Aircraft wing flaps having aerodynamic restoration doors
Aircraft wing flaps having aerodynamic restoration doors are described. An example apparatus includes a door to be rotatably coupled to a closure rib of a flap of an aircraft wing. The door is to be moveable between a deployed position and a retracted position. The flap has a leading edge and a cutout formed in the leading edge. The door is to fill a portion of the cutout when the door is in the deployed position.
1. An apparatus, comprising:
a door rotatably coupled to a closure rib of a flap of an aircraft wing, the door moveable between a deployed position and a retracted position, the flap having a leading edge and a cutout formed in the leading edge, the door filling a first portion of the cutout when the door is in the deployed position; and
a track coupled to the closure rib, the track including a trim tab, the trim tab filling a second portion of the cutout, the track receiving a deflection control rib of the aircraft wing when the flap is in a stowed position.
2. The apparatus of claim 1 , wherein the door includes an outer surface having a contoured profile, the contoured profile of the outer surface of the door aligned with a contoured profile of the leading edge of the flap when the door is in the deployed position.
3. The apparatus of claim 2 , further comprising a bulb seal coupled to the door.
4. The apparatus of claim 1 , wherein the door is guided from the deployed position to the retracted position in response to the door being contacted by a depressor, the depressor coupled to and extending downward from the deflection control rib.
5. The apparatus of claim 1 , wherein the door includes a door frame and a door skin coupled to the door frame, the door skin filling the first portion of the cutout when the door is in the deployed position.
6. The apparatus of claim 5 , further comprising a rub pad coupled to the door frame, the rub pad contacting a rub sheet coupled to the closure rib.
7. The apparatus of claim 5 , further comprising a spindle fitting coupled to the closure rib, the spindle fitting having a spindle, the door frame rotatably coupled to the spindle.
8. The apparatus of claim 7 , further comprising a nut plate coupling the spindle fitting to the closure rib, the spindle fitting positioned adjacent a first surface of the closure rib, the nut plate positioned adjacent a second surface of the closure rib located opposite the first surface of the closure rib.
9. The apparatus of claim 7 , wherein the door frame includes a stop, the stop preventing the door frame from moving past the spindle fitting as the door is moved from the deployed position toward the retracted position.
10. The apparatus of claim 7 , further comprising a spring tensioner coupled to the spindle fitting.
11. The apparatus of claim 10 , further comprising a torsion spring including a coiled portion, a first arm extending from the coiled portion, and a second arm extending from the coiled portion, the coiled portion coupled to the spindle, the first arm coupled to the door frame, the second arm contacting the spring tensioner, the torsion spring biasing the door away from the retracted position and toward the deployed position.
12. The apparatus of claim 1 , wherein the trim tab includes a mechanical stop, the mechanical stop preventing the door from moving past the deployed position as the door moves away from the retracted position.
13. The apparatus of claim 1 , wherein the deflection control rib extends through the first portion of the cutout and into the track when the door is in the retracted position and the flap is in the stowed position.
14. A flap of an aircraft wing, the flap comprising:
a leading edge having a cutout;
a closure rib;
a door rotatably coupled to the closure rib and moveable between a deployed position and a retracted position, the door filling a first portion of the cutout when the door is in the deployed position; and
a track coupled to the closure rib, the track including a trim tab, the trim tab filling a second portion of the cutout, the track receiving a deflection control rib of the aircraft wing when the flap is in a stowed position.
15. The flap of claim 14 , wherein the door includes an outer surface having a contoured profile, the contoured profile of the outer surface of the door aligned with a contoured profile of the leading edge of the flap when the door is in the deployed position.
16. The flap of claim 15 , further comprising a bulb seal coupled to the door.
17. The flap of claim 14 , wherein the door is guided from the deployed position to the retracted position in response to the door being contacted by a depressor, the depressor coupled to and extending downward from the deflection control rib.
18. A method, comprising:
moving a door rotatably coupled to a closure rib of a flap of an aircraft wing from a retracted position to a deployed position, the door filling a first portion of a cutout formed in a leading edge of the flap when the door is in the deployed position, the cutout including a second portion filled by a trim tab of a track, the track coupled to the closure rib, the track receiving a deflection control rib of the aircraft wing when the flap is in a stowed position.
19. The method of claim 18 , wherein the door includes an outer surface having a contoured profile, the contoured profile of the outer surface of the door being aligned with a contoured profile of the leading edge of the flap when the door is in the deployed position.
20. The method of claim 18 , further comprising guiding the door from the deployed position to the retracted position by contacting the door with a depressor, the depressor coupled to and extending downward from the deflection control rib.