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Power Plants > Combustion Products Used As Motive Fluid > For Nominal Other Than Power Plant Output Feature

For Nominal Other Than Power Plant Output Feature

For Nominal Other Than Power Plant Output Feature patent applications listed include Date, Patent Application Number, Patent Title, Patent Abstract summary and are linked to the corresponding patent application page.

07/03/14 - 20140182306 - Filter for aircraft apu system
An auxiliary power unit (APU) system comprises an auxiliary power unit (APU) mounted in a compartment of an aircraft. A first air inlet conduit directs air to a first component disposed in the compartment. A first dry filter element is disposed within the first air inlet conduit, and has a...

02/13/14 - 20140041394 - Integration of power generation and post combustion capture plants
A method and system for integrating a power plant and a post combustion capture plant for producing carbon dioxide. The power plant can provide electricity to the post combustion capture plant created by passing steam from a boiler through turbines and feeding the flue gas created by heating the boiler...

01/30/14 - 20140026589 - Aircraft engine
To provide an aircraft engine in which an accessory can be directly supported with no accessory gearbox intervening to thereby suppress an increase in size thereof, the aircraft engine (E) includes a take-out shaft (11) having a first end portion, connected with an engine rotary shaft (9) and extending in...

01/23/14 - 20140020402 - Turbine
In one embodiment, a turbine using CO2 includes moving blades, stator blades, a working fluid transport flow path, a coolant transport flow path, and a coolant recovery flow path. The stator blades constitute turbine stages together with the moving blades. The working fluid transport flow path is configured to transport...

10/31/13 - 20130283816 - Turboprop-powered aircraft
A turboprop-powered medium altitude long endurance aircraft, having a gas turbine engine; a heat scavenging device to scavenge heat from the gas turbine engine; and a heating device to use the scavenged heat to provide heating to the aircraft. The heat scavenging device may be placed on an engine casing...

09/12/13 - 20130232990 - Apparatus for releasing a flow cross section of a gas line
An apparatus is described for the controlled release of a flow cross section of a gas line which is connected to a combustion chamber of a gas engine. The apparatus has a check valve and a flexible device. The flexible device is provided for absorbing a force occurring as a...

05/09/13 - 20130111922 - Flexible printed circuit board harness
A gas turbine engine installation is provided that has a flexible printed circuit board (FPCB) harness to transfer electrical signals, including electrical power, around a gas turbine engine. The FPCB harness is held to the gas turbine engine installation using clips. The clips have a jaw that has two sets...

04/18/13 - 20130091859 - Auxiliary power unit fluid system fluid control
An auxiliary power unit includes a turbomachine coupled to a generator. A flow path is arranged through the generator and is configured to provide fluid to the generator. A deprime valve is arranged in the flow path and is configured to pulse fluid flow to the generator in response to...

04/18/13 - 20130091860 - Fluid separator
The invention relates to a fluid separator 40 having first and second inlets, a turbine and a separation chamber having a centrifugal separation member. The first inlet is in direct fluid communication with a turbine inlet, and in use delivers high pressure vent air flow from a first gas turbine...

04/18/13 - 20130091861 - Turbine
A turbine includes a rotor having at least two rotor members for rotating in a plane, the rotor members being substantially diametrically arranged and attached to an axis situated substantially transversely to the plane, and drive unit coupled to the axis, wherein the rotor members include a fluid contact member,...

12/20/12 - 20120317991 - Transverse mounted accessory gearbox
A gas turbine engine and an accessory gear box (AGB) are provided for. The gas turbine engine comprises a drive shaft, a compressor, a combustor and an exhaust turbine, where the exhaust turbine and the compressor are coaxially connected by the drive shaft. The gas turbine engine further comprises an...

12/20/12 - 20120317992 - Feed injector for gasification system
The present application and the resultant patent provide a feed injector nozzle for a gasification system with a reaction zone therein. The feed injector nozzle may include a number of tubes extending towards the reaction zone. The tubes may define a number of passages therebetween. A cooling water channel may...

07/19/12 - 20120180499 - Power generation system
A power generation system is provided and includes a compressor to increase a pressure of inlet ambient air and a turbine downstream from the compressor having a first stage and additional stages downstream from the first stage, the first stage structurally incorporating a combustor in which the compressed ambient air...

