40 fixed in a cutout portion formed in the rotor disk 15. The plural moving blades 13 are comprised of three types of moving blades which include regular blades 50 having a circumferential width determined through theoretical calculation, wide blades 51 having a circumferential width larger than the regular blades 50, and narrow blades 52 having a circumferential width smaller than the regular blades 50.

Abstract: A blower includes a fan, an inlet through which air is drawn into the fan, and an outlet through which an air flow from the fan is exhausted. The inlet and the outlet have slits with a specific width or an array of through holes with a specific diameter. The relationship A<C, A<B is satisfied, where A represents the width of the slits or the diameter of the through holes of the inlet, B represents a particle size of dust that is allowed to pass through in view of the dust-proof performance of the fan, and C represents the width of the slits or the diameter of the through holes of the outlet. The blowing performance can be improved within the range of dust-proof performance in which damage or functional degradation can be avoided.

Abstract: A panelled assembly has a spacer 26 of cuboid, or rectangular prism, shape located between adjacent first panels 16 in order to maintain separation of the panels 16 at a desired minimum distance during mounting of the panels. During installation, the spacer 26 abuts the first side edge 16b of one panel, and then the second side edge 16d of the circumferentially adjacent panel is made to abut the opposed side of the spacer. This results in an axially extending gap 28 of a constant width between adjacent first panels 16. Similarly, spacers 26 are located between adjacent second panels 18, adjacent third liner panels 20, adjacent fourth panels 22 and adjacent panels 24 as the panels are installed to make up the assembly. This results in axially extending gaps 28, each of a constant width, between circumferentially adjacent panels. The material from which the spacers are made is substantially the same as filler material which is used to fill the gaps between adjacent panels caused by the presence of the spacers.

Abstract: A method and system for a fan assembly that includes a fan casing having a longitudinal centerline axis extending from an upstream inlet opening to a downstream outlet opening is provided. The fan assembly also includes a first substantially cylindrical casing segment extending circumferentially about and substantially axially aligned with tips of a plurality of blades extending from a rotor hub, the first casing segment including a first inner diameter that is greater than the rotor diameter, a second casing segment configured to extend axially in a direction opposite a flow of fluid through the fan casing, the second casing segment including a second inner diameter, the second inner diameter less than the first inner diameter and the rotor diameter, and a third casing segment including the first inner diameter along a first circumferential edge, the second inner diameter along a second circumferential edge, and a surface extending therebetween.

Abstract: There is provided an air conditioner having a fan guard assembly which is easy to assemble, and the transversal crosspieces of the fan guard assembly are not easily disengaged from the longitudinal crosspieces. The air conditioner includes: an air conditioner, comprising: a housing accommodating therein an air delivery fan and having a discharge opening from which an airflow generated by the air delivery fan is blown out; and a fan guard assembly disposed between the air delivery fan and the discharge opening, in the housing, wherein the fan guard assembly includes a first member having a protruding portion protruding in such a manner as to form a retaining groove, and a second member held in the retaining groove of the first member; and the protruding portion protrudes in such a manner that, in a side view, the protruding portion intersects a rectilinear line passing a center point of the second member held by the retaining groove and an arbitrary point P1 along an edge of the discharge opening.

Abstract: A centrifugal fan includes a fan frame (20) and an impeller (40) received in the fan frame. The impeller includes a hub (41) having a circular top wall (410) and a cylindrical side wall (412) extending downwardly from a rim of the circular top wall, a plurality of blades (42) extending radially from the side wall of the hub and a blade ring (44). The blade ring includes an annular top plate (441), a cylindrical sidewall (442) extending downwardly from an outer periphery of the top plate, and a flange (443) extending outwardly from a bottom of the cylindrical sidewall. The blade ring is arranged on top surfaces of the blades received in an air inlet (24a) defined in a top surface of the fan frame, and the top plate of the blade ring and the top surface of the fan frame are coplanar with each other.

Abstract: This device transforms the energy of flowing water into useable energy and includes one or more flow diversion structures, one or more paddlewheels, and one or more generators. A gearbox or transmission may be added to increase the rotational speed of the generators. A subsea cable can be included to transmit the electrical energy from device to shore.

