| Document |
Document Title |
|
WO/2016/146945A1 |
The invention relates to a system (100) for producing energy or torque, comprising: a generator designed so as to generate energy or torque from a gas introduced at an admission of the generator; at least two compressors (101, 102) for c...
|
|
WO/2016/146939A1 |
The invention relates to a power package (1) comprising a gas turbine assembly (20) and a piston engine assembly (30), the power package (1) being characterised in that the piston engine assembly (30) is mechanically coupled to the gas t...
|
|
WO/2016/146282A1 |
The invention relates to a turbocharger (2) for a motor vehicle, comprising a housing (4) and a valve seat (12) in the housing (4); the valve seat (12) is retained in an interlocking manner in the housing (4) by means of at least one ela...
|
|
WO/2016/146285A1 |
Exhaust-gas turbocharger (1) for an internal combustion engine, having a turbine housing (2), in which a turbine wheel (3) with a shaft (4) is arranged rotatably, wherein the shaft is mounted rotatably in a bearing housing (5) by means o...
|
|
WO/2016/146189A1 |
The invention relates to a turbocharger comprising a hydrodynamic sliding bearing having a rotor and a stator, the rotor being rotatable relative to the stator. The bearing surface of the rotor lies opposite a mating surface of the stato...
|
|
WO/2016/142241A2 |
The invention relates to a turbine wheel assembly (1) for a turbine, in particular a waste heat recovery device, comprising - a turbine wheel (2), - a magnetic coupling (4) having a first and a second rotor (5, 6), which can each be rota...
|
|
WO/2016/142655A1 |
A method of modulating the power output of a hybrid gas turbine power plant in which a conventional (GT) gas turbine (2, 4, 6) is integrated, via a fluid connection(s) (1A, 9A, 11A) allowing air injection or extraction therefrom, with a ...
|
|
WO/2016/142654A1 |
A hybrid combustion turbine power plant (30) in which a conventional gas turbine (11, 12, 14) is integrated, via a fluid connection (32), with an adiabatic compressed air energy storage system (ACAES) comprising a direct TES (thermal ene...
|
|
WO/2016/139017A1 |
The invention relates to a method together with a system for the surface treatment of a workpiece, wherein a coating is applied to the workpiece and/or the coated workpiece is dried in a working space, wherein exhaust air laden with harm...
|
|
WO/2016/131154A1 |
A compound engine assembly with an engine core including at least one internal combustion engine, a turbine section including a turbine shaft in driving engagement with the engine shaft, and a compressor, and a firewall. The compressor i...
|
|
WO/2016/131502A1 |
The present invention relates to a compressed air storage power plant (20) comprising a compressed air storage unit (5), at least one compressor (1, 3) which is fluidically connected to the compressed air storage unit (5) via at least on...
|
|
WO/2016/131150A1 |
An intake assembly for a compressor providing compressed air to an internal combustion engine core, including an air conduit having at least one heat exchanger extending thereacross, an intake plenum for the compressor, a first intake co...
|
|
WO/2016/131917A1 |
A thermoacoustic engine (100) comprises an acoustic-wave generator (20), a thermoacoustic cell (10) comprising at least one module (10a, 10b, 10c) and a converter (30) converting the amplified acoustic wave into mechanical power. The the...
|
|
WO/2016/131153A1 |
A compound engine assembly with an inlet duct, a compressor, an engine core including at least one internal combustion engine, and a turbine section including a turbine shaft configured to compound power with the engine shaft. The turbin...
|
|
WO/2016/131156A1 |
A compound engine assembly including a compressor, an engine core including at least one rotary internal combustion engine and having an inlet in fluid communication with an outlet of the compressor, a turbine section having an inlet in ...
|
|
WO/2016/131155A1 |
A compound engine assembly with an inlet duct having an inlet surrounded by an inlet lip including at least one conduit extending therethrough, a compressor, an engine core including at least one internal combustion engine, a turbine sec...
