| Document |
Document Title |
|
WO/2022/029581A1 |
A method for controlling an aircraft (1) capable of hovering is described, comprising a first engine (10a); a second engine (10b); at least one rotor (3); and a transmission (8) interposed between the first and second engine (10a, 10b) a...
|
|
WO/2022/028776A1 |
A shaft bearing assembly (10) having a shaft (11) supported in a bearing housing (12) is described. The shaft bearing assembly (10) includes a pressure reduction device (13) for generating an underpressure inside the bearing housing (12)...
|
|
WO/2022/018385A1 |
The invention relates to a turbine (7) comprising a first rotor (25) and a second rotor (27) capable of pivoting about a longitudinal axis (X) in two opposite directions of rotation, the first rotor (25) comprising a radially outer drum ...
|
|
WO/2022/010344A1 |
The invention provides a solution according to which generated offshore renewable energy can be efficiently stored and recovered at a large scale and at low cost. For that purpose the invention makes use of two offshore underground reser...
|
|
WO/2022/002325A1 |
Operation of an energy storage system comprising a thermodynamic cycle including first and second thermal reservoirs (4,5) and a turbomachinery (1, 2, 3, 1', 2', 3') as energy converter for two-way conversion between electrical energy an...
|
|
WO/2022/004237A1 |
A CAES generation device is provided with: a plurality of motors 15; compressors 11-14 driven by each of the plurality of motors 15 and fluidly connected in multiple stages; an accumulation pressure tank 30 which accumulates compressed a...
|
|
WO/2021/259862A1 |
The invention relates to a modular nozzle ring for a turbine stage of a continuous flow machine. The modular nozzle ring has a carrier system having an an adjustment ring, and a blade module having a blade leaf. The blade module is detac...
|
|
WO/2021/254749A1 |
The invention relates to an intake device (1) for a compressor (2). The intake device (1) comprises a support structure (2) having a plurality of struts (3) which are arranged in the circumferential direction about an axis (4) of the sup...
|
|
WO/2021/250666A1 |
A hydraulic compressed air energy storage system includes air and liquid tanks, each of which includes interdependent volumes of liquid and air. Each tank includes dedicated passages through which incoming air may be fed, forcing outflow...
|
|
WO/2021/243949A1 |
A gas turbine power generation device using viscous force to convert pulse detonation gas energy, comprising an air intake channel (1) and a compressor (2); the air intake channel (1) is located at the front end of the gas turbine, the c...
|
|
WO/2021/243479A1 |
A vehicle-mounted type gas turbine generator set, comprising a chassis (7), a power compartment (4), an electrical compartment (6), a gas inlet filtering system (3), a ventilation filtering system (5), and hydraulic leveling systems (9)....
|
|
WO/2021/229163A1 |
The invention relates to an exhaust case (15) for a turbomachine extending along a longitudinal axis (X), comprising: an annular shroud (23) having a wall (24) extending along the longitudinal axis (X) from a first flange (25), a plurali...
|
|
WO/2021/220742A1 |
A vehicle drive device that makes it possible to reduce the noise generated by a vehicle.　This vehicle drive device 11 comprises an engine 13 and a supercharging device 18 that supercharges the engine 13. When the engine 13 is stopped,...
|
|
WO/2021/219461A1 |
The invention relates to an exhaust gas turbocharger (30) with a silencer. The silencer comprises a multiplicity of damping elements (41) which are arranged concentrically about a central axis (42) of the silencer and are spaced apart co...
|
|
WO/2021/218969A1 |
A vehicle-mounted gas turbine generator set, comprising a chassis vehicle (7), a main box body (C) and at least one of an inlet air filtration system (3), a ventilation and filtration system (5) and an exhaust system (1). The chassis veh...
|
|
WO/2021/205107A1 |
A discharge grid (22) designed to be mounted inside or at the outlet of a line (21) of a discharge valve (20) of a turbomachine (1) of an aircraft, the discharge grid (22) comprising an upstream face (24) designed to receive a gas flow (...
