COMPENSATION ASSEMBLY FOR A DAMPER OF A GAS TURBINE
The present invention relates to dampers for a gas turbine and, specifically, to a compensation assembly for a damper of a gas turbine, which is to reduce a wave generated in a combustion chamber. The damper includes a resonator cavity including a neck tube connected to the inside of the combustion...
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| creator | SOBOL KAROLINA KRYSTYNA BENZ URS WELTI CHRISTOPH |
| description | The present invention relates to dampers for a gas turbine and, specifically, to a compensation assembly for a damper of a gas turbine, which is to reduce a wave generated in a combustion chamber. The damper includes a resonator cavity including a neck tube connected to the inside of the combustion chamber in order for a fluid to flow. The compensation assembly includes a bulb shape part arranged around the neck tube and formed to allow relative rotation between the combustion chamber and the resonator cavity, wherein the bulb shape part is connected to the neck tube; and a round joint including a round socket suitable to host the bulb shape part to the inside. The round socket includes an upper collar part and a lower collar part connected to each other.
본 발명은 가스 터빈을 위한 댐퍼들에 관한 것이고, 특히 연소실에서 일어나는 파동을 감소시키기 위하여 가스 터빈의 댐퍼를 위한 보상 조립체에 관한 것이고, 댐펀느 연소실의 내부와 유체 소통하는 목부 튜브를 구비한 공명기 캐비티를 포함하고, 보상 조립체는, 목부 튜브와 결합되고 연소실과 공명기 캐비티 사이의 상대적 회전을 허용하도록 구성되고 목부 튜브 주위에 배치된 전구형 부분과, 전구형 부분을 내부적으로 호스팅하는데 적합한 구형 소켓을 포함하는 구형 조인트를 포함하며, 구형 소켓은 서로 연결된 상부 칼라 부분과 저부 칼라 부분을 포함한다. |
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본 발명은 가스 터빈을 위한 댐퍼들에 관한 것이고, 특히 연소실에서 일어나는 파동을 감소시키기 위하여 가스 터빈의 댐퍼를 위한 보상 조립체에 관한 것이고, 댐펀느 연소실의 내부와 유체 소통하는 목부 튜브를 구비한 공명기 캐비티를 포함하고, 보상 조립체는, 목부 튜브와 결합되고 연소실과 공명기 캐비티 사이의 상대적 회전을 허용하도록 구성되고 목부 튜브 주위에 배치된 전구형 부분과, 전구형 부분을 내부적으로 호스팅하는데 적합한 구형 소켓을 포함하는 구형 조인트를 포함하며, 구형 소켓은 서로 연결된 상부 칼라 부분과 저부 칼라 부분을 포함한다.</description><language>eng ; kor</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FORCOMBUSTION CHAMBERS, e.g. FIREBRIDGES ; COMBUSTION APPARATUS ; COMBUSTION ENGINES ; COMBUSTION PROCESSES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDEDFOR ; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS INCOMBUSTION CHAMBERS ; GAS-TURBINE PLANTS ; GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTIONAPPARATUS ; WEAPONS</subject><creationdate>2016</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=20160621&DB=EPODOC&CC=KR&NR=20160071327A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20160621&DB=EPODOC&CC=KR&NR=20160071327A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>SOBOL KAROLINA KRYSTYNA</creatorcontrib><creatorcontrib>BENZ URS</creatorcontrib><creatorcontrib>WELTI CHRISTOPH</creatorcontrib><title>COMPENSATION ASSEMBLY FOR A DAMPER OF A GAS TURBINE</title><description>The present invention relates to dampers for a gas turbine and, specifically, to a compensation assembly for a damper of a gas turbine, which is to reduce a wave generated in a combustion chamber. The damper includes a resonator cavity including a neck tube connected to the inside of the combustion chamber in order for a fluid to flow. The compensation assembly includes a bulb shape part arranged around the neck tube and formed to allow relative rotation between the combustion chamber and the resonator cavity, wherein the bulb shape part is connected to the neck tube; and a round joint including a round socket suitable to host the bulb shape part to the inside. The round socket includes an upper collar part and a lower collar part connected to each other.
