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公开(公告)号:US20170320561A1
公开(公告)日:2017-11-09
申请号:US15588332
申请日:2017-05-05
Applicant: AIRBUS OPERATIONS SL
Inventor: Carlos GARCIA NIETO , Fernando PEREIRA MOSQUEIRA , Iker VELEZ DE MENDIZABAL ALONSO , Enrique GUINALDO FERNANDEZ , Francisco Javier HONORATO RUIZ
Abstract: An aircraft aerodynamic surface (1) including a torsion box (2) having a front spar (21) and rear spar (22), a first control surface (3) including a front spar (31) and a trailing edge (32) and a second control surface (4) having a front spar (41), a trailing edge (42), and a pivot device (5, 6, 7, 8) for pivotally attaching the first control surface (3) and the second control surface (4) to the rear spar (22) of the torsion box (2), the first control surface is an inboard control surface (4) including two lateral ribs (9, 9′), six inner ribs (11, 12, 13, 14, 15, 10) and an inner spar (16), and the second control surface (3) is an outboard control surface which includes two lateral ribs (20, 20′), three internal ribs (17, 18, 19), two internal spars (24, 24′) and one internal spar (23).
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公开(公告)号:US20210276258A1
公开(公告)日:2021-09-09
申请号:US17196280
申请日:2021-03-09
Applicant: AIRBUS OPERATIONS SL
Inventor: Alvaro JARA RODELGO , Alfonso PARRA RUBIO , Guillermo HERNAIZ LOPEZ , Pablo VAZQUEZ SANCHEZ , Enrique GUINALDO FERNANDEZ
IPC: B29C64/30 , B29C64/118 , B33Y10/00 , B33Y30/00 , B33Y40/20
Abstract: A method for manufacturing a part layer-upon-layer using Additive Manufacturing technology, the method including: printing the part together with an elastomeric enclosure shaped thereto leaving a gap free of material therebetween, the elastomeric enclosure including at least one opening; heating the ensemble of the printed part and elastomeric enclosure or keeping an operating printing temperature; applying vacuum by the at least one opening of the elastomeric enclosure so that the elastomeric enclosure deflates thus exerting pressure to the printed part; and maintaining the printed part under vacuum and heat during a predefined time.
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