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Patent Searching and Data


Matches 401 - 450 out of 8,685

Document Document Title
WO/2014/095237A1
The invention relates to a method for operating a gas turbine (10) which, upstream of the inlet of the compressor (12), has a device for cooling the air that can be drawn in by the compressor (12). To prevent step changes in the output g...  
WO/2014/096361A1
The invention relates to a method for operating a gas turbine (10) in frequency-support mode. In order to operate the gas turbine (10) with a relatively high efficiency whilst nevertheless maintaining sufficient power reserves for freque...  
WO/2014/096694A1
The invention relates to the field of turbomachines and more specifically to a device (13) and to a method for temporarily increasing the power of at least one first turbomachine (5A). This device (13) comprises a tank (14) of liquid coo...  
WO/2014/092185A1
Provided is a multi-fuel-capable gas turbine combustor that can sufficiently use various fuels having characteristics departing from a premix characteristic range suitable for generating premixed gas, even while maintaining favorable low...  
WO/2014/080848A1
A power generation system and an operation method for the power generation system, that have: a gas turbine (11) having a compressor (21) and a combustor (22); a fuel cell (13); a discharged fuel gas supply line (45) that supplies discha...  
WO/2014/077975A3
A combined gasification and electric power generation method wherein between 30.0 and 60.0 percent of the compressed air required by an air separation unit supplying oxygen to a gasifier and nitrogen to gas turbine(s)is extracted from a ...  
WO/2014/073732A1
A dual swirling flow combustion device for a gas turbine according to the present invention comprises: a first fuel supply part which has a fuel inlet formed at one side and a fuel injection hole formed at the other side so as to inject ...  
WO/2014/074135A1
A gas turbine engine has a fan inlet and a fan configured to deliver air to an exhaust nozzle. A core gas turbine engine. including in serial order extending further into the engine, a core turbine section, a combustor and a core compres...  
WO/2014/070280A2
An airfoil array is disclosed. The airfoil array may include an endwall, and a plurality of airfoils radially projecting from the endwall. Each airfoil may have a first side and an opposite second side extending axially in chord between ...  
WO/2014/071148A1
A system is provided with a turbine combustor having a first diffusion fuel nozzle, wherein the first diffusion fuel nozzle is configured to produce a diffusion flame. The system includes a turbine driven by combustion products from the ...  
WO/2014/071118A1
A system includes a turbine having an exhaust flow path through a plurality of turbine stages, wherein the plurality of turbine stages is driven by combustion products flowing through the exhaust flow path, at least one main combustor di...  
WO/2014/070667A1
A process involving membrane-based gas separation and power generation, specifically for controlling carbon dioxide emissions from gas-fired power plants. The process includes a compression step, a combustion step, and an expansion/elect...  
WO/2014/071065A2
A system includes a turbine combustor, which includes a first wall disposed about a combustion chamber, a second wall disposed about the first wall, and a third wall disposed about the second wall. The third wall is configured to combine...  
WO/2014/071037A2
A system includes a gas turbine system having a turbine combustor, a turbine driven by combustion products from the turbine combustor, and an exhaust gas compressor driven by the turbine. The exhaust gas compressor is configured to compr...  
WO/2014/068344A3
The present invention relates to the method and structural configuration for environmentally safe waste and biomass processing to increase the efficiency of energy and heat generation. In the structural configuration of the invention sol...  
WO/2014/071215A1
A system is provided with a turbine combustor having a first diffusion fuel nozzle, wherein the first diffusion fuel nozzle is configured to produce a diffusion flame. The system includes a turbine driven by combustion products from the ...  
WO/2014/071065A3
A system includes a turbine combustor (160), which includes a first wall (264) disposed about a combustion chamber (262), a second wall (266) disposed about the first wall (264), and a third wall (268) disposed about the second wall (266...  
WO/2014/071136A3
A system includes a turbine combustor that includes a head end portion having a head end chamber, a combustion portion having a combustion chamber disposed downstream from the head end chamber, a cap disposed between the head end chamber...  
WO/2014/071063A1
A system includes a turbine combustor (150) that includes a head end portion (166) having a head end chamber, a combustion portion (168) having a combustion chamber disposed downstream from the head end chamber, a cap (331) disposed betw...  
WO/2014/068344A4
The present invention relates to the method and structural configuration for environmentally safe waste and biomass processing to increase the efficiency of energy and heat generation. In the structural configuration of the invention sol...  
WO/2014/071088A1
A system includes a gas turbine engine that includes a combustor section having one or more combustors configured to generate combustion products, a turbine section having one or more turbine stages between an upstream end and a downstre...  
WO/2014/071120A3
A system including a turbine combustor (160) with a head end portion (166) having a head end chamber, a combustion portion (168) having a combustion chamber disposed downstream from the head end chamber, a cap (331) disposed between the ...  
WO/2014/070279A2
An airfoil array is disclosed. The airfoil array may include an endwall, and a plurality of airfoils radially projecting from the endwall. Each airfoil may have a first side and an opposite second side extending axially in chord between ...  
WO/2014/069409A1
This power generation system is provided with: a gas turbine (11) having a compressor (21), a combustor (22) and a turbine (23); a first compressed air supply line (26) that supplies compressed air, which has been compressed by the compr...  
WO/2014/071037A3
