| Document |
Document Title |
|
WO/2016/031475A1 |
An axial-direction passage (45), a forced vortex passage (46), a first blade array passage (47), and a second blade array passage (48) are formed in a rotor shaft (32) of a turbine (30). Cooling air from an air extraction port (16) of a ...
|
|
WO/2016/030282A1 |
The invention relates to a turbine (1) for an internal combustion engine. The turbine (1) is arranged in an exhaust gas tract of the internal combustion engine and converts flow energy of a fluid of the internal combustion engine into me...
|
|
WO/2016/031821A1 |
This compressed fluid storage power generation device (10) is provided with: a compressor (11) having an electric motor (34) and compressor bodies (22, 24) for compressing a working fluid by being driven by the electric motor (34); a pre...
|
|
WO/2016/030351A1 |
The invention relates to a combined heat and power plant (10) for the decentralized supply of power and of heat, having at least one prime mover (12), by means of which electrical energy can be provided whilst providing waste gas, having...
|
|
WO/2016/028501A1 |
The invention relates to an exhaust-gas turbocharger (1) having a charger shaft (2); and having a bearing housing (3), which comprises a radical bearing arrangement (4), characterized in that the charger shaft (2) has a groove (10; 11; 1...
|
|
WO/2016/024447A1 |
Provided is an integrated coal gasification combined cycle power generation facility (1) equipped with: a gasification furnace (20) that generates combustible gas from pulverized coal; a gas cooler (30); gas turbine equipment (50); an au...
|
|
WO/2016/018959A1 |
A turbocharger (100) includes a two-piece thrust collar that includes inner and outer portions (136 and 138) disposed around a rotatable shaft (120). The inner portion (136) is engaged with a bushing disposed in and connected to the cent...
|
|
WO/2016/012688A1 |
The invention relates to an electronic device, in particular intended for supplying an electric machine, including two vertically adjacent electronic boards (54, 56) and a rigid intermediate portion (10) arranged between said two electro...
|
|
WO/2016/012764A1 |
A compressed air energy storage and recovery system involves at least two stages of compression and expansion and at least two stages of heat removal and restoration using heat exchangers and two different thermal fluids are used at diff...
|
|
WO/2016/012666A1 |
The invention relates to an electrical supercharger including: - a housing; - a rotary electrical machine; - a compression member coupled with said rotary electrical machine; and - an electronic device for supplying electrical power to t...
|
|
WO/2016/010764A1 |
An adjustment ring (50) is configured to facilitate vane (30) position adjustment in a variable turbine geometry turbocharger (1), and is formed of an assembly of one or more first ring portions (60) that are formed of a first material, ...
|
|
WO/2015/187423A9 |
A solar hybrid power plant comprises a combustion turbine generator, a steam power system, a solar thermal system, and an energy storage system. Heat from the solar thermal system, from the energy storage system, or from the solar therma...
|
|
WO/2016/010847A1 |
The invention relates to an exhaust-gas turbocharger (1) having a turbine housing (2) which has a turbine housing outer surface (3) and which has a spiral (4) and a turbine housing outlet (11), and having turbine housing thermal insulati...
|
|
WO/2016/001117A1 |
In this device (1) for generating electrical energy, a pressurized fluid (6) flows from a pressurized fluid container (5) to a turbine generator unit (3) that generates electrical energy. The pressurized fluid (6) cools when flowing out,...
|
|
WO/2016/003935A1 |
In one embodiment, a system includes a drive train starter system. The drive train starter system includes a generator mechanically coupled to a drive train of a gas turbine system and an exciter system electrically coupled to the genera...
|
|
WO/2016/001000A1 |
The invention relates to an AACAES system and method wherein beads are used to store heat. The heat exchange is carried out by means of at least one radial heat exchanger (3), wherein the beads and a first fluid (F1) circulate, the first...
|
|
WO/2016/001001A1 |
The invention relates to an AACAES system and method wherein a heat-transfer fluid is used to store heat. The heat-transfer fluid, comprising beads made of heat-storage material, circulates between two tanks - a hot tank (6) and a cold t...