|
|
WO/2016/131151A1 |
A compound engine assembly including an air conduit having an inlet in fluid communication with ambient air around the compound engine assembly, a compressor having an inlet in fluid communication with the air conduit, an engine core inc...
|
|
WO/2016/131143A1 |
A compound engine assembly with an engine core including at least one internal combustion engine, a compressor, and a turbine section where the turbine shaft is configured to compound power with the engine shaft. The turbine section may ...
|
|
WO/2016/131149A1 |
A compound engine assembly having an engine core including at least one internal combustion engine in driving engagement with an engine shaft, a compressor having an outlet in fluid communication with an inlet of the engine core and incl...
|
|
WO/2016/132057A1 |
The invention relates to a system (12) for recovering exhaust gas energy from at least one turboshaft engine, comprising a turbine (34) rotatably mounted about a recovery shaft (40), suitable for collecting at least one portion (14) of t...
|
|
WO/2016/131148A1 |
A compound engine assembly with an engine core including at least one internal combustion engine, a turbine section, and a compressor having an outlet in fluid communication with an inlet of the engine core. A casing is connected to the ...
|
|
WO/2016/127228A1 |
The modular complex for production of effective power through combustion of liquid and gaseous fuels comprises two modules: Module for production of heat in a single combustion chamber for burning various liquid and gaseous fuel types, c...
|
|
WO/2016/120750A1 |
Compressed gas energy storage systems, which include an integrated thermal energy storage component, are provided. The systems include a compression stage, a heat transfer unit, and a gas storage reservoir, serially linked in fluid commu...
|
|
WO/2016/121684A1 |
A cooling system (60) is provided with a high-pressure bleed line (61) for bleeding high-pressure compressed air (A1) from a first bleed position (Pb1) of a compressor (10) and sending the air to a first high-temperature component (44a),...
|
|
WO/2016/113489A1 |
The invention relates to a device for controlling an auxiliary engine (8) including a gas generator and a free turbine suitable for being connected mechanically to the rotor (12) of a helicopter in order to supply same with thrust power,...
|
|
WO/2016/104222A1 |
A compressed-air-storing power generation device 2 is provided with a first heat exchanger 16, a heat storage tank 20, a second heat exchanger 18, a heater 22, a first power distributor 24, and a control device 26. The first heat exchang...
|
|
WO/2016/103382A1 |
This combined cycle plant comprises a plurality of turbine devices (11) and connection lines (12). Each of the turbine devices (11) is provided with: a gas turbine unit (15) which includes a gas turbine (21), a first compressor (22), and...
|
|
WO/2016/102878A1 |
The invention relates to a method for detecting a high temperature fluid leak in a turbomachine (10). The turbomachine (10) comprises a source of high temperature pressurised fluid, at least one fluid distribution line (14, 15) suitable ...
|
|
WO/2016/102137A1 |
The turbomachine comprises a casing (26), there being arranged in the casing an impeller (23) arranged on a driven shaft. The turbomachine has an inflow region (21) and an outflow region (22) and, in operation, is flowed through by a wor...
|
|
WO/2016/098156A1 |
This gas turbine power generation system 100 includes: a two-shaft gas turbine 1; a power generator 2 that is driven by the two-shaft gas turbine 1 and that generates power; an electric motor 3 that is driven by power generated by the po...
|
|
WO/2016/098220A1 |
The gas turbine power generation system of the present invention repeats either the supply or absorption of power, in addition to generating power. The gas turbine power generation system is provided with a first rotation shaft, a compre...
|
|
WO/2016/098266A1 |
A gas turbine power generation system having an improved function to stabilize the power system is disclosed. The gas turbine power generation system has a dual-shaft gas turbine, an electric generator mechanically connected to a low pre...
|
|
WO/2016/095940A1 |
The invention relates to a turbocharger having a swing vane nozzle assembly - VGT - (120). The turbocharger (100) comprises a turbine housing (102) and a bearing housing (104). The swing vane nozzle assembly (120) comprises a front nozzl...
