BLADE HAVING A TIP COOLING CAVITY AND METHOD OF MAKING SAME
A blade includes an airfoil that extends from a root end to a tip end. The airfoil includes a cooling channel defined therein. The blade further includes a tip shroud extending from the tip end, and at least one fillet coupled between the tip end and the tip shroud. The at least one fillet includes...
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| creator | CHAN, Sze Bun Brian SINGH, Anshuman |
| description | A blade includes an airfoil that extends from a root end to a tip end. The airfoil includes a cooling channel defined therein. The blade further includes a tip shroud extending from the tip end, and at least one fillet coupled between the tip end and the tip shroud. The at least one fillet includes an interior wall. The interior wall at least partially defines a cavity in downstream flow communication with the cooling channel. |
| format | Patent |
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The blade further includes a tip shroud extending from the tip end, and at least one fillet coupled between the tip end and the tip shroud. The at least one fillet includes an interior wall. The interior wall at least partially defines a cavity in downstream flow communication with the cooling channel.</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>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=20210106&DB=EPODOC&CC=EP&NR=3543465B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25544,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20210106&DB=EPODOC&CC=EP&NR=3543465B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>CHAN, Sze Bun Brian</creatorcontrib><creatorcontrib>SINGH, Anshuman</creatorcontrib><title>BLADE HAVING A TIP COOLING CAVITY AND METHOD OF MAKING SAME</title><description>A blade includes an airfoil that extends from a root end to a tip end. The airfoil includes a cooling channel defined therein. The blade further includes a tip shroud extending from the tip end, and at least one fillet coupled between the tip end and the tip shroud. The at least one fillet includes an interior wall. The interior wall at least partially defines a cavity in downstream flow communication with the cooling channel.</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>eNrjZLB28nF0cVXwcAzz9HNXcFQI8QxQcPb39wHxnIGCIZEKjn4uCr6uIR7-Lgr-bgq-jt4guWBHX1ceBta0xJziVF4ozc2g4OYa4uyhm1qQH59aXJCYnJqXWhLvGmBsamJsYmbqZGhMhBIANU4oLA</recordid><startdate>20210106</startdate><enddate>20210106</enddate><creator>CHAN, Sze Bun Brian</creator><creator>SINGH, Anshuman</creator><scope>EVB</scope></search><sort><creationdate>20210106</creationdate><title>BLADE HAVING A TIP COOLING CAVITY AND METHOD OF MAKING SAME</title><author>CHAN, Sze Bun Brian ; SINGH, Anshuman</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3543465B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</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>CHAN, Sze Bun Brian</creatorcontrib><creatorcontrib>SINGH, Anshuman</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>CHAN, Sze Bun Brian</au><au>SINGH, Anshuman</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>BLADE HAVING A TIP COOLING CAVITY AND METHOD OF MAKING SAME</title><date>2021-01-06</date><risdate>2021</risdate><abstract>A blade includes an airfoil that extends from a root end to a tip end. The airfoil includes a cooling channel defined therein. The blade further includes a tip shroud extending from the tip end, and at least one fillet coupled between the tip end and the tip shroud. The at least one fillet includes an interior wall. The interior wall at least partially defines a cavity in downstream flow communication with the cooling channel.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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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 HAVING A TIP COOLING CAVITY AND METHOD OF MAKING SAME |
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