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WO/2002/063150A1 |
A Rotary Pulse Jet Engine in which combustion chamber acts as a miniature jet engine to provide thrust , consists of a rotor rotating within a closely fitting outer housing , has at its perimeter fully sealable variable volume combustion...
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WO/2002/059469A1 |
Engine (30) has a compression fan (36) coaxially mounted with reaction member (38). Casing (32) extends around reaction member (38) to form volute (52) and extends to turbine wheel (54) which is connected to compression fan (36) via axle...
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WO/2002/057632A2 |
A high-pressure water pump for supplying high pressure water for atomization in the inlet stream of a gas turbine is disclosed which includes at least one hydraulic cylinder containing a piston secured to a piston rod extending from the ...
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WO/2002/055632A1 |
Process for the production of thermally converted light products from residual feedstock and electricity from syngas obtained from thermal conversion residue as feedstock, in which process flue gas exiting from the electricity producing ...
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WO/2002/055844A1 |
A turbine suitable for use for low-power cogeneration or as a power generator for electric automobiles, the turbine being characterized in that a vane (1) curved in section and having a nozzle (2) somewhere in the inner side is construct...
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WO/2002/053894A2 |
An installation for generating energy comprises a compressor assembly for compressing air, having a low-pressure compressor, which is connected to a high-pressure compressor via a primary air path. Furthermore, a compressor turbine assem...
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WO/2002/053878A1 |
The invention provides possibility of common utilisation and reuse of products by using exchanges between individual sub-processes and systems so that the total plant achieves a higher degree of self-sufficiency in relation to the indivi...
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WO/2002/053969A1 |
The present invention relates to a device for combustion of a carbon containing fuel in a nitrogen free atmosphere, and a method for operating said device. The device may be integrated with a power generation plant (i.e. gas turbine(s)) ...
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WO/2002/046332A2 |
A process and gas generator is disclosed for generating by dry distillation of solids and gasification of solids, a fuel gas substantially free of condensable dry distillation volatiles which would interfere with the intended use of the ...
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WO/2002/038927A1 |
The invention relates to a method for operating a gas turbine system, and to a corresponding gas turbine system, in which the supply air is compressed, mixed with fuel and brought to combustion, whereby a working substance results that d...
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WO/2002/038926A1 |
The composition of moisturized fuel gas exiting a fuel gas saturator (301) is controlled using feed forward control. The level (304) of the water is manipulated by adjusting the valve (303) that controls the make-up water. The level cont...
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WO/2002/035072A2 |
A gas turbine engine comprising a combustion chamber (52), a turbine section (16) and a compressor section (12). The turbine section (16) surrounds the combustion chamber (52) and the compressor section (12) surrounds the turbine section...
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WO/2002/033226A1 |
A system is described for allowing short term power augmentation of a gas turbine (12) or a gas turbine combined cycle power plant. A reservoir of pressurized and/or liquefied gas (100) is installed to store a temporary supply of gas tur...
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WO/2002/031331A1 |
A hydrotreated liquid contains volatile hydrocarbons, hydrogen, and contaminants such as hydrogen sulfide. An inert gas, preferably nitrogen, is used to strip volatiles from the hydrotreated liquid. This stripper gas is then added to fue...
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WO/2002/029252A1 |
A two stage compressor with a mixed flow first stage, a centrifugal second stage, and an intermediate duct. The centrifugal rotor (2) has a circumferential array of radially extending centrifugal flow blades (16) between the centrifugal ...
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WO2001061151B1 |
There is designed an equipment with mutually interacting spiral teeth, comprising at least one rotor and one stator with a working surface limited by at least two sprial teeth, which are in mutual interaction by their wrappers and the sp...
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WO/2002/023027A1 |
A steam injection and inlet fogging system is provided for a gas turbine power plant (10). A waste heat recovery unit (28) is arranged to receive exhaust gas from the turbine, the former having a plurality of heat exchange sections (40, ...
