GAS TURBINE WITH A SEALING DEVICE ARRANGEMENT AT THE INTERFACE BETWEEN THE COMBUSTOR AND THE TURBINE
A sealing arrangement at the interface between a combustor and a turbine of a gas turbine, said turbine comprising deflecting vanes (2) at its inlet, which deflecting vanes (2) are each mounted within said turbine so as to define an inner or outer diameter platform (9) and are in sealing engagement...
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| creator | EROGLU, Adnan STRUEKEN, Stephan JORGENSEN, Stephen W GRAF, Frank MOHAMMED, Afzal Pasha ESCUDERO OLANO, Marcos McNALLY, Joshua R ZIERER, Thomas |
| description | A sealing arrangement at the interface between a combustor and a turbine of a gas turbine, said turbine comprising deflecting vanes (2) at its inlet, which deflecting vanes (2) are each mounted within said turbine so as to define an inner or outer diameter platform (9) and are in sealing engagement by means of an inner or outer diameter vane tooth (9a) with a seal (10) arranged at the corresponding inner or outer diameter part of the outlet of said combustor, wherein the seal (10) is movable and is pressed on said inner or outer diameter vane tooth (9a) by a differential pressure such that the pressure of the mainstream hot gas flow is a lower pressure (P2). |
| format | Patent |
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JORGENSEN, Stephen W ; GRAF, Frank ; MOHAMMED, Afzal Pasha ; ESCUDERO OLANO, Marcos ; McNALLY, Joshua R ; ZIERER, Thomas</creatorcontrib><description>A sealing arrangement at the interface between a combustor and a turbine of a gas turbine, said turbine comprising deflecting vanes (2) at its inlet, which deflecting vanes (2) are each mounted within said turbine so as to define an inner or outer diameter platform (9) and are in sealing engagement by means of an inner or outer diameter vane tooth (9a) with a seal (10) arranged at the corresponding inner or outer diameter part of the outlet of said combustor, wherein the seal (10) is movable and is pressed on said inner or outer diameter vane tooth (9a) by a differential pressure such that the pressure of the mainstream hot gas flow is a lower pressure (P2).</description><language>eng ; fre ; ger</language><subject>BLASTING ; CYLINDERS ; ENGINE PLANTS IN GENERAL ; ENGINEERING ELEMENTS AND UNITS ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; HEATING ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; PISTONS ; SEALINGS ; STEAM ENGINES ; THERMAL INSULATION IN GENERAL ; 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=20190529&DB=EPODOC&CC=EP&NR=3306037B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,778,883,25551,76302</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20190529&DB=EPODOC&CC=EP&NR=3306037B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>EROGLU, Adnan</creatorcontrib><creatorcontrib>STRUEKEN, Stephan</creatorcontrib><creatorcontrib>JORGENSEN, Stephen W</creatorcontrib><creatorcontrib>GRAF, Frank</creatorcontrib><creatorcontrib>MOHAMMED, Afzal Pasha</creatorcontrib><creatorcontrib>ESCUDERO OLANO, Marcos</creatorcontrib><creatorcontrib>McNALLY, Joshua R</creatorcontrib><creatorcontrib>ZIERER, Thomas</creatorcontrib><title>GAS TURBINE WITH A SEALING DEVICE ARRANGEMENT AT THE INTERFACE BETWEEN THE COMBUSTOR AND THE TURBINE</title><description>A sealing arrangement at the interface between a combustor and a turbine of a gas turbine, said turbine comprising deflecting vanes (2) at its inlet, which deflecting vanes (2) are each mounted within said turbine so as to define an inner or outer diameter platform (9) and are in sealing engagement by means of an inner or outer diameter vane tooth (9a) with a seal (10) arranged at the corresponding inner or outer diameter part of the outlet of said combustor, wherein the seal (10) is movable and is pressed on said inner or outer diameter vane tooth (9a) by a differential pressure such that the pressure of the mainstream hot gas flow is a lower pressure (P2).