NON UNIFORM VANE SPACING
The invention discloses a circular row (11) for a non uniform vane spacing blade (15). The circular row includes only one first group (G1) and only one second group (G2) of adjacent vanes (15), unequal first and second spacing (S1, S2) between adjacent vanes (15) in the first and second groups (G1,...
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creator | MARK JOSEPH FRISCH BRIAN RICHARD GREEN STEVEN MITCHELL TAYLOR MARK JOSEPH MIELKE CURTIS MOECKEL JOSEPH MICHAEL BRUNI PETER JOHN WOOD |
description | The invention discloses a circular row (11) for a non uniform vane spacing blade (15). The circular row includes only one first group (G1) and only one second group (G2) of adjacent vanes (15), unequal first and second spacing (S1, S2) between adjacent vanes (15) in the first and second groups (G1, G2), and first spacing (S1) greater than second spacing (S2). An embodiment with second group (G2) includes only three adjacent vanes (15). Second spacing (S2) may be about 25%-35% smaller than a nominal uniform spacing (S) used as a design parameter for designing spacing of the non-uniformly spaced stator vanes (15). Circular row 11 may be sectored. A gas turbine engine section may include one or more rings or circular rows (15)of fixed and/or variable non-uniformally spaced vanes (15). Method for designing non-uniform vane spacing for circular row (15)includes determining nominal uniform spacing (S) and forming first spacing (S1) and second spacing (S2) from nominal uniform spacing (S) of vanes (15).
本发明公开种用于非均匀间 |
format | Patent |
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本发明公开种用于非均匀间</description><language>chi ; eng</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 ; STEAM ENGINES ; WEAPONS</subject><creationdate>2017</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=20170922&DB=EPODOC&CC=CN&NR=107191231A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20170922&DB=EPODOC&CC=CN&NR=107191231A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>MARK JOSEPH FRISCH</creatorcontrib><creatorcontrib>BRIAN RICHARD GREEN</creatorcontrib><creatorcontrib>STEVEN MITCHELL TAYLOR</creatorcontrib><creatorcontrib>MARK JOSEPH MIELKE</creatorcontrib><creatorcontrib>CURTIS MOECKEL</creatorcontrib><creatorcontrib>JOSEPH MICHAEL BRUNI</creatorcontrib><creatorcontrib>PETER JOHN WOOD</creatorcontrib><title>NON UNIFORM VANE SPACING</title><description>The invention discloses a circular row (11) for a non uniform vane spacing blade (15). The circular row includes only one first group (G1) and only one second group (G2) of adjacent vanes (15), unequal first and second spacing (S1, S2) between adjacent vanes (15) in the first and second groups (G1, G2), and first spacing (S1) greater than second spacing (S2). An embodiment with second group (G2) includes only three adjacent vanes (15). Second spacing (S2) may be about 25%-35% smaller than a nominal uniform spacing (S) used as a design parameter for designing spacing of the non-uniformly spaced stator vanes (15). Circular row 11 may be sectored. A gas turbine engine section may include one or more rings or circular rows (15)of fixed and/or variable non-uniformally spaced vanes (15). Method for designing non-uniform vane spacing for circular row (15)includes determining nominal uniform spacing (S) and forming first spacing (S1) and second spacing (S2) from nominal uniform spacing (S) of vanes (15).
本发明公开种用于非均匀间</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>STEAM ENGINES</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2017</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJDw8_dTCPXzdPMP8lUIc_RzVQgOcHT29HPnYWBNS8wpTuWF0twMim6uIc4euqkF-fGpxQWJyal5qSXxzn6GBuaGloZGxoaOxsSoAQDpAR-L</recordid><startdate>20170922</startdate><enddate>20170922</enddate><creator>MARK JOSEPH FRISCH</creator><creator>BRIAN RICHARD GREEN</creator><creator>STEVEN MITCHELL TAYLOR</creator><creator>MARK JOSEPH MIELKE</creator><creator>CURTIS MOECKEL</creator><creator>JOSEPH MICHAEL BRUNI</creator><creator>PETER JOHN WOOD</creator><scope>EVB</scope></search><sort><creationdate>20170922</creationdate><title>NON UNIFORM VANE SPACING</title><author>MARK JOSEPH FRISCH ; BRIAN RICHARD GREEN ; STEVEN MITCHELL TAYLOR ; MARK JOSEPH MIELKE ; CURTIS MOECKEL ; JOSEPH MICHAEL BRUNI ; PETER JOHN WOOD</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN107191231A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2017</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>STEAM ENGINES</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>MARK JOSEPH FRISCH</creatorcontrib><creatorcontrib>BRIAN RICHARD GREEN</creatorcontrib><creatorcontrib>STEVEN MITCHELL TAYLOR</creatorcontrib><creatorcontrib>MARK JOSEPH MIELKE</creatorcontrib><creatorcontrib>CURTIS MOECKEL</creatorcontrib><creatorcontrib>JOSEPH MICHAEL BRUNI</creatorcontrib><creatorcontrib>PETER JOHN WOOD</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>MARK JOSEPH FRISCH</au><au>BRIAN RICHARD GREEN</au><au>STEVEN MITCHELL TAYLOR</au><au>MARK JOSEPH MIELKE</au><au>CURTIS MOECKEL</au><au>JOSEPH MICHAEL BRUNI</au><au>PETER JOHN WOOD</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>NON UNIFORM VANE SPACING</title><date>2017-09-22</date><risdate>2017</risdate><abstract>The invention discloses a circular row (11) for a non uniform vane spacing blade (15). The circular row includes only one first group (G1) and only one second group (G2) of adjacent vanes (15), unequal first and second spacing (S1, S2) between adjacent vanes (15) in the first and second groups (G1, G2), and first spacing (S1) greater than second spacing (S2). An embodiment with second group (G2) includes only three adjacent vanes (15). Second spacing (S2) may be about 25%-35% smaller than a nominal uniform spacing (S) used as a design parameter for designing spacing of the non-uniformly spaced stator vanes (15). Circular row 11 may be sectored. A gas turbine engine section may include one or more rings or circular rows (15)of fixed and/or variable non-uniformally spaced vanes (15). Method for designing non-uniform vane spacing for circular row (15)includes determining nominal uniform spacing (S) and forming first spacing (S1) and second spacing (S2) from nominal uniform spacing (S) of vanes (15).
本发明公开种用于非均匀间</abstract><oa>free_for_read</oa></addata></record> |
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language | chi ; eng |
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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 STEAM ENGINES WEAPONS |
title | NON UNIFORM VANE SPACING |
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