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WO/2018/146405A1 |
The invention relates to a turbofan (1) comprising a low-pressure compressor (3); a series of housings (9, 10) arranged downstream of said low-pressure compressor (3) for defining a primary stream, and comprising an upstream edge (19) de...
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WO/2018/144080A1 |
Systems and methods for integrated power and thermal management in a turbine-powered aircraft are provided. The systems may include rotationally-independent first and second auxiliary power unit shafts, a power turbine, a first compresso...
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WO/2018/144513A1 |
The invention relates to a housing assembly comprising a housing that has at least one first connection opening and one second connection opening, a first connecting piece with a first flange and a second connecting piece with a second f...
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WO/2018/140130A2 |
The turbine includes a first turbine rotor disc, a second turbine rotor disc, a first source of cooling fluid, and a first cooling fluid conduit. The first turbine rotor disc has a first outer circumference and a first plurality of blade...
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WO/2018/139646A1 |
A plant provided with: a fuel supply line for supplying high-pressure fuel gas; and at least one expander which is disposed in the fuel supply line and configured to extract power from the high-pressure fuel gas by expanding the high-pre...
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WO/2018/136291A1 |
A method of monitoring a turbomachinery is disclosed herein. The method includes measuring the pressure drop across the intake filter (66). The method further includes determining clog rate parameters for a clog rate of a filter area of ...
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WO/2018/129277A1 |
A turbocharger (100) includes a turbine wheel (110), a compressor wheel (140), a shaft (160) coupled to the turbine wheel (110) and the compressor wheel (140), and a thrust bearing (186). The thrust bearing (186) includes a loaded side (...
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WO/2018/125638A2 |
A power generation system comprising a shared hot side thermal store, a shared cold side thermal store, a plurality of power subunits, and an electrical bus is disclosed. Each of the power subunits may connected or isolated from the shar...
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WO/2018/125450A1 |
Thermocline arrays comprising a plurality of pressure vessels that are in used in place of heat exchangers in a closed thermodynamic cycle system, such as a closed Brayton cycle power generation or energy storage system. Each pressure ve...
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WO/2018/125471A1 |
Solid-state thermoclines with internal baffle structures are in used in place of heat exchangers in a closed thermodynamic cycle power generation or energy storage system, such as a closed Brayton cycle system. The baffles limit the cond...
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WO/2018/119922A1 |
A combined cycle power generation system (10) capable of recovering tail gas heat energy of a gas turbine and LNG cold energy, comprising a combustion chamber (14), a turbine (16), and an air compressor (18). The air compressor is drivin...
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WO/2018/122538A1 |
The invention relates to an intermediate housing hub (2) comprising a discharge stream conduit (18) having a given length (L1), and discharge fins (22) extendng in the discharge stream conduit (18) and having a given chord length (L2), t...
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WO/2018/119391A1 |
A turbine wheel (100) for a turbocharger includes a hub (110) and blades (120). The hub includes a primary outer surface (116), a back wall surface (115), a peripheral edge (119) extending between the primary outer surface and the back w...
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WO/2018/110473A1 |
Disclosed is a gas turbine engine system (S) comprising: a transmission (9) that changes the speed of a rotary output of an output shaft (7) of a gas turbine (GT), and transmits the rotary output to a load device (GE) which is to be driv...
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WO/2018/111665A1 |
In one aspect, a power generation system may include a core turbine engine, an electric generator, an electric motor, and an auxiliary compressor. The core turbine engine defines an axial direction, and may include a compressor and a tur...
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WO/2018/105133A1 |
Provided is a hydrogen fluid closed cycle device that includes (1) a hydrogen gas generator which generates hydrogen gas, (2) a hydrogen gas heating device and a temporary storage tank which raise the pressure of the hydrogen gas by rais...
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WO/2018/106331A1 |
An electric machine is provided which includes a rotor disk extending along a radial direction and having a rotor flange attached to or formed integrally with the rotor disk and extending substantially along the axial direction. A plural...
