DEVICE FOR PIVOTING A ROTOR OF A TURBOMACHINE FROM A FIRST POSITION INTO A SECOND POSITION

Device (12) for pivoting a rotor (10) of a turbomachine from a first - preferably horizontal - position (10a) into a second - preferably vertical - position (10c), wherein the rotor (10) comprises a plurality of rotor discs held together by at least one tension rod, said device comprising two sidewa...

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Hauptverfasser: Carsten, FOERSTER, Armin, HÜLFENHAUS
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Armin, HÜLFENHAUS
description Device (12) for pivoting a rotor (10) of a turbomachine from a first - preferably horizontal - position (10a) into a second - preferably vertical - position (10c), wherein the rotor (10) comprises a plurality of rotor discs held together by at least one tension rod, said device comprising two sidewall elements (24) arranged parallel to one another, a bridge element (28) connecting the sidewall elements (28) to one another, and a divisible turning ring (30) for form-fittingly holding an axial section of the rotor to be positioned perpendicularly (10) and two pins (32) rotatably seated in the sidewall elements (24) and arranged flush to the turning ring (30) in order to pivot the turning ring (30) about a pivot axis parallel to the horizontal plane (31). In order to achieve a particularly secure mounting of the perpendicularly positioned rotor (10) it is proposed that a disc (42) is provided in the bridge element (28), said disc being movable perpendicularly to the horizontal plane (18) in order to be bolted in a flange-like manner onto a rotor (10) retained by the device (12). Dispositivo (12) para pivotar un rotor (10) de una turbomáquina de una primera posición (10a) preferentemente horizontal a una segunda posición (10c) preferentemente vertical, comprendiendo el rotor (10) varios discos de rotor atirantados entre ellos por al menos un tirante, comprendiendo el dispositivo dos elementos laterales (24) dispuestos paralelamente uno respecto a otro, un elemento de puente (28) que une dichos elementos laterales (24) entre ellos y un anillo volvedor (30) divisible para el alojamiento por unión geométrica de una sección axial del rotor (10) que se ha de levantar y dos pivotes (32) dispuestos de forma alineada en el anillo volvedor (30) y soportados de forma giratoria en los elementos laterales (24) para pivotar el anillo volvedor (30) alrededor de un eje de pivotamiento (31) paralelo con respecto al plano horizontal. Para conseguir una fijación especialmente segura del rotor (10) colocado verticalmente se propone que dentro del elemento de puente (28) esté soportado un disco (42) desplazable perpendicularmente con respecto al plano horizontal (18) para la unión roscada a modo de brida a un rotor (10) colocado perpendicularmente y sujeto por el dispositivo (12).
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In order to achieve a particularly secure mounting of the perpendicularly positioned rotor (10) it is proposed that a disc (42) is provided in the bridge element (28), said disc being movable perpendicularly to the horizontal plane (18) in order to be bolted in a flange-like manner onto a rotor (10) retained by the device (12). 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Para conseguir una fijación especialmente segura del rotor (10) colocado verticalmente se propone que dentro del elemento de puente (28) esté soportado un disco (42) desplazable perpendicularmente con respecto al plano horizontal (18) para la unión roscada a modo de brida a un rotor (10) colocado perpendicularmente y sujeto por el dispositivo (12).</description><language>eng ; spa</language><subject>BLASTING ; ENGINE PLANTS IN GENERAL ; ENGINEERING ELEMENTS AND UNITS ; FRAMES, CASINGS, OR BEDS OF ENGINES OR OTHER MACHINES ORAPPARATUS NOT SPECIFIC TO AN ENGINE, MACHINE, OR APPARATUSPROVIDED FOR ELSEWHERE ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; HEATING ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; STANDS OR SUPPORTS ; STEAM ENGINES ; THERMAL INSULATION IN GENERAL ; WEAPONS</subject><creationdate>2016</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&amp;date=20160809&amp;DB=EPODOC&amp;CC=MX&amp;NR=341272B$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25563,76318</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20160809&amp;DB=EPODOC&amp;CC=MX&amp;NR=341272B$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Carsten, FOERSTER</creatorcontrib><creatorcontrib>Armin, HÜLFENHAUS</creatorcontrib><title>DEVICE FOR PIVOTING A ROTOR OF A TURBOMACHINE FROM A FIRST POSITION INTO A SECOND POSITION</title><description>Device (12) for pivoting a rotor (10) of a turbomachine from a first - preferably horizontal - position (10a) into a second - preferably vertical - position (10c), wherein the rotor (10) comprises a plurality of rotor discs held together by at least one tension rod, said device comprising two sidewall elements (24) arranged parallel to one another, a bridge element (28) connecting the sidewall elements (28) to one another, and a divisible turning ring (30) for form-fittingly holding an axial section of the rotor to be positioned perpendicularly (10) and two pins (32) rotatably seated in the sidewall elements (24) and arranged flush to the turning ring (30) in order to pivot the turning ring (30) about a pivot axis parallel to the horizontal plane (31). In order to achieve a particularly secure mounting of the perpendicularly positioned rotor (10) it is proposed that a disc (42) is provided in the bridge element (28), said disc being movable perpendicularly to the horizontal plane (18) in order to be bolted in a flange-like manner onto a rotor (10) retained by the device (12). Dispositivo (12) para pivotar un rotor (10) de una turbomáquina de una primera posición (10a) preferentemente horizontal a una segunda posición (10c) preferentemente vertical, comprendiendo el rotor (10) varios discos de rotor atirantados entre ellos por al menos un