| 摘要 |
A rotationally symmetrical anti-collision light (100, 200) for an aircraft utilizing light-emitting diodes (LEDs) is mounted to the fuselage of an aircraft. The LEDs (10, 10', 20, 20') may be configured in one or more concentric rings. The anti-collision light includes a reflector (30, 30') configured to redirect the light emitted by at least one of the rings, so that the light pattern satisfies predetermined specifications.
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