Matches 1 - 50 out of 221 1 2 3 4 5 >


Match Document Document Title
US20150027099 GAS TURBINE FACILITY  
A gas turbine facility 10 of an embodiment has a combustor 20 combusting fuel and oxidant, a turbine 28 rotated by combustion gas exhausted from the combustor 20, a heat exchanger 25 cooling the...
US20140041357 EXHAUST DIFFUSER INCLUDING FLOW MIXING RAMP FOR A GAS TURBINE ENGINE  
A turbine exhaust diffuser for a gas turbine engine. The diffuser includes a flow ramp positioned on an ID flowpath boundary within a flowpath of the diffuser. The flow ramp extends...
US20100332103 NOX Compliant Peak for Gas Turbine  
A gas turbine comprises a plurality of target exhaust temperature determination modules, the plurality of target exhaust temperature modules comprising a nitrogen oxide (NOx) compliance module...
US20100293973 Combined cycle exhaust powered turbine inlet air chilling  
An ammonia absorption refrigeration apparatus is disclosed that has advantageous features to enable it to be integrated with a power plant comprised of a combustion turbine plus a heat recovery...
US20150152788 GAS TURBINE ENGINE COMPRISING AN EXHAUST CONE ATTACHED TO THE EXHAUST CASING  
An assembly including an exhaust casing and an exhaust cone for a gas turbine engine, each including an axial annular flange, the two flanges being inserted into one another, one being radially...
US20120198810 STRUT AIRFOIL DESIGN FOR LOW SOLIDITY EXHAUST GAS DIFFUSER  
This disclosure relates to a strut airfoil for use in an exhaust diffuser. The strut airfoil described herein generally is asymmetric. The strut airfoil has a curved leading edge, a curved tail...
US20120216547 POWER PLANT FOR CO2 CAPTURE  
An exemplary fossil fuel fired power plant is disclosed with minimum impact of the CO2 capture system on a power part of the plant. A power plant is disclosed which is ready for the retrofit of a...
US20120159962 WATER SELF-SUFFICIENT TURBINE SYSTEM  
The present invention provides a water self-sufficient turbine system comprising: (a) a combustion turbine comprising a combustion chamber disposed between an upstream compressor coupled to a...
US20120159957 WATER SELF-SUFFICIENT TURBINE SYSTEM  
The present invention provides a water self-sufficient turbine system comprising: (a) a combustion turbine comprising a combustion chamber disposed between an upstream compressor coupled to a...
US20140137533 EXHAUST GAS DIFFUSER FOR A GAS TURBINE  
An exhaust gas diffuser for a gas turbine generally includes an inner wall that extends along an axial centerline of the exhaust gas diffuser. An outer wall is coaxially aligned with the inner...
US20140102105 SYSTEM AND METHOD FOR HEATING COMBUSTOR FUEL  
A system for heating combustor fuel includes a turbine exhaust plenum and a heat exchanger downstream from the turbine exhaust plenum. The heat exchanger has an exhaust inlet, an exhaust outlet, a...
US20110036096 INTEGRATED GASIFICATION COMBINED CYCLE (IGCC) POWER PLANT STEAM RECOVERY SYSTEM  
In an integrated gasification power plant a steam recovery system is provided. The system enables power generation equipment designed for a predominant fuel and operating condition to efficiently...
US20100293958 DESWIRLING EXHAUST MIXER  
An exhaust mixer for a gas turbine engine including a plurality of circumferentially distributed alternating inner and outer lobes, where each of the inner lobes is configured with a...
US20110162339 FLOW DISTRIBUTION OF GAS TURBINE EXHAUST USING WALLS SHAPED TO FACILITATE IMPROVED GAS FLOW  
A gas turbine transition into an emission reduction catalyst is improved by adding properly curved surfaces so as to induce the Coanda effect. Such a surface allows for a reduction in pressure...
US20090072047 AIRCRAFT DEFENSE SYSTEM AND METHOD  
A method and system for aiding an aircraft pilot to avoid being struck by a heat seeking missile includes the steps of providing a mass of water and a missile detector for detecting an incoming...
US20140090354 TURBINE EXHAUST PLUME MITIGATION SYSTEM  
Various embodiments include an exhaust plume mitigation system for a turbine and systems incorporating the exhaust plume mitigation system. In some embodiments, the exhaust plume mitigation system...
