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Matches 1 - 50 out of 8,115

Document Document Title
WO/2017/096334A1
A process based on the combined use of yttrium and magnesium to inhibit vanadium corrosion of high temperature parts of thermal equipment. The combined use of yttrium and magnesium, applied in a variable yttrium/magnesium ratio, compared...  
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/2017/084656A2
The aim of the invention is to significantly increase the electrical efficiency or the proportion of the effective work of gas turbines, even in small gas turbines or microsize gas turbines having a simple design. According to the invent...  
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/2017/083684A1
The present invention is directed to methods and systems for utilizing supercritical carbon dioxide in an open thermodynamic cycle in which no compressors are used. In some embodiments, a method for utilizing supercritical carbon dioxide...  
WO/2017/069249A1
A ventilation flow path (22), a cooling air flow path (178), a mixing space (177) and a mixed air flow path (137) are formed in this gas turbine rotor (2). The ventilation flow path (22) guides compressed air (Acom) which is axially upst...  
WO/2017/067871A1
Disclosed herein is an integrated power generation and load driving system (1), comprising in combination: a multi- shaft gas turbine engine (3) comprising a high-pressure turbine (316) meĀ¬ chanically coupled to an air compressor (312);...  
WO/2017/065038A1
[Problem] To invent an engine system as a means for reducing CO2 and NOX emissions to cope with global warming. [Solution] An engine system wherein a combustion chamber unit configured so as to have a step in which enriched oxygen and hy...  
WO/2017/064352A1
The pressure vessel (1) for processing gas that con- tains hydrocarbons for use as a fuel in an internal combustion engine (100) comprises a gas inlet (20) that is located in an upper portion of the pressure ves- sel (1) when the pressur...  
WO/2017/060585A1
The present invention relates to an aircraft comprising a fuselage, a lateral support wing (1) and a propulsion assembly (100) mounted under the wing, the wing comprising at least two structural spars (1lba, 1lbf) extending from the fuse...  
WO/2017/060623A1
The present invention relates to an aircraft propulsion assembly comprising a turbine (15), at least one fan (10) and a mechanism for transmitting power between the turbine and the fan, characterized in that the power transmission mechan...  
WO/2017/045014A1
An internal combustion engine wherein a thermo potential heat flow in combustion is maximized by providing a feedback of an optimized amount of thermo potential heat flow that is modulated in the exhaust media, into the air intake, and a...  
WO/2017/041197A1
Disclosed is a combination of a turbine of a multiple bushing transmission and bidirectional rotation wheel fan type and a gas compressor of a bushed wheel fan type, which is constituted of operating and transmission parts such as a turb...  
WO/2017/042493A1
The invention relates to a particle-trapping device (2) for a turbomachine, said particles being contained in an air stream flowing inside a turbomachine, in particular the air stream flowing in the bypass region (17) of the combustion c...  
WO/2017/036431A1
The equipment for increase of output and improvement of efficiency of a gas turbine includes a primary compressor (101) with an impeller for input medium compressing, a combustion chamber (102) for heating the compressed input media and ...  
WO/2017/039567A1
A combustor transition duct (110) comprising a main duct portion (113) having a primary opening and a secondary opening, wherein a first axis extends from a center of the primary opening to the secondary opening; an extension flange (115...  
WO/2017/041018A1
A vehicle includes a main body and a gas generator producing a gas stream. At least one fore conduit and tail conduit are fluidly coupled to the generator. First and second fore ejectors are fluidly coupled to the at least one fore condu...  
WO/2017/040635A1
The present disclosure relates to systems and methods useful for power production. In particular, a power production cycle utilizing CO2 as a working fluid may be combined with a second cycle wherein a compressed CO2 stream from the powe...  
WO/2017/032386A3
The invention is an process that been added to "6" steam generators (once through steam generators) "OTSG", to improve the Efficiency of steam production with percentage of 3%. The basic elements that consist the process see the drawing ...  
WO/2017/023331A1
A ducting arrangement (10), including: an annular duct (38) having a plurality of discrete integrated exit pieces (IEP 18) secured together to form the annular duct and an annular chamber (14) configured to deliver an annular flow of com...  
WO/2017/015775A1
An internal combustion engine using water as auxiliary power includes an engine body (1) and a sprinkler system (2). The sprinkler system (2) includes a sprinkler motor (22) and a water spray nozzle (21) connected to the outlet of the sp...  
WO/2017/013360A1
The invention concerns an aircraft propelled by a turbine engine having contrarotating fans (7, 8), the turbine engine being incorporated at the rear of a fuselage (1) of the aircraft, in the extension of same and comprising at least two...  
WO/2017/013366A1
The invention relates to an aircraft comprising a fuselage (1), which is propelled by a turbine engine with two coaxial fans, namely an upstream fan (7) and a downstream fan (8), driven by two contra-rotating rotors (5, 6) of a power tur...  
WO/2017/013318A1
The main subject of the invention is a combustion chamber (1) for a turbomachine (10), comprising a chamber end wall (16) and a plurality of air and fuel injection systems (21) distributed circumferentially about an axis (T) of the combu...  
