CPC B64D 47/06 (2013.01) [F21S 41/141 (2018.01); F21S 41/295 (2018.01); F21V 5/04 (2013.01); B64D 2203/00 (2013.01); F21W 2107/30 (2018.01); F21Y 2115/10 (2016.08)] | 4 Claims |
1. An aircraft light comprising:
at least one or more light-emitting elements as light sources; and
an inner lens configured to project light emitted from the light-emitting elements onto a desired area,
the inner lens includes a lens that splits light of a single light-emitting element in different directions,
the lens is a multi-curved surface lens including a plurality of lens surfaces whose regions partially overlap one another,
the multi-curved surface lens is a freeform lens formed by coupling three curved surfaces each having an output surface with a different curvature,
the multi-curved surface lens is divided into a first region, a second region, and a third region,
the single light-emitting element is placed in the central portion of the multi-curved surface lens in plan view in such a manner as to be at least partially related to all of the first region, the second region, and the third region,
the directions of light emission of the first region, the second region, and the third region are different from one another, wherein
when a beam emitted from the single light-emitting element passes through the multi-curved surface lens, the beam is split into three different directions.
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