Abstract: A synchronous induced wind power generation system is provided, which is comprised of a horizontally rotatable turbine-generator section that wind vanes into the prevailing wind direction. The turbine-generator section has a horizontally disposed turbine therein, and air induction shrouds at either end thereof, the anterior areas of the air induction shrouds having larger areas than the interior area of the turbine-generator section, so as to induce a large differential air pressure across the turbine. The turbine is directly coupled to a synchronous AC generator that is synchronized with an external power line in connection therewith, and directly generates synchronous AC power. Further, turbine magnetic brakes are employed 1) during synchronization with the electrical line, 2) to modulate turbine power, and 3) to protect against overspeed during high wind and loss of load.

Abstract: A method for manufacture of a compressor housing which is resistant to a titanium fire (burning titanium). A circular blank made of steel, or steel alloy, or superalloy which is incombustible in the presence of a titanium fire is hydroformed against a circular blank made from titanium or titanium alloy.

Abstract: A wind-driven electric plant comprises an inlet shell shaped as a circle and a circular outer shell with the cross section of its inside surface of a round form. Inside the circular shell, provision is made of a coaxially arranged turbine. Kinematically coupled with the turbine is a mechanism for the conversion of mechanical energy. At least a portion of the outer shell is ellipsoidal in cross section. The major axis of an ellipse defining the cross section of the outside surface of the inlet shell at an inlet of the latter is not less than 0.55 and not more than 0.95 of the dia. of a circle defining the inside surface of the outer shell in its minimum section.

Abstract: A fan housing structure including a base seat and a sideboard. The base seat has a bed section and a mating section extending along a periphery of the bed section. The bed section has a bush made of a material other than the material of the bed section. The bush is disposed on the bed section to axially protrude therefrom. The sideboard is made of a material other than the material of the base seat. The sideboard is disposed on the mating section and integrally connected with the base seat. The sideboard and the base seat together define a space therebetween. The sideboard and the bush are made of a material other than the material of the base seat and are integrally connected with the base seat by means of insert injection molding. Accordingly, the fan housing structure has enhanced structural strength and thinner thickness to save room.

Abstract: This invention relates to a clean, efficient, substantially isentropic method and apparatus for transforming the internal energy of a mass flow of a fluid, such as air, into increased flow kinetic energy and then efficiently transferring this additional kinetic energy to a power take-off means for doing useful work. The acceleration of the air flow is accomplished by passing the air flow through a set of converging nozzles which generate thrust; the nozzle thrust is then transformed into torque which turns a rotor which is coupled to a power take-off means. The method and apparatus can be made to be self-sustaining.

Abstract: A turbine blade is described which includes a blade root;a blade tip; a leading edge extending from the blade root to the blade tip; a trailing edge extending from the blade root to the blade tip; a blade root chord defined as a straight line between the leading edge and the trailing edge at the blade root; a blade tip chord defined as a straight line between the leading edge and the trailing edge at the blade tip; wherein the blade tip chord is angularly displaced from the blade root chord by a twist angle of between 50° and 90°.

Abstract: The invention relates to a nacelle for a turbojet engine, comprising a rear section forming an outer structure which defines, together with a concentric inner structure (4) comprising an inner panel (10) for surrounding a downstream part of the turbojet engine, an annular flow channel for a so-called secondary flow. The invention is characterised in that the exhaust means (11) are arranged in the inner panel in such a way that any inopportune surge is exhausted in the annular channel.

Abstract: A tip turbine engine assembly according to the present invention includes a load bearing engine support structure (12). The engine support structure (12) includes an engine support plane (P) that is substantially perpendicular to an engine centerline (A) and first rotationally fixed member (50) disposed about the engine centerline (A) and cantilevered from the engine support plane (P). A support member extends radially outward from the first rotationally fixed member (50) and structurally supports a second rotationally fixed member (58) that is coaxial with the first rotationally fixed member. A rotor is mounted on the first rotationally fixed member and rotates about the engine centerline (A).

Abstract: A steam turbine and a seal member between stationary components of a steam turbine are disclosed. The seal member is annular, with a cross-section having an elongated seal member and bulbous ends that are adapted to be inserted into grooves in the stationary components to form point seals between the bulbous ends and axial faces of the grooves. The bulbous ends are designed to rotate with respect to the axial faces of the annular grooves and the elongated member is designed to flex to maintain the point seals in response to a realignment of the components.

Abstract: A wake flow injector method and apparatus are presented to improve the power production of wind and water turbines by directly injecting higher-energy fluid or air directly into the wake flow region behind the rotor or turbine.