|
|
WO/2016/000732A1 |
The invention relates to a turbocharger unit (100) for recovering energy of exhaust gases of an internal combustion engine (10), wherein the turbocharger unit (100) comprises a turbine (104a) enclosed in a turbine housing (104b), a compr...
|
|
WO/2016/003932A1 |
In a gas turbine system (52) having an exhaust gas recirculation system (54) receiving exhaust from the gas turbine system and recycling the exhaust gas back to the gas turbine system, a blower (580) with variable guide vanes (586) is po...
|
|
WO/2016/004021A1 |
Methods and devices for cooling systems (700) are provided that are in fluid communication with bleed air from a jet engine compressor. The cooling system can include: a first precooler (210) recieving bleed air from the jet engine compr...
|
|
WO/2016/001381A1 |
The invention relates to a turbocharger unit (100) for recovering energy of exhaust gases of an internal combustion engine (10), wherein the turbocharger unit (100) comprises a turbine (104a) enclosed in a turbine housing (104b), a compr...
|
|
WO/2016/004023A1 |
Methods and devices for cooling systems (100, 700) are provided that are in fluid communication with bleed air from a jet engine compressor. The cooling systems include: a first precooler (210) recieving bleed air from the jet engine com...
|
|
WO/2016/001002A1 |
A flow straightener consisting of profiled guiding elements (31) on the interior inner wall (6) of the flow channel in the diffusor region of an axial turbine prevents flow separation on the contour of the inner wall of the diffusor.
|
|
WO/2015/197315A1 |
The invention relates to a turbocharger (1), comprising a compressor, a turbine (12), a shaft (2), and at least two ball bearings (3, 4), in which the shaft (2) is supported, wherein the shaft (2) is formed of two shaft parts (6, 7), whi...
|
|
WO/2015/195343A1 |
This disclosure provides a modular construction compressor housing (100, 200, 300) including an outer compressor housing (110, 210, 310) having an outer compressor wheel (160, 260, 260) disposed therein. The outer compressor housing (110...
|
|
WO/2015/191100A1 |
A power generation plant has two internal combustion engines (ICE) coupled in a compound configuration to operate electrical generators. A first ICE is a piston/cylinder engine producing high temperature and high pressure exhaust. The ex...
|
|
WO/2015/191220A1 |
A turbine operable with a first fluid and a second fluid is provided. The turbine includes a shaft and having a dry gas seal area, a balance area, and a shaft surface. The turbine also includes a stationary component coupled to a housing...
|
|
WO/2015/185408A1 |
The invention relates to a spiral turbine casing comprising a spiral casing wall and a base wall. The base wall and the spiral casing wall have a connection which fully extends around a central axis, wherein a portion of the base wall is...
|
|
WO/2015/185880A1 |
An adiabatic compressed air energy storage (ACAES) system comprising: a first compression stage (11), at least a first thermal energy storage TES system (40) for removing and returning thermal energy to compressed air passing through it ...
|
|
WO/2015/185407A1 |
The invention relates to a turbocharger (1), in particular for a motor vehicle, having a compressor (2) which has a compressor wheel (4) arranged on a rotatably mounted shaft (5), wherein in a pipe section (9) of an axial compressor inle...
|
|
WO/2015/178658A1 |
The present invention relates to a layout structure of a floating storage gas power plant and, more specifically, to a layout structure of a floating storage gas power plant, comprising: a cargo system for storing liquefied natural gas i...
|
|
WO/2015/178897A1 |
A method and system for providing a cooling flow from a compressor to a turbine in a gas turbine engine. First, second and third cooling air flows are provided from the compressor through respective ejectors as external bleed air flows t...
|
|
WO/2015/177409A1 |
An object of the present invention is to provide a method and a system for implementing the method so as to alleviate the disadvantages of a reciprocating combustion engine and gas turbine in electric energy production. The invention is ...
|
|
WO/2015/175253A1 |
A wind turbine and compressed gas storage system for producing electrical energy. A plurality of wind turbines is serially interconnected for staged compression to output high pressure compressed gas. Each wind turbine includes an upper ...
