Tail spar spring
According to one embodiment, an empennage attachment system features an aft attachment mechanism and a forward attachment system. The aft attachment mechanism is configured to be coupled to a tail section of a body of an aircraft and to an empennage proximate to an aft spar of the empennage. The aft...
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| creator | VanBuskirk, Matthew Carl Isaac, Mark Loring Burnett, Michael Christopher Seifert, Michael Scott |
| description | According to one embodiment, an empennage attachment system features an aft attachment mechanism and a forward attachment system. The aft attachment mechanism is configured to be coupled to a tail section of a body of an aircraft and to an empennage proximate to an aft spar of the empennage. The aft attachment mechanism defines a pitch axis such that the aft attachment mechanism allows the empennage to rotate about the pitch axis. The forward attachment system is configured to be coupled to the tail section of the body and to the empennage proximate to a forward spar of the empennage. The forward attachment system is configured to restrict rotation of the empennage about the pitch axis to an allowable range of motion. |
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| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_US10023294B2</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>US10023294B2</sourcerecordid><originalsourceid>FETCH-epo_espacenet_US10023294B23</originalsourceid><addsrcrecordid>eNrjZBAISczMUSguSCwCEkWZeek8DKxpiTnFqbxQmptB0c01xNlDN7UgPz4VqDA5NS-1JD402NDAwMjYyNLEyciYGDUAmlsfKA</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Tail spar spring</title><source>esp@cenet</source><creator>VanBuskirk, Matthew Carl ; Isaac, Mark Loring ; Burnett, Michael Christopher ; Seifert, Michael Scott</creator><creatorcontrib>VanBuskirk, Matthew Carl ; Isaac, Mark Loring ; Burnett, Michael Christopher ; Seifert, Michael Scott</creatorcontrib><description>According to one embodiment, an empennage attachment system features an aft attachment mechanism and a forward attachment system. The aft attachment mechanism is configured to be coupled to a tail section of a body of an aircraft and to an empennage proximate to an aft spar of the empennage. The aft attachment mechanism defines a pitch axis such that the aft attachment mechanism allows the empennage to rotate about the pitch axis. The forward attachment system is configured to be coupled to the tail section of the body and to the empennage proximate to a forward spar of the empennage. The forward attachment system is configured to restrict rotation of the empennage about the pitch axis to an allowable range of motion.</description><language>eng</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING</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=20180717&DB=EPODOC&CC=US&NR=10023294B2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20180717&DB=EPODOC&CC=US&NR=10023294B2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>VanBuskirk, Matthew Carl</creatorcontrib><creatorcontrib>Isaac, Mark Loring</creatorcontrib><creatorcontrib>Burnett, Michael Christopher</creatorcontrib><creatorcontrib>Seifert, Michael Scott</creatorcontrib><title>Tail spar spring</title><description>According to one embodiment, an empennage attachment system features an aft attachment mechanism and a forward attachment system. The aft attachment mechanism is configured to be coupled to a tail section of a body of an aircraft and to an empennage proximate to an aft spar of the empennage. The aft attachment mechanism defines a pitch axis such that the aft attachment mechanism allows the empennage to rotate about the pitch axis. The forward attachment system is configured to be coupled to the tail section of the body and to the empennage proximate to a forward spar of the empennage. The forward attachment system is configured to restrict rotation of the empennage about the pitch axis to an allowable range of motion.</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>2018</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZBAISczMUSguSCwCEkWZeek8DKxpiTnFqbxQmptB0c01xNlDN7UgPz4VqDA5NS-1JD402NDAwMjYyNLEyciYGDUAmlsfKA</recordid><startdate>20180717</startdate><enddate>20180717</enddate><creator>VanBuskirk, Matthew Carl</creator><creator>Isaac, Mark Loring</creator><creator>Burnett, Michael Christopher</creator><creator>Seifert, Michael Scott</creator><scope>EVB</scope></search><sort><creationdate>20180717</creationdate><title>Tail spar spring</title><author>VanBuskirk, Matthew Carl ; Isaac, Mark Loring ; Burnett, Michael Christopher ; Seifert, Michael Scott</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US10023294B23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2018</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>VanBuskirk, Matthew Carl</creatorcontrib><creatorcontrib>Isaac, Mark Loring</creatorcontrib><creatorcontrib>Burnett, Michael Christopher</creatorcontrib><creatorcontrib>Seifert, Michael Scott</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>VanBuskirk, Matthew Carl</au><au>Isaac, Mark Loring</au><au>Burnett, Michael Christopher</au><au>Seifert, Michael Scott</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Tail spar spring</title><date>2018-07-17</date><risdate>2018</risdate><abstract>According to one embodiment, an empennage attachment system features an aft attachment mechanism and a forward attachment system. The aft attachment mechanism is configured to be coupled to a tail section of a body of an aircraft and to an empennage proximate to an aft spar of the empennage. The aft attachment mechanism defines a pitch axis such that the aft attachment mechanism allows the empennage to rotate about the pitch axis. The forward attachment system is configured to be coupled to the tail section of the body and to the empennage proximate to a forward spar of the empennage. The forward attachment system is configured to restrict rotation of the empennage about the pitch axis to an allowable range of motion.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng |
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| subjects | AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING |
| title | Tail spar spring |
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