Abstract: An intermediate housing floor for a fluid kinetic machine is provided. The intermediate housing floor includes a partial joint at which the intermediate housing floor may be divided during installation and/or removal into/from the fluid kinetic machine and is made up of at least two overlapping partial joint surfaces at sections of the intermediate housing floor that face one another. A recess is provided in the area of the overlap in at least the one partial joint surface, a coating is kept in the recess. The coating protrudes from the one partial joint surface as a protrusion in the removed state of the intermediate housing floor in which the intermediate housing floor is divided at the partial joint so that in the installed state of the intermediate housing floor the coating abuts against the other partial joint surface facing the one partial joint surface, whereupon the partial joint is sealed.

Abstract: A fan device includes: a fan housing configured with a receiving space defined among opposite top and bottom walls, and a surrounding side wall; and a fan impeller mounted in the receiving space, disposed adjacent to an air outlet in the top wall and operable to rotate about a central axis transverse to the top and bottom walls of the fan housing. The fan impeller includes a hub body disposed coaxially with the central axis, and a plurality of angularly spaced apart fan blades extending outwardly and radially from the hub body. An angular distance between each adjacent pair of the fan blades is different from that of any other adjacent pair of the fan blades.

Abstract: A fan device includes: a fan housing configured with a receiving space defined among opposite top and bottom walls, and a surrounding side wall; a fan impeller mounted in the receiving space, disposed adjacent to an air outlet in the top wall and operable to rotate about a central axis transverse to the top and bottom walls of the fan housing; and an air-guiding unit mounted fixedly in the receiving space and disposed adjacent to an air inlet in the bottom wall. The air-guiding unit includes a central connecting member disposed axially with the central axis, and a plurality of angularly spaced apart air-guiding blades interconnecting the central connecting member and the surrounding sidewall. An angular distance between each adjacent pair of the air-guiding blades is different from that of any other adjacent pair of the air-guiding blades.

Abstract: A support arrangement for an exhaust hood. The inner casing in the inventive arrangement is supported directly by the curb foundation. As a result, the effect of pressure changes in the exhaust hood are eliminated and the effect of temperature changes of the exhaust hood are reduced relative to the positioning of the inner casing and the rotor within it. Shaft bearings may be outside the exhaust hood located in a standard directly on the foundation. Rotor end packing may also be attached to the standard. The exhaust hood can be a much simpler design with less structural supports and less fabrication time. Easier maintenance is facilitated because the shaft bearings are not tucked under the exhaust hood and the end packing can be removed without removal of a large section of the exhaust hood.

Abstract: The location of in-pipe turbines within a piping system and their relationships to other devices in the piping system is dependent on several factors for the ideal operation of these turbines, whether from the nozzle shooting liquid into air, or providing a stable pressure to the turbine and the generator. Several solutions to this issue are presented.

Abstract: A fan is disclosed herein. The fan includes a shaft rotatable about an axis. The fan also includes a blade engaged with the shaft for rotation about the axis. The fan also includes a case encircling the axis. The case is positioned radially outward of the blade and the shaft. The fan also includes a blanket mounted to the case. The case and the blanket are operable to cooperate with one another to prevent the blade from escaping the case upon the blade separating from the shaft. The blanket is at least partially impregnated with shear thickening fluid.

Abstract: An arrangement with a nacelle and with at least one instrument of a wind turbine is disclosed. The instrument is connected with a rod. A channel penetrates the wall of the nacelle. The channel interacts with the rod in a way that the rod and its assigned instrument are moved through the channel between a first and a second position. The instrument is positioned inside the nacelle at the first position for installation and/or service purposes, while the instrument is positioned outside the nacelle at the second position for operation purposes of the instrument.

Abstract: A seal assembly for a turbo machine, such as a turbo jet, includes a housing having a retainer secured relative to the housing. A seal is arranged between the housing and the retainer. The seal provides an opening configured to receive a penetrating element. The seal comprises a composite material. In one example, an anti-rotation feature prevents the seal from rotating relative to the housing. The anti-rotation feature includes a rivet received in a hole in the seal that cooperates with at least one of the housing and the retainer to maintain the seal in a desired angular position.

Abstract: The invention relates to a hydrodynamic torque converter having a pump shell including blades, a turbine shell including blades, a torus-shaped flow cycle. The blades are configured to be attached at the respective shells through inner walls and the inner walls of the turbine shell and of the pump shell form an inner torus with outer surfaces facing the flow cycle and an end of an extension of the inner wall of at least one shell and an end of an extension of an adjacent shell are disposed in a plane and extend over one another and define a gap between one another. A transition from the extensions is configured to be hydrodynamically smooth.

