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Title:
VARIOUS FULL ROTOR BLADE STEAM GAS TURBINE COMBINED- ENGINE
Document Type and Number:
Japanese Patent JP2002303152
Kind Code:
A
Abstract:

To switch to the driving of an internal combustion engine of zero combustion gas exhaust and to prevent the global warming with an electricity bill of 1/3 by allowing a gas turbine exhaust temperature to be close to -273°C, and coagulating the water and the water vapor while using the very low temperature combustion gas as a core for fractional recovery, as the prevention of global warming is urgent need.

The combustion gas exhaust temperature is allowed to be close to -273°C by unlimitedly performing the combustion heat exchange by means of a combustor/heat exchanger of a full rotor blade steam gas turbine combined-engine, the approximately whole amount of heat of the compressed air higher than -273°C is recovered to recover the heat of about two times of that in a conventional boiler, the heating high temperature can be surely and easily achieved by annular-type casting of every stage in a process of increasing the output of a gas turbine by 20-30 times and 4-6 times of an existing gas turbine, and further a vaporization film is formed between a heating high temperature turbine blade and the water of gravitational power of 1700 times and the like to remarkably reduce the heat consumption frictional loss with a simple structure, whereby the full rotor blade steam gas turbine combined-engine of idea output of 24-36 times of the existing gas turbine can be provided, and the thermodynamic brainwashing is excluded.


Inventors:
TANIGAWA HIROYASU
Application Number:
JP2001312338A
Publication Date:
October 18, 2002
Filing Date:
October 10, 2001
Export Citation:
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Assignee:
TANIGAWA HIROYASU
TANIGAWA KAZUNAGA
International Classes:
A01K61/00; F02C3/067; F02C3/113; F02C3/26; F02C3/30; F16H13/04; F16H13/08; F16H13/12; (IPC1-7): F02C3/113; A01K61/00; F02C3/067; F02C3/26; F02C3/30; F16H13/04; F16H13/08; F16H13/12