Articulated flap support forward fairing

1. An articulating flap support housing comprising:

a flap connected to a wing, the flap having a range of deployed positions;

an aft fairing connected to the flap and configured to rotate with the flap through the range of deployed positions;

a forward fairing rotatably connected to the aft fairing, the forward fairing acting as a counterbalance to the aft fairing and flap; and

an articulation mechanism interconnecting the aft fairing and the forward fairing, the articulation mechanism configured to maintain a position of the forward fairing relative to the wing through the range of deployed positions,

wherein the articulation mechanism comprises:

a forward fairing attachment foot engaged to a bottom aft end of the forward fairing; and

an aft fairing attachment foot engaged to a bottom forward end of the aft fairing, the aft fairing attachment foot pivotally connected to the forward fairing attachment foot whereby the forward fairing rotates relative to the aft fairing.

2. The articulating flap support housing as defined in claim 1 further comprising: a flap support mounted to the wing; and a flap deployment system connecting the flap support and the flap, the flap deployment system configured to extend and rotate the flap through the range of deployed positions.

3. The articulating flap support housing as defined in claim 2 wherein the flap deployment system comprises:

a drive link having a first end rotatably connected at a forward fitting proximate a forward end of the flap and a second end rotatably connected to the flap support, the drive link rotatable for extending the flap over the range of deployed positions; and,

a trailing link having a leading end rotatably connected to the flap support and a trailing end rotatably connected to an aft fitting on the flap, the trailing link configured to urge the flap to rotate downward responsive to rotation of the drive link.

4. The articulating flap support housing as defined in claim 1 further comprising a balance axle rotatably connecting the aft faring attachment foot and the forward faring attachment foot.

5. The articulating flap support housing as defined in claim 1 wherein the articulation mechanism further comprises: at least one bellcrank having a central pivot connected to the drive link; at least one fairing link connected proximate an upper aft end portion of the forward fairing and rotatably connected to a first arm of the at least one bellcrank; and, at least one flap support link rotatably connected between the flap support and a second arm of the at least one bellcrank.

6. The articulating flap support housing as defined in claim 5 wherein

the at least one bellcrank comprises an outboard bellcrank having a first central pivot on an outboard side of the drive link and an inboard bellcrank having a second central pivot on an inboard side of the drive link;

the at least one fairing link comprises an outboard fairing link connected to an upper aft end of an outboard side of the forward fairing and rotatably connected to a first arm of the outboard bellcrank and an inboard fairing link connected to an upper aft end of an inboard side of the forward fairing and rotatably connected to a first arm of the inboard bellcrank; and,

the at least one flap support link comprises an outboard flap support link connected to an outboard side of the flap support and a second arm of the outboard bellcrank and an inboard flap support link connected to an inboard side of the flap support and a second arm of the inboard bellcrank.

7. The articulating flap support housing as defined in claim 6 wherein the outboard fairing link is rotatably connected to a first pad secured to the upper aft end of the outboard side of the forward fairing and the inboard fairing link is rotatably connected to a second pad secured to the upper aft end of the inboard side of the forward fairing with a second rotatable pad.

8. The articulating flap support housing as defined in claim 6 wherein the first central pivot of the outboard bellcrank and second central pivot of the inboard bellcrank are provided by a first pivot pin extending through the drive link.

9. The articulating flap support housing as defined in claim 6 wherein rotatable connection of the outboard flap support link and inboard flap support link to the flap support is provided by a second pivot pin extending through the flap support.

10. An aircraft wing assembly comprising:

a wing;

a flap support mounted to the wing;

a drive link having a first end rotatably connected at a first pivot proximate a forward end of a flap and a second end rotatably connected to the flap support, the drive link rotatable for extending the flap over a range of deployed positions;

an aft fairing connected to the flap and configured to rotate with the flap through the range of deployed positions;

a forward fairing rotatably connected to the aft fairing to the aft fairing and acting as a counterbalance to the aft fairing and the flap; and

an articulation mechanism having

a forward fairing attachment foot engaged to a bottom aft end of the forward fairing and an aft fairing attachment foot engaged to a bottom forward end of the aft fairing, the aft fairing attachment foot pivotally connected to the forward fairing attachment foot whereby the forward fairing rotates relative to the aft fairing;

an outboard bellcrank having a central pivot connected to an outboard side of the drive link; an outboard fairing link connected to an upper aft end of an outboard side of the forward fairing and rotatably connected to a first arm of the outboard bellcrank;

an outboard flap support link connected to an outboard side of the flap support and a second arm of the outboard bellcrank;

an inboard bellcrank having a central pivot connected to a inboard side of the drive link;

an inboard fairing link connected to an upper aft end of an inboard side of the forward fairing and rotatably connected to a first arm of the inboard bellcrank; and

an inboard flap support link connected to an inboard side of the flap support and a second arm of the inboard bellcrank.

11. The aircraft wing assembly as defined in claim 10 wherein the articulation mechanism is configured to maintain relative orientation between the forward fairing and a lower wing skin.

12. A method for counterbalancing a deployable flap and aft fairing, the method comprising:

connecting a flap to a wing, the flap having a range of deployed positions;

connecting an aft fairing to the flap;

rotating the aft fairing with the flap through the range of deployed positions;

rotatably connecting a forward fairing solely through an articulation mechanism to the aft fairing, the forward fairing acting as a counterbalance to the aft fairing and the flap;

interconnecting the aft fairing and the forward fairing with an articulation mechanism; and

maintaining a position of the forward fairing relative to the wing through the range of deployed positions with the articulation mechanism,

wherein the step of interconnecting the aft fairing and the forward fairing further comprises:

engaging a forward fairing attachment foot to a bottom aft end of the forward fairing;

engaging an aft fairing attachment foot to a bottom forward end of the aft fairing; and

pivotally connecting the aft fairing attachment foot to the forward fairing attachment foot whereby the forward fairing rotates relative to the aft fairing.

13. The method as defined in claim 12 wherein the step of interconnecting the aft fairing and the forward fairing further comprises:

connecting at least one bellcrank, rotatable at a central pivot, to a drive link, the drive link having a first end rotatably connected at a first pivot proximate a forward end of the flap and a second end rotatably connected to a flap support;

rotating the drive link for extending the flap over the range of deployed positions;

rotatably connecting at least one fairing link proximate an upper aft end portion of the forward fairing and rotatably connecting the at least one faring link to a first arm of the at least one bellcrank; and

rotatably connecting at least one flap support link between the flap support and a second arm of the at least one bellcrank.

14. The method as defined in claim 13 wherein the step of connecting at least one bellcrank comprises rotatably connecting an outboard bellcrank to an outboard side of the drive link and rotatably connecting an inboard bellcrank to an inboard side of the drive link, and the step of rotatably connecting at least one fairing link comprises rotatably connecting an outboard flap support link to an outboard upper aft portion of the forward fairing and rotatably connecting an outboard faring link to a first arm of the outboard bellcrank, and rotatably connecting an inboard flap support link to an inboard upper aft portion of the forward fairing and rotatably connecting an inboard faring link to a first arm of the inboard bellcrank, and the step of rotatably connecting at least one flap support link comprises rotatably connecting an outboard flap support link between the flap support and a second arm of the outboard bellcrank and rotatably connecting an inboard flap support link between the flap support and a second arm of the inboard bellcrank.