TURBOMACHINE BLADE COOLING CIRCUIT
The present disclosure is generally directed to a core configured for the manufacturing of a turbine engine blade by lost-wax casting. The core includes a first convex curved outer face and a second concave curved outer face. The first and second faces have a plurality of recesses, each recess inclu...
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| creator | VOLLEBREGT, Matthieu, Jean, Luc TAMI LIZUZU, Joseph, Toussaint NI, Jun GUERARD, Coralie, Cinthia HERB, Vincent, Marc |
| description | The present disclosure is generally directed to a core configured for the manufacturing of a turbine engine blade by lost-wax casting. The core includes a first convex curved outer face and a second concave curved outer face. The first and second faces have a plurality of recesses, each recess including a spherical portion. |
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The core includes a first convex curved outer face and a second concave curved outer face. The first and second faces have a plurality of recesses, each recess including a spherical portion.</description><language>eng ; fre ; ger</language><subject>BLASTING ; CASTING ; ENGINE PLANTS IN GENERAL ; FOUNDRY MOULDING ; HEATING ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; PERFORMING OPERATIONS ; POWDER METALLURGY ; STEAM ENGINES ; TRANSPORTING ; WEAPONS</subject><creationdate>2019</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=20190501&DB=EPODOC&CC=EP&NR=3475011A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25555,76308</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20190501&DB=EPODOC&CC=EP&NR=3475011A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>VOLLEBREGT, Matthieu, Jean, Luc</creatorcontrib><creatorcontrib>TAMI LIZUZU, Joseph, Toussaint</creatorcontrib><creatorcontrib>NI, Jun</creatorcontrib><creatorcontrib>GUERARD, Coralie, Cinthia</creatorcontrib><creatorcontrib>HERB, Vincent, Marc</creatorcontrib><title>TURBOMACHINE BLADE COOLING CIRCUIT</title><description>The present disclosure is generally directed to a core configured for the manufacturing of a turbine engine blade by lost-wax casting. 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The core includes a first convex curved outer face and a second concave curved outer face. The first and second faces have a plurality of recesses, each recess including a spherical portion.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| source | esp@cenet |
| subjects | BLASTING CASTING ENGINE PLANTS IN GENERAL FOUNDRY MOULDING HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PERFORMING OPERATIONS POWDER METALLURGY STEAM ENGINES TRANSPORTING WEAPONS |
| title | TURBOMACHINE BLADE COOLING CIRCUIT |
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