A system includes a gas turbine system having a turbine combustor, a turbine driven by combustion products from the turbine combustor, and an exhaust gas compressor driven by the turbine. The exhaust gas compressor is configured to compr...  
WO/2014/071089A1
In one embodiment, a system includes at least one sensor configured to communicate a signal representative of a gas turbine operations. The system further includes a controller communicatively coupled to the sensor. The system additional...  
WO/2014/071121A1
A system includes a turbine combustor that includes a head end portion having a head end chamber, a combustion portion having a combustion chamber disposed downstream from the head end chamber, a cap disposed between the head end chamber...  
WO/2014/065185A1
A power generation system having a gas turbine engine that utilizes sunlight is provided with: a compressor (1) for compressing air (A), which is the working medium; a solar heater (3) for heating the air compressed by the compressor usi...  
WO/2014/060758A1
A heat engine (10) comprising: a feeder stage (20) comprising: a first compressor (24) for compressing first gas received at pressure P1 from a gas source to an elevated pressure and temperature; a reactor (28) for receiving gas compress...  
WO/2014/062220A1
A turbofan engine structural guide vane is mounted to a forward bulkhead of a core engine case structure at an inner end and to a fan case at an outer end. A plurality of shear pins extend from the aft portion of the structural guide van...  
WO/2014/062367A3
A system and methods for increasing a combustibility of a low BTU natural gas are provided herein. The method includes increasing the adiabatic flame temperature of the low BTU natural gas using heavy hydrocarbons, wherein the heavy hydr...  
WO/2014/058463A1
A disclosed gas turbine engine includes a compressor section including a first compressor disposed axially forward of a second compressor, a combustor in fluid communication with the compressor section and a turbine section in fluid comm...  
WO/2014/058466A1
A gas turbine engine has a compressor section, a compressor case substantially surrounding the compressor section, and a diffuser case attached at an attachment interface to the compressor case. The attachment interface is between a forw...  
WO/2014/058455A1
A bearing support bracket for supporting the bearing assembly includes individually adjustable features for defining and enabling a desired stiffness.  
WO/2014/055110A1
A static guide vane for use in a fan section of a gas turbine engine includes an outer platform and an inner platform. The inner and outer platforms are connected by an airfoil. The airfoil have channels extending into a main body of the...  
WO/2014/055104A1
A gas turbine engine design process includes the steps of determining the location of a hot streak downstream of a combustor nozzle, and determining whether it would be most beneficial to have the hot streak initially impact a pressure s...  
WO/2014/055122A1
A geared architecture for a gas turbine engine includes a central gear supported for rotation about the axis, a plurality of intermediate gears engaged with the central gear and a ring gear circumscribing the intermediate gears. A first ...  
WO/2014/055113A9
A gas turbine engine includes a fan rotating structure including a plurality of fan blades supported on a hub that defines a frontal area. A turbine section drives the fan through a geared architecture about the axis. The fan rotating st...  
WO/2014/055113A1
A gas turbine engine includes a fan rotating structure including a plurality of fan blades supported on a hub that defines a frontal area. A turbine section drives the fan through a geared architecture about the axis. The fan rotating st...  
WO/2014/055106A1
A gas turbine engine includes a compressor section, a combustor in fluid communication with the compressor section, a turbine section in fluid communication with the combustor, and a bleed system that is configured to receive bleed air f...  
WO/2014/051688A1
A seal damper system includes a plurality of circumferentially spaced blades that each include a platform and an airfoil that extends radially outwardly from the platform. A pocket is arranged circumferentially intermediate the blades an...  
WO/2014/047685A1
The invention provides methods of generating electric power from underground coal seams with capture of carbon dioxide.  
WO/2014/052007A1
A mid-turbine frame (MTF) system for a gas turbine engine is disclosed. The MTF includes an inner case, an outer case and a fairing sandwiched between the inner and outer cases. The fairing includes an inner ring spaced apart from and co...  
WO/2014/051690A1
A combustor assembly for a gas turbine engine includes a combustor shell, a TOBI, a case, and a joint for securing the combustor shell, TOBI and case together. The joint has a combustor flange integral to the combustor shell. A TOBI flan...  
WO/2014/044254A3
The invention relates to a system for producing hot water and/or steam having a high-temperature reservoir for use in a gas turbine power station, wherein the energy for charging is provided from at least one external energy source and/o...  
WO/2014/044254A4
The invention relates to a system for producing hot water and/or steam having a high-temperature reservoir for use in a gas turbine power station, wherein the energy for charging is provided from at least one external energy source and/o...  
WO/2014/043051A1
Provided herein is a method, device and installation for devolatizing a solid feedstock, comprising carbon-based waste selected from the group consisting of hazardous material, biomass, animal manure, tires, municipal solid waste and ref...  
WO/2014/037128A1
A gas turbine plant (1) comprising at least one gas turbine (10) with a compressor stage (11) and an expansion stage (12), an exhaust gas line (20) to guide the flow of exhaust gas exiting from the expansion stage (12) during operation o...  
WO/2014/039246A1
An industrial gas turbine engine (10) rated for at least 75 MW maximum output, including: a can annular combustion assembly (80); and a single rotor shaft (114); wherein a combustion section length (112) between a trailing edge (28) of a...  
WO/2014/039826A8
A gas turbine engine compressor spacer (230) includes a body (229) with a hollow cylinder shape. The body (229) includes an outer surface (232) with an axially forward end. The body (229) also includes a forward face (233) extending radi...  

Matches 401 - 450 out of 8,685