Patent ID: 9007236
Filing Date: 2015-04-14
Classification: B64F

Abstract:
1. A light system for landing helicopters under hazardous conditions and, comprising a plurality of light units: a) each said light unit has a mechanical body comprising a means for lighting and two electrical connectors; b) said means for lighting and said two electrical connectors of each said mechanical body, each said light unit are electrically connected in parallel, wherein said two electrical connectors of each said light unit being of the female type; c) said light units joined together by means for connecting said light units; d) said light units are connected in parallel with each other; e) said light system of said light units has an input electric power cable; f) said light units are electrically connected in parallel with said input electric power cable of said light system, and g) whereby said light units of said light system can be manually placed in a circle, and can form a light circle when said light system is electrically connected to a power supply through said input power cable.