AIR TURBINE STARTER WITH PRIMARY AND SECONDARY AIR FLOW PATHS
An air turbine starter (10) that includes a housing (30). The housing (30) can circumscribe a turbine (54) that is coupled to a gear train (80) in a gear box (82) via a drive shaft (72). A primary air flow path (36) is defined between a primary inlet (32) and a primary outlet (34). Air in the primar...
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| creator | MORYA, Pankaj Kumar MEYERS, Shiloh YAMARTHI, David KERLEY, Steven CHHABRA, Parmeet Singh |
| description | An air turbine starter (10) that includes a housing (30). The housing (30) can circumscribe a turbine (54) that is coupled to a gear train (80) in a gear box (82) via a drive shaft (72). A primary air flow path (36) is defined between a primary inlet (32) and a primary outlet (34). Air in the primary air flow path (36) can flow into a secondary air flow path (56) or rotate the turbine (54), that converts energy from the air flow to rotational mechanical energy. Air in the secondary air flow path (56) can pass through at least a first cavity (74) and first passage (100) before rejoining the primary air flow (36) or joining ambient air. |
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The housing (30) can circumscribe a turbine (54) that is coupled to a gear train (80) in a gear box (82) via a drive shaft (72). A primary air flow path (36) is defined between a primary inlet (32) and a primary outlet (34). Air in the primary air flow path (36) can flow into a secondary air flow path (56) or rotate the turbine (54), that converts energy from the air flow to rotational mechanical energy. Air in the secondary air flow path (56) can pass through at least a first cavity (74) and first passage (100) before rejoining the primary air flow (36) or joining ambient air.</description><language>eng ; fre ; ger</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>2022</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=20220216&DB=EPODOC&CC=EP&NR=3954884A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20220216&DB=EPODOC&CC=EP&NR=3954884A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>MORYA, Pankaj Kumar</creatorcontrib><creatorcontrib>MEYERS, Shiloh</creatorcontrib><creatorcontrib>YAMARTHI, David</creatorcontrib><creatorcontrib>KERLEY, Steven</creatorcontrib><creatorcontrib>CHHABRA, Parmeet Singh</creatorcontrib><title>AIR TURBINE STARTER WITH PRIMARY AND SECONDARY AIR FLOW PATHS</title><description>An air turbine starter (10) that includes a housing (30). The housing (30) can circumscribe a turbine (54) that is coupled to a gear train (80) in a gear box (82) via a drive shaft (72). A primary air flow path (36) is defined between a primary inlet (32) and a primary outlet (34). Air in the primary air flow path (36) can flow into a secondary air flow path (56) or rotate the turbine (54), that converts energy from the air flow to rotational mechanical energy. Air in the secondary air flow path (56) can pass through at least a first cavity (74) and first passage (100) before rejoining the primary air flow (36) or joining ambient air.</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>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLB19AxSCAkNcvL0c1UIDnEMCnENUgj3DPFQCAjy9HUMilRw9HNRCHZ19vdzAfOAyt18_MMVAhxDPIJ5GFjTEnOKU3mhNDeDgptriLOHbmpBfnxqcUFicmpeakm8a4CxpamJhYWJo6ExEUoA4Kwphw</recordid><startdate>20220216</startdate><enddate>20220216</enddate><creator>MORYA, Pankaj Kumar</creator><creator>MEYERS, Shiloh</creator><creator>YAMARTHI, David</creator><creator>KERLEY, Steven</creator><creator>CHHABRA, Parmeet Singh</creator><scope>EVB</scope></search><sort><creationdate>20220216</creationdate><title>AIR TURBINE STARTER WITH PRIMARY AND SECONDARY AIR FLOW PATHS</title><author>MORYA, Pankaj Kumar ; MEYERS, Shiloh ; YAMARTHI, David ; KERLEY, Steven ; CHHABRA, Parmeet Singh</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3954884A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2022</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>MORYA, Pankaj Kumar</creatorcontrib><creatorcontrib>MEYERS, Shiloh</creatorcontrib><creatorcontrib>YAMARTHI, David</creatorcontrib><creatorcontrib>KERLEY, Steven</creatorcontrib><creatorcontrib>CHHABRA, Parmeet Singh</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>MORYA, Pankaj Kumar</au><au>MEYERS, Shiloh</au><au>YAMARTHI, David</au><au>KERLEY, Steven</au><au>CHHABRA, Parmeet Singh</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AIR TURBINE STARTER WITH PRIMARY AND SECONDARY AIR FLOW PATHS</title><date>2022-02-16</date><risdate>2022</risdate><abstract>An air turbine starter (10) that includes a housing (30). The housing (30) can circumscribe a turbine (54) that is coupled to a gear train (80) in a gear box (82) via a drive shaft (72). A primary air flow path (36) is defined between a primary inlet (32) and a primary outlet (34). Air in the primary air flow path (36) can flow into a secondary air flow path (56) or rotate the turbine (54), that converts energy from the air flow to rotational mechanical energy. Air in the secondary air flow path (56) can pass through at least a first cavity (74) and first passage (100) before rejoining the primary air flow (36) or joining ambient air.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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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 PRIMARY AND SECONDARY AIR FLOW PATHS |
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