US20140367476 SYSTEM FOR HEATING THE CABIN OF AN AIRCRAFT PROVIDED WITH AN ANNULAR HEAT EXCHANGER AROUND THE EXHAUSE NOZZLE  
A heating system (50) for heating a cabin (2) of an aircraft (1), said heating system including an annular heat exchanger (10) positioned around an exhaust pipe (21) of a turbine engine (20), and...
US20150128557 MICROSCALE DISTRIBUTED ENERGY COGENERATION METHOD AND SYSTEM  
A microscale energy cogeneration system includes at least a micro/nano-turbine set for converting fuel into mechanical energy, and a generator for converting mechanical energy produced by said...
US20100269480 Gas turbine exhaust diffuser  
A gas turbine including an exhaust diffuser with a flow splitter located between the inner wall and outer wall defining the exhaust gas flow path. In one aspect the flow splitter being moveable...
US20120167546 COMBINED-CYCLE POWER PLANT  
A method involves operating a combined-cycle power plant (10), which has a gas turbine (11) with a compressor (12) and a turbine (13), a heat recovery steam generator (17) which is connected...
US20120186261 SYSTEM AND METHOD FOR A GAS TURBINE EXHAUST DIFFUSER  
In one aspect, an exhaust diffuser for a gas turbine is disclosed. The exhaust diffuser may generally include an inner casing and an outer casing spaced radially apart from the inner casing so as...
US20110162380 METHOD TO INCREASE NET PLANT OUTPUT OF A DERATED IGCC PLANT  
In certain embodiments, a carbon capture integrated gasification combined cycle (IGCC) system includes a supplemental gas turbine engine configured to burn a high-hydrogen syngas to generate power...
US20120260667 Power Plant  
A power plant is provided and includes a gas turbine engine to generate power, a heat recovery steam generator (HRSG) to produce steam from high energy fluids produced from the generation of power...
US20140096500 EXHAUST DIFFUSER  
An exhaust diffuser includes an outer shroud and an inner shroud radially separated from the outer shroud so as to define a fluid passage between the outer shroud and the inner shroud. A strut...
US20120159956 TOP CYCLE POWER GENERATION WITH HIGH RADIANT AND EMISSIVITY EXHAUST  
The present invention generally relates to power generation methods and secondary processes requiring high radiant and emissivity homogeneous combustion to maximize production output. In one...
US20150218967 BIFURCATED DUCTS INCLUDING PLENUMS FOR STABILIZING FLOW THERETHROUGH AND EXHAUST SYSTEMS INCLUDING THE SAME  
Plenums for bifurcated ducts and bifurcated ducts are provided for stabilizing flow therethrough. The plenum comprises an outer cylindrical body intersected by a pair of exhaust duct stubs that...
US20140217231 ROTARY WING AIRCRAFT HAVING COLLOCATED EXHAUST DUCT AND PROPELLER SHAFT  
An exhaust system for reducing infrared emissions of a rotary wing aircraft includes an exhaust duct having a fore end for connection with an aft turbine section of an engine of the rotary wing...
US20140096501 UPTURNED EXHAUST SYSTEM FOR ROTARY WING AIRCRAFT  
An exhaust system for reducing infrared emissions of a rotary wing aircraft includes a manifold; an opening in the manifold, the opening configured to face upwards and away from the rotary wing...
US20120260668 Combined Cycle Power Plant  
A combined cycle power plant is provided and includes a gas turbine engine to generate power, a heat recovery steam generator (HRSG) to produce steam from high energy fluids produced from the...
US20140215999 AFT EXHAUST SYSTEM FOR ROTARY WING AIRCRAFT  
An exhaust system for reducing infrared emissions of a rotary wing aircraft includes a duct assembly having an inlet portion and an outlet portion; the inlet portion configured to receive exhaust...
US20090235634 SYSTEM FOR EXTENDING THE TURNDOWN RANGE OF A TURBOMACHINE  
A system for heating the inlet-air of a gas turbine is provided. The system may incorporate an external energy source to increase the temperature of the inlet-air. The system may extend the...
US20070033946 Helicopter defense system and method  
A method and system for aiding a helicopter pilot to avoid being struck by a heat seeking missile includes the steps of providing a mass of water and a missile detector for detecting an incoming...
US20120090328 POWER PLANT  
A power plant includes a gas turbine unit adapted to feed whose flue gases into a boiler of a steam turbine unit, to be then diverted into a recirculated flow and discharged flow. The recirculated...
US20150143812 Exhaust Plume Cooling  
An exhaust plume cooling device for cooling an exhaust gas plume to reduce deleterious heat effects on impinged and surrounding surfaces. The device is supportable in a position downstream of an...
