Damper for a turbine rotor assembly
A damper (36) for a turbine rotor assembly (22) of a gas turbine engine (100) may include a forward plate (76) with a forward face (45) and an aft face (75), and an aft plate (78) with a forward face (88) and an aft face (87). The aft face of the forward plate may be connected to the forward face of...
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| creator | FAULDER LESLIE JOHN TARCZY JEFFREY EUGENE |
| description | A damper (36) for a turbine rotor assembly (22) of a gas turbine engine (100) may include a forward plate (76) with a forward face (45) and an aft face (75), and an aft plate (78) with a forward face (88) and an aft face (87). The aft face of the forward plate may be connected to the forward face of the aft plate with a longitudinal structure (80). An area of the aft plate in a plane transverse to the longitudinal structure may be greater than an area of the forward plate in the plane transverse to the longitudinal structure. The damper may also include a pocket (71) on the forward face of the forward plate. |
| format | Patent |
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The aft face of the forward plate may be connected to the forward face of the aft plate with a longitudinal structure (80). An area of the aft plate in a plane transverse to the longitudinal structure may be greater than an area of the forward plate in the plane transverse to the longitudinal structure. The damper may also include a pocket (71) on the forward face of the forward plate.</description><language>eng</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>2015</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=20150708&DB=EPODOC&CC=CN&NR=104769223A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20150708&DB=EPODOC&CC=CN&NR=104769223A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>FAULDER LESLIE JOHN</creatorcontrib><creatorcontrib>TARCZY JEFFREY EUGENE</creatorcontrib><title>Damper for a turbine rotor assembly</title><description>A damper (36) for a turbine rotor assembly (22) of a gas turbine engine (100) may include a forward plate (76) with a forward face (45) and an aft face (75), and an aft plate (78) with a forward face (88) and an aft face (87). The aft face of the forward plate may be connected to the forward face of the aft plate with a longitudinal structure (80). An area of the aft plate in a plane transverse to the longitudinal structure may be greater than an area of the forward plate in the plane transverse to the longitudinal structure. The damper may also include a pocket (71) on the forward face of the forward plate.</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>2015</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFB2ScwtSC1SSMsvUkhUKCktSsrMS1Uoyi8B8YuLU3OTcip5GFjTEnOKU3mhNDeDoptriLOHbmpBfnxqcUFicmpeakm8s5-hgYm5maWRkbGjMTFqAMhuJj4</recordid><startdate>20150708</startdate><enddate>20150708</enddate><creator>FAULDER LESLIE JOHN</creator><creator>TARCZY JEFFREY EUGENE</creator><scope>EVB</scope></search><sort><creationdate>20150708</creationdate><title>Damper for a turbine rotor assembly</title><author>FAULDER LESLIE JOHN ; TARCZY JEFFREY EUGENE</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN104769223A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2015</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>FAULDER LESLIE JOHN</creatorcontrib><creatorcontrib>TARCZY JEFFREY EUGENE</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>FAULDER LESLIE JOHN</au><au>TARCZY JEFFREY EUGENE</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Damper for a turbine rotor assembly</title><date>2015-07-08</date><risdate>2015</risdate><abstract>A damper (36) for a turbine rotor assembly (22) of a gas turbine engine (100) may include a forward plate (76) with a forward face (45) and an aft face (75), and an aft plate (78) with a forward face (88) and an aft face (87). The aft face of the forward plate may be connected to the forward face of the aft plate with a longitudinal structure (80). An area of the aft plate in a plane transverse to the longitudinal structure may be greater than an area of the forward plate in the plane transverse to the longitudinal structure. The damper may also include a pocket (71) on the forward face of the forward plate.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng |
| recordid | cdi_epo_espacenet_CN104769223A |
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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 | Damper for a turbine rotor assembly |
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