VANE CLUSTER AND CORRESPONDING GAS TURBINE ENGINE
A vane cluster (100) for a gas turbine engine (20) includes an outer diameter platform (110) and an inner diameter platform (120). A plurality of vanes (130) span from the outer diameter platform (110) to the inner diameter platform (120). At least one inbound region (102) is defined between a first...
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creator | TANNER, Stephanie MORAN, Jason B McMAHON, Shawn M ANDERSON, Kristopher K MONGILLO, Jr, Dominic J WHITFIELD, Christopher PERRON, Christopher ANIELLO, Justin M BARTLING, Brett Alan |
description | A vane cluster (100) for a gas turbine engine (20) includes an outer diameter platform (110) and an inner diameter platform (120). A plurality of vanes (130) span from the outer diameter platform (110) to the inner diameter platform (120). At least one inbound region (102) is defined between a first vane (130) of the plurality of vanes (130) and a second vane (130) of the plurality of vanes (130). The first vane (130) includes a suction side facing the inbound region (102). Each of the vanes (130) includes a leading edge core passage and a trailing edge core passage. A plurality of electrical discharge machined (EDM) holes (140) are disposed within at least 12.7mm of a leading edge (104) of the first vane (130). Each of the EDM holes (140) connect the leading edge core passage of the vane (130) to an exterior surface of the vane (130). |
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A plurality of vanes (130) span from the outer diameter platform (110) to the inner diameter platform (120). At least one inbound region (102) is defined between a first vane (130) of the plurality of vanes (130) and a second vane (130) of the plurality of vanes (130). The first vane (130) includes a suction side facing the inbound region (102). Each of the vanes (130) includes a leading edge core passage and a trailing edge core passage. A plurality of electrical discharge machined (EDM) holes (140) are disposed within at least 12.7mm of a leading edge (104) of the first vane (130). Each of the EDM holes (140) connect the leading edge core passage of the vane (130) to an exterior surface of the vane (130).</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>2024</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=20241225&DB=EPODOC&CC=EP&NR=3450697B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20241225&DB=EPODOC&CC=EP&NR=3450697B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>TANNER, Stephanie</creatorcontrib><creatorcontrib>MORAN, Jason B</creatorcontrib><creatorcontrib>McMAHON, Shawn M</creatorcontrib><creatorcontrib>ANDERSON, Kristopher K</creatorcontrib><creatorcontrib>MONGILLO, Jr, Dominic J</creatorcontrib><creatorcontrib>WHITFIELD, Christopher</creatorcontrib><creatorcontrib>PERRON, Christopher</creatorcontrib><creatorcontrib>ANIELLO, Justin M</creatorcontrib><creatorcontrib>BARTLING, Brett Alan</creatorcontrib><title>VANE CLUSTER AND CORRESPONDING GAS TURBINE ENGINE</title><description>A vane cluster (100) for a gas turbine engine (20) includes an outer diameter platform (110) and an inner diameter platform (120). A plurality of vanes (130) span from the outer diameter platform (110) to the inner diameter platform (120). At least one inbound region (102) is defined between a first vane (130) of the plurality of vanes (130) and a second vane (130) of the plurality of vanes (130). The first vane (130) includes a suction side facing the inbound region (102). Each of the vanes (130) includes a leading edge core passage and a trailing edge core passage. A plurality of electrical discharge machined (EDM) holes (140) are disposed within at least 12.7mm of a leading edge (104) of the first vane (130). Each of the EDM holes (140) connect the leading edge core passage of the vane (130) to an exterior surface of the vane (130).</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>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDAMc_RzVXD2CQ0OcQ1ScPRzUXD2DwpyDQ7w93Px9HNXcHcMVggJDXLyBKpy9XMHUjwMrGmJOcWpvFCam0HBzTXE2UM3tSA_PrW4IDE5NS-1JN41wNjE1MDM0tzJ0JgIJQAGTiYs</recordid><startdate>20241225</startdate><enddate>20241225</enddate><creator>TANNER, Stephanie</creator><creator>MORAN, Jason B</creator><creator>McMAHON, Shawn M</creator><creator>ANDERSON, Kristopher K</creator><creator>MONGILLO, Jr, Dominic J</creator><creator>WHITFIELD, Christopher</creator><creator>PERRON, Christopher</creator><creator>ANIELLO, Justin M</creator><creator>BARTLING, Brett Alan</creator><scope>EVB</scope></search><sort><creationdate>20241225</creationdate><title>VANE CLUSTER AND CORRESPONDING GAS TURBINE ENGINE</title><author>TANNER, Stephanie ; MORAN, Jason B ; McMAHON, Shawn M ; ANDERSON, Kristopher K ; MONGILLO, Jr, Dominic J ; WHITFIELD, Christopher ; PERRON, Christopher ; ANIELLO, Justin M ; BARTLING, Brett Alan</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3450697B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2024</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>TANNER, Stephanie</creatorcontrib><creatorcontrib>MORAN, Jason B</creatorcontrib><creatorcontrib>McMAHON, Shawn M</creatorcontrib><creatorcontrib>ANDERSON, Kristopher K</creatorcontrib><creatorcontrib>MONGILLO, Jr, Dominic J</creatorcontrib><creatorcontrib>WHITFIELD, Christopher</creatorcontrib><creatorcontrib>PERRON, Christopher</creatorcontrib><creatorcontrib>ANIELLO, Justin M</creatorcontrib><creatorcontrib>BARTLING, Brett Alan</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>TANNER, Stephanie</au><au>MORAN, Jason B</au><au>McMAHON, Shawn M</au><au>ANDERSON, Kristopher K</au><au>MONGILLO, Jr, Dominic J</au><au>WHITFIELD, Christopher</au><au>PERRON, Christopher</au><au>ANIELLO, Justin M</au><au>BARTLING, Brett Alan</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>VANE CLUSTER AND CORRESPONDING GAS TURBINE ENGINE</title><date>2024-12-25</date><risdate>2024</risdate><abstract>A vane cluster (100) for a gas turbine engine (20) includes an outer diameter platform (110) and an inner diameter platform (120). A plurality of vanes (130) span from the outer diameter platform (110) to the inner diameter platform (120). At least one inbound region (102) is defined between a first vane (130) of the plurality of vanes (130) and a second vane (130) of the plurality of vanes (130). The first vane (130) includes a suction side facing the inbound region (102). Each of the vanes (130) includes a leading edge core passage and a trailing edge core passage. A plurality of electrical discharge machined (EDM) holes (140) are disposed within at least 12.7mm of a leading edge (104) of the first vane (130). Each of the EDM holes (140) connect the leading edge core passage of the vane (130) to an exterior surface of the vane (130).</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 | VANE CLUSTER AND CORRESPONDING GAS TURBINE ENGINE |
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