# US 10,501,203 B2 · Combined aircraft wing scan and runway turn-off light unit and aircraft comprising the same > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 10,501,203 B2 - Document ID: US10501203B2 - Status: Granted - Kind: B2 - Application number: 15/983,142 - Filed: 2018-05-18 - Published: 2018-11-22 - Granted: 2019-12-10 - Earliest claimed: 2017-05-19 - Assignees: Goodrich Lighting Systems GmbH - Applicants: Goodrich Lighting Systems GmbH - Inventors: Andre Hessling-Von Heimendahl; Anil Kumar Jha - Web page: https://patentgrep.com/patent/US10501203B2 ## CPC - B64D 47/04: the lighting devices being primarily intended to illuminate the way ahead - B64D 47/06: for indicating aircraft presence - F21S 41/141: Light emitting diodes [LED] - F21S 41/25: Projection lenses - F21S 43/14: Light emitting diodes [LED] - F21S 43/26: {Refractors, transparent cover plates, light guides or filters not provided in groups F21S43/235 - F21S43/255} - B64D: EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT - F21S: NON-PORTABLE LIGHTING DEVICES; SYSTEMS THEREOF; VEHICLE LIGHTING DEVICES SPECIALLY ADAPTED FOR VEHICLE EXTERIORS ## Abstract A combined aircraft wing scan and runway turn-off light unit includes a housing for mounting the combined aircraft wing scan and runway turn-off light unit to a side portion of a fuselage of an aircraft; at least one light source; and an optical system for shaping a light emission distribution of the combined aircraft wing scan and runway turn-off light unit; wherein the light emission distribution comprises a first illumination region for illuminating a wing region of the aircraft and a second illumination region for illuminating a lateral forward airfield region. ## Claims ### Claim 1 Combined aircraft wing scan and runway turn-off light unit, comprising: a housing for mounting the combined aircraft wing scan and runway turn-off light unit to a side portion of a fuselage of an aircraft, at least one light source, and an optical system for shaping a light emission distribution of the combined aircraft wing scan and runway turn-off light unit, wherein the light emission distribution comprises a first illumination region for illuminating a wing region of the aircraft and a second illumination region for illuminating a lateral forward airfield region, wherein the at least one light source comprises a plurality of light sources having at least one first light source and at least one second light source, wherein the optical system comprises at least one first optical system for directing the light from the at least one first light source to the first illumination region and at least one second optical system for directing the light from the at least one second light source to the second illumination region, and wherein the at least one first light source, the at least one second light source, the at least one first optical system, and the at least one second optical system are stationary within the combined aircraft wing scan and runway turn-off light unit. ### Claim 2 (depends on 1) A combined aircraft wing scan and runway turn-off light unit according to claim 1, wherein the first illumination region has a wing illumination reference direction and provides for wing illumination with a horizontal opening angle of between 10° and 30° around the wing illumination reference direction. ### Claim 3 (depends on 2) A combined aircraft wing scan and runway turn-off light unit according to claim 2, wherein the wing illumination reference direction has a lateral angle of between 35° and 55°, with respect to a rearward longitudinal direction of the aircraft. ### Claim 4 (depends on 1) A combined aircraft wing scan and runway turn-off light unit according claim 1, wherein the second illumination region has an airfield illumination reference direction and provides for airfield illumination with a horizontal opening angle of between 20° and 70°, around the airfield illumination reference direction. ### Claim 5 (depends on 4) A combined aircraft wing scan and runway turn-off light unit according to claim 4, wherein the airfield illumination reference direction has a lateral angle of between 35° and 55°, with respect to a forward longitudinal direction of the aircraft. ### Claim 6 (depends on 1) A combined aircraft wing scan and runway turn-off light unit according claim 1, wherein, between the first illumination region and the second illumination region, the light intensity distribution has a light intensity of less than 10% of a peak light intensity in the second illumination region. ### Claim 7 (depends on 1) A combined aircraft wing scan and runway turn-off light unit according to claim 1, wherein the at least one light source comprises at least one LED. ### Claim 8 (depends on 1) A combined aircraft wing scan and runway turn-off light unit according to claim 1, further comprising a single power supply, with the at least one first light source and the at least one second light source sharing the single power supply. ### Claim 9 (depends on 1) A combined aircraft wing scan and runway turn-off light unit according to claim 1, further comprising a switching circuit, with the switching circuit providing power to either the at least one first light source or to the at least one second light source. ### Claim 10 A combined aircraft wing scan and runway turn-off light unit, comprising: a housing for mounting the combined aircraft wing scan and runway turn-off light unit to a side portion of a fuselage of an aircraft; at least one light source; and an optical system for shaping a light emission distribution of the combined aircraft wing scan and runway turn-off light unit, wherein the light emission distribution comprises a first illumination region for illuminating a wing region of the aircraft and a second illumination region for illuminating a lateral forward airfield region, wherein the at least one light source is exactly one light source and wherein the optical system further comprises a lens for splitting light from the exactly one light source between the first illumination region and the second illumination region, wherein the exactly one light source and the lens are stationary within the combined aircraft wing scan and runway turn-off light unit. ### Claim 11 An aircraft comprising: an aircraft fuselage, extending from a nose to a tail of the aircraft, a left wing, having a left wing root, and a right wing, having a right wing root, and at least one combined aircraft wing scan and runway turn-off light unit that includes: a housing for mounting the combined aircraft wing scan and runway turn-off light unit to a side portion of a fuselage of an aircraft, at least one light source, and an optical system for shaping a light emission distribution of the combined aircraft wing scan and runway turn-off light unit, wherein the light emission distribution comprises a first illumination region for illuminating a wing region of the aircraft and a second illumination region for illuminating a lateral forward airfield region, wherein the at least one light source comprises a plurality of light sources having at least one first light source and at least one second light source, wherein the optical system comprises at least one first optical system for directing the light from the at least one first light source to the first illumination region and at least one second optical system for directing the light from the at least one second light source to the second illumination region, and wherein the at least one first light source, the at least one second light source, the at least one first optical system, and the at least one second optical system are stationary within the combined aircraft wing scan and runway turn-off light unit, wherein the at least one combined aircraft wing scan and runway turn-off light unit is mounted to at least one of a left side portion and a right side portion of the aircraft fuselage. ### Claim 12 (depends on 11) An aircraft according to claim 11, wherein the at least one combined aircraft wing scan and runway turn-off light unit is positioned between 30% and 70% of the distance between the nose and a respective one of the left wing root and the right wing root. ### Claim 13 (depends on 12) An aircraft according to claim 12, wherein the at least one combined aircraft wing scan and runway turn-off light unit is positioned between 40% and 60% of the distance between the nose and the respective one of the left wing root and the right wing root.