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Matches 1 - 50 out of 8,051

Document Document Title
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/2016/181664A1
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...  
WO/2016/129030A1
A gas turbine system (1) is equipped with: a two-shaft gas turbine (2) having a gas turbine compressor (10) that takes in and compresses air (A), a combustor (11) that mixes and burns compressed air (CA) generated by the gas turbine comp...  
WO/2016/126980A1
A system includes a turbine combustor having a first volume (76) configured to receive a combustion fluid and to direct the combustion fluid into a combustion chamber (60) and a second volume (92) configured to receive a first flow of an...  
WO/2016/126873A1
A gas turbine system includes a turbine combustor, a turbine, an exhaust gas compressor, an exhaust gas recirculation (EGR) system, a carbon black recovery system, and a carbon black production controller. The carbon black production con...  
WO/2016/126985A1
A system includes a turbine combustor having a first volume (76) configured to receive a combustion fluid and to direct the combustion fluid into a combustion chamber. The turbine combustor includes a second volume (92) configured to rec...  
WO/2016/127187A3
A process for retrofitting an electric power plant that uses two 60 Hertz large frame heavy duty industrial gas turbine engines to drive electric generators and produce electricity, where each of the two industrial engines can produce up...  
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/2016/108477A1
Provided are a high-voltage application-type combustor and a method for applying an electric field by means of the same combustor, the high-voltage application-type combustor comprising: a premix chamber (410) arranged on an upper end of...  
WO/2016/109730A1
A system includes an exhaust gas recirculation (EGR) gas turbine system which includes a combustor configured to receive and combust a fuel with an oxidant and a turbine driven by combustion products from the combustor and a turbine driv...  
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/2016/091604A1
The method allows to control a test apparatus for a gas turbine engine; WI values of one or more tentative fuel gas mixtures are predicted by calculations and the predicted WI values are used for setting the composition of a fuel gas mix...  
WO/2016/079223A1
The invention relates to a thermal energy machine (1), in particular a gas turbine (2), comprising a compressor (3) for compressing an air mass flow (5) flowing along the machine longitudinal central axis (6) in an axial flow direction (...  
WO/2016/064785A1
A co-generation process for a regenerator in an FCC system having a reactor and a regenerator includes the steps of introducing flue gas from the regenerator into a heating unit at a first location of the heating unit, and introducing an...  
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/2016/056180A1
A fuel injecting device (36) for a combustor (12) has a pilot burner (40) and a main burner (4). The main burner (4) has at least one first fuel injection port (41a) to supply a first fuel to an upstream section of a combustion chamber (...  
WO/2016/056580A1
Provided is a turbine stator blade cooling structure that can suppress the use of compressed air. Also provided is a gas turbine engine that is provided with the turbine stator blade cooling structure. A turbine blade cooling structure t...  
WO/2016/056579A1
Provided is a combustor that has an efficient cooling structure. Also provided is a gas turbine engine that is provided with the combustor. A combustor that is for a gas turbine and that is provided with a combustion cylinder and with a ...  
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/2016/051758A1
A gas turbine (100) according to the present invention uses hydrogen gas as a fuel, has a fuel injection nozzle (23), and is provided with: a combustor (20), at the interior of which a combustion chamber (24) is formed; a water-vapor sup...  

Matches 1 - 50 out of 8,051