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WO/2017/147029A1 |
In general, the present invention is directed towards various underground energy storage systems and equipment for generating energy. The present invention encompasses various configurations of underground storage systems, pumps, and tur...
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WO/2017/144160A1 |
The invention relates to a rotor assembly for an exhaust gas turbocharger, comprising a turbine wheel, a compressor wheel (5) connected to the turbine wheel for conjoint rotation by means of a shaft (3), and an intermediate component (8)...
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WO/2017/139948A1 |
An automation thermal power installation employing a closed-loop control technology, comprising a gas turbine power generating mechanism, an exhaust gas treatment mechanism and an exhaust heat recovery mechanism that are connected in seq...
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WO/2017/142780A1 |
A vane lever for a guide apparatus of a turbocharger may include a base. The base may include a bore disposed therethrough. An arm may extend from the base and may be receivable in an aperture of an adjustment ring of the guide apparatus...
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WO/2017/138461A1 |
This slag cyclone is provided with a cyclone body (50) into which a mixed fluid of water and pressurized slag is guided and which centrifugally separates the slag from the water, and a pressure container (51) for accommodating the cyclon...
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WO/2017/138320A1 |
A compressed air energy storage generation device 2 is provided with: a motor 12; a hydraulic compressor 14; a pressure accumulator tank 18; an expander 20; and an electric generator 22. The device 2 is also provided with a generating-ai...
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WO/2017/139729A1 |
A method and aircraft for providing bleed air to environmental control systems of an aircraft using a gas turbine engine, including determining a bleed air demand for the environmental control systems, supplying low pressure and high pre...
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WO/2017/133872A1 |
The invention relates to a method for compensating for the axial force of a rotor (2) of a gas turbine (1), having the following steps: - detecting a measurement value in order to characterize the axial thrust of the rotor (2) of the gas...
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WO/2017/133873A1 |
The invention relates to a gas turbine (1) having an axially adjustable rotor (2), comprising the following components: at least one external compressor air bleed (3) for bleeding compressor air; a control valve (4) for adjusting the amo...
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WO/2017/134505A1 |
The present invention relates to a system for producing energy from sewage and agricultural and domestic waste by means of four apparatuses. The waste or product from each apparatus is used as feedstock or a catalyst in a process carried...
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WO/2017/126383A1 |
A gas turbine cooling system (50) is provided with a cooling air line (51) for guiding compressed air compressed in an air compressor (10) to high-temperature components, a cooler (63) for cooling the compressed air in the cooling air li...
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WO/2017/125186A1 |
The invention relates to a turbocharger (1) comprising a turbine (3) to which emissions can be supplied by two fluid ducts (5, 6) between which a separation wall (7) extends; a closeable fluid connection hole (4) in the separation wall (...
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WO/2017/123686A1 |
A gas turbine system includes a gas turbine engine, an exhaust processing system disposed downstream of and fluidly coupled to the gas turbine engine, and an air delivery system that may supply treated air to the gas turbine engine and t...
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WO/2017/122468A1 |
A function-of-state acquisition unit acquires the function of state of a turbine. A time calculation unit calculates the time period of possible operation of a turbine in an over-firing operation, on the basis of the function of state an...
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WO/2017/122469A1 |
A function-of-state acquisition unit acquires the function of state of a turbine, including turbine temperature. A variable calculation unit calculates past variables pertaining to the history of the function of state. A time calculation...
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WO/2017/120031A1 |
A turbocharger (119) for use with an internal combustion engine (100) includes a compressor wheel (213) having a central hub (302) having a centerline, a root portion and an end portion. A plurality of blades (308) is formed around the c...
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WO/2017/120030A1 |
A compressor (136) for a turbocharger (119) for use with an internal combustion engine (100) includes a compressor wheel (213) having a central hub (302) having a centerline, a root portion, and an end portion. A plurality of blades (308...
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WO/2017/120032A1 |
A compressor (136) in a turbocharger (119) for an internal combustion engine (100) includes a compressor wheel (213) that includes a central hub (302) having a centerline, a root portion and an end portion. A plurality of blades (308) is...
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WO/2017/105525A1 |
Bypass air from downstream of the compressor is directed into a heat exchanger that draws heat from the exhaust gas of the engine. The bypass air does not include fuel, and instead is heated by the exhaust gas in the heat exchanger. The ...
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WO/2017/098782A1 |
This fuel cell system is provided with: a fuel cell; an electric compressor that supplies a cathode gas to the fuel cell; a cathode exhaust gas passage through which flows a cathode exhaust gas discharged from the fuel cell; a turbine pr...
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WO/2017/097294A1 |
The invention relates to a bearing assembly for a compressor of an internal combustion engine. The bearing assembly comprises an outer ring (3) having an outer cylindrical surface with a first and a second axial section (14, 15). The bea...
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WO/2017/093768A1 |
A system comprising two or more thermal stores, a single store for pressurised air and a means of collecting relatively low-grade heat offers the potential for an energy storage system that achieves two desirable aims at the same time: (...
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WO/2017/095628A1 |
An inlet swirl device (78) is located upstream of the compressor of a turbocharger. The inlet swirl device selectively influences the flow by inducing a swirl motion. In a number of variations, the geometry of the blades (84) are modifie...
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WO/2017/089730A1 |
The invention relates to a turbomachine (24) of "open rotor" or turboprop type, comprising a nacelle (26) defining an air inlet (28), a central hub (30) and an annular air intake duct (32) surrounding the central hub (30) and opening int...
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WO/2017/090709A1 |
A gas turbine (1) is provided with a compressor (10), a turbine (30), a bleed line (61), and a component introducing line (66). The bleed line (61) extracts, as bleed air, compressed air from an intermediate compression stage (19a) of th...