Abstract: An invention for capturing and converting the hydro kinetic energy in ocean and tidal currents into mechanical energy for generating electricity. An internal turbine enclosed in a external turbine cylinder rotates opposite of internal turbine. Current is compressed into high pressure within internal turbine, the high pressure is vented into the rear low pressure side of external turbine producing additional energy. The internal and external turbines are enclosed in a cowling to maximize current through both counter rotating turbines. Permanent magnet rings are coupled to both turbine tips that rotate peripheral to stators. The cowling and turbines are balanced around the main center shaft, it is finned at the rear to steer the apparatus into the current. Counter rotation produces a neutral output torque with increased energy output that is transmitted via underwater cable to onshore grid.

Abstract: A fan housing includes a plastic casing having a skirt-board and a lateral wall. The skirt-board includes inner and outer peripheries spaced in a radial direction while the plastic casing further includes a first coupling portion formed along the inner periphery of the skirt-board. The lateral wall extends from a face of the skirt-board along the outer periphery of the skirt-board in an axial direction perpendicular to the radial direction. The fan housing includes a metal frame having a shaft coupling member and a second coupling portion. The second coupling portion of the metal frame is coupled to the first coupling portion of the plastic casing. A motor can be mounted to the metal frame of the fan housing, and an impeller can be rotatably coupled to the motor to form a heat dissipating fan.

Abstract: A gas turbine engine comprising a nacelle and a breather duct. The breather duct provides communication between a component of the engine within the nacelle and the exterior of the nacelle and opens at an exhaust port on the external surface of the nacelle. There is at least one clean air outlet bounding the exhaust port and arranged to expel, in use, a vortical flow of clean air to form an aerodynamic barrier between the external surface of the nacelle and a flow of breather air expelled from the exhaust port.

Abstract: An exemplary fan assembly includes a fan and a snap-on cover. The fan includes a bracket and an impeller disposed in the bracket. The cover includes a base body, a number of first clasps extending outwardly from a first side of the base body, a number of retaining clasps extending outwardly from an opposite second side of the base body, and an operation portion connecting the retaining clasps. The base body is disposed on the bracket, the first clasps clasp a first side of the bracket, the retaining portions clasp an opposite second side of the bracket, and the operation portion presses the bracket.

Abstract: A fluidkinetic energy converter includes a passageway-filled enclosure. Turbines are mounted in the passageways and fluid flow may be concentrated on subparts of the turbines by inner fluid flow deflectors or dividers. The energy converter enclosure can include dividers at both inlets and outlets in order to be adaptable for either river or tidal environments. Notably, apart from the turbines and energy generating components, the enclosure may be implemented such as to have no moving parts, thereby reducing complexity, cost, and weight.

Abstract: A fan with pressurizing structure includes a rotor having a main body, blades spaced on the main body, a magnetic body annularly mounted in the main body, and a shaft axially connected to an inner side of the main body; a frame having a sleeve and at least one bearing rotatably received in the sleeve, and an opposing end of the shaft being inserted into the bearing; a stator assembly fitted around the sleeve and including silicon steel plates and a base plate; and a plurality of first pressurizing sections selectively provided on one of the base plate and an end face of the magnetic body. With the first pressurizing sections, deposition of moisture and salt fog in the sleeve and the rotor can be prevented to avoid corroded and damaged bearing and rotor shaft, and the service life of the whole fan is increased.

Abstract: A casing for a turbomachine rotor wheel includes a plurality of circumferential grooves, each of substantially constant section, with the section areas of the circumferential grooves decreasing from upstream to downstream on going from the first groove to the last groove. By treating the casing in this way, the efficiency of the rotor wheel is optimized and its surge margin is improved.

Abstract: The present invention relates to a casing (5) for a rotor of a turbomachine, more particularly for a fan (1) of a turbojet engine (2), comprising a peripheral shroud (6) designed to form a clamping collar around the casing, characterized in that the shroud has at least one fitting (12, 13) or flange for the attachment of equipment.

Abstract: Geometries of foil shapes that act particularly well to increase the power output of adjacent vertical axis turbines are presented.