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WO/2018/107006A1 |
Disclosed are methods useful in applications relating to blast furnace processes. The methods of the present invention provide enhanced deposition inhibition of particulate matter in top-pressure recovery turbines. The methods of the pre...
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WO/2018/106528A1 |
A waste heat recovery system including a drive unit, the drive unit having a drive shaft, a compressor, the compressor operably coupled to the drive shaft, wherein operation of the drive unit drives the compressor, and a waste heat recov...
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WO/2018/106359A1 |
An aircraft has a gas turbine engine including a compressor section that includes at least one compressor bleed. An environmental control system has an air input configured to receive pressurized cabin air. An intercooler has an input an...
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WO/2018/100033A1 |
The invention provides a vehicle engine system, comprising: a hydraulic pump for providing an oil supply during braking; an accumulator configured to : receive the oil supply during braking; store the oil supply under pressure; and relea...
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WO/2018/102268A1 |
A turbocharger (100) includes a turbine wheel (110), a compressor wheel (140), and a shaft (160) coupled to the turbine wheel (110) and the compressor wheel (140). The turbocharger (100) additionally includes a bearing housing (170) cont...
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WO/2018/101989A1 |
System for storage of electricity in the form of thermal energy, and release of thermal energy during times of demand. The system includes a unit for containing at least one electrically conducting phase change material and electrical ci...
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WO/2018/099618A1 |
The invention relates to a turbocharger, comprising a turbine for expanding a first medium and a compressor for compressing a second medium by using energy obtained in the turbine as the first medium is expanded, wherein the turbine has ...
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WO/2018/102244A1 |
The invention relates to a turbine with variable turbine geometry for an internal combustion engine. The turbine comprises a bearing housing, a turbine housing, and a cartridge which has a blade bearing ring for mounting a plurality of a...
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WO/2018/096239A1 |
Bypass turbomachine (30) comprising a system (46) for bleeding gas from a primary stream to a secondary stream, said system comprising two coaxial rings (54, 56) extending one around the other, a perforated internal first ring (54) situa...
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WO/2018/087478A1 |
The invention relates to a turboprop engine (19) comprising a propeller shaft (21) and a gas generator (22) which runs along the propeller shaft (21), the gas generator (22) comprising a high pressure shaft (24) and a hollow low pressure...
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WO/2018/087694A1 |
The present disclosure relates to systems and methods useful for power production. In particular, a power production cycle, comprising a first combustor (102) and a turbine (103), utilizing CO2 as a working fluid may be configured for si...
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WO/2018/088184A1 |
The gas turbine plant is provided with a gas turbine (10), a heating device (60), a decomposition gas line (70), and a decomposition gas compressor (85). The heating device (60) heats ammonia so that the ammonia is pyrolyzed and decompos...
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WO/2018/077963A1 |
The invention relates to a system having a primary current generating assembly (10) comprising a primary thermal engine (7) and having a secondary current generating assembly (9), in particular an electric turbo compound installation, fo...
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WO/2018/076926A1 |
An engine driven by gunpowder, relating to the technical field of engines and comprising an engine, a gas storing bag (3), a draft fan (6) and a gunpowder burner; the engine comprises an engine housing (1) which is provided therein with ...
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WO/2018/077839A1 |
The gas turbine system (101) comprises: a compressor section (10) with a main inlet, a main outlet, and a bleed outlet (15), a combustor section (20) with a main inlet fluidly connected to the main outlet of the compressor section (10), ...
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WO/2018/072860A1 |
The invention relates to a turbine (10) for a turbocharger, having a turbine casing (12) and having a turbine wheel (14), which is accommodated in a rotatable manner in the turbine casing (12), has a plurality of runner blades (20) and c...
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WO/2018/073608A1 |
A method is proposed for designing a turbine of a turbocharger of an engine system having an exhaust gas recirculation (EGR) path. At at least one engine speed, such as the peak torque speed, a pressure drop along the EGR path is determi...
