| Document |
Document Title |
|
WO/2006/090019A1 |
The invention concerns a pressurized gas turbine system comprising an inner rotor (2), an outer rotor (3) provided with rolling elements (40) arranged between the inner and outer rotors, sealing members (45) for hermetically sealing the ...
|
|
WO/2006/086905A2 |
The invention relates to a boat, particularly a submarine (1), comprising at least one propulsion (2, 3). According to the invention, the at least one propulsion (2, 3) operates according to the hydrojet principle, and the at least one p...
|
|
WO/2006/083242A1 |
A rotary ram-in compressor for use in gas turbine engines and the like, having a plurality of vanes attached to discs, with the opposing parts of each two adjacent vanes defining a feeding channel in-between. In operation, working gases ...
|
|
WO/2006/070497A1 |
A convection temperature difference prime motive power device (S1), comprising an inner tube (10) rotatably pivoted on an outer shell (1), having a gas supply port (11) formed at its axial one end, and having a gas discharge port (12) fo...
|
|
WO/2006/068529A1 |
The present invention refers to a new type of rotor (2) , characterized by an asymmetrical successive positioning of several closed or opened alveoli which make up a pallets assembly with closed or opened outline, each thereof having one...
|
|
WO/2006/068633A1 |
The inventive rotary engine comprises a stator (1), rotors (2) arranged therein and a channel (3) which formed by the stator (1) and the rotors (2) and in which screens (4) are placed, wherein a combustion chamber (6) is mounted on the s...
|
|
WO/2006/062522A1 |
A high torque turbine rotor for a lightweight hand held tool for grinding and polishing having a rotor that includes two separate high pressure air chambers separated by a common housing wall, each air chamber having peripheral air expel...
|
|
WO/2006/059971A2 |
A tip turbine engine assembly includes an integral engine outer case (8) located radially outward from a fan assembly (30). The integral outer case (8) includes a rear portion (124) and a forward portion (128) with an arcuate portion (13...
|
|
WO/2006/060003A2 |
A fan-turbine rotor assembly for a tip turbine engine includes an outer periphery scalloped by a multitude of elongated openings which define an inducer receipt section to receive an inducer section and a hollow fan blade section. Each f...
|
|
WO/2006/048401A1 |
A turbine (100) of a turbine engine is disclosed, in particular, a steam turbine for a steam turbine engine. The turbine comprises at least one radial or diagonal turbine stage (120) with radial or diagonal feed stream and axial exhaust ...
|
|
WO/2006/035934A1 |
Oil supply grooves (74, 84) are formed in the rotary shaft (70) of a compression mechanism (50) and the rotary shaft (80) of an expansion mechanism (60) that are integrated with an electric motor (40). Both rotary shafts (70, 80) are cou...
|
|
WO/2006/030779A1 |
A heat pump for realizing boosting and carrying means widely applicable to Rankine cycle and others, capable of increasing the reliability of a heat pump system since a mechanical loss is absent and mechanical parts are not required, and...
|
|
WO/2006/022551A1 |
A liquid turbine device including a turbine wheel (10), in which the turbine wheel (10) includes more than one set of blades (18, 20, 22) in radial succession.
|
|
WO/2006/021513A1 |
The invention relates to a steam turbine (10) comprising at least two steam chambers (24a-e) which are surrounded by an essentially tubular shaped housing (12) and which are separated by at least one separating wall (14a-d) which is arra...
|
|
WO/2006/022812A1 |
A winglet includes a vertical member and a mounting member. The mounting member is configured to facilitate the mounting of the winglet to the tip of a fan blade. The vertical member is configured to extend perpendicularly relative the t...
|
|
WO/2006/019927A2 |
Vanes (20) positioned immediately adjacent the swept area (21) of a moving friction brake rotor (12) induce a flow of air over the rotor (12) by displacing the boundary layer of gases from the rotor surface and conducting such layer alon...
|
|
WO/2006/014517A2 |
A molten metal pump includes an impeller, a pump base housing at least partially enclosing the impeller, a shaft connected to the impeller, a motor connected to the shaft, a motor mount plate for supporting the motor; and a post for conn...
