LOAD TRANSFER IN A TURBINE EXHAUST CASE
A turbine exhaust case (200) of a gas turbine engine (20) is provided. This turbine exhaust case (200) includes a first gas turbine engine exhaust case (204), a second gas turbine engine exhaust case (308), a strut (212) and a fastener (334a, 334b). The second gas turbine engine exhaust case (308) i...
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creator | PALMER, Paul W KANTANY, Nicholas W OLSON, Anders C BAKER, Eric STAFFIER, Peter |
description | A turbine exhaust case (200) of a gas turbine engine (20) is provided. This turbine exhaust case (200) includes a first gas turbine engine exhaust case (204), a second gas turbine engine exhaust case (308), a strut (212) and a fastener (334a, 334b). The second gas turbine engine exhaust case (308) includes a flange (338a) and a bracket (338b). The strut (212) is coupled to the first case (204) and the second case (308). The fastener (334a, 334b) fastens the flange (338a) and the strut (212). The second gas turbine engine exhaust case (308) is coaxial with the first gas turbine engine exhaust case (204). The strut (212) contacts the bracket (338b) when the engine (20) is powered-on. |
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This turbine exhaust case (200) includes a first gas turbine engine exhaust case (204), a second gas turbine engine exhaust case (308), a strut (212) and a fastener (334a, 334b). The second gas turbine engine exhaust case (308) includes a flange (338a) and a bracket (338b). The strut (212) is coupled to the first case (204) and the second case (308). The fastener (334a, 334b) fastens the flange (338a) and the strut (212). The second gas turbine engine exhaust case (308) is coaxial with the first gas turbine engine exhaust case (204). The strut (212) contacts the bracket (338b) when the engine (20) is powered-on.</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=20210602&DB=EPODOC&CC=EP&NR=3584411B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20210602&DB=EPODOC&CC=EP&NR=3584411B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>PALMER, Paul W</creatorcontrib><creatorcontrib>KANTANY, Nicholas W</creatorcontrib><creatorcontrib>OLSON, Anders C</creatorcontrib><creatorcontrib>BAKER, Eric</creatorcontrib><creatorcontrib>STAFFIER, Peter</creatorcontrib><title>LOAD TRANSFER IN A TURBINE EXHAUST CASE</title><description>A turbine exhaust case (200) of a gas turbine engine (20) is provided. This turbine exhaust case (200) includes a first gas turbine engine exhaust case (204), a second gas turbine engine exhaust case (308), a strut (212) and a fastener (334a, 334b). The second gas turbine engine exhaust case (308) includes a flange (338a) and a bracket (338b). The strut (212) is coupled to the first case (204) and the second case (308). The fastener (334a, 334b) fastens the flange (338a) and the strut (212). The second gas turbine engine exhaust case (308) is coaxial with the first gas turbine engine exhaust case (204). The strut (212) contacts the bracket (338b) when the engine (20) is powered-on.</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>eNrjZFD38Xd0UQgJcvQLdnMNUvD0U3BUCAkNcvL0c1VwjfBwDA0OUXB2DHblYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxrgHGphYmJoaGTobGRCgBAIF0IyA</recordid><startdate>20210602</startdate><enddate>20210602</enddate><creator>PALMER, Paul W</creator><creator>KANTANY, Nicholas W</creator><creator>OLSON, Anders C</creator><creator>BAKER, Eric</creator><creator>STAFFIER, Peter</creator><scope>EVB</scope></search><sort><creationdate>20210602</creationdate><title>LOAD TRANSFER IN A TURBINE EXHAUST CASE</title><author>PALMER, Paul W ; KANTANY, Nicholas W ; OLSON, Anders C ; BAKER, Eric ; STAFFIER, Peter</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3584411B13</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>PALMER, Paul W</creatorcontrib><creatorcontrib>KANTANY, Nicholas W</creatorcontrib><creatorcontrib>OLSON, Anders C</creatorcontrib><creatorcontrib>BAKER, Eric</creatorcontrib><creatorcontrib>STAFFIER, Peter</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>PALMER, Paul W</au><au>KANTANY, Nicholas W</au><au>OLSON, Anders C</au><au>BAKER, Eric</au><au>STAFFIER, Peter</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>LOAD TRANSFER IN A TURBINE EXHAUST CASE</title><date>2021-06-02</date><risdate>2021</risdate><abstract>A turbine exhaust case (200) of a gas turbine engine (20) is provided. This turbine exhaust case (200) includes a first gas turbine engine exhaust case (204), a second gas turbine engine exhaust case (308), a strut (212) and a fastener (334a, 334b). The second gas turbine engine exhaust case (308) includes a flange (338a) and a bracket (338b). The strut (212) is coupled to the first case (204) and the second case (308). The fastener (334a, 334b) fastens the flange (338a) and the strut (212). The second gas turbine engine exhaust case (308) is coaxial with the first gas turbine engine exhaust case (204). The strut (212) contacts the bracket (338b) when the engine (20) is powered-on.</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 | LOAD TRANSFER IN A TURBINE EXHAUST CASE |
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