# US 11,077,959 B2 · Combined forward navigation and anti-collision light for an aircraft 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 11,077,959 B2 - Document ID: US11077959B2 - Status: Granted - Kind: B2 - Application number: 16/702,606 - Filed: 2019-12-04 - Published: 2020-06-18 - Granted: 2021-08-03 - Earliest claimed: 2018-12-17 - Assignees: Goodrich Lighting Systems GmbH - Applicants: Goodrich Lighting Systems GmbH - Inventors: Anil Kumar Jha - Web page: https://patentgrep.com/patent/US11077959B2 ## CPC - B64D 47/06: for indicating aircraft presence - B64D 47/04: the lighting devices being primarily intended to illuminate the way ahead - G08G 5/50: Navigation or guidance aids - G08G 5/55: for a single aircraft - G08G 5/80: Anti-collision systems - B64D 2203/00: Aircraft or airfield lights using LEDs - B64D: EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT - G08G: TRAFFIC CONTROL SYSTEMS (guiding railway traffic, ensuring the safety of railway traffic B61L; arrangement of road signs or traffic signals E01F9/00; radar or analogous systems, sonar systems, lidar systems specially adapted for traffic control G01S13/91, G01S15/88, G01S17/88; {radar or analogous systems, sonar systems, lidar systems specially adapted for anti-collision purposes G01S13/93, G01S15/93, G01S17/93}) ## Abstract A combined forward navigation and anti-collision light for an aircraft includes a forward navigation light source; a first lens, arranged over the forward navigation light source, with the forward navigation light source and the first lens in operation generating a forward navigation light output; an anti-collision light source; a second lens, arranged over the anti-collision light source, with the anti-collision light source and the second lens in operation generating an anti-collision light output; and a mounting structure, to which the forward navigation light source, the first lens, the anti-collision light source, and the second lens are mounted, wherein the mounting structure provides a common mounting plane, with the forward navigation light source and the anti-collision light source being arranged on the common mounting plane. ## Claims ### Claim 1 A combined forward navigation and anti-collision light for an aircraft, comprising: a forward navigation light source; a first lens, arranged over the forward navigation light source, with the forward navigation light source and the first lens in operation generating a forward navigation light output; an anti-collision light source; a second lens, arranged over the anti-collision light source, with the anti-collision light source and the second lens in operation generating an anti-collision light output; a mounting structure, to which the forward navigation light source, the first lens, the anti-collision light source, and the second lens are mounted; wherein the mounting structure provides a common mounting plane, with the forward navigation light source and the anti-collision light source being arranged on the common mounting plane; an end of life detector, arranged between the forward navigation light source and the anti-collision light source; and a third lens, arranged over the end of life detector, with the third lens directing light from the forward navigation light source and from the anti-collision light source towards the end of life detector. ### Claim 2 (depends on 1) A combined forward navigation and anti-collision light according to claim 1, wherein the mounting structure comprises a common mounting board, in particular a common printed circuit board, to which the forward navigation light source and the anti-collision light source are mounted. ### Claim 3 (depends on 1) A combined forward navigation and anti-collision light according to claim 1, wherein the forward navigation light source comprises a first LED, having its main light emission direction orthogonal to the common mounting plane, and wherein the anti-collision light source comprises a second LED, having its main light emission direction orthogonal to the common mounting plane. ### Claim 4 (depends on 1) A combined forward navigation and anti-collision light according to claim 1, wherein the anti-collision light output is asymmetric with respect to a straight out light emission plane of the anti-collision light source, orthogonal to the common mounting plane and extending through the anti-collision light source. ### Claim 5 (depends on 4) A combined forward navigation and anti-collision light according to claim 4, wherein between 50% and 90% of the anti-collision light output is on an outboard side of the straight out light emission plane of the anti-collision light source. ### Claim 6 (depends on 1) A combined forward navigation and anti-collision light according to claim 1, wherein the first lens has a first total internal reflection surface positioned on an outboard side of a straight out light emission plane of the forward navigation light source, orthogonal to the common mounting plane and extending through the forward navigation light source, the first total internal reflection surface reflecting light towards the inboard side of the straight out light emission plane of the forward navigation light source. ### Claim 7 (depends on 1) A combined forward navigation and anti-collision light according to claim 1, wherein the second lens has a second total internal reflection surface positioned on an inboard side of the straight out light emission plane of the anti-collision light source, the second total internal reflection surface reflecting light towards the outboard side of the straight out light emission plane of the anti-collision light source. ### Claim 8 (depends on 1) A combined forward navigation and anti-collision light according to claim 1, wherein the first lens is symmetric with respect to a horizontal plane, orthogonal to the common mounting plane and extending through the forward navigation light source, or wherein the second lens is symmetric with respect to a horizontal plane, orthogonal to the common mounting plane and extending through the anti-collision light source. ### Claim 9 (depends on 1) A combined forward navigation and anti-collision light according to claim 1, wherein the common mounting plane is vertical. ### Claim 10 (depends on 1) A combined forward navigation and anti-collision light according to claim 1, wherein the forward navigation light output has a horizontal opening angle (α) of between 110° and 130° and wherein the anti-collision light output has a horizontal opening angle (β) of between 100° and 140. ### Claim 11 (depends on 1) A combined forward navigation and anti-collision light according to claim 1, wherein the common mounting plane has an outboard angle of between 30° and 50°, with respect to a flight direction of the aircraft. ### Claim 12 (depends on 1) A combined forward navigation and anti-collision light according to claim 1, comprising at least two anti-collision light sources and at least two second lenses, respectively arranged over the at least two anti-collision light sources, with one anti-collision light source and one second lens in operation generating a white strobe anti-collision light output and with another anti-collision light source and another second lens in operation generating a red beacon anti-collision light output. ### Claim 13 (depends on 1) An Aircraft comprising: a fuselage, a left wing, a right wing, a left light that is a combined forward navigation and anti-collision light in accordance with claim 1, the left light being arranged in the left wing, and a right light that is a combined forward navigation and anti-collision light in accordance with claim 1, the right light being arranged in the right wing. ### Claim 14 (depends on 13) An aircraft according to claim 13, wherein the common mounting plane of the left light is angled between 30° and 50° outboard to the left with respect to a flight direction of the aircraft, and wherein the common mounting plane of the right light is angled between 30° and 50° outboard to the right with respect to the flight direction of the aircraft.