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WO/2002/020952A1 |
The present invention relates to a partially-gasified air-preheated coal-fired combined cycle power generation system and power generation method, the system is constituted mainly by a coal gas block, which includes a pressured fluidized...
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WO/2002/014664A1 |
A gas turbine engine having a compressor (12), a regenerator (14), a combustor (16), a high pressure turbine (18), and a power turbine (20) is arranged for directing gas from the high pressure turbine (18) to the regenerator (14) and tha...
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WO/2002/014663A1 |
The invention relates to a method for converting thermal energy into mechanical work, whereby a first (4) and a second means (9) for storing thermal energy are alternately connected into a turbine branch (T). In order to increase the eff...
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WO/2002/012691A1 |
A gas turbine engine and a method of operating the same at idle speed are presented. The engine has a drive motor for causing the compressor to rotate and a motor control system having a motor power-up module with an input connected to t...
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WO/2002/008592A1 |
The invention relates to a gas turbine (3) with reheat in the turbine section (11), whereby a fuel injection device (37) is provided for the injection of fuel (33) in to a combustion air flow (61) in the direction of flow before a coolin...
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WO/2002/004794A2 |
A multi-channel combustion device including at least one radially partitioned inlet zone within an inlet port, and a plurality of circumferentially spaced chambers (12) in which deflagration or detonative combustion occurs. The inlet por...
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WO2000066887A9 |
The invention is a method and apparatus for generating work comprising a combustor (1) to form a gas stream; a regenerator (2) for reacting, in the presence of heat from the gas stream, a strong liquor to form a carbon dioxide stream and...
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WO/2001/096722A1 |
A method and apparatus for reducing emissions in combustion systems, particularly gas turbines. A mixture (70) of diluent and fuel is created, wherein the diluent and fuel are at a predetermined diluent-to-fuel ratio. The mixture (70) is...
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WO/2001/095409A2 |
The efficiency of a combination reformer/fuel cell system is significantly improved by recapturing the energy value of heat generated in the fuel cell and producing additional power. The cooling water (40) from the fuel (44) cell is mixe...
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WO/2001/092704A1 |
A pulsed detonation engine wave rotor apparatus (22) and method of using a pressure wave to compress a buffer gas disposed within the engine flow passages (41). The high pressure buffer gas is routed out of the wave rotor (22) and subseq...
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WO/2001/092702A1 |
A gas turbine unit has a fuel gas compressor system (5) for increasing the pressure of a fuel gas before entering a fuel system of the gas turbine unit, the fuel gas compressor system comprising at least one compressor (10, 12), gas inle...
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WO/2001/092703A1 |
The invention concerns a method of operating a combustion plant comprising at least a first gas turbine (26), a second turbine (34, 50) and a membrane reactor device (16) which comprises a membrane filter device (18) for separating oxyge...
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WO/2001/092688A2 |
Improvements to an annular, radial flow gas turbine engine (14) and airborne vehicle (10) utilizing the same for jet propulsion are disclosed herein. The engine (14) includes counter-rotating rotors and a compressor section with counter-...
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WO/2001/090548A1 |
A semi-closed combined cycle system (100) is provided which converts an open cycle gas turbine (10) into a non-polluting power system. The prior art gas turbine (10) includes a compressor (20) which compresses air (A') and combusts the a...
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WO/2001/088342A1 |
A land based gas turbine plant includes a turbine compressor (24), a turbine section (34), and a combustor (28) between the compressor and the turbine section. A heat recovery boiler (18) incorporating at least one heat exchange section ...
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WO/2001/086130A1 |
A gas turbine unit (20) has a rotor unit (10) comprising a mono-shaft (30), a compressor wheel (40), a turbine wheel (50), a tie bolt (60), and a tie bolt nut (70). The mono-shaft (30) is essentially cylinder-shaped with a centre through...
