AIRCRAFT EMPENNAGE WITH A HORIZONTAL STABILIZER INTERFACING AT THE VERTICAL STABILIZER ROOT
Aircraft empennage comprising:- A vertical tail plane (2).- A rear fuselage section (1) being attached to the vertical tail plane (2) and comprising a skin (1.1) and internal reinforcing members.- A horizontal tail plane (3) comprising two lateral torsion boxes (31, 32) and a framework (33) located...
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| creator | HONORATO RUIZ, Francisco Javier MURUZABAL SOPELANA, Maria |
| description | Aircraft empennage comprising:- A vertical tail plane (2).- A rear fuselage section (1) being attached to the vertical tail plane (2) and comprising a skin (1.1) and internal reinforcing members.- A horizontal tail plane (3) comprising two lateral torsion boxes (31, 32) and a framework (33) located between the two lateral torsion boxes (31, 32) comprising a front spar (34), a rear spar (35) and two ribs (36, 37) extending between the front (34) and the rear spar (35) and each adjacent to a lateral torsion box (31, 32). The framework (33) enclosing a portion of the vertical tail plane (2) along its spanwise direction.The aircraft empennage comprising an attachment assembly attaching the framework (33) to the rear fuselage section (1), the attachment assembly crossing the skin (1.1) and extending between the internal reinforcing members of the rear fuselage section (1) and the framework (33). |
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The framework (33) enclosing a portion of the vertical tail plane (2) along its spanwise direction.The aircraft empennage comprising an attachment assembly attaching the framework (33) to the rear fuselage section (1), the attachment assembly crossing the skin (1.1) and extending between the internal reinforcing members of the rear fuselage section (1) and the framework (33).</description><language>eng ; fre ; ger</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2024</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=20240403&DB=EPODOC&CC=EP&NR=4043336B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25563,76318</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20240403&DB=EPODOC&CC=EP&NR=4043336B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>HONORATO RUIZ, Francisco Javier</creatorcontrib><creatorcontrib>MURUZABAL SOPELANA, Maria</creatorcontrib><title>AIRCRAFT EMPENNAGE WITH A HORIZONTAL STABILIZER INTERFACING AT THE VERTICAL STABILIZER ROOT</title><description>Aircraft empennage comprising:- A vertical tail plane (2).- A rear fuselage section (1) being attached to the vertical tail plane (2) and comprising a skin (1.1) and internal reinforcing members.- A horizontal tail plane (3) comprising two lateral torsion boxes (31, 32) and a framework (33) located between the two lateral torsion boxes (31, 32) comprising a front spar (34), a rear spar (35) and two ribs (36, 37) extending between the front (34) and the rear spar (35) and each adjacent to a lateral torsion box (31, 32). The framework (33) enclosing a portion of the vertical tail plane (2) along its spanwise direction.The aircraft empennage comprising an attachment assembly attaching the framework (33) to the rear fuselage section (1), the attachment assembly crossing the skin (1.1) and extending between the internal reinforcing members of the rear fuselage section (1) and the framework (33).</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>2024</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNyrEKwjAQANAsDqL-w_2AoKS4X8OlOahJOQ-FOpQi5yRaqP-Pi4ub01ve0l2RJQhGBTp2lDM2BBfWBAipCPclK7ZwUqy55Z4EOCtJxMC5AVTQRHAmUQ6_TUrRtVvcx8dsm68rB5E0pK1Nr8HmabzZ094DddWu8t4f6r3_o3wAND0xzQ</recordid><startdate>20240403</startdate><enddate>20240403</enddate><creator>HONORATO RUIZ, Francisco Javier</creator><creator>MURUZABAL SOPELANA, Maria</creator><scope>EVB</scope></search><sort><creationdate>20240403</creationdate><title>AIRCRAFT EMPENNAGE WITH A HORIZONTAL STABILIZER INTERFACING AT THE VERTICAL STABILIZER ROOT</title><author>HONORATO RUIZ, Francisco Javier ; MURUZABAL SOPELANA, Maria</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP4043336B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2024</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>HONORATO RUIZ, Francisco Javier</creatorcontrib><creatorcontrib>MURUZABAL SOPELANA, Maria</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>HONORATO RUIZ, Francisco Javier</au><au>MURUZABAL SOPELANA, Maria</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AIRCRAFT EMPENNAGE WITH A HORIZONTAL STABILIZER INTERFACING AT THE VERTICAL STABILIZER ROOT</title><date>2024-04-03</date><risdate>2024</risdate><abstract>Aircraft empennage comprising:- A vertical tail plane (2).- A rear fuselage section (1) being attached to the vertical tail plane (2) and comprising a skin (1.1) and internal reinforcing members.- A horizontal tail plane (3) comprising two lateral torsion boxes (31, 32) and a framework (33) located between the two lateral torsion boxes (31, 32) comprising a front spar (34), a rear spar (35) and two ribs (36, 37) extending between the front (34) and the rear spar (35) and each adjacent to a lateral torsion box (31, 32). The framework (33) enclosing a portion of the vertical tail plane (2) along its spanwise direction.The aircraft empennage comprising an attachment assembly attaching the framework (33) to the rear fuselage section (1), the attachment assembly crossing the skin (1.1) and extending between the internal reinforcing members of the rear fuselage section (1) and the framework (33).</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| subjects | AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING |
| title | AIRCRAFT EMPENNAGE WITH A HORIZONTAL STABILIZER INTERFACING AT THE VERTICAL STABILIZER ROOT |
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