Blade for a turbo machine, blade assembly, gas turbine, and method for manufacturing a blade for a turbo machine
A blade for turbo machine is provided. The blade for a turbo machine includes an airfoil body extending in a radial direction between a root end and a tip end and including an inner void extending from the root end in the radial direction, a root body integrally formed with the airfoil body, extendi...
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creator | Krueckels, Joerg Tsypkaykin, Igor Martin, Stefan Emanuel Hoffmann, Willy H Beaumont, Wade |
description | A blade for turbo machine is provided. The blade for a turbo machine includes an airfoil body extending in a radial direction between a root end and a tip end and including an inner void extending from the root end in the radial direction, a root body integrally formed with the airfoil body, extending from the root end of the air foil body to a bottom end in the radial direction, and including a receiving slot extending from the bottom end in the radial direction and opening into the inner void of the air foil body, and an insert positioned in the receiving slot of the root body and including a plurality of through holes extending in the radial direction to form a fluid connection to the inner void of the air foil body. |
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The blade for a turbo machine includes an airfoil body extending in a radial direction between a root end and a tip end and including an inner void extending from the root end in the radial direction, a root body integrally formed with the airfoil body, extending from the root end of the air foil body to a bottom end in the radial direction, and including a receiving slot extending from the bottom end in the radial direction and opening into the inner void of the air foil body, and an insert positioned in the receiving slot of the root body and including a plurality of through holes extending in the radial direction to form a fluid connection to the inner void of the air foil body.</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>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=20230620&DB=EPODOC&CC=US&NR=11680490B2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76516</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230620&DB=EPODOC&CC=US&NR=11680490B2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Krueckels, Joerg</creatorcontrib><creatorcontrib>Tsypkaykin, Igor</creatorcontrib><creatorcontrib>Martin, Stefan Emanuel</creatorcontrib><creatorcontrib>Hoffmann, Willy H</creatorcontrib><creatorcontrib>Beaumont, Wade</creatorcontrib><title>Blade for a turbo machine, blade assembly, gas turbine, and method for manufacturing a blade for a turbo machine</title><description>A blade for turbo machine is provided. The blade for a turbo machine includes an airfoil body extending in a radial direction between a root end and a tip end and including an inner void extending from the root end in the radial direction, a root body integrally formed with the airfoil body, extending from the root end of the air foil body to a bottom end in the radial direction, and including a receiving slot extending from the bottom end in the radial direction and opening into the inner void of the air foil body, and an insert positioned in the receiving slot of the root body and including a plurality of through holes extending in the radial direction to form a fluid connection to the inner void of the air foil body.</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>eNrjZChwyklMSVVIyy9SSFQoKS1KylfITUzOyMxL1VFIAkslFhen5iblVOoopCcWg5WAJRPzUhRyU0sy8lPAmnMT80rTEpOB0pl56UCjknAZy8PAmpaYU5zKC6W5GRTdXEOcPXRTC_LjU4sLEpNT81JL4kODDQ3NLAxMLA2cjIyJUQMATXZBxw</recordid><startdate>20230620</startdate><enddate>20230620</enddate><creator>Krueckels, Joerg</creator><creator>Tsypkaykin, Igor</creator><creator>Martin, Stefan Emanuel</creator><creator>Hoffmann, Willy H</creator><creator>Beaumont, Wade</creator><scope>EVB</scope></search><sort><creationdate>20230620</creationdate><title>Blade for a turbo machine, blade assembly, gas turbine, and method for manufacturing a blade for a turbo machine</title><author>Krueckels, Joerg ; Tsypkaykin, Igor ; Martin, Stefan Emanuel ; Hoffmann, Willy H ; Beaumont, Wade</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US11680490B23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</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>Krueckels, Joerg</creatorcontrib><creatorcontrib>Tsypkaykin, Igor</creatorcontrib><creatorcontrib>Martin, Stefan Emanuel</creatorcontrib><creatorcontrib>Hoffmann, Willy H</creatorcontrib><creatorcontrib>Beaumont, Wade</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Krueckels, Joerg</au><au>Tsypkaykin, Igor</au><au>Martin, Stefan Emanuel</au><au>Hoffmann, Willy H</au><au>Beaumont, Wade</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Blade for a turbo machine, blade assembly, gas turbine, and method for manufacturing a blade for a turbo machine</title><date>2023-06-20</date><risdate>2023</risdate><abstract>A blade for turbo machine is provided. The blade for a turbo machine includes an airfoil body extending in a radial direction between a root end and a tip end and including an inner void extending from the root end in the radial direction, a root body integrally formed with the airfoil body, extending from the root end of the air foil body to a bottom end in the radial direction, and including a receiving slot extending from the bottom end in the radial direction and opening into the inner void of the air foil body, and an insert positioned in the receiving slot of the root body and including a plurality of through holes extending in the radial direction to form a fluid connection to the inner void of the air foil body.</abstract><oa>free_for_read</oa></addata></record> |
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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 | Blade for a turbo machine, blade assembly, gas turbine, and method for manufacturing a blade for a turbo machine |
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