HIGH-PRESSURE COMPRESSOR ROTOR BLADE WITH LEADING EDGE HAVING INDENT SEGMENT
A rotor blade (208) comprises a mount (210) and a blade (212) that extends from the mount along a radial axis (121). The leading edge (222) includes an indent segment (232). The leading edge has a leading edge radial length (221) measured along the radial axis. The indent segment has an indent radia...
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| creator | REYNOLDS, Bruce David VOGIATZIS, Costas CONNER, Bruce David GENTRY, Timothy |
| description | A rotor blade (208) comprises a mount (210) and a blade (212) that extends from the mount along a radial axis (121). The leading edge (222) includes an indent segment (232). The leading edge has a leading edge radial length (221) measured along the radial axis. The indent segment has an indent radial length (258) measured along the radial axis. The indent segment has an indent depth (256). A first ratio of the indent radial length to the leading edge radial length is at most 0.5. A second ratio of the indent depth to the indent radial length is at least 0.05. |
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The leading edge (222) includes an indent segment (232). The leading edge has a leading edge radial length (221) measured along the radial axis. The indent segment has an indent radial length (258) measured along the radial axis. The indent segment has an indent depth (256). A first ratio of the indent radial length to the leading edge radial length is at most 0.5. A second ratio of the indent depth to the indent radial length is at least 0.05.</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>2023</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=20230503&DB=EPODOC&CC=EP&NR=3372786B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76516</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230503&DB=EPODOC&CC=EP&NR=3372786B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>REYNOLDS, Bruce David</creatorcontrib><creatorcontrib>VOGIATZIS, Costas</creatorcontrib><creatorcontrib>CONNER, Bruce David</creatorcontrib><creatorcontrib>GENTRY, Timothy</creatorcontrib><title>HIGH-PRESSURE COMPRESSOR ROTOR BLADE WITH LEADING EDGE HAVING INDENT SEGMENT</title><description>A rotor blade (208) comprises a mount (210) and a blade (212) that extends from the mount along a radial axis (121). The leading edge (222) includes an indent segment (232). The leading edge has a leading edge radial length (221) measured along the radial axis. The indent segment has an indent radial length (258) measured along the radial axis. The indent segment has an indent depth (256). A first ratio of the indent radial length to the leading edge radial length is at most 0.5. A second ratio of the indent depth to the indent radial length is at least 0.05.</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>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZPDx8HT30A0Icg0ODg1yVXD29wWz_YMUgvxDgKSTj6OLq0K4Z4iHgo-ro4unn7uCq4u7q4KHYxiI7enn4uoXohDs6u4LpHkYWNMSc4pTeaE0N4OCm2uIs4duakF-fGpxQWJyal5qSbxrgLGxuZG5hZmToTERSgBqyi2d</recordid><startdate>20230503</startdate><enddate>20230503</enddate><creator>REYNOLDS, Bruce David</creator><creator>VOGIATZIS, Costas</creator><creator>CONNER, Bruce David</creator><creator>GENTRY, Timothy</creator><scope>EVB</scope></search><sort><creationdate>20230503</creationdate><title>HIGH-PRESSURE COMPRESSOR ROTOR BLADE WITH LEADING EDGE HAVING INDENT SEGMENT</title><author>REYNOLDS, Bruce David ; VOGIATZIS, Costas ; CONNER, Bruce David ; GENTRY, Timothy</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3372786B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2023</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>REYNOLDS, Bruce David</creatorcontrib><creatorcontrib>VOGIATZIS, Costas</creatorcontrib><creatorcontrib>CONNER, Bruce David</creatorcontrib><creatorcontrib>GENTRY, Timothy</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>REYNOLDS, Bruce David</au><au>VOGIATZIS, Costas</au><au>CONNER, Bruce David</au><au>GENTRY, Timothy</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>HIGH-PRESSURE COMPRESSOR ROTOR BLADE WITH LEADING EDGE HAVING INDENT SEGMENT</title><date>2023-05-03</date><risdate>2023</risdate><abstract>A rotor blade (208) comprises a mount (210) and a blade (212) that extends from the mount along a radial axis (121). The leading edge (222) includes an indent segment (232). The leading edge has a leading edge radial length (221) measured along the radial axis. The indent segment has an indent radial length (258) measured along the radial axis. The indent segment has an indent depth (256). A first ratio of the indent radial length to the leading edge radial length is at most 0.5. A second ratio of the indent depth to the indent radial length is at least 0.05.</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 | HIGH-PRESSURE COMPRESSOR ROTOR BLADE WITH LEADING EDGE HAVING INDENT SEGMENT |
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