HAT-STRINGER ASSEMBLIES FOR AN AIRCRAFT AND METHODS OF FORMING SAME
A hat-stringer assembly (100) for an aircraft (500) comprises a hat stringer (110) with a first hat-stringer leg (140), a second hat-stringer leg (150), a first hat-stringer sidewall (114), a connecting wall (112), a second hat-stringer sidewall (116), and a ventilation opening (128), extending thro...
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creator | Patterson, Steve L Levine, Daniel M Loesche, Christopher R Stulc, Jeffrey F Barnes, Jeffrey E Hanson, Garrett C |
description | A hat-stringer assembly (100) for an aircraft (500) comprises a hat stringer (110) with a first hat-stringer leg (140), a second hat-stringer leg (150), a first hat-stringer sidewall (114), a connecting wall (112), a second hat-stringer sidewall (116), and a ventilation opening (128), extending through the connecting wall (112). The hat stringer assembly (100) also comprises a fitting (200), comprising a first channel member (210) in contact with the first hat-stringer sidewall (114) and the first hat-stringer leg (140). The fitting (200) also comprises a second channel member (240) in contact with the second hat-stringer sidewall (116) and the second hat-stringer leg (150). The fitting (200) further comprises a web cap (260), in contact with the first channel member (210) and the second channel member (240). The web cap (260) comprises a web-cap opening (262), which is in fluidic communication with the ventilation opening (128). |
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The hat stringer assembly (100) also comprises a fitting (200), comprising a first channel member (210) in contact with the first hat-stringer sidewall (114) and the first hat-stringer leg (140). The fitting (200) also comprises a second channel member (240) in contact with the second hat-stringer sidewall (116) and the second hat-stringer leg (150). The fitting (200) further comprises a web cap (260), in contact with the first channel member (210) and the second channel member (240). The web cap (260) comprises a web-cap opening (262), which is in fluidic communication with the ventilation opening (128).</description><language>eng</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING</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=20230202&DB=EPODOC&CC=US&NR=2023031639A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76516</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230202&DB=EPODOC&CC=US&NR=2023031639A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Patterson, Steve L</creatorcontrib><creatorcontrib>Levine, Daniel M</creatorcontrib><creatorcontrib>Loesche, Christopher R</creatorcontrib><creatorcontrib>Stulc, Jeffrey F</creatorcontrib><creatorcontrib>Barnes, Jeffrey E</creatorcontrib><creatorcontrib>Hanson, Garrett C</creatorcontrib><title>HAT-STRINGER ASSEMBLIES FOR AN AIRCRAFT AND METHODS OF FORMING SAME</title><description>A hat-stringer assembly (100) for an aircraft (500) comprises a hat stringer (110) with a first hat-stringer leg (140), a second hat-stringer leg (150), a first hat-stringer sidewall (114), a connecting wall (112), a second hat-stringer sidewall (116), and a ventilation opening (128), extending through the connecting wall (112). The hat stringer assembly (100) also comprises a fitting (200), comprising a first channel member (210) in contact with the first hat-stringer sidewall (114) and the first hat-stringer leg (140). The fitting (200) also comprises a second channel member (240) in contact with the second hat-stringer sidewall (116) and the second hat-stringer leg (150). The fitting (200) further comprises a web cap (260), in contact with the first channel member (210) and the second channel member (240). The web cap (260) comprises a web-cap opening (262), which is in fluidic communication with the ventilation opening (128).</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>HELICOPTERS</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHD2cAzRDQ4J8vRzdw1ScAwOdvV18vF0DVZw8wdy_RQcPYOcgxzdQoBsFwVf1xAPf5dgBX83kLQvUI9CsKOvKw8Da1piTnEqL5TmZlB2cw1x9tBNLciPTy0uSExOzUstiQ8NNjIwMjYwNjQztnQ0NCZOFQC0miwO</recordid><startdate>20230202</startdate><enddate>20230202</enddate><creator>Patterson, Steve L</creator><creator>Levine, Daniel M</creator><creator>Loesche, Christopher R</creator><creator>Stulc, Jeffrey F</creator><creator>Barnes, Jeffrey E</creator><creator>Hanson, Garrett C</creator><scope>EVB</scope></search><sort><creationdate>20230202</creationdate><title>HAT-STRINGER ASSEMBLIES FOR AN AIRCRAFT AND METHODS OF FORMING SAME</title><author>Patterson, Steve L ; Levine, Daniel M ; Loesche, Christopher R ; Stulc, Jeffrey F ; Barnes, Jeffrey E ; Hanson, Garrett C</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2023031639A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2023</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>HELICOPTERS</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>Patterson, Steve L</creatorcontrib><creatorcontrib>Levine, Daniel M</creatorcontrib><creatorcontrib>Loesche, Christopher R</creatorcontrib><creatorcontrib>Stulc, Jeffrey F</creatorcontrib><creatorcontrib>Barnes, Jeffrey E</creatorcontrib><creatorcontrib>Hanson, Garrett C</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Patterson, Steve L</au><au>Levine, Daniel M</au><au>Loesche, Christopher R</au><au>Stulc, Jeffrey F</au><au>Barnes, Jeffrey E</au><au>Hanson, Garrett C</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>HAT-STRINGER ASSEMBLIES FOR AN AIRCRAFT AND METHODS OF FORMING SAME</title><date>2023-02-02</date><risdate>2023</risdate><abstract>A hat-stringer assembly (100) for an aircraft (500) comprises a hat stringer (110) with a first hat-stringer leg (140), a second hat-stringer leg (150), a first hat-stringer sidewall (114), a connecting wall (112), a second hat-stringer sidewall (116), and a ventilation opening (128), extending through the connecting wall (112). The hat stringer assembly (100) also comprises a fitting (200), comprising a first channel member (210) in contact with the first hat-stringer sidewall (114) and the first hat-stringer leg (140). The fitting (200) also comprises a second channel member (240) in contact with the second hat-stringer sidewall (116) and the second hat-stringer leg (150). The fitting (200) further comprises a web cap (260), in contact with the first channel member (210) and the second channel member (240). The web cap (260) comprises a web-cap opening (262), which is in fluidic communication with the ventilation opening (128).</abstract><oa>free_for_read</oa></addata></record> |
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subjects | AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING |
title | HAT-STRINGER ASSEMBLIES FOR AN AIRCRAFT AND METHODS OF FORMING SAME |
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