Abstract: A fan shroud assembly for use with a cooling system of a vehicle, the cooling system comprising at least one of a radiator and a fan, the fan shroud assembly comprising: a shroud having a first surface, a second surface, and a sidewall extending therebetween, the first surface connected to at least a portion of the vehicle such that the shroud is at least partially positioned behind the radiator; a shroud nozzle extending from the second surface of the shroud, wherein the shroud nozzle houses at least a portion of the fan; and wherein the fan shroud assembly provides fluid communication between the fan and the radiator, and further wherein the fluid communicated through the fan shroud assembly is substantially evenly distributed over the radiator.

Abstract: A vortical energy wind apparatus translates wind gusts to vertical air streams that disrupt the streams of air in the atmosphere that pose high tornado-risks. The apparatus comprises a lower half-spheroid part and an upper half-spheroid part both placed by their convexities to each other. A toroidal-shaped axial-symmetric core has a set of curved blades is attached to the core. Streams of air penetrate a rotary wheel inside it, and the blades attached to the core rotate the wheel. Essentially, the upper part acts like an upside-down wing at streamlining the wind and an exit hole centered at a top of the upper part provides means for the vortical stream of air to leave the apparatus.

Abstract: An apparatus for pumping or compressing a fluid, the apparatus comprising: a housing having a front wall, a rear wall and one or more side walls interconnecting the front and rear walls to define a fluid rotation chamber; at least one inlet located substantially centrally in the front wall; an impeller located at least partially within the at least one inlet such that at least a portion of the impeller extends outwardly beyond at least a portion of the front wall; and at least one outlet, wherein rotation of the impeller causes fluid entering the apparatus through the at least one inlet to rotate within the fluid rotation chamber prior to exiting the apparatus through the at least one outlet.

Abstract: An impingement baffle for a gas turbine engine is provided. The impingement baffle is a one piece impingement ring with one opening and with fastening elements at both free ends of the impingement ring to enable the closing of the impingement ring. A gas turbine engine including at least one such an impingement baffle is also provided.

Abstract: A wind turbine (10) comprising: a rotor (12), the axis of rotation extending longitudinally through said rotor (12); a plurality of blades (18) mounted to the rotor (12) to drive the rotor (12) in response to an airflow: and an airflow deflector (30) located for directing airflow through the rotor (12) to increase the efficiency of the turbine (10). The airflow deflector (30) is located inward of the blades (18) which have a fixed pitch relative to the centre of rotation of the rotor (12). Airflow deflector (30) is located around the centre of rotation of rotor (12). The blades (18) also are aerodynamically configured to provide lift due to airflow behavior through the rotor (12) and airflow deflector (30).

Abstract: A side channel compressor for compressing a gas comprises a housing (3), a side channel (30), located in the housing (3) and having a cross-sectional area (A), for compressing a gas, a gas inlet opening (31) formed in the housing (3), the gas inlet opening (31) being in flow connection with the side channel (30) for introducing a gas, a gas outlet opening (32) formed in the housing (3) for discharging the gas to be compressed from the side channel (30), wherein the gas outlet opening (32) is in flow connection with the gas inlet opening (31) via the side channel (30), and an impeller (2) which is mounted for rotation in the housing (3) and comprises impeller blades (1) disposed in the side channel (30), wherein the cross-sectional area (A) of the side channel (30) decreases non-monotonically from the gas inlet opening (31) towards the gas outlet opening (32).

Abstract: Provided is a method and apparatus for monitoring a mixture of at least two components. Also provided is a rotor blade of a wind power installation, a gondola casing of a wind power installation and a wind power installation itself. To provide a method in which the composition of the mixture can be easily monitored without damaging the workpiece produced therefrom, a dye is added to each component, wherein added to each component is its own color which is different from that of the other components, and the mixture of those components is monitored colorimetrically. A gondola casing and/or a rotor blade is manufactured by using such a method to determine amounts of components to include in a material of which the gondola casing or rotor blade is to be made.

Abstract: The invention relates to a sectored distributor (112) for a turbomachine, including two coaxial platforms mutually connected by radial blades, the inner platform (130) being connected to an annular partition (138) for suspending an annular mounting (140) carrying elements (136) made of material subject to abrasion, this mounting sliding circumferentially on the partition and comprising a means engaging with means corresponding to the inner periphery of the partition to ensure radial restraint of the mounting on this partition.

Abstract: A turbomachine casing assembly comprises a first casing portion for at least partially encasing one or more rotating aerofoil structures of a turbomachine and a second casing portion; the first casing portion being movable with respect to the second casing portion. One or more resilient elements are arranged so as to resist movement of the first casing portion with respect to the second casing portion.