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WO/2001/083963A1 |
An annular combustor (10) has an annular inner shell (15), an annular outer shell (20) and a dome end wall (30) connecting the inner shell (15) with the outer shell (20). A dam (45) is positioned between the dome end wall (30) and the ex...
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WO/2001/075277A1 |
A method of generating power with sequestration of carbon-dioxide includes compressing ambient air, separating substantially pure oxygen from the air and then further compressing the oxygen. After compression the oxygen is divided into a...
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WO/2001/073267A1 |
A hybrid combined cycle power generation system (figure 3) for producing alternating current power comprising of at least one industrial gas turbine and at least one aeroderivative turbine. The system may also include an HRSG and a steam...
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WO/2001/062592A2 |
An air inlet assembly for bringing air to an auxiliary power unit (10) mounted in the APU compartment (12) of an aircraft (14). The assembly includes a duct (30) extending from an intake (32) contoured to conform to the aircraft fuselage...
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WO/2001/057379A1 |
A gasification combined cycle plant is combined with a Kalina bottoming cycle. Thermal energy streams (31, 69, 169) from a gasification system (48, 50, 52) are provided in heat exchange with the working fluid mixture of a Kalina cycle to...
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WO/2001/053660A1 |
Disclosed is a gas and steam turbine installation (1) comprising a gasification device (132) for fossile fuel. The gasification device (132) and the combustion chamber (6) of the gas turbine (2) are connected by means of a gas line (130)...
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WO/2001/051773A1 |
An elevated pressure power plant (100) for cleanly and efficiently oxidizing, gasifying or combusting a fuel. The fuel is oxidized or gasified in a reaction chamber (210) at a pressure range from approximately 700 psia to 2000 psia, or f...
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WO2000020738A9 |
A gas turbine engine has a turbine (12) mounted downstream of a compressor (16) and a compressor turbine (18) mounted downstream of the turbine (12) for driving the compressor (16). The compressor turbine (18) has a rotor disk that is me...
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WO/2001/045822A1 |
A filter assembly is made for filtering hot gas within a cleanup system pressure vessel (22), where the filter assembly (60) contains a filter housing (62) having an interior chamber (66), and a filter element (28) attached to the bottom...
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WO/2001/042636A1 |
The invention is directed to a method of fueling gas turbines from natural gas reserves with relatively low methane concentrations. The invention permits the use of such reserves to be used to fuel gas turbines to generate electric power...
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WO/2001/036566A1 |
A light portion is extracted from feed oil by a separation system. The light portion is then subject to a hydrotreatment to obtain impurity-removed fuel oil which is stored in an intermediate tank. A residue of the feed oil after extract...
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WO/2001/034955A1 |
A process is described for achieving a reduction in regulated emissions of combustion products from power generation apparatus including an industrial gas turbine or turbines, while at the same time providing a desired level of power pro...
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WO/2001/031180A2 |
A gas turbine engine comprising a compressor, a power turbine, a counter-rotating compressor turbine for powering the compressor and a heat exchanger interconnected among them, uses a mixer to mix waste fluid heater by the heat exchanger...
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WO/2001/029376A1 |
Engine with rotary combustion chamber (20) and ram jet compressor (7). An engine which is particularly suitable for propulsion of a water craft using direct thrust has a rotary body (1, 4) which includes a ram jet compression section (12...
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WO/2001/027451A1 |
A method of operating a gas turbine engine having a compressor, a combustor between a waste fluid compressor and a power turbine, a counter-rotating compressor turbine installed downstream of the power turbine, and a heat exchanger havin...
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WO/2001/018404A1 |
A deswirler system for a centrifugal compressor of a gas turbine engine that improves overall engine performance as a result of exhibiting significantly reduced friction losses. The deswirler system generally entails an annular-shaped ma...
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WO/2001/016471A1 |
The invention relates to a method in which an air mass flow (m) supplied to a compressor (8) in a power plant (2) is divided in a flow divider (20) into a smaller partial flow (t1) and into a larger partial flow (t2). The smaller partial...
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