ARTICLE OF MANUFACTURE
An article of manufacture has a first component configured for use with a turbomachine. The first component is configured for attachment to a second component, and reduces the possibility of attachment with an undesired third component by modification of a. characteristic of the first component. Thi...
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| creator | DELVERNOIS PAUL GRIFFIN LUMPKIN JAMIE DEAN GAU SAN-DAR DUONG JOHN MONTELEONE FRANCO DUTKA MICHAEL JAMES CHALUVADI VENKATA SIVA PRASAD RENGARAJAN GOVINDARAJAN SHRUM ALEXANDER DAVID TIPTON THOMAS ROBBINS MCKEEVER MATTHEW JOHN BONINI ERIC RICHARD BLOHM MARC EDWARD LATIMER JEREMY PETER LAMASTER CHRISTOPHER EDWARD CHIU YA-TIEN AARON KELVIN RONO |
| description | An article of manufacture has a first component configured for use with a turbomachine. The first component is configured for attachment to a second component, and reduces the possibility of attachment with an undesired third component by modification of a. characteristic of the first component. This modification is matched by a complementary characteristic of the second component. The first component has a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a scalable table selected from the group consisting of TABLES 1-11. Cartesian coordinate values of X, Y and Z are non-dimensional values convertible to dimensional distances by multiplying by a number. X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height. The airfoil profile sections at each Z height being joined with one another to form a complete airfoil shape. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_US2014030098A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>US2014030098A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_US2014030098A13</originalsourceid><addsrcrecordid>eNrjZBBzDArxdPZxVfB3U_B19At1c3QOCQ1y5WFgTUvMKU7lhdLcDMpuriHOHrqpBfnxqcUFicmpeakl8aHBRgaGJgbGBgaWFo6GxsSpAgApVh_7</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>ARTICLE OF MANUFACTURE</title><source>esp@cenet</source><creator>DELVERNOIS PAUL GRIFFIN ; LUMPKIN JAMIE DEAN ; GAU SAN-DAR ; DUONG JOHN ; MONTELEONE FRANCO ; DUTKA MICHAEL JAMES ; CHALUVADI VENKATA SIVA PRASAD ; RENGARAJAN GOVINDARAJAN ; SHRUM ALEXANDER DAVID ; TIPTON THOMAS ROBBINS ; MCKEEVER MATTHEW JOHN ; BONINI ERIC RICHARD ; BLOHM MARC EDWARD ; LATIMER JEREMY PETER ; LAMASTER CHRISTOPHER EDWARD ; CHIU YA-TIEN ; AARON KELVIN RONO</creator><creatorcontrib>DELVERNOIS PAUL GRIFFIN ; LUMPKIN JAMIE DEAN ; GAU SAN-DAR ; DUONG JOHN ; MONTELEONE FRANCO ; DUTKA MICHAEL JAMES ; CHALUVADI VENKATA SIVA PRASAD ; RENGARAJAN GOVINDARAJAN ; SHRUM ALEXANDER DAVID ; TIPTON THOMAS ROBBINS ; MCKEEVER MATTHEW JOHN ; BONINI ERIC RICHARD ; BLOHM MARC EDWARD ; LATIMER JEREMY PETER ; LAMASTER CHRISTOPHER EDWARD ; CHIU YA-TIEN ; AARON KELVIN RONO</creatorcontrib><description>An article of manufacture has a first component configured for use with a turbomachine. The first component is configured for attachment to a second component, and reduces the possibility of attachment with an undesired third component by modification of a. characteristic of the first component. This modification is matched by a complementary characteristic of the second component. The first component has a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a scalable table selected from the group consisting of TABLES 1-11. Cartesian coordinate values of X, Y and Z are non-dimensional values convertible to dimensional distances by multiplying by a number. X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height. The airfoil profile sections at each Z height being joined with one another to form a complete airfoil shape.</description><language>eng</language><subject>BLASTING ; ENGINE PLANTS IN GENERAL ; HEATING ; INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS ; INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; NON-POSITIVE DISPLACEMENT PUMPS ; POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS ; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS ; STEAM ENGINES ; WEAPONS</subject><creationdate>2014</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=20140130&DB=EPODOC&CC=US&NR=2014030098A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20140130&DB=EPODOC&CC=US&NR=2014030098A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>DELVERNOIS PAUL GRIFFIN</creatorcontrib><creatorcontrib>LUMPKIN JAMIE DEAN</creatorcontrib><creatorcontrib>GAU SAN-DAR</creatorcontrib><creatorcontrib>DUONG JOHN</creatorcontrib><creatorcontrib>MONTELEONE FRANCO</creatorcontrib><creatorcontrib>DUTKA MICHAEL JAMES</creatorcontrib><creatorcontrib>CHALUVADI VENKATA SIVA PRASAD</creatorcontrib><creatorcontrib>RENGARAJAN GOVINDARAJAN</creatorcontrib><creatorcontrib>SHRUM ALEXANDER DAVID</creatorcontrib><creatorcontrib>TIPTON THOMAS ROBBINS</creatorcontrib><creatorcontrib>MCKEEVER MATTHEW JOHN</creatorcontrib><creatorcontrib>BONINI ERIC RICHARD</creatorcontrib><creatorcontrib>BLOHM MARC EDWARD</creatorcontrib><creatorcontrib>LATIMER JEREMY PETER</creatorcontrib><creatorcontrib>LAMASTER CHRISTOPHER EDWARD</creatorcontrib><creatorcontrib>CHIU YA-TIEN</creatorcontrib><creatorcontrib>AARON KELVIN RONO</creatorcontrib><title>ARTICLE OF MANUFACTURE</title><description>An article of manufacture has a first component configured for use with a turbomachine. The first component is configured for attachment to a second component, and reduces the possibility of attachment with an undesired third component by modification of a. characteristic of the first component. This modification is matched by a complementary characteristic of the second component. The first component has a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a scalable table selected from the group consisting of TABLES 1-11. Cartesian coordinate values of X, Y and Z are non-dimensional values convertible to dimensional distances by multiplying by a number. X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height. 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The first component is configured for attachment to a second component, and reduces the possibility of attachment with an undesired third component by modification of a. characteristic of the first component. This modification is matched by a complementary characteristic of the second component. The first component has a nominal airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a scalable table selected from the group consisting of TABLES 1-11. Cartesian coordinate values of X, Y and Z are non-dimensional values convertible to dimensional distances by multiplying by a number. X and Y are coordinates which, when connected by continuing arcs, define airfoil profile sections at each Z height. The airfoil profile sections at each Z height being joined with one another to form a complete airfoil shape.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | BLASTING ENGINE PLANTS IN GENERAL HEATING INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS STEAM ENGINES WEAPONS |
| title | ARTICLE OF MANUFACTURE |
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