GEOTHERMAL TURBINE

PROBLEM TO BE SOLVED: To provide a geothermal turbine which can be operated with high efficiency.SOLUTION: In a geothermal turbine, the throat area of a nozzle blade constituting an initial-stage reserve nozzle diaphragm is smaller than the throat area of a nozzle blade constituting an initial-stage...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	MAEDOMARI JIYUNICHIROU, SUZUKI ATSUHIDE
Format:	Patent
Sprache:	eng ; jpn
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL ENGINE PLANTS NOT OTHERWISE PROVIDED FOR ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HEATING LIGHTING MACHINES OR ENGINES FOR LIQUIDS MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING MECHANICAL-POWER PRODUCING DEVICES OR MECHANISMS, NOTOTHERWISE PROVIDED FOR OR USING ENERGY SOURCES NOT OTHERWISEPROVIDED FOR NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR PRODUCING MECHANICAL POWER REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGYGENERATION, TRANSMISSION OR DISTRIBUTION SPRING, WEIGHT, INERTIA OR LIKE MOTORS STEAM ACCUMULATORS STEAM ENGINE PLANTS STEAM ENGINES TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE WEAPONS WIND, SPRING WEIGHT AND MISCELLANEOUS MOTORS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To provide a geothermal turbine which can be operated with high efficiency.SOLUTION: In a geothermal turbine, the throat area of a nozzle blade constituting an initial-stage reserve nozzle diaphragm is smaller than the throat area of a nozzle blade constituting an initial-stage nozzle diaphragm. 【課題】高い効率で運用することが可能な地熱タービンを提供する。【解決手段】地熱タービンは、初段予備ノズルダイヤフラムを構成するノズル翼のスロート面積が、初段ノズルタイヤフラムを構成するノズル翼のスロート面積よりも小さい。【選択図】図３