AIR ACCELERATION AT LEADING EDGE OF WING
Air acceleration at leading edge of aircraft wing. In one embodiment, a slat disposed along a leading edge of a wing of an aircraft. The slat includes a skin structure having an aerodynamic shape, and a hollow space within the skin structure. The slat further includes a nozzle disposed on the skin s...
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Main Authors | , , |
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Format | Patent |
Language | English |
Published |
14.04.2022
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Subjects | |
Online Access | Get full text |
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Summary: | Air acceleration at leading edge of aircraft wing. In one embodiment, a slat disposed along a leading edge of a wing of an aircraft. The slat includes a skin structure having an aerodynamic shape, and a hollow space within the skin structure. The slat further includes a nozzle disposed on the skin structure to accelerate air collected in the hollow space into an external environment outside the slat to increase lift and reduce drag for the wing. |
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Bibliography: | Application Number: US202117378532 |