|
|
WO/2016/091348A1 |
The invention relates to a turbomachine (10) for an energy converter, in particular a fuel cell, wherein the turbomachine has a compressor (12) for compressing air to be fed to the energy converter, comprising at least one housing elemen...
|
|
WO/2016/091475A1 |
The invention relates to a device for temporarily storing gas and heat, comprising at least one pressure container (10), multiple compressors (3, 8, 9), by means of which a gas (1) can be compressed, and multiple compression stages, whic...
|
|
WO/2016/089659A1 |
An energy storage system includes an intercooler coupled to an axial compressor and a multi-stage radial compressor including a first stage radial compressor and a second stage radial compressor, coupled to the intercooler. The energy st...
|
|
WO/2016/087125A1 |
The invention relates to a supercharger device and to a method for operating said supercharger device for an internal combustion engine (1), comprising an exhaust gas turbocharger (4) and a recuperation charger (12) which has a compresso...
|
|
WO/2016/083004A1 |
The invention relates to a supercharging device and to an operating method for said supercharging device for an internal combustion engine (1), which supercharging device has an exhaust-gas turbocharger (4) and a recuperation charger (12...
|
|
WO/2016/083732A1 |
The invention concerns a turbomachine (10), comprising:- a discharge device (62) of a compressor (56), in particular a high-pressure compressor, comprising at least one discharge valve (66) of said compressor (56) of which one outlet is ...
|
|
WO/2016/078444A1 |
Disclosed are a variable geometry wastegate turbine meeting the requirements of EGR circulation and a guide vane assembly, wherein the guide vane assembly comprises a guide vane support disk which is provided on a power turbine wheel int...
|
|
WO/2016/079523A1 |
In an effort to increase the reliability and net power and efficiency benefit of the axial-and mixed-flow turbocharger turbine, there is provided, a tapered, axially translatable ("sliding nozzle") flow restrictor member (197) to provide...
|
|
WO/2016/079454A1 |
The invention relates to a device forming a seal for a relief valve in a turbine engine, the valve comprising: a gate intended for being mounted mobile between a position for sealing an air port made inside a casing of the turbine engine...
|
|
WO/2016/079485A1 |
A waste heat recovery system suitable for high temperature gases above 400°C is combined with compressed air energy storage. Atmospheric air is compressed in a multistage compression process using intercoolers and an aftercooler which t...
|
|
WO/2016/071040A1 |
The present invention relates to an optimized propulsion system comprising at least one turbomachine (2) and a supercharged internal combustion engine (1) which are mechanically coupled. According to the invention, the propulsion system ...
|
|
WO/2016/072998A1 |
A compressor includes a purge flow extraction path extending radially and configured to direct an airflow radially inwardly. Also included is a center bore at least partially defined by a rotor structure extending axially and fluidly cou...
|
|
WO/2016/066539A1 |
The invention relates to a gas turbine (10) having at least one discharge line (20) for discharging compressor air, in particular discharge air of the compressor, which is fluidically connected to an impulse braking device (30) such that...
|
|
WO/2016/068861A1 |
The present disclosure provides a combined cycle power plant (10) comprising a gas turbine (26), a heat-recovery steam generator (34) receiving exhaust gas (33) from the gas turbine (26) for producing steam (35), a steam turbine (32) rec...
|
|
WO/2016/057112A1 |
A centrifugal compressor diffuser (42) includes a plurality of diffuser flow passages (22) extending through an annular diffuser housing (20) and circumferentially bounded by diffuser vanes (23) and axially bounded by forward and aft wal...
|
|
WO/2016/055278A1 |
A (micro) gas turbine arrangement has a gas turbine device (12) with a combustion chamber system (28), a turbine (30) driven by an exhaust gas stream (32) from the combustion chamber system, and a compressor (22) for supplying the combus...
|
|
WO/2016/057262A1 |
A variable turbine geometry turbine (20) includes a flow control device (100). The device (100) includes vanes (114) that are fixed to the turbine housing (22) and protrude into the throat (34) between the turbine volute (26) and turbine...
|