05/24/12 - 20120125012 - Processes and systems for discharging amine byproducts formed in an amine-based solvent
Embodiments of a process for discharging amine byproducts formed in an amine-based solvent are provided. The process comprises the steps of contacting the amine-based solvent with flue gas comprising carbon dioxide, oxygen, nitrogen, NOx, SOx, or mixtures thereof to form a carbon dioxide-laden amine-based solvent that contains the amine byproducts....

10/06/11 - 20110239660 - Mounting arrangement for gas turbine engine accessories and gearbox therefor
Gas turbine engine accessories are mounted on an accessory gearbox therefor which is in turn mounted on a case of the engine such that the accessories extend from the gearbox in directions generally parallel to circumferential tangents to the engine case for compactness, ease in installation and removal of the...

07/07/11 - 20110162385 - System for providing air flow to a sulfur recovery unit
A system includes a sulfur recovery unit including a thermal reactor having an acid gas inlet and an air inlet. The acid gas inlet is configured to receive a flow of acid gas, and the air inlet is configured to receive an air flow of pressurized air extracted from a...

09/23/10 - 20100236255 - Gas turbine equipment utilizing high humidity
A gas turbine equipment utilizing high humidity, for preventing generation of white smoke throughout a year, and for restraining radiation of extra heat so as to restrain lowering of heat efficiency, the equipment comprising a humidifying device for humidifying compressed gas for combustion, a heat recovery device for recovering exhaust...

05/06/10 - 20100107650 - Gas turbine engine accessory system
In one embodiment, a gas turbine engine may include an accessory system integrated in a frame between a bypass flow path and a core flow path. A shaft may be provided between the accessory system and a core shaft of the gas turbine engine. The integrated accessory system may include...

05/06/10 - 20100107651 - Hybrid propulsive engine including at least one independently rotatable compressor stator
One aspect relates to a hybrid propulsive technique, comprising providing a flow of a working fluid through at least a portion of an at least one jet engine. The hybrid propulsive technique comprises extracting energy from the working fluid that is at least partially converted into electrical power, and converting...

05/06/10 - 20100107652 - Hybrid propulsive engine including at least one independently rotatable compressor rotor
One aspect relates to a hybrid propulsive technique, comprising providing at least some first thrust associated with a flow of a working fluid through at least a portion of an at least one axial flow jet engine. The hybrid propulsive technique includes extracting energy at least partially in the form...

02/11/10 - 20100031669 - Free turbine generator for aircraft
A turbine engine for an aircraft is disclosed. The turbine includes a turbine generator which is not connected to the low or high pressure spools of the turbine engine. The generator is used to create power for use in electrical systems in the aircraft. In some embodiments, the free-turbine airfoils...

01/07/10 - 20100000225 - Combined heat, ice, power, and steam system
A power generation plant generates electrical power to be distributed to consumers via a power grid. The plant also provides some of the power to a fuel processing facility that provides fuel for the plant, and re-cycles the by-products of the power generation process to provide at least some of...

01/07/10 - 20100000226 - Turbofan engine with at least one apparatus for driving at least one generator
A turbofan engine (1) includes at least one apparatus (30) for driving at least one generator (22, 35), with the engine including a pre-compressor (4), at least one compressor (10) and at least two engine shafts (13, 15) rotatably arranged in an engine casing. At least one first generator (22)...

11/05/09 - 20090272121 - Gas turbine aircraft engine with power variability
A gas turbine aircraft engine with power variability is provided. The gas turbine aircraft engine comprises a compressor and a turbine mounted on a common shaft, and, a continuously variable transmission coupled to the shaft for transmitting power to a propulsion load....

10/15/09 - 20090255270 - Jet engine with at least one emergency drive unit
A jet engine (1) includes at least one emergency drive unit (10), with the jet engine (1) having at least one engine shaft (2a) coupled via at least one gear train (4) with at least one auxiliary gearbox (7), which is connected to at least one auxiliary equipment (8), especially...

05/07/09 - 20090113896 - Control apparatus and method for gas-turbine engine
There is provided a control apparatus for a gas-turbine engine which is configured in such a manner that a portion of compressed air from a compressor is supplied to a combustion chamber and the other portion of the compressed air is sent to the outside of the engine to be...

02/26/09 - 20090049841 - Gas turbine engine with a means of driving the accessory gear box, and method of fitting said engine
The invention relates to a twin-spool gas turbine engine comprising a high-pressure rotor (and a low-pressure rotor, which rotors are mounted in bearings supported by an intermediate casing, at least one accessory gear box, a drive means, driving radial and coaxial shafts for transmitting movement to the accessory gear box,...