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Matches 1 - 50 out of 7,692

Document Document Title
WO/2017/160154A1
A process for generating power using a gas turbine, comprising the steps of: (i) vaporising and pre-heating liquid ammonia to produce pre-heated ammonia gas; (ii) introducing the pre-heated ammonia gas into an ammonia-cracking device sui...  
WO/2017/160200A1
The present invention relates to a compressor arrangement in an air line (9) supplying charged air to a combustion engine (2). The compressor arrangement comprises a compressor unit (14) comprising a housing (15) including an air intake ...  
WO/2017/159149A1
This CAES power generation apparatus 2 is provided with: a motor 14 which is driven by electricity generated using renewable energy; a compressor 16 which is driven by the motor 14; a pressure accumulator tank 20 which stores compressed ...  
WO/2017/159397A1
A multistage axial compressor according to the present invention is provided with a rotating shaft to which a plurality of moving blades is attached, a casing that surrounds the rotating shaft and that forms a flow path for a working flu...  
WO/2017/158378A1
The turbine arrangement includes a turbine including a turbine housing which defines a turbine cavity within which a turbine wheel is supported for rotation, a turbine inlet upstream of the turbine wheel and a turbine outlet downstream o...  
WO/2017/154459A1
A compressed air storage power generation device 2 is provided with a third heat exchanger 30 and fourth heat exchangers 40a, 40b. The third heat exchanger 30 exchanges heat between air exhausted from an expander 24 and a second heat med...  
WO/2017/148630A1
The invention relates to a rotor (01) for use in a gas turbine, comprising a plurality of compressor segments (21), a plurality of central segments (31), and a plurality of turbine segments (41); the compressor segments (21) and the turb...  
WO/2017/147810A1
Provided is a power generating system using multiple gas channels for power generation, comprising a central control unit (11), and a power generating mechanism electrically connected to the central control unit (11). The power generatin...  
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...  
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)...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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 (...  
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...  
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...  
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...  
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...  
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...  
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...  
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 ...  
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...  
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...  
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: (...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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 ...  
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...  
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 ...  
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 ...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  

Matches 1 - 50 out of 7,692