|
|
WO/2015/174246A1 |
By using a combustion exhaust gas (18) from a power turbine (16), a high-pressure secondary compressed air (12C) is subjected to heat exchange in a first heat exchange unit (19A) of an exhaust heat recovery device (19), and by using resu...
|
|
WO/2015/164076A1 |
An exhaust gas turbocharger (1) includes a turbine section (2) having a turbine housing (11) and a turbine wheel (4) disposed in the turbine housing (11). The turbine housing (11) defines a fluid inlet (13), a fluid outlet (10), and a vo...
|
|
WO/2015/159956A1 |
An engine (10) that jets out combustion gas as a driving force is provided. This engine (10) has: a combustion chamber (11); a fuel supply passage (13) for supplying a fuel-air mixture into the combustion chamber (11); an igniter (42) fo...
|
|
WO/2015/157012A1 |
The present invention discloses a novel apparatus and methods for augmenting the power of a gas turbine engine, improving gas turbine engine operation, and reducing the response time necessary to meet changing demands of a power plant. I...
|
|
WO/2015/155818A1 |
This floating liquefied-gas production facility (1) is equipped with: a gas turbine unit (20); a liquefaction facility (90) that has a primary refrigeration compressor (40) driven by the gas turbine unit (20), and cools natural gas; a dr...
|
|
WO/2015/154584A1 |
A solar thermal and BIGCC-integrated hybrid power generation system comprising a solar energy concentrating collector system (9), biomass gasification equipment (1), a gas-fired electric generator (7), a steam turbine (13), and a steam e...
|
|
WO/2015/149124A1 |
A combined cycle gas turbine power generating system, comprises: a gas turbine, a heat recovery steam generator; a steam turbine system; an energy storage system which stores energy in the form of heat energy; and a heat energy distribut...
|
|
WO/2015/149904A1 |
The invention relates to a turbine wheel (12) for a turbine, in particular of an exhaust gas turbocharger, comprising a main body (14), to which turbine-wheel blades (10) are connected, which each have at least one thickness and an exten...
|
|
WO/2015/150104A1 |
The invention relates to a system for heat storage and heat exchange between a gas and a solid material, characterised in that it comprises a tank (LF) containing a volume of particles formed from at least the solid material, the gas cir...
|
|
WO/2015/146786A1 |
The present invention is provided with: a compressor (11) that compresses air (A); a combustor (21) that combusts a fuel (F) in the compressed air (A) and generates a combusted gas (G); a plurality of cooled air coolers (54) that extract...
|
|
WO/2015/145034A1 |
The invention concerns an architecture of a propulsion system of a multi-engine helicopter comprising turboshaft engines (5, 6), characterised in that it comprises: at least one hybrid turboshaft engine (5), capable of operating in at le...
|
|
WO/2015/145036A1 |
The invention relates to the architecture of a multi-engine helicopter propulsion system comprising turboshaft engines, each turboshaft engine comprising a gas generator (17, 27) and a free turbine (10, 20) rotated by the gases from the ...
|
|
WO/2015/145031A1 |
The aircraft turbine engine rapid reactivation system includes an electrical machine (60) supplied with DC power by an onboard electrical power supply network (10). The system also includes: - a switch (50) positioned between the onboard...
|
|
WO/2015/146170A1 |
[Problem] To control the temperature of dehydrogenation to an appropriate range to enable efficient and stable hydrogen generation when exhaust gas of power generation is used as a heat source for the dehydrogenation. [Solution] A hydrog...
|
|
WO/2015/145040A1 |
The invention relates to an emergency start device for a helicopter turbine engine (6). Said device is characterized in that it includes: - a hydraulic engine (7) mechanically connected to said turbine engine (6); - a hydropneumatic stor...
|
|
WO/2015/135878A1 |
A turbomachine assembly (1) comprises: -a shaft (10), -a radial gas expander (2) supported on the shaft (10) between at one first bearing (11) and a second bearing (12), -a compressor (3) supported on the shaft(10) in overhung position a...
|
