AIRCRAFT EMPENNAGE
    1.
    发明申请
    AIRCRAFT EMPENNAGE 审中-公开

    公开(公告)号:US20170320561A1

    公开(公告)日:2017-11-09

    申请号:US15588332

    申请日:2017-05-05

    CPC classification number: B64C9/00 B64C5/02 B64C9/02 Y02T50/44

    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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