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WO/2018/070394A1 |
The purpose of the present invention is to provide a furnace wall in which a throat section with a smaller channel diameter than other regions can be formed using all peripheral wall pipes. Provided is a furnace wall comprising: a plural...
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WO/2018/067345A1 |
A method of assembling an electrified turbocharger comprising assembling a rotor assembly onto a shaft; balancing the shaft and rotor assembly; attaching at least one bearing onto the shaft adjacent the rotor assembly; inserting a stator...
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WO/2018/059804A1 |
The invention is related to a gas turbine arrangement for at least dual fuel operation, comprising a plurality of fuel manifolds (21,22,23), each connected to each of at least one combustor (12) and a control system (17). A first manifol...
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WO/2018/060030A1 |
A rotating device for a compressor of a gas turbine is presented. The rotating device, connectible with the compressor, includes a first shaft, a second shaft, rotatable blades, a bearing assembly, an external drive and an input port for...
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WO/2018/060068A1 |
The invention relates to an impeller (14) for a continuous-flow machine (10), in particular a radial continuous-flow machine. The impeller (14) has a number of blades (16), which are received spaced apart from each other on the circumfer...
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WO/2018/059726A1 |
The invention relates to a turbine (26) for an exhaust gas turbocharger (24) of an internal combustion engine (10), having a turbine housing (30) which has a receiving region (32), having a turbine wheel (34) which is arranged at least p...
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WO/2018/055375A1 |
A mixed-flow turbine wheel (214) is proposed which, compared to existing mixed-flow turbine wheels, has reduced mass and moment of inertia because radially-outer portions of existing mixed-flow turbine wheels are omitted. In a first poss...
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WO/2018/050455A1 |
- The invention relates to a container for storing a pressurised fluid such as compressed air. In particular, the container is in the form of at least one tube formed from an arrangement of concentric layers (C1, C2, C3, C4), this arrang...
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WO/2018/051127A1 |
There is provided a system and method for guiding a flow of fluid having a variable mass flow rate onto a turbine (110), the turbine comprising a blade (115) and configured to rotate about an axis of rotation (150), the method using a fl...
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WO/2018/050347A1 |
The invention relates to a turbocharger (1) for an internal combustion engine, which has a bearing housing (41), in which a rotor shaft (14) is rotatably mounted; a compressor (30) having a compressor wheel (13), which is arranged for co...
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WO/2018/051080A1 |
A radial flow gas turbine generator (10) where the gas turbine generator (10) includes a shaft (30) having a rotor (20) of the generator (10), a compressor wheel (16) and a turbine wheel (18) fixed thereto. The shaft (30) is supported fo...
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WO/2018/046181A1 |
The invention relates to an expansion machine (11), comprising a machine housing (20) having a rotatably mounted shaft (21) carrying a rotor (22), wherein a medium is supplied to the rotor (22) during operation, and a rotor (22) having a...
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WO/2018/044558A1 |
The invention relates to the compression of a pyrolysis product to facilitate light olefin separation. The pyrolysis product is produced in a pyrolysis reaction. A power generator produces a first shaft power and a second shaft power. Th...
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WO/2018/043568A1 |
This two-shaft gas turbine equipment is provided with: an induction motor (22) which transmits and receives power to and from an external system (1); and a speed reducer (40) which makes the rotational speed of a motor rotor (22r) of the...
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WO/2018/045153A1 |
A turbocharger includes a compressor and an airflow adjustment assembly. The airflow adjustment assembly includes a plurality of guide vanes. Each of the plurality of guide vanes has a guide tip and a guide base spaced from the guide tip...
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WO/2018/038992A1 |
A gas turbine engine includes a compressor section and a turbine section together defining a core air flowpath. The rotary component is rotatable with the compressor section and the turbine section. The gas turbine engine additionally in...
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