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WO/2017/084876A1 |
A gas turbine system comprising a source (3) of ammonia and a source (1) of an oxygen-containing gas; a first combustion chamber (2) connected to receive ammonia, a hydrogen-rich gas stream (24) and oxygen-containing gas; a turbine (6) c...
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WO/2017/080924A1 |
The device serves for sealing off a bearing housing (10), which accommodates a lubricating oil, of an exhaust-gas turbocharger having a rotor (2) which is led through the bearing housing in the direction of an adjoining compressor housin...
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WO/2017/077305A1 |
An aircraft environmental control system (4) for controlling a temperature of a fluid, the control system (4) comprising: a first temperature sensor (30) configured to measure a first temperature and to generate a first signal, the first...
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WO/2017/076943A1 |
The device is used to separate lubricating oil streams within a bearing housing (10), which receives lubricating oil, of a turbocharger, which comprises an axial turbine and which has a shaft (11) that is led from a compressor housing to...
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WO/2017/078589A1 |
Herein a four stroke internal combustion engine (2) is disclosed. The internal combustion engine (2) comprises at least one cylinder arrangement (4), an exhaust conduit (6), and at least one turbine. The cylinder arrangement (4) comprise...
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WO/2017/077309A1 |
An aircraft environmental control system (4) for controlling a temperature of a fluid, the control system (4) comprising: a temperature sensor (30) configured to measure a temperature of the fluid and to generate a signal, the first sign...
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WO/2017/077867A1 |
A compressed air energy storage power generation device 2 equipped with: a compressor 10 mechanically connected to a motor 30; a first pressure storage tank 12 storing compressed air from the compressor 10; an expansion device 14 driven ...
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WO/2017/073433A1 |
A heat pump 2 is provided with: a motor 6 driven by input power; a first compressor 8 that is mechanically connected to the motor 6 and compresses air; a first heat exchanger 14 for exchanging heat between water and compressed air compre...
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WO/2017/068911A1 |
Provided is a power supply system provided with an energy storage device and a power generation device in which fuel and renewable energy are used for a regional system linked to an external power system, wherein the power supply system ...
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WO/2017/067635A1 |
The invention relates to a controller for an exhaust gas turbocharger comprising an exhaust gas pipe section (2) through which a flow can pass, a bearing section, and a flow-through air guiding section (13), wherein the exhaust gas pipe ...
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WO/2017/069922A1 |
Apparatus, systems, and methods store energy by liquefying a gas such as air, for example, and then recover the energy by regasifying the liquid and combusting or otherwise reacting the gas with a fuel to drive a heat engine. The process...
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WO/2017/060086A1 |
The invention relates to a method for introducing a balancing mark into the compressor wheel of a turbocharger. According to the method, a milling tool is first moved in a first direction in order to introduce a recess into the compresso...
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WO/2017/055765A1 |
The invention relates to a device (10) for de-icing an air intake lip (12) of an aircraft turbojet engine nacelle (14), the device (10) comprising a de-icing circuit in which a heat transfer fluid (22) circulates, said heat transfer flui...
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WO/2017/055766A1 |
The invention relates to a device (10) for de-icing an air intake lip (12) of an aircraft turbojet engine nacelle (14), the device (10) comprising a de-icing circuit in which a heat transfer fluid (22) circulates, said heat transfer flui...
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WO/2017/057144A1 |
A compressed air storage power generation device 2 is provided with a motor 8a, a compressor 10, a pressure accumulation tank 12, an expander 14, a generator 16, a first heat exchanger 18a and a cold takeout part 13. The motor 8a is driv...
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WO/2017/054971A1 |
The invention is related to a compressor arrangement (100) and a gas turbine engine comprising such a compressor arrangement (100). The compressor arrangement (100) comprises a main compressor section (10), which again comprises boundary...
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WO/2017/050502A1 |
The invention relates to a method for assembling a rolling bearing onto a rotor of a turbocharger, having the following steps: introducing a mounting sleeve into the intermediate space between two rolling bearings of the rotor, comprisin...
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WO/2017/048192A1 |
A power generation system comprising: a liquefied natural gas (LNG) regasification unit configured to perform a regasification process to regasify LNG supplied from an LNG source to produce natural gas, the regasification process produci...
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WO/2017/048568A1 |
A cartridge for use in a pulse energy enhanced turbine of a turbocharger. At least first and second fixed separating blades (12) are provided between a nozzle ring (6) and a disk (29), the separating blades (12) maintaining separation of...
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WO/2017/048611A1 |
A number of variations may include a product comprising: a vane lever comprising a first end; a second end; a top surface; and a bottom surface; and an opening defined by an inner surface which extends through the top surface and the bot...
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WO/2017/045738A1 |
The invention relates to a turbine wheel (10) for a turbine of an exhaust gas turbocharger, comprising at least one turbine blade (14) against which exhaust gas can flow; the maximum ratio of the wheel outlet diameter (A) of the turbine ...
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WO/2016/029184A9 |
The present disclosure relates to a power generation system (100), and a related method of power generation, that use closed supercritical fluid cycles (106), and in particular, to a power generation system and related methods where mult...
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WO/2017/042122A1 |
A compressed air energy storage system (1) is described, comprising a compressor (3) fluidly coupled to a compressed air reservoir (9) and an expansion train (10) comprising at least a first turbine (7). The system (1) further comprises ...
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WO/2017/042448A1 |
Casing for rotary machines, in particular for turbomachines, comprising a chamber (2) intended to house a turbine, and a gas circulation duct (3) opening into said chamber, the casing having at least one cavity (4) surrounding at least p...
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WO/2017/042872A1 |
The present invention achieves an integrated life-saving system technology which can efficiently use the simple oxygen generating properties and high energy storage qualities of nitrous oxide (N2O) that is used, for example, as a tranqui...
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