Power plants – Combustion products used as motive fluid – Multiple fluid-operated motors
Reexamination Certificate
2002-06-19
2004-04-27
Koczo, Michael (Department: 3746)
Power plants
Combustion products used as motive fluid
Multiple fluid-operated motors
Reexamination Certificate
active
06725643
ABSTRACT:
BACKGROUND OF THE INVENTION
This invention relates to a new gas turbine power generator with ultra high efficiency.
Actual gas turbine power generator systems, working on simple Brayton cycle, have a limited thermal efficiency near 30%, low power density and degraded thermal efficiency at part loads. This low level of efficiency and power density is the result of low pressure ratio, reduced turbine inlet temperature and a very high air-fuel ratio. Degraded efficiency at part loads is a result of lower pressure ratios associated with reduced power and a lower turbine inlet temperature.
Additionally, typical gas turbines combustion is associated with high level of NOX emission. The result of all these associated, undesirable characteristics is the limited use of gas turbines for power generation leaving the use of gas turbines only for-Peak Shave-power generation and limited time operation (2-3 hours from 24) resulting in high investment for very low income. Typical gas turbines are using a waste-gate system for controlling the overloads. This novel invention eliminates these disadvantages by select integrated turbine configurations that improve the efficiency of power generation for different power demands.
SUMMARY OF THE INVENTION
A first characteristic of the new gas turbine power generator is the capability to work at very high pressure ratios of 60-100, which produces thermal efficiencies in the range of 70-80%, eliminating the complexity and ultra high cost of combined cycles in conventional multiple-stage, external co-generation systems.
A second characteristic of the new gas turbine power generator is the capability to operate at a constant pressure ratio in all the practical ranges of operation, from full load to part loads, resulting in a constant maximum thermal efficiency and in a constant optimum minimum flat specific fuel consumption, using new arrangements of counter rotating gas turbine and counter rotating compressor assemblies, and integrated turbine configurations.
A third characteristic of the new gas turbine power generator is the capability to work at variable mass flow, from full capacity to low mass flow with constant pressure ratio, using the counter rotating compressor and counter rotating turbine, or the cascade of power generation using integrated turbine configurations.
A fourth characteristic of the new gas turbine power generator is the implementation of a preferred high frequency pulsatory combustion, eliminating the compact combustion flame, by including in select configurations multiple air and steam infusions for reduction of local high temperature concentrations.
A fifth characteristic of the new gas turbine power generator in select systems is the combined steam generation and combustion chamber for internal steam co-generation and low compression work.
A sixth characteristic of the new gas turbine power generator in select systems is the use of new electrical motor generator machines based on this concept and the implementation of an intake side-driving shaft, eliminating the necessity for high pressure sealing systems.
A seventh characteristic of the new gas turbine power generator is the elimination of the waste-gate system.
An eighth characteristic of the new gas turbine power generator in select systems is to have all the compressors and turbines attached in total axial balance, with zero axial loads, forming groups of modules for turbo compressors-turbines, compressors-compressors and turbines-turbines.
A ninth characteristic of the new gas turbine power generator in select systems is a combination of multiple integrated gas turbines for a cascade of power generation.
A tenth characteristic is the preferred inclusion of air assisted foil bearings for minimizing system losses.
REFERENCES:
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patent: 2390959 (1945-12-01), Pfenninger
patent: 3765169 (1973-10-01), Kyrklund
patent: 4843813 (1989-07-01), Paul
patent: 5119624 (1992-06-01), McKenna
patent: 6282897 (2001-09-01), Paul
patent: 6418707 (2002-07-01), Paul
patent: 6460324 (2002-10-01), Rakhmailov
Koczo Michael
Peterson Richard Esty
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