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...
Gespeichert in:
Hauptverfasser: | , |
---|---|
Format: | Patent |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext bestellen |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | |
---|---|
container_issue | |
container_start_page | |
container_title | |
container_volume | |
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. |
format | Patent |
fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN104806343A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN104806343A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN104806343A3</originalsourceid><addsrcrecordid>eNrjZBANKc_XLS5JTE9VKChKLS4uLcqsSi3iYWBNS8wpTuWF0twMim6uIc4euqkF-fGpxQWJyal5qSXxzn6GBiYWBmbGJsaOxsSoAQCNZyFf</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Two-stage pressurizer</title><source>esp@cenet</source><creator>EGUCHI MASATOSHI ; ZHANG YANHUI</creator><creatorcontrib>EGUCHI MASATOSHI ; ZHANG YANHUI</creatorcontrib><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.</description><language>eng</language><subject>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</subject><creationdate>2015</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20150729&DB=EPODOC&CC=CN&NR=104806343A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20150729&DB=EPODOC&CC=CN&NR=104806343A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>EGUCHI MASATOSHI</creatorcontrib><creatorcontrib>ZHANG YANHUI</creatorcontrib><title>Two-stage pressurizer</title><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.</description><subject>BLASTING</subject><subject>CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION</subject><subject>COMBUSTION ENGINES</subject><subject>COMBUSTION ENGINES IN GENERAL</subject><subject>GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC</subject><subject>GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>INTERNAL-COMBUSTION PISTON ENGINES</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS</subject><subject>TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2015</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZBANKc_XLS5JTE9VKChKLS4uLcqsSi3iYWBNS8wpTuWF0twMim6uIc4euqkF-fGpxQWJyal5qSXxzn6GBiYWBmbGJsaOxsSoAQCNZyFf</recordid><startdate>20150729</startdate><enddate>20150729</enddate><creator>EGUCHI MASATOSHI</creator><creator>ZHANG YANHUI</creator><scope>EVB</scope></search><sort><creationdate>20150729</creationdate><title>Two-stage pressurizer</title><author>EGUCHI MASATOSHI ; ZHANG YANHUI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN104806343A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2015</creationdate><topic>BLASTING</topic><topic>CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION</topic><topic>COMBUSTION ENGINES</topic><topic>COMBUSTION ENGINES IN GENERAL</topic><topic>GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC</topic><topic>GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>INTERNAL-COMBUSTION PISTON ENGINES</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS</topic><topic>TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>EGUCHI MASATOSHI</creatorcontrib><creatorcontrib>ZHANG YANHUI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>EGUCHI MASATOSHI</au><au>ZHANG YANHUI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Two-stage pressurizer</title><date>2015-07-29</date><risdate>2015</risdate><abstract>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.</abstract><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | eng |
recordid | cdi_epo_espacenet_CN104806343A |
source | esp@cenet |
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 |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-27T03%3A19%3A25IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=EGUCHI%20MASATOSHI&rft.date=2015-07-29&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN104806343A%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true |