MULTISPAR LIFTING SURFACE
A multispar lifting surface (30) comprising a multispar torsion box (32) having corner reinforcements (25), a movable control surface, and an axial rod fitting (40). The movable control surface comprises a movable element (1), a hinged connection (6.1) joined to the movable element (1), and an axial...
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creator | BALSA GONZALEZ, Alberto KOBIERECKI, Robert |
description | A multispar lifting surface (30) comprising a multispar torsion box (32) having corner reinforcements (25), a movable control surface, and an axial rod fitting (40). The movable control surface comprises a movable element (1), a hinged connection (6.1) joined to the movable element (1), and an axial rod (7) joining the hinged connection (6.1) to the rear spar (5) of the multispar torsion box (32).The axial rod fitting (40) is configured to join the axial rod (7) and the multispar torsion box (32); and comprises a longitudinal profile (10) resting against the rear spar (5), and a lug (20) joined to the longitudinal profile (10) at one end and to the axial rod (7) at another end; the lug (20) defining a plane comprising the longitudinal axis of the axial rod (7). This multispar lifting surface (30) is able to support sideward forces without any additional structure. |
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The movable control surface comprises a movable element (1), a hinged connection (6.1) joined to the movable element (1), and an axial rod (7) joining the hinged connection (6.1) to the rear spar (5) of the multispar torsion box (32).The axial rod fitting (40) is configured to join the axial rod (7) and the multispar torsion box (32); and comprises a longitudinal profile (10) resting against the rear spar (5), and a lug (20) joined to the longitudinal profile (10) at one end and to the axial rod (7) at another end; the lug (20) defining a plane comprising the longitudinal axis of the axial rod (7). This multispar lifting surface (30) is able to support sideward forces without any additional structure.</description><language>eng ; fre ; ger</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=20231018&DB=EPODOC&CC=EP&NR=4005919B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20231018&DB=EPODOC&CC=EP&NR=4005919B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>BALSA GONZALEZ, Alberto</creatorcontrib><creatorcontrib>KOBIERECKI, Robert</creatorcontrib><title>MULTISPAR LIFTING SURFACE</title><description>A multispar lifting surface (30) comprising a multispar torsion box (32) having corner reinforcements (25), a movable control surface, and an axial rod fitting (40). The movable control surface comprises a movable element (1), a hinged connection (6.1) joined to the movable element (1), and an axial rod (7) joining the hinged connection (6.1) to the rear spar (5) of the multispar torsion box (32).The axial rod fitting (40) is configured to join the axial rod (7) and the multispar torsion box (32); and comprises a longitudinal profile (10) resting against the rear spar (5), and a lug (20) joined to the longitudinal profile (10) at one end and to the axial rod (7) at another end; the lug (20) defining a plane comprising the longitudinal axis of the axial rod (7). This multispar lifting surface (30) is able to support sideward forces without any additional structure.</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>eNrjZJD0DfUJ8QwOcAxS8PF0C_H0c1cIDg1yc3R25WFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8a4BJgYGppaGlk6GxkQoAQDk8h-5</recordid><startdate>20231018</startdate><enddate>20231018</enddate><creator>BALSA GONZALEZ, Alberto</creator><creator>KOBIERECKI, Robert</creator><scope>EVB</scope></search><sort><creationdate>20231018</creationdate><title>MULTISPAR LIFTING SURFACE</title><author>BALSA GONZALEZ, Alberto ; KOBIERECKI, Robert</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP4005919B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</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>BALSA GONZALEZ, Alberto</creatorcontrib><creatorcontrib>KOBIERECKI, Robert</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>BALSA GONZALEZ, Alberto</au><au>KOBIERECKI, Robert</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>MULTISPAR LIFTING SURFACE</title><date>2023-10-18</date><risdate>2023</risdate><abstract>A multispar lifting surface (30) comprising a multispar torsion box (32) having corner reinforcements (25), a movable control surface, and an axial rod fitting (40). The movable control surface comprises a movable element (1), a hinged connection (6.1) joined to the movable element (1), and an axial rod (7) joining the hinged connection (6.1) to the rear spar (5) of the multispar torsion box (32).The axial rod fitting (40) is configured to join the axial rod (7) and the multispar torsion box (32); and comprises a longitudinal profile (10) resting against the rear spar (5), and a lug (20) joined to the longitudinal profile (10) at one end and to the axial rod (7) at another end; the lug (20) defining a plane comprising the longitudinal axis of the axial rod (7). This multispar lifting surface (30) is able to support sideward forces without any additional structure.</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 | MULTISPAR LIFTING SURFACE |
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