tirante, comprendiendo el dispositivo dos elementos laterales (24) dispuestos paralelamente uno respecto a otro, un elemento de puente (28) que une dichos elementos laterales (24) entre ellos y un anillo volvedor (30) divisible para el alojamiento por unión geométrica de una sección axial del rotor (10) que se ha de levantar y dos pivotes (32) dispuestos de forma alineada en el anillo volvedor (30) y soportados de forma giratoria en los elementos laterales (24) para pivotar el anillo volvedor (30) alrededor de un eje de pivotamiento (31) paralelo con respecto al plano horizontal. Para conseguir una fijación especialmente segura del rotor (10) colocado verticalmente se propone que dentro del elemento de puente (28) esté soportado un disco (42) desplazable perpendicularmente con respecto al plano horizontal (18) para la unión roscada a modo de brida a un rotor (10) colocado perpendicularmente y sujeto por el dispositivo (12).</description><subject>BLASTING</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>ENGINEERING ELEMENTS AND UNITS</subject><subject>FRAMES, CASINGS, OR BEDS OF ENGINES OR OTHER MACHINES ORAPPARATUS NOT SPECIFIC TO AN ENGINE, MACHINE, OR APPARATUSPROVIDED FOR ELSEWHERE</subject><subject>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</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>STANDS OR SUPPORTS</subject><subject>STEAM ENGINES</subject><subject>THERMAL INSULATION IN GENERAL</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2016</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZIhycQ3zdHZVcPMPUgjwDPMP8fRzV3BUCPIPAQr4uwGZIaFBTv6-js4enn5AZUH-vkAxN8-g4BCFAP9gzxBPfz8FT78Qf6BosKuzv58LXJiHgTUtMac4lRdKczPIubmGOHvophbkx6cWFyQmp-allsT7RhibGBqZGzkZE1QAAAagMF4</recordid><startdate>20160809</startdate><enddate>20160809</enddate><creator>Carsten, FOERSTER</creator><creator>Armin, HÜLFENHAUS</creator><scope>EVB</scope></search><sort><creationdate>20160809</creationdate><title>DEVICE FOR PIVOTING A ROTOR OF A TURBOMACHINE FROM A FIRST POSITION INTO A SECOND POSITION</title><author>Carsten, FOERSTER ; Armin, HÜLFENHAUS</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_MX341272B3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; spa</language><creationdate>2016</creationdate><topic>BLASTING</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>ENGINEERING ELEMENTS AND UNITS</topic><topic>FRAMES, CASINGS, OR BEDS OF ENGINES OR OTHER MACHINES ORAPPARATUS NOT SPECIFIC TO AN ENGINE, MACHINE, OR APPARATUSPROVIDED FOR ELSEWHERE</topic><topic>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</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>STANDS OR SUPPORTS</topic><topic>STEAM ENGINES</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>Carsten, FOERSTER</creatorcontrib><creatorcontrib>Armin, HÜLFENHAUS</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Carsten, FOERSTER</au><au>Armin, HÜLFENHAUS</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>DEVICE FOR PIVOTING A ROTOR OF A TURBOMACHINE FROM A FIRST POSITION INTO A SECOND POSITION</title><date>2016-08-09</date><risdate>2016</risdate><abstract>Device (12) for pivoting a rotor (10) of a turbomachine from a first - preferably horizontal - position (10a) into a second - preferably vertical - position (10c), wherein the rotor (10) comprises a plurality of rotor discs held together by at least one tension rod, said device comprising two sidewall elements (24) arranged parallel to one another, a bridge element (28) connecting the sidewall elements (28) to one another, and a divisible turning ring (30) for form-fittingly holding an axial section of the rotor to be positioned perpendicularly (10) and two pins (32) rotatably seated in the sidewall elements (24) and arranged flush to the turning ring (30) in order to pivot the turning ring (30) about a pivot axis parallel to the horizontal plane (31). In order to achieve a particularly secure mounting of the perpendicularly positioned rotor (10) it is proposed that a disc (42) is provided in the bridge element (28), said disc being movable perpendicularly to the horizontal plane (18) in order to be bolted in a flange-like manner onto a rotor (10) retained by the device (12). Dispositivo (12) para pivotar un rotor (10) de una turbomáquina de una primera posición (10a) preferentemente horizontal a una segunda posición (10c) preferentemente vertical, comprendiendo el rotor (10) varios discos de rotor atirantados entre ellos por al menos un tirante, comprendiendo el dispositivo dos elementos laterales (24) dispuestos paralelamente uno respecto a otro, un elemento de puente (28) que une dichos elementos laterales (24) entre ellos y un anillo volvedor (30) divisible para el alojamiento por unión geométrica de una sección axial del rotor (10) que se ha de levantar y dos pivotes (32) dispuestos de forma alineada en el anillo volvedor (30) y soportados de forma giratoria en los elementos laterales (24) para pivotar el anillo volvedor (30) alrededor de un eje de pivotamiento (31) paralelo con respecto al plano horizontal. Para conseguir una fijación especialmente segura del rotor (10) colocado verticalmente se propone que dentro del elemento de puente (28) esté soportado un disco (42) desplazable perpendicularmente con respecto al plano horizontal (18) para la unión roscada a modo de brida a un rotor (10) colocado perpendicularmente y sujeto por el dispositivo (12).</abstract><oa>free_for_read</oa></addata></record>
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subjects BLASTING
ENGINE PLANTS IN GENERAL
ENGINEERING ELEMENTS AND UNITS
FRAMES, CASINGS, OR BEDS OF ENGINES OR OTHER MACHINES ORAPPARATUS NOT SPECIFIC TO AN ENGINE, MACHINE, OR APPARATUSPROVIDED FOR ELSEWHERE
GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS
HEATING
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
STANDS OR SUPPORTS
STEAM ENGINES
THERMAL INSULATION IN GENERAL
WEAPONS
title DEVICE FOR PIVOTING A ROTOR OF A TURBOMACHINE FROM A FIRST POSITION INTO A SECOND POSITION
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