|
|
WO/2021/205120A1 |
An acoustic treatment grid (22) designed to be mounted inside or at the outlet of a line (21) of a discharge valve (20) of a turbomachine (1) of an aircraft, this being designed to convey a gaseous flow (F), the grid (22) comprising a pe...
|
|
WO/2021/168570A1 |
Systems, methods, and devices for energy storage are provided. A system for energy storage includes a thermomechanical-electrical conversion subsystem for converting energy formats and a mechanical and thermal storage unit for storing en...
|
|
WO/2021/163760A1 |
There is provided a compact turbine-compressor assembly 25. The turbine-compressor assembly 25 includes a turbine wheel 39 with one or more turbine blades 41 and a compressor wheel 47 that includes one or more compressor blades 49. The c...
|
|
WO/2021/165823A1 |
Energy storage (10) comprising a first container (20) comprising an inner space, at least one plurality of pressure vessels (40) for compressed air that are stacked in rows inside the inner space of the first container (20), at least one...
|
|
WO/2021/160952A1 |
An electrical assembly for an aeronautical turbine engine, comprising an electric machine (70) configured to be disposed in a turbine engine (100) and comprising a stator (72) and a rotor (71) comprising magnets, the assembly comprising ...
|
|
WO/2021/155881A1 |
The invention relates to an adjustable guide apparatus for an exhaust gas guide section of an exhaust gas turbocharger, comprising a bearing ring (4) having a plurality of guide vanes (5), wherein the guide vanes (5) are rotatably mounte...
|
|
WO/2021/156743A1 |
A compact cooling and boosting gas turbine system provides combined cooling, heating, and electrical power with high energy efficiency. The system has a pressure booster and a turbo-compressor. The pressure booster includes a fuel inlet,...
|
|
WO/2021/158639A1 |
Pumped heat energy storage systems and methods utilizing reversible turbomachines alternately acting as compressor and turbines to reversibly circulate working fluid through heat exchangers, including a hot-side heat exchanger and a cold...
|
|
WO/2021/158641A1 |
Pumped heat energy storage systems that can be used to store and extract electrical energy. A motor/generator system is releasably coupled and decoupled via clutches from a charge mode powertrain and a generation mode powertrain dependin...
|
|
WO/2021/151885A1 |
A reforming process comprising for production of a hydrogen-containing synthesis gas with a thermally integrated gas turbine engine wherein the hot exhaust gas of the gas turbine engine is the heat source for preheating one or more proce...
|
|
WO/2021/146513A1 |
A gas microturbine that includes a closed-loop oil distribution system that includes an oil reservoir, an oil- supply circuit, an oil-scavenge circuit, and a pump. The oil reservoir is configured to contain a provision of oil. The oil-su...
|
|
WO/2021/143416A1 |
A solar gas turbine power generation system employing a photothermal principle comprises a gas turbine (1), a solar energy acquisition apparatus (21), and a solar reflector (2). The gas turbine (1) comprises a pneumatic impeller (102), a...
|
|
WO/2021/140025A1 |
Thermal power station and method for generating electric power in a thermal power station The invention relates to a thermal power station (1) comprising (a) at least one thermal energy storage (10) having a housing (11), a storage chamb...
|
|
WO/2021/139985A1 |
A turbocharging assembly (100) is described. The turbocharging assembly (100) includes a housing (130) having a first housing part (130A) for enclosing a first stage (110), particularly a low-pressure stage, comprising a first turbine (1...
|
|
WO/2021/138093A2 |
Processes, systems, and apparatus are provided for producing a compressed process gas comprising light olefin such as ethylene. The process utilizes a pyrolysis reactor to produce the process gas. A power generator utilizes a turbine ope...
|
|
WO/2021/129430A1 |
A three-in-one cycle system, comprising: a gas turbine system (1) comprising an integrated starter-generator motor (103), an air compressor (102), a turbine (103), and a heat regenerator (101), the heat regenerator (101) comprising a fir...
|
|
WO/2021/129424A1 |
A combined circulation system of a micro gas turbine, the system comprising: a micro gas turbine (100), a heat exchanger unit (200), a circulation water tank (300), a piston engine (400), and a power generation apparatus (500). An exhaus...
