SLAT FOR AN AIRCRAFT WING, METHOD FOR MANUFACTURING SUCH A SLAT
摘要:
A slat for an aircraft wing and a method for assembling said slat, the slat comprising:
- a skin wherein an outer surface of the skin forms an aerodynamic surface of the slat body and wherein the skin comprises an upper skin part and a lower skin part extending continuously from a leading edge of the skin such that the upper skin part extends further than the lower skin part seen in a direction along a center line of the slat;
- a plurality of stiffeners are assembled to an inner surface of the skin;
- a spar extending between the upper skin part and the lower skin part that is connected to the upper skin part and the lower skin part;
- wherein the spar is provided with lugs for connection to an actuation system.
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