Two-stage pressurizer

The invention discloses a two-stage pressurizer. The two-stage pressurizer comprises a split type switching valve, a turbine shell exit piping, a gas compressor shell entrance piping, a split type check valve, a turbine, two turbine shafts, a bearing shell, a gas compressor impeller, a turbine shell...

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Hauptverfasser: EGUCHI MASATOSHI, ZHANG YANHUI
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creator EGUCHI MASATOSHI
ZHANG YANHUI
description The invention discloses a two-stage pressurizer. The two-stage pressurizer comprises a split type switching valve, a turbine shell exit piping, a gas compressor shell entrance piping, a split type check valve, a turbine, two turbine shafts, a bearing shell, a gas compressor impeller, a turbine shell, a gas compressor shell, a waste gas bypass valve and an actuator; a turbine shell separation strip separates the turbine shell into a low-speed turbine shell cavity and a high-speed turbine shell cavity; a gas compressor shell separation strip separates the gas compressor shell into a low-speed gas compressor cavity channel and a high-speed gas compressor cavity channel; the two turbine shafts are opposite in rotation direction, and the waste gas bypass valve is mounted on a turbine shell low-speed pressurizing waste gas entrance pipe. According to the two-stage pressurizer, the two turbine shafts rotate in opposite directions, and the turbine rotation directions of a low-speed pressurizing area and a high-speed pressurizing area are opposite; the gas compressor impeller rotation directions of the low-speed pressurizing area and the high-speed pressurizing area are opposite, so that the structure design arrangement of one integrated turbine shell, the gas compressor shell and one exhaust divided manifold is achieved, the space can be largely reduced, and the problem that an engine is inconvenient to arrange is solved; a waste gas bypass valve of the high-speed pressurizing area and a split type switching valve actuator are omitted, so that the manufacturing cost is reduced.
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subjects BLASTING
CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION
COMBUSTION ENGINES
COMBUSTION ENGINES IN GENERAL
GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
INTERNAL-COMBUSTION PISTON ENGINES
LIGHTING
MECHANICAL ENGINEERING
TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE
WEAPONS
title Two-stage pressurizer
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