TRAILING EDGE FOR A COMPOSITE MULTISPAR INTEGRATED LIFTING SURFACE AND METHOD FOR MANUFACTURING SAID TRAILING EDGE
Trailing edge (2) for a composite multispar integrated lifting surface (1) comprising:- A first C-shape composite form (10) that comprises a web (11) and two flanges (12). The web (11) forming a portion of the rear spar (20) of a torsion box (3). The two flanges (12) extending along the skin (21) ch...
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| creator | LOZANO GARCIA, Jose Luis BALSA-GONZALEZ, Alberto KOBIERECKI, Robert |
| description | Trailing edge (2) for a composite multispar integrated lifting surface (1) comprising:- A first C-shape composite form (10) that comprises a web (11) and two flanges (12). The web (11) forming a portion of the rear spar (20) of a torsion box (3). The two flanges (12) extending along the skin (21) chordwise direction.- A second C-shape composite form (15) comprising a web (16) and two flanges (17). The web (16) forming an auxiliary spar (22). The flanges (17) extending along the skin (21) chordwise direction.The first C-shape composite form (10) and the second C-shape composite form (15) forming a first auxiliary cell (30) and a second cell (31). The first auxiliary cell (30) being delimited by the first C-shape composite form (10) and the second C-shape composite form (15). The second cell (31) being an open cell delimited by the second C-shape composite form (15). |
| format | Patent |
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The web (11) forming a portion of the rear spar (20) of a torsion box (3). The two flanges (12) extending along the skin (21) chordwise direction.- A second C-shape composite form (15) comprising a web (16) and two flanges (17). The web (16) forming an auxiliary spar (22). The flanges (17) extending along the skin (21) chordwise direction.The first C-shape composite form (10) and the second C-shape composite form (15) forming a first auxiliary cell (30) and a second cell (31). The first auxiliary cell (30) being delimited by the first C-shape composite form (10) and the second C-shape composite form (15). The second cell (31) being an open cell delimited by the second C-shape composite form (15).</description><language>eng ; fre ; ger</language><subject>AEROPLANES ; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCESIN A PLASTIC STATE ; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR ; SHAPING OR JOINING OF PLASTICS ; TRANSPORTING ; WORKING OF PLASTICS ; WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</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=20230510&DB=EPODOC&CC=EP&NR=3835038B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25562,76317</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230510&DB=EPODOC&CC=EP&NR=3835038B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LOZANO GARCIA, Jose Luis</creatorcontrib><creatorcontrib>BALSA-GONZALEZ, Alberto</creatorcontrib><creatorcontrib>KOBIERECKI, Robert</creatorcontrib><title>TRAILING EDGE FOR A COMPOSITE MULTISPAR INTEGRATED LIFTING SURFACE AND METHOD FOR MANUFACTURING SAID TRAILING EDGE</title><description>Trailing edge (2) for a composite multispar integrated lifting surface (1) comprising:- A first C-shape composite form (10) that comprises a web (11) and two flanges (12). The web (11) forming a portion of the rear spar (20) of a torsion box (3). The two flanges (12) extending along the skin (21) chordwise direction.- A second C-shape composite form (15) comprising a web (16) and two flanges (17). The web (16) forming an auxiliary spar (22). The flanges (17) extending along the skin (21) chordwise direction.The first C-shape composite form (10) and the second C-shape composite form (15) forming a first auxiliary cell (30) and a second cell (31). The first auxiliary cell (30) being delimited by the first C-shape composite form (10) and the second C-shape composite form (15). 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The web (11) forming a portion of the rear spar (20) of a torsion box (3). The two flanges (12) extending along the skin (21) chordwise direction.- A second C-shape composite form (15) comprising a web (16) and two flanges (17). The web (16) forming an auxiliary spar (22). The flanges (17) extending along the skin (21) chordwise direction.The first C-shape composite form (10) and the second C-shape composite form (15) forming a first auxiliary cell (30) and a second cell (31). The first auxiliary cell (30) being delimited by the first C-shape composite form (10) and the second C-shape composite form (15). The second cell (31) being an open cell delimited by the second C-shape composite form (15).</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| subjects | AEROPLANES AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCESIN A PLASTIC STATE SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR SHAPING OR JOINING OF PLASTICS TRANSPORTING WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL |
| title | TRAILING EDGE FOR A COMPOSITE MULTISPAR INTEGRATED LIFTING SURFACE AND METHOD FOR MANUFACTURING SAID TRAILING EDGE |
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