COMPRESSOR ROTOR BLADE AIRFOIL
A rotor blade (44) includes an airfoil (100) having an airfoil shape (150). The airfoil shape (150) has a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in one of Table I, Table II, Table III, or Table IV. The Cartesian coordinate values of X, Y...
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| creator | DUTKA, Michael James DEIVERNOIS, Paul G BLOHM, Marcus Edward SCHUHLE, Lauren Alexandra CHALUVADI, Venkata Siva Prasad DEJORIS, Timothy E HUBBERT, Corey Lynn LATIMER, Jeremy Peter |
| description | A rotor blade (44) includes an airfoil (100) having an airfoil shape (150). The airfoil shape (150) has a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in one of Table I, Table II, Table III, or Table IV. The Cartesian coordinate values of X, Y and Z are non-dimensional values from 0% to 100% convertible to dimensional distances expressed in a unit of distance by multiplying the Cartesian coordinate values of X, Y and Z by a scaling factor of the airfoil in the unit of distance. The X and Y values, when connected by smooth continuing arcs, define airfoil profile sections at each Z value. The airfoil profile sections at Z values are joined smoothly with one another to form a complete airfoil shape (150). |
| format | Patent |
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The airfoil shape (150) has a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in one of Table I, Table II, Table III, or Table IV. The Cartesian coordinate values of X, Y and Z are non-dimensional values from 0% to 100% convertible to dimensional distances expressed in a unit of distance by multiplying the Cartesian coordinate values of X, Y and Z by a scaling factor of the airfoil in the unit of distance. The X and Y values, when connected by smooth continuing arcs, define airfoil profile sections at each Z value. The airfoil profile sections at Z values are joined smoothly with one another to form a complete airfoil shape (150).</description><language>eng ; fre ; ger</language><subject>BLASTING ; ENGINE PLANTS IN GENERAL ; HEATING ; 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>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=20221102&DB=EPODOC&CC=EP&NR=4083380A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20221102&DB=EPODOC&CC=EP&NR=4083380A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>DUTKA, Michael James</creatorcontrib><creatorcontrib>DEIVERNOIS, Paul G</creatorcontrib><creatorcontrib>BLOHM, Marcus Edward</creatorcontrib><creatorcontrib>SCHUHLE, Lauren Alexandra</creatorcontrib><creatorcontrib>CHALUVADI, Venkata Siva Prasad</creatorcontrib><creatorcontrib>DEJORIS, Timothy E</creatorcontrib><creatorcontrib>HUBBERT, Corey Lynn</creatorcontrib><creatorcontrib>LATIMER, Jeremy Peter</creatorcontrib><title>COMPRESSOR ROTOR BLADE AIRFOIL</title><description>A rotor blade (44) includes an airfoil (100) having an airfoil shape (150). The airfoil shape (150) has a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in one of Table I, Table II, Table III, or Table IV. The Cartesian coordinate values of X, Y and Z are non-dimensional values from 0% to 100% convertible to dimensional distances expressed in a unit of distance by multiplying the Cartesian coordinate values of X, Y and Z by a scaling factor of the airfoil in the unit of distance. The X and Y values, when connected by smooth continuing arcs, define airfoil profile sections at each Z value. The airfoil profile sections at Z values are joined smoothly with one another to form a complete airfoil shape (150).</description><subject>BLASTING</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>HEATING</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>NON-POSITIVE DISPLACEMENT PUMPS</subject><subject>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</subject><subject>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</subject><subject>STEAM ENGINES</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJBz9vcNCHINDvYPUgjyDwGSTj6OLq4Kjp5Bbv6ePjwMrGmJOcWpvFCam0HBzTXE2UM3tSA_PrW4IDE5NS-1JN41wMTAwtjYwsDR0JgIJQB83iEC</recordid><startdate>20221102</startdate><enddate>20221102</enddate><creator>DUTKA, Michael James</creator><creator>DEIVERNOIS, Paul G</creator><creator>BLOHM, Marcus Edward</creator><creator>SCHUHLE, Lauren Alexandra</creator><creator>CHALUVADI, Venkata Siva Prasad</creator><creator>DEJORIS, Timothy E</creator><creator>HUBBERT, Corey Lynn</creator><creator>LATIMER, Jeremy Peter</creator><scope>EVB</scope></search><sort><creationdate>20221102</creationdate><title>COMPRESSOR ROTOR BLADE AIRFOIL</title><author>DUTKA, Michael James ; DEIVERNOIS, Paul G ; BLOHM, Marcus Edward ; SCHUHLE, Lauren Alexandra ; CHALUVADI, Venkata Siva Prasad ; DEJORIS, Timothy E ; HUBBERT, Corey Lynn ; LATIMER, Jeremy Peter</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP4083380A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2022</creationdate><topic>BLASTING</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>HEATING</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>NON-POSITIVE DISPLACEMENT PUMPS</topic><topic>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</topic><topic>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</topic><topic>STEAM ENGINES</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>DUTKA, Michael James</creatorcontrib><creatorcontrib>DEIVERNOIS, Paul G</creatorcontrib><creatorcontrib>BLOHM, Marcus Edward</creatorcontrib><creatorcontrib>SCHUHLE, Lauren Alexandra</creatorcontrib><creatorcontrib>CHALUVADI, Venkata Siva Prasad</creatorcontrib><creatorcontrib>DEJORIS, Timothy E</creatorcontrib><creatorcontrib>HUBBERT, Corey Lynn</creatorcontrib><creatorcontrib>LATIMER, Jeremy Peter</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>DUTKA, Michael James</au><au>DEIVERNOIS, Paul G</au><au>BLOHM, Marcus Edward</au><au>SCHUHLE, Lauren Alexandra</au><au>CHALUVADI, Venkata Siva Prasad</au><au>DEJORIS, Timothy E</au><au>HUBBERT, Corey Lynn</au><au>LATIMER, Jeremy Peter</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>COMPRESSOR ROTOR BLADE AIRFOIL</title><date>2022-11-02</date><risdate>2022</risdate><abstract>A rotor blade (44) includes an airfoil (100) having an airfoil shape (150). The airfoil shape (150) has a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in one of Table I, Table II, Table III, or Table IV. The Cartesian coordinate values of X, Y and Z are non-dimensional values from 0% to 100% convertible to dimensional distances expressed in a unit of distance by multiplying the Cartesian coordinate values of X, Y and Z by a scaling factor of the airfoil in the unit of distance. The X and Y values, when connected by smooth continuing arcs, define airfoil profile sections at each Z value. The airfoil profile sections at Z values are joined smoothly with one another to form a complete airfoil shape (150).</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| subjects | BLASTING ENGINE PLANTS IN GENERAL HEATING 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 | COMPRESSOR ROTOR BLADE AIRFOIL |
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