WING-FUSELAGE INTEGRATED AIRFRAME BEAMS FOR TILTROTOR AIRCRAFT

WING-FUSELAGE INTEGRATED AIRFRAME BEAMS FOR TILTROTOR AIRCRAFT

An airframe for a tiltrotor aircraft (10) includes a wing airframe (24; 106) including a rib (20a, 20b; 124a, 124b), a fuselage airframe (26; 102) including a fore-aft overhead beam (28a, 28b; 126a, 126b) and a cradle support assembly (56a, 56b; 110a, 110b). The cradle support assembly (56a, 56b; 11...

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Hauptverfasser: KOOIMAN, James Everett, ZIMMERMAN, Brett Rodney, BAINES, Andrew G, BRUNKEN, Jr, John Elton, MCCULLOUGH, John Richard
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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creator KOOIMAN, James Everett
ZIMMERMAN, Brett Rodney
BAINES, Andrew G
BRUNKEN, Jr, John Elton
MCCULLOUGH, John Richard
description An airframe for a tiltrotor aircraft (10) includes a wing airframe (24; 106) including a rib (20a, 20b; 124a, 124b), a fuselage airframe (26; 102) including a fore-aft overhead beam (28a, 28b; 126a, 126b) and a cradle support assembly (56a, 56b; 110a, 110b). The cradle support assembly (56a, 56b; 110a, 110b) includes a forward wing support (146a, 146b) coupled to the fore-aft overhead beam (28a, 28b; 126a, 126b) and the wing airframe (24, 106) and an aft wing support (148a, 148b) coupled to the fore-aft overhead beam (28a, 28b; 126a, 126b) and the wing airframe (24, 106). The rib (20a, 20b; 124a, 124b), the fore-aft overhead beam (28a, 28b; 126a, 126b), the forward wing support (146a, 146b) and the aft wing support (148a, 148b) are substantially aligned to form a wing-fuselage integrated airframe beam assembly (32a, 32b; 108a, 108b) to support the wing airframe (24, 106).
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The cradle support assembly (56a, 56b; 110a, 110b) includes a forward wing support (146a, 146b) coupled to the fore-aft overhead beam (28a, 28b; 126a, 126b) and the wing airframe (24, 106) and an aft wing support (148a, 148b) coupled to the fore-aft overhead beam (28a, 28b; 126a, 126b) and the wing airframe (24, 106). The rib (20a, 20b; 124a, 124b), the fore-aft overhead beam (28a, 28b; 126a, 126b), the forward wing support (146a, 146b) and the aft wing support (148a, 148b) are substantially aligned to form a wing-fuselage integrated airframe beam assembly (32a, 32b; 108a, 108b) to support the wing airframe (24, 106).</description><language>eng ; fre ; ger</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2020</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&amp;date=20200318&amp;DB=EPODOC&amp;CC=EP&amp;NR=3461737B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20200318&amp;DB=EPODOC&amp;CC=EP&amp;NR=3461737B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KOOIMAN, James Everett</creatorcontrib><creatorcontrib>ZIMMERMAN, Brett Rodney</creatorcontrib><creatorcontrib>BAINES, Andrew G</creatorcontrib><creatorcontrib>BRUNKEN, Jr, John Elton</creatorcontrib><creatorcontrib>MCCULLOUGH, John Richard</creatorcontrib><title>WING-FUSELAGE INTEGRATED AIRFRAME BEAMS FOR TILTROTOR AIRCRAFT</title><description>An airframe for a tiltrotor aircraft (10) includes a wing airframe (24; 106) including a rib (20a, 20b; 124a, 124b), a fuselage airframe (26; 102) including a fore-aft overhead beam (28a, 28b; 126a, 126b) and a cradle support assembly (56a, 56b; 110a, 110b). 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subjects AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
title WING-FUSELAGE INTEGRATED AIRFRAME BEAMS FOR TILTROTOR AIRCRAFT
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