ROTOR COMPRISING A ROTOR COMPONENT ARRANGED BETWEEN TWO ROTOR DISKS
A rotor of a gas turbine, having two adjacent rotor disks having a plurality of blade-holding grooves for receiving rotor blades, distributed around the periphery thereof, and having an axially extending peripheral ring projection radially beneath the blade-holding grooves. A peripheral rotor compon...
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creator | Kolk, Karsten Veitsman, Vyacheslav Schröder, Peter Ross, Christopher W Waddell, Andrew Kury, Peter Hoell, Harald Bagaeva, Yulia |
description | A rotor of a gas turbine, having two adjacent rotor disks having a plurality of blade-holding grooves for receiving rotor blades, distributed around the periphery thereof, and having an axially extending peripheral ring projection radially beneath the blade-holding grooves. A peripheral rotor component is fixed to the ring projections, between the rotor disks. In order to protect the periphery, the rotor disk or the rotor component includes at least two recesses arranged on the periphery in a distributed manner, in each of which engaging shoulders of the rotor component or the rotor disk engage. |
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A peripheral rotor component is fixed to the ring projections, between the rotor disks. In order to protect the periphery, the rotor disk or the rotor component includes at least two recesses arranged on the periphery in a distributed manner, in each of which engaging shoulders of the rotor component or the rotor disk engage.</description><language>eng</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>2021</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=20211007&DB=EPODOC&CC=US&NR=2021310359A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20211007&DB=EPODOC&CC=US&NR=2021310359A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Kolk, Karsten</creatorcontrib><creatorcontrib>Veitsman, Vyacheslav</creatorcontrib><creatorcontrib>Schröder, Peter</creatorcontrib><creatorcontrib>Ross, Christopher W</creatorcontrib><creatorcontrib>Waddell, Andrew</creatorcontrib><creatorcontrib>Kury, Peter</creatorcontrib><creatorcontrib>Hoell, Harald</creatorcontrib><creatorcontrib>Bagaeva, Yulia</creatorcontrib><title>ROTOR COMPRISING A ROTOR COMPONENT ARRANGED BETWEEN TWO ROTOR DISKS</title><description>A rotor of a gas turbine, having two adjacent rotor disks having a plurality of blade-holding grooves for receiving rotor blades, distributed around the periphery thereof, and having an axially extending peripheral ring projection radially beneath the blade-holding grooves. A peripheral rotor component is fixed to the ring projections, between the rotor disks. In order to protect the periphery, the rotor disk or the rotor component includes at least two recesses arranged on the periphery in a distributed manner, in each of which engaging shoulders of the rotor component or the rotor disk engage.</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>2021</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHAO8g_xD1Jw9vcNCPIM9vRzV3BUQAj5-7n6hSg4BgU5-rm7uig4uYaEu7r6KYSE-0MVuXgGewfzMLCmJeYUp_JCaW4GZTfXEGcP3dSC_PjU4oLE5NS81JL40GAjAyNDY0MDY1NLR0Nj4lQBAP-1LKk</recordid><startdate>20211007</startdate><enddate>20211007</enddate><creator>Kolk, Karsten</creator><creator>Veitsman, Vyacheslav</creator><creator>Schröder, Peter</creator><creator>Ross, Christopher W</creator><creator>Waddell, Andrew</creator><creator>Kury, Peter</creator><creator>Hoell, Harald</creator><creator>Bagaeva, Yulia</creator><scope>EVB</scope></search><sort><creationdate>20211007</creationdate><title>ROTOR COMPRISING A ROTOR COMPONENT ARRANGED BETWEEN TWO ROTOR DISKS</title><author>Kolk, Karsten ; Veitsman, Vyacheslav ; Schröder, Peter ; Ross, Christopher W ; Waddell, Andrew ; Kury, Peter ; Hoell, Harald ; Bagaeva, Yulia</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2021310359A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2021</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>Kolk, Karsten</creatorcontrib><creatorcontrib>Veitsman, Vyacheslav</creatorcontrib><creatorcontrib>Schröder, Peter</creatorcontrib><creatorcontrib>Ross, Christopher W</creatorcontrib><creatorcontrib>Waddell, Andrew</creatorcontrib><creatorcontrib>Kury, Peter</creatorcontrib><creatorcontrib>Hoell, Harald</creatorcontrib><creatorcontrib>Bagaeva, Yulia</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Kolk, Karsten</au><au>Veitsman, Vyacheslav</au><au>Schröder, Peter</au><au>Ross, Christopher W</au><au>Waddell, Andrew</au><au>Kury, Peter</au><au>Hoell, Harald</au><au>Bagaeva, Yulia</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>ROTOR COMPRISING A ROTOR COMPONENT ARRANGED BETWEEN TWO ROTOR DISKS</title><date>2021-10-07</date><risdate>2021</risdate><abstract>A rotor of a gas turbine, having two adjacent rotor disks having a plurality of blade-holding grooves for receiving rotor blades, distributed around the periphery thereof, and having an axially extending peripheral ring projection radially beneath the blade-holding grooves. A peripheral rotor component is fixed to the ring projections, between the rotor disks. In order to protect the periphery, the rotor disk or the rotor component includes at least two recesses arranged on the periphery in a distributed manner, in each of which engaging shoulders of the rotor component or the rotor disk engage.</abstract><oa>free_for_read</oa></addata></record> |
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language | eng |
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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 | ROTOR COMPRISING A ROTOR COMPONENT ARRANGED BETWEEN TWO ROTOR DISKS |
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