|
|
WO/2006/008353A1 |
The invention relates to a device enabling the explosion of hydrogen and air or oxygen in an enclosure, propelling disks fixed to a core (3). Any gaseous fluids can be supplied to said device consisting of at least two cannons (2) which ...
|
|
WO/2006/001855A2 |
A gas flow enhancer for a combustion engine includes a housing, configured to receive an inlet flow of gas at an inlet pressure, and enclosing an expansion chamber. Disposed within the expansion chamber are a set of inner vanes and outer...
|
|
WO/2006/001825A2 |
A cooled shroud assembly (19) includes an angled slot (25) and a plurality of dilution jet openings (26). The shroud forward cavity is modified such that at least one recirculation zone (21) is produced. The angled slot (25) forces; an a...
|
|
WO/2006/000600A1 |
The invention relates to a universal turbine for the collection or axial generation of kinetic energy in fluids. The invention comprises a tubular-type rotor in which identically-dimensioned helical blades are fixed at equidistant angula...
|
|
WO/2005/124109A1 |
A two staged fluid propulsion apparatus of the type which utilizes prior art pitched blades combined with solid boundary layer disks supported by a novel rotating tubular flow conduit perforated to allow fluid flow to from the interior o...
|
|
WO/2005/121547A2 |
A bladeless pressurized fluid turbine engine having a bladeless turbine, internal, concentric or circumferential shaft fluid ways which transmit pressurized gas to the turbine, and a pressurized fluid intake assembly. The intake assembly...
|
|
WO/2005/121548A2 |
A bladeless pressurized fluid turbine engine having a bladeless turbine, internal, concentric or circumferential shaft fluid ways which transmit pressurized gas to the turbine, and a pair of opposing pressurized fluid intake assemblies. ...
|
|
WO/2005/119011A1 |
The radiator cooling fan replacement (10) to increase engine efficiency is a multi-stage centrifugal air pump supercharger that replaces the radiator fan while at the same time increases air density of its output air. The centrifugal air...
|
|
WO/2005/119056A1 |
The invention relates to a method and to a device which uses the internal energy of fluids by means of a flow process and a turbomachine, in addition to the uses of said method according to four steps. In the first step, the angular mome...
|
|
WO/2005/116443A1 |
A hydroelectric turbine rising a flexible, collapsible shroud (3) to control water flow into a turbine housing (1), and a flotation chamber (8) to maintain the turbine housing (1) at a desired floating height, wherein water flow into and...
|
|
WO/2005/108759A1 |
An apparatus and method is provided for improving efficiency of a transonic gas turbine engine compressor (20) by bleeding off a shockwave-induced boundary layer from the gas flow passage (42) of the compressor using an array of bleed ho...
|
|
WO/2005/106205A1 |
A bladeless fluid machine that contains a stator (1) in which a bladeless rotor (2) of a rotationally symmetrical shape is installed. Between the stator and rotor there is a coaxial channel (7). The stator (1) is equipped with at least o...
|
|
WO/2005/090794A1 |
A centrifugal compressor and a method of manufacturing an impeller, the method wherein a projected part (17) is formed at the approximately radial center part of the impeller (11) on the negative pressure surface side of its a blade (16)...
|
|
WO/2005/088117A1 |
A turbine having a housing (20) containing a rotatable concentric inner member (30) with a central shaft (40) and a plurality of generaily axially oriented blades (33) extending between an exterior face of a peripheral wall of the inner ...
|
|
WO/2005/081766A2 |
Turbo-machinery and methods are disclosed for a bladeless conical radial turbine wherein fluid is directed axially within the pump body to produce an axial output. The rotor comprises a plurality of spaced apart conical elements. A plura...
|
|
WO/2005/075794A1 |
The invention relates to a steam turbine installation (10) which comprises a heating-up zone (12) having at least one heater (14, 16, 18, 20, 24, 26) for feed-water to be fed to a steam generator, such as a heat exchanger, steam boiler o...
|
|
WO/2005/073514A1 |
A pump casing for a centrifugal pump of the type that is used to process abrasive slurries is disclosed having at least one side or side liner that has a radially extending portion oriented toward the cutwater of the pump casing to local...