|
|
WO/2021/131459A1 |
This exhaust gas processing equipment is provided with an exhaust line through which exhaust gas discharged from a boiler circulates, a carbon dioxide recovering device for recovering carbon dioxide included in the exhaust gas, and an ex...
|
|
WO/2021/129429A1 |
A 3-in-1 combined circulation system, a transportation vehicle, and a charging system. The circulation system comprises: an air compressor system, comprising a heat regenerator (101), an electric motor (103), and an air compressor (102) ...
|
|
WO/2021/128816A1 |
Disclosed are a thrust bearing and a turbocharger. The thrust bearing cooperates with a thrust plate so as to be used in the turbocharger; the middle of the thrust bearing is provided with a through mounting hole (3); an oil inlet hole (...
|
|
WO/2021/129431A1 |
A combined cooling, heating and power micro gas turbine device, comprising a micro gas turbine (2). The micro gas turbine (2) comprises: a gas compressor (20), a turbine (21), and a combustion chamber assembly. The combustion chamber ass...
|
|
WO/2021/121899A1 |
The invention relates to a method for operating a multistage air compression system for a fuel cell system. At least one stage of the air compression is carried out using a compressor (1) with a compressor wheel (2) which is arranged on ...
|
|
WO/2021/125320A1 |
The purpose of the present invention is to provide, in a device to be compressed: a compressed air supply system capable of preventing the occurrence of draining at the time of activation while suppressing complication of a configuration...
|
|
WO/2021/119981A1 |
A system used for providing mobile power: the equipment required for mobile power is integrated onto three transportation vehicles, and may be combined into one overall transportation, greatly reducing the connection time required for on...
|
|
WO/2021/124953A1 |
The present invention provides a compressor system including a plurality of compressor trains each including a gas turbine and a compression part including a compressor driven by the gas turbine, and a fluid feeding part for distributing...
|
|
WO/2021/123952A1 |
Device for expanding a fluid, wherein the device (1) is provided with an expander element (2) for expanding the fluid, a generator (3) and a transmission (4) between the two, characterized in that the generator (3) is a liquid-cooled gen...
|
|
WO/2021/126478A1 |
A turbocharger having a turbine housing including an outer surface and an inner surface defining an exhaust passage, an exhaust inlet port in fluid communication with the exhaust passage, and a tucked exhaust inlet flange surrounding the...
|
|
WO/2021/119049A1 |
A pumped heat energy storage (PHES) system, involving an annular ducting arrangement is provided. Disclosed embodiments are believed to resolve the issue of containing a high temperature working fluid at elevated pressure by appropriatel...
|
|
WO/2021/110765A1 |
A centering device (10) for centering a turbine housing (40) with respect to a central axis (33) of a radial turbine of a turbo system is described. The centering device (10) includes a ring-shaped body (11) having an outer diameter D1 a...
|
|
WO/2021/106986A1 |
The present invention comprises: a heat transfer medium flow channel through which a heat transfer medium flows; a first economizer provided to the heat transfer medium flow channel; a second economizer provided upstream of the first eco...
|
|
WO/2021/094406A1 |
A pin member is proposed for a turbo-machine having a shroud arranged to rotate within a turbine housing. The pin member is configured to limit this rotation. It is a one- piece element comprising a cylindrical body and a limit surface f...
|
|
WO/2021/078919A1 |
Power plant system and method of operating the same, the power plant system (100) comprising a solid oxide fuel cell (1, SOFC) and a gas turbine (GT), wherein the fuel cell (1) and the gas turbine are set up such that compressed charge a...
|
|
WO/2021/074521A1 |
The invention relates to a propulsion unit (1) comprising: a gas generator (100) comprising: *a compressor (110), *a combustion chamber (120), *a turbine (130), at least two compressed-air propulsion modules (200), each propulsion module...
|
|
WO/2021/069929A1 |
A pumped heat storage apparatus has a prime mover, a power take off, first and second fluid working machines functioning as a compressor (8) and as an expander (10), a working fluid circulation pathway with high and low pressure sides, a...
|
