INLET GUIDE WHEEL FOR A TURBO ENGINE
An embodiment of the invention relates to an inlet guide wheel for a turbo engine with a plurality of guide vanes that radially extend inside a flow channel of the turbo engine, and that respectively comprise: a first, radially outer aerofoil that comprises a radially inner end, and a second, radial...
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creator | HEINICHEN, Frank |
description | An embodiment of the invention relates to an inlet guide wheel for a turbo engine with a plurality of guide vanes that radially extend inside a flow channel of the turbo engine, and that respectively comprise: a first, radially outer aerofoil that comprises a radially inner end, and a second, radially inner aerofoil that comprises a radially outer end, wherein the first aerofoil and/or the second aerofoil is embodied in a rotatable manner. It is provided that the first aerofoil and the second aerofoil are separated by a tip shroud which at least partially covers both the radially inner end of the first aerofoil and the radially outer end of the second aerofoil. |
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It is provided that the first aerofoil and the second aerofoil are separated by a tip shroud which at least partially covers both the radially inner end of the first aerofoil and the radially outer end of the second aerofoil.</description><language>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>2018</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=20180524&DB=EPODOC&CC=US&NR=2018142569A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20180524&DB=EPODOC&CC=US&NR=2018142569A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>HEINICHEN, Frank</creatorcontrib><title>INLET GUIDE WHEEL FOR A TURBO ENGINE</title><description>An embodiment of the invention relates to an inlet guide wheel for a turbo engine with a plurality of guide vanes that radially extend inside a flow channel of the turbo engine, and that respectively comprise: a first, radially outer aerofoil that comprises a radially inner end, and a second, radially inner aerofoil that comprises a radially outer end, wherein the first aerofoil and/or the second aerofoil is embodied in a rotatable manner. It is provided that the first aerofoil and the second aerofoil are separated by a tip shroud which at least partially covers both the radially inner end of the first aerofoil and the radially outer end of the second aerofoil.</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>2018</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFDx9PNxDVFwD_V0cVUI93B19VFw8w9ScFQICQ1y8ldw9XP39HPlYWBNS8wpTuWF0twMym6uIc4euqkF-fGpxQWJyal5qSXxocFGBoYWhiZGpmaWjobGxKkCAN6bI5Q</recordid><startdate>20180524</startdate><enddate>20180524</enddate><creator>HEINICHEN, Frank</creator><scope>EVB</scope></search><sort><creationdate>20180524</creationdate><title>INLET GUIDE WHEEL FOR A TURBO ENGINE</title><author>HEINICHEN, Frank</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2018142569A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2018</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>HEINICHEN, Frank</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>HEINICHEN, Frank</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>INLET GUIDE WHEEL FOR A TURBO ENGINE</title><date>2018-05-24</date><risdate>2018</risdate><abstract>An embodiment of the invention relates to an inlet guide wheel for a turbo engine with a plurality of guide vanes that radially extend inside a flow channel of the turbo engine, and that respectively comprise: a first, radially outer aerofoil that comprises a radially inner end, and a second, radially inner aerofoil that comprises a radially outer end, wherein the first aerofoil and/or the second aerofoil is embodied in a rotatable manner. It is provided that the first aerofoil and the second aerofoil are separated by a tip shroud which at least partially covers both the radially inner end of the first aerofoil and the radially outer end of the second aerofoil.</abstract><oa>free_for_read</oa></addata></record> |
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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 | INLET GUIDE WHEEL FOR A TURBO ENGINE |
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