TURBINE SHROUD ASSEMBLY
A turbine component includes an outer shroud 14 arranged within a turbine 10 and further including opposed extending portions 16, 18. The component further provides an inner shroud 22 shielding the outer shroud 14 from a gas path within the turbine 10 during operation of the turbine 10 and including...
Gespeichert in:
| Hauptverfasser: | , , |
|---|---|
| Format: | Patent |
| Sprache: | eng ; fre ; ger |
| 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 | HAFNER, Matthew Troy DELVAUX, John McConnell TAXACHER, Glenn Curtis |
| description | A turbine component includes an outer shroud 14 arranged within a turbine 10 and further including opposed extending portions 16, 18. The component further provides an inner shroud 22 shielding the outer shroud 14 from a gas path within the turbine 10 during operation of the turbine 10 and including opposed arcuate portions 26, 28 extending around and in direct contact with a corresponding extending portion 16, 18 of the outer shroud 14 for supporting the inner shroud 22 from the outer shroud 14. The component further provides a load path forming region 34 at least partially extending between facing surfaces of each arcuate portion 26, 28 and corresponding extending portion 16, 18. During operation of the turbine 10, load path forming regions 34 extend into direct contact between at least a portion of the facing surfaces of each arcuate portion 26, 28 and corresponding extending portion 16, 18, resulting in formation of a loading arrangement 36 having generally evenly distributed radial load forces at the load path forming regions 34. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP3425168B1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP3425168B1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP3425168B13</originalsourceid><addsrcrecordid>eNrjZBAPCQ1y8vRzVQj2CPIPdVFwDA529XXyieRhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGuAcYmRqaGZhZOhsZEKAEApskfMA</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>TURBINE SHROUD ASSEMBLY</title><source>esp@cenet</source><creator>HAFNER, Matthew Troy ; DELVAUX, John McConnell ; TAXACHER, Glenn Curtis</creator><creatorcontrib>HAFNER, Matthew Troy ; DELVAUX, John McConnell ; TAXACHER, Glenn Curtis</creatorcontrib><description>A turbine component includes an outer shroud 14 arranged within a turbine 10 and further including opposed extending portions 16, 18. The component further provides an inner shroud 22 shielding the outer shroud 14 from a gas path within the turbine 10 during operation of the turbine 10 and including opposed arcuate portions 26, 28 extending around and in direct contact with a corresponding extending portion 16, 18 of the outer shroud 14 for supporting the inner shroud 22 from the outer shroud 14. The component further provides a load path forming region 34 at least partially extending between facing surfaces of each arcuate portion 26, 28 and corresponding extending portion 16, 18. During operation of the turbine 10, load path forming regions 34 extend into direct contact between at least a portion of the facing surfaces of each arcuate portion 26, 28 and corresponding extending portion 16, 18, resulting in formation of a loading arrangement 36 having generally evenly distributed radial load forces at the load path forming regions 34.</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>2023</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=20230726&DB=EPODOC&CC=EP&NR=3425168B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230726&DB=EPODOC&CC=EP&NR=3425168B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>HAFNER, Matthew Troy</creatorcontrib><creatorcontrib>DELVAUX, John McConnell</creatorcontrib><creatorcontrib>TAXACHER, Glenn Curtis</creatorcontrib><title>TURBINE SHROUD ASSEMBLY</title><description>A turbine component includes an outer shroud 14 arranged within a turbine 10 and further including opposed extending portions 16, 18. The component further provides an inner shroud 22 shielding the outer shroud 14 from a gas path within the turbine 10 during operation of the turbine 10 and including opposed arcuate portions 26, 28 extending around and in direct contact with a corresponding extending portion 16, 18 of the outer shroud 14 for supporting the inner shroud 22 from the outer shroud 14. The component further provides a load path forming region 34 at least partially extending between facing surfaces of each arcuate portion 26, 28 and corresponding extending portion 16, 18. During operation of the turbine 10, load path forming regions 34 extend into direct contact between at least a portion of the facing surfaces of each arcuate portion 26, 28 and corresponding extending portion 16, 18, resulting in formation of a loading arrangement 36 having generally evenly distributed radial load forces at the load path forming regions 34.</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>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZBAPCQ1y8vRzVQj2CPIPdVFwDA529XXyieRhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGuAcYmRqaGZhZOhsZEKAEApskfMA</recordid><startdate>20230726</startdate><enddate>20230726</enddate><creator>HAFNER, Matthew Troy</creator><creator>DELVAUX, John McConnell</creator><creator>TAXACHER, Glenn Curtis</creator><scope>EVB</scope></search><sort><creationdate>20230726</creationdate><title>TURBINE SHROUD ASSEMBLY</title><author>HAFNER, Matthew Troy ; DELVAUX, John McConnell ; TAXACHER, Glenn Curtis</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3425168B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2023</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>HAFNER, Matthew Troy</creatorcontrib><creatorcontrib>DELVAUX, John McConnell</creatorcontrib><creatorcontrib>TAXACHER, Glenn Curtis</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>HAFNER, Matthew Troy</au><au>DELVAUX, John McConnell</au><au>TAXACHER, Glenn Curtis</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>TURBINE SHROUD ASSEMBLY</title><date>2023-07-26</date><risdate>2023</risdate><abstract>A turbine component includes an outer shroud 14 arranged within a turbine 10 and further including opposed extending portions 16, 18. The component further provides an inner shroud 22 shielding the outer shroud 14 from a gas path within the turbine 10 during operation of the turbine 10 and including opposed arcuate portions 26, 28 extending around and in direct contact with a corresponding extending portion 16, 18 of the outer shroud 14 for supporting the inner shroud 22 from the outer shroud 14. The component further provides a load path forming region 34 at least partially extending between facing surfaces of each arcuate portion 26, 28 and corresponding extending portion 16, 18. During operation of the turbine 10, load path forming regions 34 extend into direct contact between at least a portion of the facing surfaces of each arcuate portion 26, 28 and corresponding extending portion 16, 18, resulting in formation of a loading arrangement 36 having generally evenly distributed radial load forces at the load path forming regions 34.</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng ; fre ; ger |
| recordid | cdi_epo_espacenet_EP3425168B1 |
| 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 | TURBINE SHROUD ASSEMBLY |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-02T07%3A54%3A35IST&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=HAFNER,%20Matthew%20Troy&rft.date=2023-07-26&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP3425168B1%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 |