US20110016844 DEVICE FOR REDUCING TURBOPROP INFRARED EMISSIONS  
According to the invention, fresh air (E) at the turboprop outlet is captured and mixed with the warm airflow (F) created by said turboprop to lower the temperature.
US20150013341 Exhaust Mixer with Offset Lobes  
An exhaust mixer for a gas turbine engine where each outer lobe has at the downstream end a circumferential offset in a direction corresponding to that of the swirl component of the flow entering...
US20150075131 EXHAUST COLLECTOR WITH CURVED SIDE PANEL  
An exhaust collector for a gas turbine engine is disclosed. The exhaust collector includes a front panel, a rear panel, and a side panel. The side panel includes a circumferential portion, a first...
US20140047813 EXHAUST COLLECTOR WITH RADIAL AND CIRCUMFERENTIAL FLOW BREAKS  
An exhaust collector having a radial inlet configured to receive exhaust gas in a radial direction, an outlet configured to deliver exhaust gas in and outlet direction, and an enclosure configured...
US20140150402 SYSTEM AND METHOD FOR BURNING VANADIUM-CONTAINING FUELS  
In one aspect, a combustion system is configured to facilitate preventing the formation of vanadium pentoxide (V2O5) and decrease a concentration of at least one of vanadium trioxide (V2O3) and...
US20090025362 INFRARED SUPPRESSION SYSTEM WITH SPIRAL SEPTUM  
An InfraRed Suppression System (IRSS) includes a double-walled exhaust duct and double walled septum. The double walled structure provides a flow path for secondary (non-exhaust gas) cooling air...
US20140174052 EXHAUST DIFFUSER AND METHOD FOR MANUFACTURING AN EXHAUST DIFFUSER  
An exhaust diffuser and method for manufacturing an exhaust diffuser is provided. An exhaust diffuser for a torque-generating turbine, in particular a torque-generating gas turbine is provided,...
US20150000298 FUEL CONDITIONER, COMBUSTOR AND GAS TURBINE IMPROVEMENTS  
Advanced gas turbines and associated components, systems and methods are disclosed herein. A gas turbine configured in accordance with a particular embodiment includes a rotor operably coupled to...
US20100300061 Selective Catalytic Reduction System and Process for Treating NOx Emissions Using a Palladium and Rhodium or Ruthenium Catalyst  
A process for the catalytic reduction of nitrogen oxides (NOx) in a gas stream (29) in the presence of H2 is provided. The process comprises contacting the gas stream with a catalyst system (38)...
US20140298771 GAS TURBINE EXHAUST DIFFUSER  
A gas turbine exhaust diffuser includes a frustoconical portion that defines an interior surface and an axial centerline. In particular embodiments, the interior surface may have a slope greater...
US20100050654 SYSTEM FOR HOT SOLIDS COMBUSTION AND GASIFICATION  
In a retrofit system for hot solids combustion and gasification, a chemical looping system includes an endothermic reducer reactor 12 having at least one materials inlet 22 for introducing...
US20120222426 INTEGRATED GAS TURBINE, SAGD BOILER AND CARBON CAPTURE  
An integrated power generation system for reducing carbon dioxide emissions is provided. The integrated system comprises a gas turbine having an air inlet, a fuel inlet and an exhaust gas outlet;...
US20080289313 DIRECT HEATING ORGANIC RANKINE CYCLE  
The present invention provides an organic Rankine cycle power system, which comprises means for superheating vaporized organic motive fluid, an organic turbine module coupled to a generator, and a...
US20140150399 DIVERTER DAMPER  
The invention relates to a diverter damper for controlling a gas flow in a gas duct of large cross section, said diverter damper comprising:—a housing having an inlet and two outlets,—a pivotable...
US20110056179 TURBINE EXHAUST DIFFUSER WITH REGION OF REDUCED FLOW AREA AND OUTER BOUNDARY GAS FLOW  
An exhaust diffuser system and method for a turbine engine. The outer boundary may include a region in which the outer boundary extends radially inwardly toward the hub structure and may direct at...
US20100031625 SYSTEMS AND METHOD FOR CONTROLLING STACK TEMPERATURE  
Systems and a method for controlling a temperature of an exhaust gas stack are provided. The system includes a first heat exchanger positioned upstream in exhaust gas flow communication to an...

Matches 1 - 50 out of 221 1 2 3 4 5 >