Rotor of a gas turbine
A rotor of a thermal turbomachine, particularly a gas turbine, is provided. The rotor includes a plurality of individual rotor components that are held together by a tie-bold and combined into a unit. The tie-bolt is supported by the assembly of the surrounding rotor components including the tie-bol...
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| creator | SCHNEIDER OLIVER EHEHALT ULRICH SCHROEDER PETER AHAUS GUIDO KOLK KARSTEN HOELL HARALD LOCH WALTER NIMPTSCH HARALD BENKLER FRANCOIS SCHNEIDER PETER-ANDREAS VEITSMAN VYACHESLAV |
| description | A rotor of a thermal turbomachine, particularly a gas turbine, is provided. The rotor includes a plurality of individual rotor components that are held together by a tie-bold and combined into a unit. The tie-bolt is supported by the assembly of the surrounding rotor components including the tie-bolt and the rotor disks. A hollow shaft which is made up of two tubular sections and a support wheel further support the rotor. |
| format | Patent |
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The rotor includes a plurality of individual rotor components that are held together by a tie-bold and combined into a unit. The tie-bolt is supported by the assembly of the surrounding rotor components including the tie-bolt and the rotor disks. A hollow shaft which is made up of two tubular sections and a support wheel further support the rotor.</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>2014</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=20140204&DB=EPODOC&CC=US&NR=8641365B2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25562,76317</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20140204&DB=EPODOC&CC=US&NR=8641365B2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>SCHNEIDER OLIVER</creatorcontrib><creatorcontrib>EHEHALT ULRICH</creatorcontrib><creatorcontrib>SCHROEDER PETER</creatorcontrib><creatorcontrib>AHAUS GUIDO</creatorcontrib><creatorcontrib>KOLK KARSTEN</creatorcontrib><creatorcontrib>HOELL HARALD</creatorcontrib><creatorcontrib>LOCH WALTER</creatorcontrib><creatorcontrib>NIMPTSCH HARALD</creatorcontrib><creatorcontrib>BENKLER FRANCOIS</creatorcontrib><creatorcontrib>SCHNEIDER PETER-ANDREAS</creatorcontrib><creatorcontrib>VEITSMAN VYACHESLAV</creatorcontrib><title>Rotor of a gas turbine</title><description>A rotor of a thermal turbomachine, particularly a gas turbine, is provided. The rotor includes a plurality of individual rotor components that are held together by a tie-bold and combined into a unit. The tie-bolt is supported by the assembly of the surrounding rotor components including the tie-bolt and the rotor disks. A hollow shaft which is made up of two tubular sections and a support wheel further support the rotor.</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>2014</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZBALyi_JL1LIT1NIVEhPLFYoKS1KysxL5WFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8aHBFmYmhsZmpk5GxkQoAQAzWCDR</recordid><startdate>20140204</startdate><enddate>20140204</enddate><creator>SCHNEIDER OLIVER</creator><creator>EHEHALT ULRICH</creator><creator>SCHROEDER PETER</creator><creator>AHAUS GUIDO</creator><creator>KOLK KARSTEN</creator><creator>HOELL HARALD</creator><creator>LOCH WALTER</creator><creator>NIMPTSCH HARALD</creator><creator>BENKLER FRANCOIS</creator><creator>SCHNEIDER PETER-ANDREAS</creator><creator>VEITSMAN VYACHESLAV</creator><scope>EVB</scope></search><sort><creationdate>20140204</creationdate><title>Rotor of a gas turbine</title><author>SCHNEIDER OLIVER ; EHEHALT ULRICH ; SCHROEDER PETER ; AHAUS GUIDO ; KOLK KARSTEN ; HOELL HARALD ; LOCH WALTER ; NIMPTSCH HARALD ; BENKLER FRANCOIS ; SCHNEIDER PETER-ANDREAS ; VEITSMAN VYACHESLAV</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US8641365B23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2014</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>SCHNEIDER OLIVER</creatorcontrib><creatorcontrib>EHEHALT ULRICH</creatorcontrib><creatorcontrib>SCHROEDER PETER</creatorcontrib><creatorcontrib>AHAUS GUIDO</creatorcontrib><creatorcontrib>KOLK KARSTEN</creatorcontrib><creatorcontrib>HOELL HARALD</creatorcontrib><creatorcontrib>LOCH WALTER</creatorcontrib><creatorcontrib>NIMPTSCH HARALD</creatorcontrib><creatorcontrib>BENKLER FRANCOIS</creatorcontrib><creatorcontrib>SCHNEIDER PETER-ANDREAS</creatorcontrib><creatorcontrib>VEITSMAN VYACHESLAV</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>SCHNEIDER OLIVER</au><au>EHEHALT ULRICH</au><au>SCHROEDER PETER</au><au>AHAUS GUIDO</au><au>KOLK KARSTEN</au><au>HOELL HARALD</au><au>LOCH WALTER</au><au>NIMPTSCH HARALD</au><au>BENKLER FRANCOIS</au><au>SCHNEIDER PETER-ANDREAS</au><au>VEITSMAN VYACHESLAV</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Rotor of a gas turbine</title><date>2014-02-04</date><risdate>2014</risdate><abstract>A rotor of a thermal turbomachine, particularly a gas turbine, is provided. The rotor includes a plurality of individual rotor components that are held together by a tie-bold and combined into a unit. The tie-bolt is supported by the assembly of the surrounding rotor components including the tie-bolt and the rotor disks. A hollow shaft which is made up of two tubular sections and a support wheel further support the rotor.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng |
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| source | esp@cenet |
| 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 of a gas turbine |
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