|
|
WO/2005/066464A1 |
At least one embodiment of the present inventive technology focuses on a vaneless diffuser adapted for establishment extra-radially of a centrifugal fan, wherein the diffuser may effect an optimal transformation of velocity pressure into...
|
|
WO/2005/066461A1 |
A steam driven engine comprising means (32) for delivering pressurised steam at right angles onto drive vanes (17, 18, 19) located on two or more interconnected co-axial rotatable cylindrical rotors (11, 12, 13) across each of which the ...
|
|
WO/2005/033490A1 |
This invention is a spiral machine component for gaseous and/or liquid fluids which represents the rotating part of the machine that can operate as a pump, compressor or turbine for all types of fluid. The spiral machine component for ga...
|
|
WO/2005/033476A1 |
A steam turbine comprises a base, means for inlet and controlling of compressed steam at the front end of the base, a front supporting part, and a rear supporting part at the back end of the base. The stator is integrated with the cylind...
|
|
WO/2005/024230A2 |
A pump device (10a, 10b, 10c) includes means for both transferring rotational momentum to the fluid by viscous forces, and imparting centrifugal forces to the fluid. The pump (10a, 10b) can include a wiper (44) extending partially across...
|
|
WO/2005/008135A2 |
A trapped vortex combustor for gas turbine engines. An annular combustor housing is provided having a plurality of inlet centerbodies disposed along a helical axis. The inlet centerbodies include a leading edge structure, opposing sidewa...
|
|
WO/2005/005783A1 |
The invention relates to a steam turbine comprising a first partial turbine (2) that is connected to a second partial turbine (3) in a fluidic manner via a transition region (1). Said transition region (1) comprises a flow deviating arra...
|
|
WO/2004/109074A2 |
Pressurized gas turbine engine with efficiency enhanced by an electrothernodynamic power convertor. The turbine has peripheral nozzles which are supplied with pressurized gas or pressurized liquid by internal nozzle gas ways. Pressurized...
|
|
WO/2004/099621A1 |
A turbine rotor (10) has a spiral involute channel (18) formed in a rotor disk (12). In one embodiment, the channel (18) has an inlet (22) near the center (14) of the disk (12) and an outlet (24) near the periphery (16) of the disk (12)....
|
|
WO/2004/097203A1 |
An apparatus works on the basis of the cyclone principle, as in a whirlwind or liquid or gas whirl or cosmic whirl, to transmit motor energy to a medium (liquid, gas, or vacuum) and to use this energy for various purposes, such as a driv...
|
|
WO/2004/074638A1 |
The invention relates to a device for effecting heat transfer to rotating equipment, in particular gas turbines. A gas turbine (10) comprises a first rotating unit (11), i.e. an internal shaft and a second fixed unit (16), i.e. a housing...
|
|
WO/2004/064230A1 |
The invention relates to a turbo-machine (1) comprising a rotor (3), a stator (5), and a flow channel (7) for an actuating fluid (A) used to drive the rotor (3). Said turbo-machine (1) comprises a magnet (9) for producing a pre-determina...
|
|
WO2004022921B1 |
The invention relates to a gas turbine comprising a radial-type turbine wheel and a fixed distributor which is supplied by a volute and which surrounds the wheel. The aforementioned distributor ensures that the inlet gases arriving from ...
|
|
WO/2004/034405A2 |
An apparatus and method for generating cavitation in fluids is disclosed. The apparatus includes a housing (4) for receiving a rotor (14), which is driven by a motive force (6). Multiple embodiments of the rotors are disclosed including,...
|
|
WO/2004/029432A2 |
A gas turbine engine. The engine is based on the use of a gas turbine driven rotor having a compression ramp traveling at a local supersonic inlet velocity (based on the combination of inlet gas velocity and tangential speed of the ramp)...
|
|
WO/2004/025085A1 |
A fluid flow actuated drive means (10) includes a rotatably mounted impeller (12) which defines a set of circumferentially spaced outer chambers (14) which extend inwardly from openings (16) along a peripheral edge (18) of the impeller (...
|
