GAS TURBINE AND GAS TURBINE MANUFACTURING METHOD
According to an embodiment, a gas turbine (10, 10a) includes: a casing (13, 15); a rotor shaft (11) penetrating through the casing (13, 15); a plurality of turbine stages (12) which are in the casing (13, 15) and are arranged along an axial direction of the rotor shaft (11) and through which a worki...
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creator | Tashima, Tsuguhisa Ono, Takahiro Iwai, Shogo Takagi, Norikazu |
description | According to an embodiment, a gas turbine (10, 10a) includes: a casing (13, 15); a rotor shaft (11) penetrating through the casing (13, 15); a plurality of turbine stages (12) which are in the casing (13, 15) and are arranged along an axial direction of the rotor shaft (11) and through which a working fluid passes; two bearings (16a, 16b) disposed on outer sides of the casing (13, 15) in terms of the axial direction and supporting the rotor shaft (11) in a rotatable manner; and a plurality of outlet pipes (20) through which the working fluid having finished work in the turbine stages (12) is discharged. The outlet pipes (20) are provided in an upper half and a lower half of the casing (13, 15). |
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fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP3960999A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP3960999A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP3960999A13</originalsourceid><addsrcrecordid>eNrjZDBwdwxWCAkNcvL0c1Vw9HNRQOb7OvqFujk6A7mefu4Kvq4hHv4uPAysaYk5xam8UJqbQcHNNcTZQze1ID8-tbggMTk1L7Uk3jXA2NLMwNLS0tHQmAglANagJek</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>GAS TURBINE AND GAS TURBINE MANUFACTURING METHOD</title><source>esp@cenet</source><creator>Tashima, Tsuguhisa ; Ono, Takahiro ; Iwai, Shogo ; Takagi, Norikazu</creator><creatorcontrib>Tashima, Tsuguhisa ; Ono, Takahiro ; Iwai, Shogo ; Takagi, Norikazu</creatorcontrib><description>According to an embodiment, a gas turbine (10, 10a) includes: a casing (13, 15); a rotor shaft (11) penetrating through the casing (13, 15); a plurality of turbine stages (12) which are in the casing (13, 15) and are arranged along an axial direction of the rotor shaft (11) and through which a working fluid passes; two bearings (16a, 16b) disposed on outer sides of the casing (13, 15) in terms of the axial direction and supporting the rotor shaft (11) in a rotatable manner; and a plurality of outlet pipes (20) through which the working fluid having finished work in the turbine stages (12) is discharged. The outlet pipes (20) are provided in an upper half and a lower half of the casing (13, 15).</description><language>eng ; fre ; ger</language><subject>BLASTING ; ENGINE PLANTS IN GENERAL ; HEATING ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; STEAM ENGINES ; WEAPONS</subject><creationdate>2022</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=20220302&DB=EPODOC&CC=EP&NR=3960999A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20220302&DB=EPODOC&CC=EP&NR=3960999A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Tashima, Tsuguhisa</creatorcontrib><creatorcontrib>Ono, Takahiro</creatorcontrib><creatorcontrib>Iwai, Shogo</creatorcontrib><creatorcontrib>Takagi, Norikazu</creatorcontrib><title>GAS TURBINE AND GAS TURBINE MANUFACTURING METHOD</title><description>According to an embodiment, a gas turbine (10, 10a) includes: a casing (13, 15); a rotor shaft (11) penetrating through the casing (13, 15); a plurality of turbine stages (12) which are in the casing (13, 15) and are arranged along an axial direction of the rotor shaft (11) and through which a working fluid passes; two bearings (16a, 16b) disposed on outer sides of the casing (13, 15) in terms of the axial direction and supporting the rotor shaft (11) in a rotatable manner; and a plurality of outlet pipes (20) through which the working fluid having finished work in the turbine stages (12) is discharged. The outlet pipes (20) are provided in an upper half and a lower half of the casing (13, 15).</description><subject>BLASTING</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>STEAM ENGINES</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDBwdwxWCAkNcvL0c1Vw9HNRQOb7OvqFujk6A7mefu4Kvq4hHv4uPAysaYk5xam8UJqbQcHNNcTZQze1ID8-tbggMTk1L7Uk3jXA2NLMwNLS0tHQmAglANagJek</recordid><startdate>20220302</startdate><enddate>20220302</enddate><creator>Tashima, Tsuguhisa</creator><creator>Ono, Takahiro</creator><creator>Iwai, Shogo</creator><creator>Takagi, Norikazu</creator><scope>EVB</scope></search><sort><creationdate>20220302</creationdate><title>GAS TURBINE AND GAS TURBINE MANUFACTURING METHOD</title><author>Tashima, Tsuguhisa ; Ono, Takahiro ; Iwai, Shogo ; Takagi, Norikazu</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3960999A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2022</creationdate><topic>BLASTING</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>STEAM ENGINES</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>Tashima, Tsuguhisa</creatorcontrib><creatorcontrib>Ono, Takahiro</creatorcontrib><creatorcontrib>Iwai, Shogo</creatorcontrib><creatorcontrib>Takagi, Norikazu</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Tashima, Tsuguhisa</au><au>Ono, Takahiro</au><au>Iwai, Shogo</au><au>Takagi, Norikazu</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>GAS TURBINE AND GAS TURBINE MANUFACTURING METHOD</title><date>2022-03-02</date><risdate>2022</risdate><abstract>According to an embodiment, a gas turbine (10, 10a) includes: a casing (13, 15); a rotor shaft (11) penetrating through the casing (13, 15); a plurality of turbine stages (12) which are in the casing (13, 15) and are arranged along an axial direction of the rotor shaft (11) and through which a working fluid passes; two bearings (16a, 16b) disposed on outer sides of the casing (13, 15) in terms of the axial direction and supporting the rotor shaft (11) in a rotatable manner; and a plurality of outlet pipes (20) through which the working fluid having finished work in the turbine stages (12) is discharged. The outlet pipes (20) are provided in an upper half and a lower half of the casing (13, 15).</abstract><oa>free_for_read</oa></addata></record> |
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language | eng ; fre ; ger |
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subjects | BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS |
title | GAS TURBINE AND GAS TURBINE MANUFACTURING METHOD |
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