AIR TURBINE STARTER WITH CONTAINMENT ASSEMBLY
공기 터빈 스타터는 주요 공기 흐름 유로를 갖는 내부를 형성하는 하우징을 포함한다. 내부에 위치하는 회전식 터빈 부재는 주요 공기 유로 내로 연장되는 복수 개의 둘레방향으로 이격된 블레이드를 포함한다. 격납 조립체는 하우징에 커플링되고 복수 개의 둘레방향으로 이격된 블레이드의 적어도 일부를 에워싼다. 격납 조립체는 튜브와 라미네이트를 포함한다. An air turbine starter (10, 310) that includes a housing (30, 330) defining an interior (31, 331) having a...
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| creator | SEBASTIAN MERIN PATIL SHARAD PUNDLIK MEYERS SHILOH MONTEGOMERY BADDAM NAGENDRA JONNALAGADDA DATTU GV |
| description | 공기 터빈 스타터는 주요 공기 흐름 유로를 갖는 내부를 형성하는 하우징을 포함한다. 내부에 위치하는 회전식 터빈 부재는 주요 공기 유로 내로 연장되는 복수 개의 둘레방향으로 이격된 블레이드를 포함한다. 격납 조립체는 하우징에 커플링되고 복수 개의 둘레방향으로 이격된 블레이드의 적어도 일부를 에워싼다. 격납 조립체는 튜브와 라미네이트를 포함한다.
An air turbine starter (10, 310) that includes a housing (30, 330) defining an interior (31, 331) having a primary air flow path (36, 336). A rotatable turbine member (42, 342) located in the interior (31, 331) includes a plurality of circumferentially spaced blades (43, 343) that extend into the primary air flow path (36, 336). A containment assembly (44, 144, 344, 444) couples to the housing (30, 330) and circumscribes at least a portion of the plurality of circumferentially spaced blades (43, 343). The containment assembly (44, 144, 344, 444) includes a tube (346) and a laminate (348, 448, 448a, 448b, 448c, 448d). |
| format | Patent |
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An air turbine starter (10, 310) that includes a housing (30, 330) defining an interior (31, 331) having a primary air flow path (36, 336). A rotatable turbine member (42, 342) located in the interior (31, 331) includes a plurality of circumferentially spaced blades (43, 343) that extend into the primary air flow path (36, 336). A containment assembly (44, 144, 344, 444) couples to the housing (30, 330) and circumscribes at least a portion of the plurality of circumferentially spaced blades (43, 343). The containment assembly (44, 144, 344, 444) includes a tube (346) and a laminate (348, 448, 448a, 448b, 448c, 448d).</description><language>eng ; kor</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; ENGINE PLANTS IN GENERAL ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; 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=20241126&DB=EPODOC&CC=KR&NR=20240166930A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20241126&DB=EPODOC&CC=KR&NR=20240166930A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>SEBASTIAN MERIN</creatorcontrib><creatorcontrib>PATIL SHARAD PUNDLIK</creatorcontrib><creatorcontrib>MEYERS SHILOH MONTEGOMERY</creatorcontrib><creatorcontrib>BADDAM NAGENDRA</creatorcontrib><creatorcontrib>JONNALAGADDA DATTU GV</creatorcontrib><title>AIR TURBINE STARTER WITH CONTAINMENT ASSEMBLY</title><description>공기 터빈 스타터는 주요 공기 흐름 유로를 갖는 내부를 형성하는 하우징을 포함한다. 내부에 위치하는 회전식 터빈 부재는 주요 공기 유로 내로 연장되는 복수 개의 둘레방향으로 이격된 블레이드를 포함한다. 격납 조립체는 하우징에 커플링되고 복수 개의 둘레방향으로 이격된 블레이드의 적어도 일부를 에워싼다. 격납 조립체는 튜브와 라미네이트를 포함한다.
An air turbine starter (10, 310) that includes a housing (30, 330) defining an interior (31, 331) having a primary air flow path (36, 336). A rotatable turbine member (42, 342) located in the interior (31, 331) includes a plurality of circumferentially spaced blades (43, 343) that extend into the primary air flow path (36, 336). A containment assembly (44, 144, 344, 444) couples to the housing (30, 330) and circumscribes at least a portion of the plurality of circumferentially spaced blades (43, 343). The containment assembly (44, 144, 344, 444) includes a tube (346) and a laminate (348, 448, 448a, 448b, 448c, 448d).</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</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>eNrjZNB19AxSCAkNcvL0c1UIDnEMCnENUgj3DPFQcPb3C3H09PN19QtRcAwOdvV18onkYWBNS8wpTuWF0twMym6uIc4euqkF-fGpxQWJyal5qSXx3kFGBkYmBoZmZpbGBo7GxKkCAGeEJog</recordid><startdate>20241126</startdate><enddate>20241126</enddate><creator>SEBASTIAN MERIN</creator><creator>PATIL SHARAD PUNDLIK</creator><creator>MEYERS SHILOH MONTEGOMERY</creator><creator>BADDAM NAGENDRA</creator><creator>JONNALAGADDA DATTU GV</creator><scope>EVB</scope></search><sort><creationdate>20241126</creationdate><title>AIR TURBINE STARTER WITH CONTAINMENT ASSEMBLY</title><author>SEBASTIAN MERIN ; PATIL SHARAD PUNDLIK ; MEYERS SHILOH MONTEGOMERY ; BADDAM NAGENDRA ; JONNALAGADDA DATTU GV</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_KR20240166930A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; kor</language><creationdate>2024</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</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>SEBASTIAN MERIN</creatorcontrib><creatorcontrib>PATIL SHARAD PUNDLIK</creatorcontrib><creatorcontrib>MEYERS SHILOH MONTEGOMERY</creatorcontrib><creatorcontrib>BADDAM NAGENDRA</creatorcontrib><creatorcontrib>JONNALAGADDA DATTU GV</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>SEBASTIAN MERIN</au><au>PATIL SHARAD PUNDLIK</au><au>MEYERS SHILOH MONTEGOMERY</au><au>BADDAM NAGENDRA</au><au>JONNALAGADDA DATTU GV</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AIR TURBINE STARTER WITH CONTAINMENT ASSEMBLY</title><date>2024-11-26</date><risdate>2024</risdate><abstract>공기 터빈 스타터는 주요 공기 흐름 유로를 갖는 내부를 형성하는 하우징을 포함한다. 내부에 위치하는 회전식 터빈 부재는 주요 공기 유로 내로 연장되는 복수 개의 둘레방향으로 이격된 블레이드를 포함한다. 격납 조립체는 하우징에 커플링되고 복수 개의 둘레방향으로 이격된 블레이드의 적어도 일부를 에워싼다. 격납 조립체는 튜브와 라미네이트를 포함한다.
An air turbine starter (10, 310) that includes a housing (30, 330) defining an interior (31, 331) having a primary air flow path (36, 336). A rotatable turbine member (42, 342) located in the interior (31, 331) includes a plurality of circumferentially spaced blades (43, 343) that extend into the primary air flow path (36, 336). A containment assembly (44, 144, 344, 444) couples to the housing (30, 330) and circumscribes at least a portion of the plurality of circumferentially spaced blades (43, 343). The containment assembly (44, 144, 344, 444) includes a tube (346) and a laminate (348, 448, 448a, 448b, 448c, 448d).</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; kor |
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| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS |
| title | AIR TURBINE STARTER WITH CONTAINMENT ASSEMBLY |
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