</description><subject>BLASTING</subject><subject>CYLINDERS</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>ENGINEERING ELEMENTS AND UNITS</subject><subject>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</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>PISTONS</subject><subject>SEALINGS</subject><subject>STEAM ENGINES</subject><subject>THERMAL INSULATION IN GENERAL</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjMEKgkAURd20iOof3g8ExkCt34xXHchnjM9citS0ihLs_ynED2h14JzLXSf3ghvSNlgvoM5rSUwN-OyloAxX70AcAkuBCqLESlqCvChCzr9ooR0gs3V1ZdtG60As2WyW422yegzPKe4WbhLKoa7cx_Hdx2kcbvEVPz0uxqTH1Jzswfwx-QKc5DOW</recordid><startdate>20190529</startdate><enddate>20190529</enddate><creator>EROGLU, Adnan</creator><creator>STRUEKEN, Stephan</creator><creator>JORGENSEN, Stephen W</creator><creator>GRAF, Frank</creator><creator>MOHAMMED, Afzal Pasha</creator><creator>ESCUDERO OLANO, Marcos</creator><creator>McNALLY, Joshua R</creator><creator>ZIERER, Thomas</creator><scope>EVB</scope></search><sort><creationdate>20190529</creationdate><title>GAS TURBINE WITH A SEALING DEVICE ARRANGEMENT AT THE INTERFACE BETWEEN THE COMBUSTOR AND THE TURBINE</title><author>EROGLU, Adnan ; STRUEKEN, Stephan ; JORGENSEN, Stephen W ; GRAF, Frank ; MOHAMMED, Afzal Pasha ; ESCUDERO OLANO, Marcos ; McNALLY, Joshua R ; ZIERER, Thomas</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3306037B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2019</creationdate><topic>BLASTING</topic><topic>CYLINDERS</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>ENGINEERING ELEMENTS AND UNITS</topic><topic>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</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>PISTONS</topic><topic>SEALINGS</topic><topic>STEAM ENGINES</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>EROGLU, Adnan</creatorcontrib><creatorcontrib>STRUEKEN, Stephan</creatorcontrib><creatorcontrib>JORGENSEN, Stephen W</creatorcontrib><creatorcontrib>GRAF, Frank</creatorcontrib><creatorcontrib>MOHAMMED, Afzal Pasha</creatorcontrib><creatorcontrib>ESCUDERO OLANO, Marcos</creatorcontrib><creatorcontrib>McNALLY, Joshua R</creatorcontrib><creatorcontrib>ZIERER, Thomas</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>EROGLU, Adnan</au><au>STRUEKEN, Stephan</au><au>JORGENSEN, Stephen W</au><au>GRAF, Frank</au><au>MOHAMMED, Afzal Pasha</au><au>ESCUDERO OLANO, Marcos</au><au>McNALLY, Joshua R</au><au>ZIERER, Thomas</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>GAS TURBINE WITH A SEALING DEVICE ARRANGEMENT AT THE INTERFACE BETWEEN THE COMBUSTOR AND THE TURBINE</title><date>2019-05-29</date><risdate>2019</risdate><abstract>A sealing arrangement at the interface between a combustor and a turbine of a gas turbine, said turbine comprising deflecting vanes (2) at its inlet, which deflecting vanes (2) are each mounted within said turbine so as to define an inner or outer diameter platform (9) and are in sealing engagement by means of an inner or outer diameter vane tooth (9a) with a seal (10) arranged at the corresponding inner or outer diameter part of the outlet of said combustor, wherein the seal (10) is movable and is pressed on said inner or outer diameter vane tooth (9a) by a differential pressure such that the pressure of the mainstream hot gas flow is a lower pressure (P2).</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| subjects | BLASTING CYLINDERS ENGINE PLANTS IN GENERAL ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PISTONS SEALINGS STEAM ENGINES THERMAL INSULATION IN GENERAL WEAPONS |
| title | GAS TURBINE WITH A SEALING DEVICE ARRANGEMENT AT THE INTERFACE BETWEEN THE COMBUSTOR AND THE TURBINE |
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