WO/2017/015343A1
A system and related method for providing a highly reactive fuel to a combustor of a gas turbine are disclosed herein. The system includes a fuel supply system that is in fluid communication with a fuel supply. The fuel supply system inc...  
WO/2017/013356A1
The invention relates to an exhaust casing for a turbine engine of an aircraft, including: a collar (4), a hub (5), hollow arms (63) connecting said collar (4) to said hub (5), and an opening piece (3) which is located on the collar (4) ...  
WO2017011151A1
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/2017/008037A1
An engine comprises a compression portion and a combustion portion. The compression portion comprises twin-screw rotors, male engaged with female. The combustion portion comprises twin-screw rotors, male engaged with female. The male com...  
WO/2017/005694A1
The invention relates to a burner for a gas turbine (10), wherein the burner (30) comprises a combustion chamber (28), a first injector (103) adapted to inject a first fuel into the combustion chamber (28) and a second injector (104) ada...  
WO/2016/208998A1
A method for controlling a gas turbine combustor, according to one embodiment for achieving the objective of the present invention, may comprise: a detection step of obtaining combustion oscillation values through first detection units p...  
WO/2016/205116A1
The present disclosure relates to systems and methods that provide power generation using predominantly CO2 as a working fluid. In particular, the present disclosure provides for particular configurations for startup of a power generatio...  
WO/2016/195999A1
Apparatus, systems, and methods store energy by liquefying a gas such as air, for example, and then recover the energy by regasifying the cryogenic liquid and combusting or otherwise reacting the gas with a fuel to drive a heat engine. C...  
WO/2016/189188A1
A power plant (10) comprising a first turbine-compressor unit (12) provided with a first compressor part (14) and a first turbine part (20); a gas heater unit (24) arranged in fluid connection with the first compressor part (14) and the ...  
WO/2016/189189A1
A power plant (10) comprising a first turbine-compressor unit (12) provided with a first compressor part (14) and a first turbine part (20); a gas heater unit (24) arranged in fluid connection with the first compressor part (14) and the ...  
WO/2016/181307A1
The invention relates to a turbine, in particular a combustion gas turbine, which drives a high-speed generator for generating electricity, said turbine having a high efficiency. The turbine has at least one combustion chamber (6), which...  
WO/2016/183588A2
A power generation system burns a fuel in a gas in a combustion chamber, producing one or more combustion products and heating a working fluid, preferably supercritical CO2, that is chemically the same as a combustion product. The workin...  
WO/2016/183588A3
A power generation system bums a fuel in a gas in a combustion chamber, producing one or more combustion products and heating a working fluid, preferably supercritical C02, that is chemically the same as a combustion product. The working...  
WO/2016/181664A1
Provided is a method for efficiently producing high-density air without futilely increasing the pressure and temperature. This method for producing high-density air is characterized by: mixing fine water particles W into a raw material a...  
WO/2016/174341A1
The invention relates to a turboshaft engine for a helicopter, comprising a case (5) inside which a gas generator (6) and a turbine (7) are accommodated, the turbine (7) being mounted on a power shaft (8) that extends along a longitudina...  
WO/2016/175753A1
A fuel delivery system (10) for a gas turbine engine (12) that employs a technique for purging fuel delivery tubes (82). The fuel delivery system includes a multifunction valve (64) that has a flow through position (66) and a bi-directio...  
WO/2016/174340A1
The invention relates to a turboshaft engine comprising a case (5) inside which a gas generator (6) and a free turbine (7) are accommodated, the turbine (7) being mounted on a power shaft (8) designed to be mechanically coupled to/uncoup...  
WO/2016/174175A1
A gas turbine drive system in mechanical drive configuration is described. The gas turbine drive system comprises a gas turbine engine (1) drivingly connected to a driven turbomachine (3). The gas turbine engine includes a dry low NOx em...  
WO/2016/166024A1
The invention relates to a method for operating a power plant (1) and to a power plant (1) which can be operated at locations with an insufficient fuel supply. For this purpose, the power plant (1) comprises a gas turbine (2), a gas liqu...  
WO/2016/164932A1
The examples provided herein, including any summary of above summary of example aspects, serves to provide a basic understanding of the present disclosure. Such summary is not an extensive overview of all contemplated aspects, and is int...  
WO/2016/162718A1
A method for operating a gas turbine using a liquid fuel combustible contaminate with vanadium and/or potassium and/or sodium, characterized in that Yttrium and/or Magnesium is injected in the fuel in a selective way.  
WO/2016/157224A1
Described is a propulsion system (1) for hypersonic aircraft, having an air inlet (10) of a fluid (110), a containment duct (20) and an exhaust nozzle (30). The propulsion system (1) comprises a bypass duct (40) for a flow (100) of fluid...  
WO/2016/153692A1
A supercritical carbon dioxide power generation Brayton cycle system and method that employs an alternate heat recuperation method and apparatus that utilizes switched banks of bead filled tanks to accumulate and recover the thermal ener...  
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/2016/128925A1
The present invention relates to a radial centrifugal turbomachine provided with an adjusting device (25) operatively active at the axial inlet (12) of the fixed casing (6) of the turbomachine (1 ). The adjusting device (25) comprises an...  

Matches 1 - 50 out of 8,115