About 16 results
https://drivepatents.com/patents/969019 · 8 Oct 2014
The invention relates to a gas turbine power plant (1), comprising a gas turbine (10) having a compressor (11), a combustion chamber (12), and an expander (13), as well as a water storage tank (20) at least partially filled with water, which is fluidically...
https://drivepatents.com/patents/971879 · 30 Jul 2014
A system and method is provided that improves the under frequency response of gas turbines by providing a fast-response power augmentation system. The system includes a tank (102) storing a blended mixture of motive fuel such as ethanol or methanol and dem...
https://drivepatents.com/patents/987428 · 14 Aug 2013
The method involves providing a compressor (4), a combustor (10), a turbine (12), and a flow channel (16) in gas turbine (1). The thermal energy is acquired from outlet of turbine by heat exchanger (22) in the flow channel. The thermal energy is transferre...
https://drivepatents.com/patents/991243 · 1 May 2013
A system includes a gas turbine engine having a combustor (10), a liquid fuel supply (50) coupled to the combustor (16), and a water supply (15) coupled to the liquid fuel supply (50). The water supply (15) is configured to flow water (15) through the liqu...
https://drivepatents.com/patents/991242 · 1 May 2013
A system includes a turbine fuel supply system (40). The turbine fuel supply system includes a first turbine fuel mixer (52) configured to mix a first liquid fuel (42) and a first deaerated water (15) to generate a first fuel mixture. The first fuel mixtur...
https://drivepatents.com/patents/993364 · 30 Jan 2013
In an axial compressor (10) for compressing air, particularly for a gas turbine, the axial compressor (10) has a rotor (11), which is rotatable around a machine axis (27), having a multiplicity of rotor blades (14) and also a casing (13, 13a, b) enclosing ...
https://drivepatents.com/patents/993336 · 30 Jan 2013
Method for injecting water into a multistage axial compressor (10) of a gas turbine to increase the power output, even under changing boundary conditions, wherein water is being injected at a plurality of points (18a - d) along the axial compressor; the in...
https://drivepatents.com/patents/996092 · 14 Nov 2012
A gas turbine engine (10) comprising a compressor (20), a combustion chamber (30) and a turbine (40) arranged in flow series, wherein the gas turbine engine further comprises: one or more combustion zones; a source of steam (60) configured to deliver steam...
https://drivepatents.com/patents/999784 · 1 Aug 2012
A drain discharge equipment of a compressor having a separator 13A, 13B for separating drain discharged from the compressor to compressed air and liquid drain, which is disposed on some part of a drain capture pipe 7, 8 connected between stages and/or to a...
https://drivepatents.com/patents/1010280 · 10 Aug 2011
A gas turbine engine steam injector (76) includes an annular steam injection manifold (80) aftwardly bounded by an aft manifold wall (81) having steam injection holes (78) disposed therethrough and located axially aft and radially inwardly of a diffuser ou...