Articulated cover assembly for wing leading edge slat telescopic tube duct
An aircraft wing is provided having a wing leading edge, a cut-out opening in the wing leading edge, a telescopic tube extending through the cut-out opening and connected to an internal duct of a wing leading edge slat to establish fluid communication with heated air associated with an aircraft anti-icing system, wherein the telescopic tube is moveable between retracted and extended conditions in response to the wing leading edge slat being moved between slat retraction and deployment positions, respectively, and a cover assembly comprising a cover member operatively connected to the telescopic tube to close the cut-out opening and allow synchronous movement of the cover member with the telescopic tube in response to the telescopic tube being moved between the retracted and extended conditions thereof.
1. An aircraft wing comprising:
a wing leading edge;
a cut-out opening in the wing leading edge;
a telescopic tube extendable through the cut-out opening and connected to an internal duct of the wing leading edge to establish fluid communication with heated air associated with an aircraft anti-icing system, wherein the telescopic tube is moveable between retracted and extended conditions in response to a wing leading edge slat being moved between slat retraction and deployment positions, respectively;
a cover assembly comprising a cover member operatively connected to the telescopic tube to close the cut-out opening and allow synchronous movement of the cover member with the telescopic tube in response to the telescopic tube being moved between the retracted and extended conditions thereof; and
an articulated connection between the cover member and the telescopic tube.
2. The aircraft wing according to claim 1 , wherein the cover assembly further comprises a connection yoke which establishes the articulated connection between the cover member and the telescopic tube.
3. The aircraft wing according to claim 2 , wherein connection yoke is a generally inverted U-shaped structure having a pair of downwardly and outwardly extending side arms and a central support plate.
4. The aircraft wing according to claim 3 , wherein each of the side arms are fixed to a respective side portion of the telescopic tube, and the central support plate is connected to the cover member to allow rotational articulation about a generally vertical axis.
5. The aircraft wing according to claim 4 , wherein
the cover member comprises a connection bracket which includes a substantially horizontal oriented central connection boss, and wherein
the connection yoke comprises a central bushing and pin assembly to operatively interconnect the central support plate to the central connection boss and thereby allow rotational articulation of the cover member about the generally vertical axis defined by the bushing and pin assembly.
6. The aircraft wing according to claim 5 , wherein
the connection bracket further includes a spaced apart pair of substantially vertically oriented lateral connection bosses, and wherein
the connection yoke comprises a pair of lateral bushing and pin assemblies.
7. The aircraft wing according to claim 1 , wherein the cover member is convexly curved and includes a pair of spaced apart pair of opposed side support plates.
8. The aircraft wing according to claim 7 , wherein the cover assembly comprises at least one fixed position roller, and wherein the side support plates define at least one elongate channel to receive the at least one fixed position roller to allow the cover member to be moved forwardly upon movement of the telescopic tube from the retracted condition to the extended condition thereof.
9. The aircraft wing according to claim 8 , wherein the cover assembly comprises a pair of fixed position rollers, and wherein each of the side support plates comprises a channel to receive therein a respective one of the rollers.
10. The aircraft wing according to claim 8 , wherein the cover assembly further comprises a connection yoke which establishes articulated connection between the cover member and the telescopic tube.
11. The aircraft wing according to claim 10 , wherein the connection yoke comprises a central support plate and a pair of side arms extending downwardly and outwardly from the central support plate, wherein each of the side arms are fixed to a respective side portion of the telescopic tube, and the central support plate is connected to the cover member to allow rotational articulation about a generally vertical axis.
12. The aircraft wing according to claim 11 , wherein
the cover member comprises a connection bracket which includes a substantially horizontal oriented central connection boss, and wherein
the connection yoke comprises a central bushing and pin assembly to operatively interconnect the central support plate to the central connection boss and thereby allow rotational articulation of the cover member about the generally vertical axis defined by the bushing and pin assembly.
13. The aircraft wing according to claim 12 , wherein
the connection bracket further includes a spaced apart pair of substantially vertically oriented lateral connection bosses, and wherein
the connection yoke comprises a pair of lateral bushing and pin assemblies.
14. The aircraft wing according to claim 10 , wherein connection yoke is a generally inverted U-shaped structure having a pair of downwardly and outwardly extending side arms each fixed to a respective side of the telescopic tube, and a central support plate connected to the cover member to allow articulated movement of the cover member relative to the telescopic tube.
15. An aircraft which comprises the aircraft wing according to claim 1 .