Attachment of piloting feature
A fan assembly for use in a gas turbine engine of an aircraft includes a fan disk having a number of fan blades and a windage shield coupled to the fan disk to move therewith. The fan assembly supplies air for use in the engine. The windage shield rotates with the fan disk during operation of the ga...
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creator | Engebretsen, Eric W Kappes, Matthew J Conrad, Rodney D Bailey, Patrick E Lacombe, Samuel J |
description | A fan assembly for use in a gas turbine engine of an aircraft includes a fan disk having a number of fan blades and a windage shield coupled to the fan disk to move therewith. The fan assembly supplies air for use in the engine. The windage shield rotates with the fan disk during operation of the gas turbine engine and directs air supplied by the fan blade. |
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The fan assembly supplies air for use in the engine. The windage shield rotates with the fan disk during operation of the gas turbine engine and directs air supplied by the fan blade.</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>2019</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=20191119&DB=EPODOC&CC=US&NR=10480321B2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76516</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20191119&DB=EPODOC&CC=US&NR=10480321B2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Engebretsen, Eric W</creatorcontrib><creatorcontrib>Kappes, Matthew J</creatorcontrib><creatorcontrib>Conrad, Rodney D</creatorcontrib><creatorcontrib>Bailey, Patrick E</creatorcontrib><creatorcontrib>Lacombe, Samuel J</creatorcontrib><title>Attachment of piloting feature</title><description>A fan assembly for use in a gas turbine engine of an aircraft includes a fan disk having a number of fan blades and a windage shield coupled to the fan disk to move therewith. The fan assembly supplies air for use in the engine. The windage shield rotates with the fan disk during operation of the gas turbine engine and directs air supplied by the fan blade.</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>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJBzLClJTM7ITc0rUchPUyjIzMkvycxLV0hLTSwpLUrlYWBNS8wpTuWF0twMim6uIc4euqkF-fGpxQWJyal5qSXxocGGBiYWBsZGhk5GxsSoAQAEmySv</recordid><startdate>20191119</startdate><enddate>20191119</enddate><creator>Engebretsen, Eric W</creator><creator>Kappes, Matthew J</creator><creator>Conrad, Rodney D</creator><creator>Bailey, Patrick E</creator><creator>Lacombe, Samuel J</creator><scope>EVB</scope></search><sort><creationdate>20191119</creationdate><title>Attachment of piloting feature</title><author>Engebretsen, Eric W ; Kappes, Matthew J ; Conrad, Rodney D ; Bailey, Patrick E ; Lacombe, Samuel J</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US10480321B23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2019</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>Engebretsen, Eric W</creatorcontrib><creatorcontrib>Kappes, Matthew J</creatorcontrib><creatorcontrib>Conrad, Rodney D</creatorcontrib><creatorcontrib>Bailey, Patrick E</creatorcontrib><creatorcontrib>Lacombe, Samuel J</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Engebretsen, Eric W</au><au>Kappes, Matthew J</au><au>Conrad, Rodney D</au><au>Bailey, Patrick E</au><au>Lacombe, Samuel J</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Attachment of piloting feature</title><date>2019-11-19</date><risdate>2019</risdate><abstract>A fan assembly for use in a gas turbine engine of an aircraft includes a fan disk having a number of fan blades and a windage shield coupled to the fan disk to move therewith. The fan assembly supplies air for use in the engine. The windage shield rotates with the fan disk during operation of the gas turbine engine and directs air supplied by the fan blade.</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 | Attachment of piloting feature |
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