본 발명은 가스 터빈을 위한 댐퍼들에 관한 것이고, 특히 연소실에서 일어나는 파동을 감소시키기 위하여 가스 터빈의 댐퍼를 위한 보상 조립체에 관한 것이고, 댐펀느 연소실의 내부와 유체 소통하는 목부 튜브를 구비한 공명기 캐비티를 포함하고, 보상 조립체는, 목부 튜브와 결합되고 연소실과 공명기 캐비티 사이의 상대적 회전을 허용하도록 구성되고 목부 튜브 주위에 배치된 전구형 부분과, 전구형 부분을 내부적으로 호스팅하는데 적합한 구형 소켓을 포함하는 구형 조인트를 포함하며, 구형 소켓은 서로 연결된 상부 칼라 부분과 저부 칼라 부분을 포함한다.</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FORCOMBUSTION CHAMBERS, e.g. FIREBRIDGES</subject><subject>COMBUSTION APPARATUS</subject><subject>COMBUSTION ENGINES</subject><subject>COMBUSTION PROCESSES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDEDFOR</subject><subject>DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS INCOMBUSTION CHAMBERS</subject><subject>GAS-TURBINE PLANTS</subject><subject>GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTIONAPPARATUS</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2016</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDB29vcNcPULdgzx9PdTcAwOdvV18olUcPMPUnBUcHEEygUp-LsB2e6OwQohoUFOnn6uPAysaYk5xam8UJqbQdnNNcTZQze1ID8-tbggMTk1L7Uk3jvIyMDQzMDA3NDYyNzRmDhVABOLJ4s</recordid><startdate>20160621</startdate><enddate>20160621</enddate><creator>SOBOL KAROLINA KRYSTYNA</creator><creator>BENZ URS</creator><creator>WELTI CHRISTOPH</creator><scope>EVB</scope></search><sort><creationdate>20160621</creationdate><title>COMPENSATION ASSEMBLY FOR A DAMPER OF A GAS TURBINE</title><author>SOBOL KAROLINA KRYSTYNA ; BENZ URS ; WELTI CHRISTOPH</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_KR20160071327A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; kor</language><creationdate>2016</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FORCOMBUSTION CHAMBERS, e.g. FIREBRIDGES</topic><topic>COMBUSTION APPARATUS</topic><topic>COMBUSTION ENGINES</topic><topic>COMBUSTION PROCESSES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDEDFOR</topic><topic>DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS INCOMBUSTION CHAMBERS</topic><topic>GAS-TURBINE PLANTS</topic><topic>GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTIONAPPARATUS</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>SOBOL KAROLINA KRYSTYNA</creatorcontrib><creatorcontrib>BENZ URS</creatorcontrib><creatorcontrib>WELTI CHRISTOPH</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>SOBOL KAROLINA KRYSTYNA</au><au>BENZ URS</au><au>WELTI CHRISTOPH</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>COMPENSATION ASSEMBLY FOR A DAMPER OF A GAS TURBINE</title><date>2016-06-21</date><risdate>2016</risdate><abstract>The present invention relates to dampers for a gas turbine and, specifically, to a compensation assembly for a damper of a gas turbine, which is to reduce a wave generated in a combustion chamber. The damper includes a resonator cavity including a neck tube connected to the inside of the combustion chamber in order for a fluid to flow. The compensation assembly includes a bulb shape part arranged around the neck tube and formed to allow relative rotation between the combustion chamber and the resonator cavity, wherein the bulb shape part is connected to the neck tube; and a round joint including a round socket suitable to host the bulb shape part to the inside. The round socket includes an upper collar part and a lower collar part connected to each other.
본 발명은 가스 터빈을 위한 댐퍼들에 관한 것이고, 특히 연소실에서 일어나는 파동을 감소시키기 위하여 가스 터빈의 댐퍼를 위한 보상 조립체에 관한 것이고, 댐펀느 연소실의 내부와 유체 소통하는 목부 튜브를 구비한 공명기 캐비티를 포함하고, 보상 조립체는, 목부 튜브와 결합되고 연소실과 공명기 캐비티 사이의 상대적 회전을 허용하도록 구성되고 목부 튜브 주위에 배치된 전구형 부분과, 전구형 부분을 내부적으로 호스팅하는데 적합한 구형 소켓을 포함하는 구형 조인트를 포함하며, 구형 소켓은 서로 연결된 상부 칼라 부분과 저부 칼라 부분을 포함한다.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FORCOMBUSTION CHAMBERS, e.g. FIREBRIDGES COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDEDFOR DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS INCOMBUSTION CHAMBERS GAS-TURBINE PLANTS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTIONAPPARATUS WEAPONS |
| title | COMPENSATION ASSEMBLY FOR A DAMPER OF A GAS TURBINE |
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