Turbine airfoil and corresponding method of manufacturing
A ridged turbine airfoil (1) for use in turbine engines exposed to high temperatures and a method of manufacturing the ridged turbine airfoil is disclosed. The turbine airfoil (1) comprises an outer wall (2) with an outer surface (3). The outer wall (2) comprises an arrangement (5) of raised ridges...
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 | MAIER, SIMON MÖLLER, BETTINA NEDDEMEYER, TORSTEN BERGANDER, KATHARINA MAIZ, KHALED DREHER, HORST-MICHAEL |
| description | A ridged turbine airfoil (1) for use in turbine engines exposed to high temperatures and a method of manufacturing the ridged turbine airfoil is disclosed. The turbine airfoil (1) comprises an outer wall (2) with an outer surface (3). The outer wall (2) comprises an arrangement (5) of raised ridges (8) having a predefined height (6) located on a region (7) of the outer surface (3) wherein each ridge (8) encloses an area (19) for receiving at least a portion (9) of a TBC layer (4). The TBC layer (4) is to be applied on the outer surface (3). The ridges (8) can be made from a similar material the airfoil (1) is made from to withstand the high temperatures. The area enclosed (19) by the raised ridges (8) enclosing the portion of TBC layer (4) preferably has a hexagonal (20), rectangular (21) or circular (22) shape. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP2857637A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP2857637A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP2857637A13</originalsourceid><addsrcrecordid>eNrjZLAMKS1KysxLVUjMLErLz8xRSMxLUUjOLypKLS7Iz0vJzEtXyE0tychPUchPU8hNzCtNS0wuKS0CivMwsKYl5hSn8kJpbgYFN9cQZw_d1IL8eKDuxOTUvNSSeNcAIwtTczNjc0dDYyKUAAAWFC7N</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Turbine airfoil and corresponding method of manufacturing</title><source>esp@cenet</source><creator>MAIER, SIMON ; MÖLLER, BETTINA ; NEDDEMEYER, TORSTEN ; BERGANDER, KATHARINA ; MAIZ, KHALED ; DREHER, HORST-MICHAEL</creator><creatorcontrib>MAIER, SIMON ; MÖLLER, BETTINA ; NEDDEMEYER, TORSTEN ; BERGANDER, KATHARINA ; MAIZ, KHALED ; DREHER, HORST-MICHAEL</creatorcontrib><description>A ridged turbine airfoil (1) for use in turbine engines exposed to high temperatures and a method of manufacturing the ridged turbine airfoil is disclosed. The turbine airfoil (1) comprises an outer wall (2) with an outer surface (3). The outer wall (2) comprises an arrangement (5) of raised ridges (8) having a predefined height (6) located on a region (7) of the outer surface (3) wherein each ridge (8) encloses an area (19) for receiving at least a portion (9) of a TBC layer (4). The TBC layer (4) is to be applied on the outer surface (3). The ridges (8) can be made from a similar material the airfoil (1) is made from to withstand the high temperatures. The area enclosed (19) by the raised ridges (8) enclosing the portion of TBC layer (4) preferably has a hexagonal (20), rectangular (21) or circular (22) shape.</description><language>eng ; fre ; ger</language><subject>BLASTING ; ENGINE PLANTS IN GENERAL ; HEATING ; INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS ; INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; STEAM ENGINES ; WEAPONS</subject><creationdate>2015</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=20150408&DB=EPODOC&CC=EP&NR=2857637A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,309,781,886,25566,76549</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20150408&DB=EPODOC&CC=EP&NR=2857637A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>MAIER, SIMON</creatorcontrib><creatorcontrib>MÖLLER, BETTINA</creatorcontrib><creatorcontrib>NEDDEMEYER, TORSTEN</creatorcontrib><creatorcontrib>BERGANDER, KATHARINA</creatorcontrib><creatorcontrib>MAIZ, KHALED</creatorcontrib><creatorcontrib>DREHER, HORST-MICHAEL</creatorcontrib><title>Turbine airfoil and corresponding method of manufacturing</title><description>A ridged turbine airfoil (1) for use in turbine engines exposed to high temperatures and a method of manufacturing the ridged turbine airfoil is disclosed. The turbine airfoil (1) comprises an outer wall (2) with an outer surface (3). The outer wall (2) comprises an arrangement (5) of raised ridges (8) having a predefined height (6) located on a region (7) of the outer surface (3) wherein each ridge (8) encloses an area (19) for receiving at least a portion (9) of a TBC layer (4). The TBC layer (4) is to be applied on the outer surface (3). The ridges (8) can be made from a similar material the airfoil (1) is made from to withstand the high temperatures. The area enclosed (19) by the raised ridges (8) enclosing the portion of TBC layer (4) preferably has a hexagonal (20), rectangular (21) or circular (22) shape.