SPINNER AFT-EXTENDED FORWARD RETURN FLANGE
A spinner (15) for a fan assembly (11) of a gas turbine engine (10), a method of fabricating a spinner for a fan assembly (11) of a gas turbine engine (10), and a gas turbine engine (10) are disclosed. The fan section (11) may include a nosecap (25). The spinner (15) may include a forward end (17),...
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creator | KLING, Colin J LUSSIER, Darin X |
description | A spinner (15) for a fan assembly (11) of a gas turbine engine (10), a method of fabricating a spinner for a fan assembly (11) of a gas turbine engine (10), and a gas turbine engine (10) are disclosed. The fan section (11) may include a nosecap (25). The spinner (15) may include a forward end (17), an aft end (18), and a return flange (30) associated with the forward end (17). The return flange (30) may include a forward flange (34) extending forward towards the nosecap (25) and an aft flange (32) extending aft towards the aft end (18). |
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The fan section (11) may include a nosecap (25). The spinner (15) may include a forward end (17), an aft end (18), and a return flange (30) associated with the forward end (17). The return flange (30) may include a forward flange (34) extending forward towards the nosecap (25) and an aft flange (32) extending aft towards the aft end (18).</description><language>eng ; fre ; ger</language><subject>AEROPLANES ; AIR INTAKES FOR JET-PROPULSION PLANTS ; AIRCRAFT ; AVIATION ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; COSMONAUTICS ; GAS-TURBINE PLANTS ; HEATING ; HELICOPTERS ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; PERFORMING OPERATIONS ; TRANSPORTING ; WEAPONS</subject><creationdate>2021</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=20210526&DB=EPODOC&CC=EP&NR=2980385B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76516</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20210526&DB=EPODOC&CC=EP&NR=2980385B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KLING, Colin J</creatorcontrib><creatorcontrib>LUSSIER, Darin X</creatorcontrib><title>SPINNER AFT-EXTENDED FORWARD RETURN FLANGE</title><description>A spinner (15) for a fan assembly (11) of a gas turbine engine (10), a method of fabricating a spinner for a fan assembly (11) of a gas turbine engine (10), and a gas turbine engine (10) are disclosed. The fan section (11) may include a nosecap (25). The spinner (15) may include a forward end (17), an aft end (18), and a return flange (30) associated with the forward end (17). The return flange (30) may include a forward flange (34) extending forward towards the nosecap (25) and an aft flange (32) extending aft towards the aft end (18).</description><subject>AEROPLANES</subject><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>COSMONAUTICS</subject><subject>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HELICOPTERS</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2021</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNAKDvD083MNUnB0C9F1jQhx9XNxdVFw8w8KdwxyUQhyDQkN8lNw83H0c3flYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxrgFGlhYGxhamTobGRCgBABJYJFs</recordid><startdate>20210526</startdate><enddate>20210526</enddate><creator>KLING, Colin J</creator><creator>LUSSIER, Darin X</creator><scope>EVB</scope></search><sort><creationdate>20210526</creationdate><title>SPINNER AFT-EXTENDED FORWARD RETURN FLANGE</title><author>KLING, Colin J ; LUSSIER, Darin X</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2980385B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2021</creationdate><topic>AEROPLANES</topic><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>COSMONAUTICS</topic><topic>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HELICOPTERS</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>KLING, Colin J</creatorcontrib><creatorcontrib>LUSSIER, Darin X</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>KLING, Colin J</au><au>LUSSIER, Darin X</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>SPINNER AFT-EXTENDED FORWARD RETURN FLANGE</title><date>2021-05-26</date><risdate>2021</risdate><abstract>A spinner (15) for a fan assembly (11) of a gas turbine engine (10), a method of fabricating a spinner for a fan assembly (11) of a gas turbine engine (10), and a gas turbine engine (10) are disclosed. The fan section (11) may include a nosecap (25). The spinner (15) may include a forward end (17), an aft end (18), and a return flange (30) associated with the forward end (17). The return flange (30) may include a forward flange (34) extending forward towards the nosecap (25) and an aft flange (32) extending aft towards the aft end (18).</abstract><oa>free_for_read</oa></addata></record> |
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language | eng ; fre ; ger |
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subjects | AEROPLANES AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS GAS-TURBINE PLANTS HEATING HELICOPTERS HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS TRANSPORTING WEAPONS |
title | SPINNER AFT-EXTENDED FORWARD RETURN FLANGE |
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