</description><subject>BLASTING</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>HEATING</subject><subject>INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS</subject><subject>INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04</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>2015</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLAMKS1KysxLVUjMLErLz8xRSMxLUUjOLypKLS7Iz0vJzEtXyE0tychPUchPU8hNzCtNS0wuKS0CivMwsKYl5hSn8kJpbgYFN9cQZw_d1IL8eKDuxOTUvNSSeNcAIwtTczNjc0dDYyKUAAAWFC7N</recordid><startdate>20150408</startdate><enddate>20150408</enddate><creator>MAIER, SIMON</creator><creator>MÖLLER, BETTINA</creator><creator>NEDDEMEYER, TORSTEN</creator><creator>BERGANDER, KATHARINA</creator><creator>MAIZ, KHALED</creator><creator>DREHER, HORST-MICHAEL</creator><scope>EVB</scope></search><sort><creationdate>20150408</creationdate><title>Turbine airfoil and corresponding method of manufacturing</title><author>MAIER, SIMON ; MÖLLER, BETTINA ; NEDDEMEYER, TORSTEN ; BERGANDER, KATHARINA ; MAIZ, KHALED ; DREHER, HORST-MICHAEL</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2857637A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2015</creationdate><topic>BLASTING</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>HEATING</topic><topic>INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS</topic><topic>INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04</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>MAIER, SIMON</creatorcontrib><creatorcontrib>MÖLLER, BETTINA</creatorcontrib><creatorcontrib>NEDDEMEYER, TORSTEN</creatorcontrib><creatorcontrib>BERGANDER, KATHARINA</creatorcontrib><creatorcontrib>MAIZ, KHALED</creatorcontrib><creatorcontrib>DREHER, HORST-MICHAEL</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>MAIER, SIMON</au><au>MÖLLER, BETTINA</au><au>NEDDEMEYER, TORSTEN</au><au>BERGANDER, KATHARINA</au><au>MAIZ, KHALED</au><au>DREHER, HORST-MICHAEL</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Turbine airfoil and corresponding method of manufacturing</title><date>2015-04-08</date><risdate>2015</risdate><abstract>A ridged turbine airfoil (1) for use in turbine engines exposed to high temperatures and a method of manufacturing the ridged turbine airfoil is disclosed. The turbine airfoil (1) comprises an outer wall (2) with an outer surface (3). The outer wall (2) comprises an arrangement (5) of raised ridges (8) having a predefined height (6) located on a region (7) of the outer surface (3) wherein each ridge (8) encloses an area (19) for receiving at least a portion (9) of a TBC layer (4). The TBC layer (4) is to be applied on the outer surface (3). The ridges (8) can be made from a similar material the airfoil (1) is made from to withstand the high temperatures. The area enclosed (19) by the raised ridges (8) enclosing the portion of TBC layer (4) preferably has a hexagonal (20), rectangular (21) or circular (22) shape.</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng ; fre ; ger |
| recordid | cdi_epo_espacenet_EP2857637A1 |
| source | esp@cenet |
| subjects | BLASTING ENGINE PLANTS IN GENERAL HEATING INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS |
| title | Turbine airfoil and corresponding method of manufacturing |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-18T11%3A30%3A40IST&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=MAIER,%20SIMON&rft.date=2015-04-08&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP2857637A1%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 |